Atomic dopant species that are commonly used in ion implantation.
\r\n\tThe purpose of this book is to provide the readers with an understanding of the characteristics of the crisis itself, recognize the wide range and multi-layer of the crisis from a real situation, give ideas on how to minimize the damage, and find ways to increase resilience in the future. To adapt to the rapidly and diversely changing world, the necessary experience and appropriate management for all kinds of crisis issues will be discussed as well. At the same time, it is intended to suggest elements such as verified scientific and empirical knowledge and applicable technologies; more effective risk management operation; modeling of the risks, manuals, management plans, and strategies.
\r\n\t
Semiconductor device manufacturing is facing stringent challenges in advanced COMS process technology nodes. Ion implantation technology has always been a good solution of last resort since it’s got a much wider latitude and stronger flexibility to accommodate new challenges than any other process steps in device fabrication. It is not unusual that people utilize ion implantation not just for doping the silicon substrate, but also for compensating the shortfalls of other process steps. In the past decade, the process window, typically large enough for ion implant engineers to maneuver has gotten narrow, so narrow to a degree so that itself started to create problems which none other process steps can resolve, or compensate. These problems include dopant atoms activation, co-implant species of choice, pre-amorphization implant species of choice, implant damage control, runaway low-energy implant cost. High mass molecular (HMM) ion implantation is investigated in response to all these ion implant related problems.
\n\t\t\tIon implantation is a process whereby energetic ions impinge on a target, penetrating below the target surface and giving rise to a controlled, predictable, ion distribution. Here we will focus on Si technology; hence the target will be mostly Si. Implanted ions are typically dopants, such as Boron, Phosphorus, Arsenic, Indium and Antimony. Table 1 shows these commonly used dopant elements in the periodic table of the elements. However, the scaling of device features into the sub-100nm regime has added species such as Ge, C, N, and Xe to this list. Implantation energies cover a wide range from 0.2 keV to >3 MeV; doses range from 1 x 1011 cm2 to more than 1 x 1016 cm2; incident angles cover normal incidence (a tilt angle of 0º) to 60º.
\n\t\t\tThe industry has been using BF2\n\t\t\t\t+, as the molecular form of Boron, to implant in order to attain higher throughput for low-energy applications. This species has the disadvantage of co-implanting fluorine, which retards boron activation and increases contact resistance, both undesirable consequences for doping process (Foad, 2005). HMM implants have recently been introduced as an alternative. As the molecular structure shown in Fig. 1, Octadecaborane (B18H22), which has 18 effective dopant atoms in one molecule, has been proven a viable replacement for boron in poly-doping and BF2 for ultra-shallow junction (USJ) formation.
\n\t\t\tBesides the advantage of higher productivity, HMM implant process advantages have been noticed and explored. Due to its heavy mass, HMM ion implant can eliminate the use of pre-amorphization implant (PAI). We can use the HMM ions that contains either dopant or co-implant species to replace PAI (Ameen, 2008). Implant damage control is also possible by the use of HMM ion implantation, due to germanium PAI elimination.
\n\t\t\t\n\t\t\t\t\t\t\t | \n\t\t\t\t\t
Atomic dopant species that are commonly used in ion implantation.
Structure of Octadecaborane (B18H22) molecule.
Attempts have been made to implant molecular carbon (C16H10), of which the molecular structure is shown in Fig. 2, to replace Ge-PAI plus monomer carbon for advanced logic manufacturing. The latter mentioned monatomic implants are nowadays popular co-implants for USJ formation in the metal-oxide-semiconductor field-effect transistor (MOSFET) source and drain extension (SDE) doping process (Pawlak, 2006). Carbon is a standard co-implant in the MOSFET SDE implant sequence due to its capability of reducing dopant transient enhanced diffusion (TED). This is achieved through trapping of crystalline interstitial defects by the carbon atoms that are incorporated in the lattice substitutional sites (Carroll, 1998). Unless the silicon substrate is amorphized, the carbon implant could not be incorporated in the silicon lattice sites when undergone thermal annealing. In this case Ge-PAI is required, because carbon mass is too light to cause self-amorphization under most conditions. The use of molecular carbon opens up the possibility of replacing the traditionally used Ge-PAI, which is also known to leave residual damage leading to junction leakage.
\n\t\t\tStructure of C16H10 molecule
Semiconductor devices have become omnipresent due to their amazingly miniature in sizes, ever expanding functionalities in time, inexpensive manufacturing cost, and etc. Most of these reasons have to do with one historical event; the advent of commercial ion implanters. Impurity doping process is a major manufacturing step that needs to be repeated over and over for many times for the semiconductor material going from basic substrate to electrically functioning devices. Forty years ago, doping of semiconductor had been predominantly a thermal process, where the impurity is introduced at the substrate surface, and within a closed chamber at an elevated temperature, such as a furnace, the dopant atoms are allowed to diffuse into the substrate under a thermal equilibrium process. The speed, or the distance of impurity atom diffusion is dependent on the surface impurity concentration and process temperature. Usually, this temperature of operation is in the 1000 degree Celsius region. The atom diffusion energy is no greater than several eV’s. This makes the doping process long and expensive.
\n\t\t\tDue to the advent of commercial ion implanters, the impurity doping process has shifted from predominantly thermally enhanced in nature to predominantly kinetically driven in nature. The impurity atoms are now being stripped of or bestowed with electrons in a part of the implanter called the “ion source”, where they become ions to be accelerated in high electrical fields. Once the charge particles, or ions have gained the desired energies, they are collimated and then impinging into the substrate at high initial speeds. All of these actions are performed at room temperature. Although the process temperature for ion implantation is relatively low, the dopant ions acquire energies in the keV range. Therefore, the process time is less than one one-thousandth of that of a thermal process. Thus, the productivity is higher, and the cost is significantly lower too.
\n\t\t\tThese advantages provide the semiconductor manufacturers with motivation to quickly adopt ion implantation in the process flow. They also give the process engineers and device engineers a lot of freedom to utilize the technique without having to wary of process constraints and tradeoffs too much. However, in the past decade, the process window, typically large enough for ion implant engineers to maneuver has gotten narrow, so narrow to a degree so that itself started to create problems, which none other process steps can resolve or compensate. These problems include insufficient dopant activation, co-implant species of choice, pre-amorphization implant species of choice, implant damage control, runaway low-energy implant cost
\n\t\t\ta) Diffusion process is in thermodynamic equilibrium and energies are thermal (~eV) and random (isotropic); b) Ion implantation is a process in which energetic, charged particles (atoms or molecules) are accelerated into the near surface of a target substrate at depths from ~10nm to ~1000nm (1 micron)
As time progresses, the process issue and cost issue are still the driving forces that motivate us to look at high mass molecular ion implantation, as oppose to monatomic implantation. However, among these two, the aspect of process requirements usually plays a dominant role in tool selection for semiconductor manufacturing. One obvious reason is that if people can quickly translate process benefits to device performance improvement, or geometry scaling down (in other words, device real estate saving), the cost it associated can be readily justified. In this chapter, we will also address the productivity and cost issue. However, the aspect of cost can hardly be the primary factor for choosing a process. We would like to make sure the production method we choose today can be extended to cover for the future needs. Only by taking the whole picture into consideration, then one can start to appreciate molecular ion implantation being a production method for now and the future.
\n\t\tAn ion implant process is basically putting the dopant atoms into the silicon substrate by bombarding the silicon wafers with very energetic ions. This process would inevitable result in crystal damage. The implant damage can take many different forms, such as non-equilibrium excess of vacant lattice sites (vacancies) and self-interstitial atoms (interstitials), vacancy clusters, interstitial clusters, dopant-interstitial and dopant-vacancy clusters, and locally amorphized regions of the crystalline silicon target. Iso-valent ions such as Si, or Ge are sometimes implanted to intentionally take advantage of this collateral damage. The annealing of this damage, and the electrical activation of the implanted dopants, requires that the implanted target receive a subsequent heat treatment. The as-implanted defect configurations evolve during post-implant thermal processing, giving rise to transient enhanced dopant diffusion (TED), and the formation of relatively stable dislocation arrays, which if present in active device regions can lead to degradation of electrical performance. An understanding of all these phenomena is therefore crucial to the design of the implant recipe and the post-implant thermal treatment.
\n\t\t\tIn advanced CMOS processing, this amorphous layer plays important roles for several purposes. The top three are, 1) dopant channeling prevention; 2) dopant activation enhancement; 3) end-of-range (EOR) defect reduction. In other words, they represent the properties of controlled junction depth; higher conductivities; and lower junction leakage currents in the CMOS device respectively.
\n\t\t\tAchieving an implant profile without appreciable channeling is of practical importance to avoid that slight differences in beam orientation across the wafer result in radically different implant profiles. There are three different methods to prevent implant from channeling. As shown in fig. 4 a) the first choice is by tilting the wafer, which is the easiest way to achieve if it serves the purpose. However, only at high energies, where the critical angles are relatively small, this method can be effective. At low energies, the tradeoff between the amount of angle being tilted and the compromise it incurs to implant profile starts to become significant. If a low tilt angle is not sufficient for preventing implant channeling, we may have to go to a higher tilt angle. On the other hand, the implant shadowing effect, which is caused by device surface topology blocking the incident beam at an angle, starts to get intolerable. Therefore, merely by tilting the wafer plane away from beam incident angle might not be effective. The second alternative is to use sacrificial oxide to prevent implant channeling. This is shown in fig. 4 b). Since ion implantation may also introduce metal contamination to the wafer, it has been a common practice to use a thin layer of sacrificial oxide, from 100Å to 200Å thick to block the elemental contamination from penetrating the wafer surface. Once the implant process is done, this layer of sacrificial oxide would be stripped of from a wet bench using buffered oxide etching solution. However, due to advanced devices are very sensitive to “substrate loss”, or so to speak “dopant loss”, people have begun to move away from using sacrificial oxide. Finally, the most inconvenient method for preventing implant channeling is, as depicted in fig. 4 c), by inserting a pre-amorphization implant before dopant implant. Usually, this implant species of choice is non-electrically active, or iso-valent atom, such as germanium or silicon. It is indeed an effective way to prevent implant channeling. The drawback is that it adds an additional implant step to the process.
\n\t\t\ta) Tilting wafer off the channeling plane. b) Thin sacrificial oxide for randomizing the direction of incident ions. c) Pre-amorphization implant to randomize the lattice atoms, thus destroy the crystal channels.
After ion implantation, the substrate needs to be treated with thermal processes. This is because the silicon substrate is damaged by ion bombardment, and needs to be “annealed”, which is a thermal treatment to recover its crystalline structure. Meanwhile dopant atoms can be incorporated into the crystal lattice and become electrically active. As depicted in fig. 5, these two goals should be achieved simultaneously. Since this thermal treatment can also cause dopant diffusion, there would be some dopant redistribution.
\n\t\t\tThe implant damage and inactive dopant atoms left in the silicon substrate need a post implant anneal to active the dopant and recover the crystalline structure.
From the logic manufacturing side, when the technology moved beyond 0.25um (deep sub-micron) era, the requirement of SDE is demanding USJ formation. This requirement is in response to the potential short channel effect (SCE) associated with device shrinkage. The geometry of device structure has to be tightly controlled now. In short, the “as implanted” dopant profile and dopant redistribution during anneal need to be well managed. For shallow junctions, dopant concentration levels can be very high. These implanted atoms tend to form high density crystal defects. The thermal budget for implant anneal has been greatly reduced for advanced logic devices due to the concern of excessive dopant re-distribution when the device is undergone high temperature thermal anneal. However, if the thermal budget is insufficient, the crystal defects could not be totally removed, and would lead to adverse effects on device performance, such as high device leakage currents.
\n\t\t\tIt has been known for some time that boron diffusion can be enhanced by damage introduced by the implant process. For example, fig. 6 shows the enhanced diffusion of a boron marker produced by molecular beam epitaxy on a silicon substrate, which was subsequently damaged by 1x1014 cm-2 silicon implants at various energies and then subjected to a 950ºC/30s anneal. The enhancement scales linearly with the projected range of the implant which is approximately where the damage induced excess interstitials are initially located (\n\t\t\t\t\tAgarwal, 1997\n\t\t\t\t; Gossmann, 2000).
\n\t\t\tThe phenomenon of transient enhanced diffusion (TED) after ion implantation increases the challenge of forming ultra-shallow junctions (\n\t\t\t\t\tAgarwal, 1997\n\t\t\t\t, \n\t\t\t\t\t1999\n\t\t\t\ta, 1999b). Ion implantation leads to the displacement of silicon atoms from their lattice positions, creating pairs of vacancies and interstitials. During the initial stage of post-implantation annealing most of the vacancies and interstitials recombine leaving behind a net excess of interstitials approximately equal to the implanted ion dose; this is also referred to as the “+1” approximation (Giles, 1991). These excess interstitials quickly coalesce into extended defects, such as {311}’s (Eaglasham 1994; Stolk, 1997), or more stable dislocation loops. While these extended defects have lower free energy than individual interstitials (Eaglasham 1994; Rafferty, 1996), they are still metastable and dissolve with continued annealing. As they dissolve, they release excess interstitials into the lattice. Since boron diffuses by an interstitial mechanism (Gossmann, 1997) its diffusivity is enhanced by the excess interstitials with the time averaged diffusivity enhancement equal to the time averaged interstitial supersaturation. Both the interstitial supersaturation and the diffusivity enhancement end soon after the defects have dissolved. This phenomenon is depicted in fig. 7.
\n\t\t\tEnhancement in diffusion of a boron marker layer, grown by molecular beam epitaxy during a 950ºC/30s anneal, following implantation of 1x1014 cm-2 Si at various energies (
Boron diffuses by an interstitial mechanism; its diffusivity is enhanced by the excess interstitials.
The increase in junction depth, Δxj, due to TED to be expressed as (Gossmann, 1998; Rafferty, 1996)
\n\t\t\twhere N is the number of interstitials trapped in the defects (approximately equal to the implanted dose) and Rp is the projected ion range (where the excess interstitials are initially located). The linear dependence on Rp has been demonstrated experimentally, as shown in fig. 6. The activation energy of Δxj\n\t\t\t\t2 is negative because the interstitial supersaturation due to the presence of the extended defects is larger at lower temperatures. This implies that the final junction will be deeper if the defects are annealed out at a lower temperature than at a higher temperature. This is a key reason why junction anneals are done in a rapid thermal annealing (RTA) rather than in a conventional furnace with a ramp-up rate of a few degrees per minute. An RTA spends significantly less time during the temperature ramp-up at lower temperatures where the diffusivity enhancement is larger.
\n\t\t\tSince the increase in junction depth due to TED depends on the implant dose (Eq. 1), it is possible that for a high dose implant some damage will remain after a fast ramp-up, allowing TED to continue during the ramp down (\n\t\t\t\t\tAgarwal, 1999\n\t\t\t\t). As the ramp-up rate is increased, the temperature at which TED runs out is pushed up until the TED is pushed over to the ramp-down side of the anneal (Agarwal, 2000). This is illustrated in fig. 8.
\n\t\t\tSchematic illustration of TED continuing during ramp down of a spike anneal that is sufficiently fast (
In the sub-keV regime, there is more than one way to arrive at the same junction properties. It is very important to minimize the dose first, before reducing the energy further. The dependence of the sheet resistance and junction depth data on the different implant and annealing parameters is summarized in fig. 9. Increasing the ramp-up rate leads to a more shallow junction with higher resistivity. The same is also true when a smaller dose or energy is used. Modifying the implant parameters first helps avoid the risk of poor process repeatability which necessarily accompanies the use of higher ramp-up rates.
\n\t\t\tAs the advanced logic manufacturers manage the implant and anneal together in an effort to meet the process requirements, the treadmill of device scaling is relentlessly pushing the implant dose higher and energy lower. The conventional USJ scaling is inevitably hitting the limits. The USJ formation for SDE is key for 65nm technology node and beyond (Foad, 2005). The obstacles include boron TED, low boron solubility limit in silicon, and most of all, post-anneal residual implant damage. For high dose applications, not all implant damage can be removed by the anneal process due to insufficient thermal budgets from “spike” RTA or ms laser spike anneal (LSA) processes. If this damage is in the wrong place, increased device leakage and catastrophic p-n junction shorts are probable. This scenario is depicted in fig. 10. Engineering the type, extent, and location of post-anneal residual implant damage is one of the primary objects of Front End of Line (FEOL) process integration.
\n\t\t\tSheet resistance vs. junction depth as a function of ramp rate, implantation dose and implantation energy. Note the similarity between increasing the ramp-up rate or reducing the energy and dose (
When the EOR defect damage is in the wrong place, increased device leakage and catastrophic p-n junction shorts are probable.
Molecular implants have long been considered by the IC manufactures as alternatives to atomic implants for low-energy applications (Jacobson, 2001). The major benefit of using molecular species implants is wafer throughput improvement due to higher effect beam currents when implanting at low energy. A molecular ion dissociates into its constituent atoms at the wafer surface. The constituent atoms then continue with a fraction of the total energy. This phenomenon can be utilized to gain wafer throughput in the sub-5.0keV range as implanters in general can deliver higher molecular beam currents at higher extraction voltages, and still provide equivalent processes to the low-energy monatomic implants.
\n\t\t\tA well-known and long-used example of this in production environments is BF2\n\t\t\t\t+ implantation as a means of delivering a lower effective energy boron as the molecular type of p-type dopant. More recent experimentation with molecular n-type dopants has demonstrated that As2 and P2 can provide production-worthy beam current and throughput improvements with comparable process results (Chang, 2003).
\n\t\t\tThe formation of aggressive n-type junctions has not posed as severe a challenge as p-type junctions in the past, due to the much larger atomic mass (75 amu for As, versus 11 amu for B) and lower diffusivity in Si. Arsenic dimer implant requires twice the ion energy of the monatomic implant. However, the effective fluence of a dimer implant is two times that of a monatomic implant, since both atoms in the dimer ion contribute to the total dopant dose. Therefore, it requires only half the dose of a monatomic implant. These conditions can be expressed by equations (2) and (3).
\n\t\t\tSince ion implanters can in general produce more
In recent years significant advances have been made in the development of high mass molecular (HMM) beam sources for dopant implantations into silicon. The driver for the development of these sources has been the need for very low energy implants. Energy is partitioned between the atoms of a molecule in direct proportion to their mass. For example, the widely used molecular ion BF2\n\t\t\t\t\t+ with atomic mass ~49 having a single boron atom of mass ~11 results in the implantation of boron at an energy that is ~11/49 of the molecular ion energy, e.g. a 10 keV BF2 implant, for example, is energetically equivalent to a 2.24 keV B implant.
\n\t\t\t\tA much more dramatic example of this energy partitioning may be achieved with decaborane (B10H14) (Jacobson, 2001) where a 10keV implant is equivalent to a ~1 keV implant. Recently, another large boron containing molecule, Octadecaborane (B18H22) has also been identified as a useful molecule for this application (Perel, 2001). It is important to note that with these molecules, one milliampere of ion beam current is equivalent to 10 (for decaborane) or 18 milliamperes (for octadecaborane) of boron current. For this reason the molecular beam obviates many of the space charge limitations associated with the ultra-low energy Boron beams. Conventional ion sources are not suitable for decaborane or octadecaborane implantation since the high arc chamber temperature causes disassociation of the molecule. Ionization chamber temperatures below 300ºC are required and a different approach to electron impact ionization of the molecule is required. Figure 11 shows a commercially available octadecaborane ion source (\n\t\t\t\t\t\tJacobson, 2005\n\t\t\t\t\t). Also, the ionization process results in a distribution of ions of the form B10Hx or B18Hx with the result that the mass resolved spectrum consists of a typically up to 10 peaks, all containing the same boron content but with varying hydrogen content. As a result, the acceptance of the mass resolving system must be increased to allow for maximum utilization of the available molecular ion current (Perel, 2001). Figure 12 gives a typical mass resolved spectrum obtained from a decaborane source (\n\t\t\t\t\t\tJacobson, 2005\n\t\t\t\t\t).
\n\t\t\t\tIon Source Suitable of Decaborane or Octadecaborane Ion Beam Generation (
Typical mass resolved spectrum obtained from a decaborane source.
The aggressive scaling of DRAM puts severe constraints on the gate formation. Single work function polysilicon gate for PMOS with buried channel will suffer serious short channel effect as the scale shrinkage continues. Meanwhile, its high leakage is not tolerable for the requirements of low power high performance devices. The high leakage comes from the fact that the buried channel is away from the surface; hence, the gate can’t control the channel as effectively as surface channel. As the dual work function poly gate shows the advantage of easiness of Vt control and resistance to short channel effects, Surface-channel PMOS with P+ poly gate will take substitution of buried-channel PMOS with N+ poly gate for advanced devices inevitably. Figure 13 shows the channel current flowing underneath the surface in a buried-channel PMOS device of the left, and on the surface in a surface-channel PMOS device on right.
\n\t\t\t\tOctadecaborane (B18H22) implant technology was evaluated for p+ poly gate doping process in a 72nm node stack DRAM device. For DRAM manufacturing, the 7x-nm-class is about the technology node where the device performance requires dual-poly gate structure for tuning the PMOS and NMOS work functions separately. Since the gate poly is in-situly dosed with n-type dopant during CVD polysilicon deposition, the PMOS gate poly needs to be doped heavily with p-type dopant afterwards, in order to counter dope the gate and transform it from originally n-type to p-type poly. Therefore, it requires low energy (< 5keV) and high dose boron implant (> 5×1015 /cm3). The evaluation criteria were to improve the productivity of the process, which was initially built with conventional atomic boron implantation (11B), while maintaining process equivalency. Before implanting into device wafers, process matching to conventional boron implant was done using both crystalline silicon and poly-silicon on Si wafers (Chang, 2008). For the crystalline silicon wafers, the Rs of blanket B18HX\n\t\t\t\t\t+ implants were compared to that of atomic boron. For the poly-Si silicon wafers, SIMS dopant profiles were compared. For the device wafers, boron penetration, gate depletion, and final yield were compared. In addition, B18H22 implant splits of various energies and doses have been studied for their sensitivities to the electrical performance of the p-MOSFET in the 72nm node stack DRAM devices. In this study, we have demonstrated that B18H22 can provide up to 5× wafer throughput advantage over conventional atomic boron process due to much higher effective beam currents. Besides the significant productivity improvement, B18H22 implant device characteristics were well matched to the baseline atomic boron process.
\n\t\t\t\tThe channel current flowing underneath the surface in a buried-channel PMOS device of the left, and on the surface in a surface-channel PMOS device on right.
In a BF2\n\t\t\t\t\t+ implant, the extraction energy is 49/11 times the desired Boron energy. Under the same principle, a B18H22 implant extraction energy is 210/11 times the desired Boron energy. These conditions can be expressed by equations (4) and (5).
\n\t\t\t\tSince ion implanters can in general produce more
In this study, we used Axcelis’ OptimaHD Imax implanter for molecular boron implants. The Imax was developed for ionizing, transporting and implanting molecular species such as C16H10 and B18H22. Figure 14 shows the Rs of B18 implant versus POR boron implant for the P+ gate poly process. The B18-implanted wafers require higher doses to match the POR Rs. The slightly under-dosing of the B18H22 implant in this case could be caused by a difference in dose retention between B18 and monomer boron. For low-energy implants, as dose increases, the fraction of dopant loss increases due to the sputtering, where near surface atoms leave the target during implantation due to recoil collisions. This phenomenon is depicted in fig. 15. While a detailed comparison of B18 and B has not been carried out, the retained dose of B18 as a function of energy has been reported (Harris, 2006). From the dose sensitivity test, a dose trim factor of 1.17 (17% higher dose) was determined for the P+ gate poly process, which has a lower target Rs.
\n\t\t\t\tP+ poly process Rs matching for the recipe of B/2keV/1.5×1015cm-2\n\t\t\t\t\t\t
For low-energy implants, as dose increases, the fraction of dopant loss increases due to the sputtering, where near surface atoms leave the target during implantation due to recoil collisions
In this test, wafers of poly implant conditions were subject to secondary ion mass spectrometry (SIMS) profile analysis. Figures 16 and 17 show the implant profiles of as-implanted and annealed implants from TPOR and Imax. The poly thickness is 90nmin this case. The annealing condition is RTP for a 20s soak at 965C. The implant dose for B18 has been adjusted to account for dopant loss. Meanwhile, the split conditions were designed for a process window check. Table 2 shows the comparison of the accumulated doses in SIMS.
\n\t\t\t\tAs implanted SIMS profiles for B and B18 implants.
Annealed SIMS profiles for B and B18 implants.
\n\t\t\t\t\t\t\t\t | \n\t\t\t\t\t\t
Accumulated SIMS dose for all samples.
\n\t\t\t\t\tFigure 17 shows that B18 implants seems to get a near surface bump as their signature. This could be due to the hydrogen effect. Since for every B18 ion implanted into the wafer, 22 hydrogen atoms would also be implanted. And hydrogen would enhance boron out diffusion. In some literatures, the possibility of hydrogen induced boron pile up in the surface has been discussed (Berry, 2008). Nevertheless, B and B18 implant profiles are matched at the oxide interface for as-implanted and annealed samples. Since the dopant concentrations match at the critical depth of the profile, we can view the SIMS profiles as matched in this case. Therefore, the implant matrix for the product wafers is to split the dose at target, ±10%, ±20% and ±30% for the P+ poly doping recipe. Device PMOS Vth does have a trend corresponding to different dosages. As the dosage gets high, the Vth gets high too. However, the biggest deviation is less than 10mV, we can say that the device results are all meeting the specification (Chang, 2008).
\n\t\t\tAs device scaling continues previously acceptable implant technologies for p-MOSFET SDE are struggling to meet advanced device requirements. There are three metrics that must be simultaneously achieved; those are device leakage, p-type dopant activation and junction depth control. In order to meet all of these goals, we found that molecular carbon implant is particularly well suited for USJ formation of the p-MOSFET SDE.
\n\t\t\t\tDue to preserving device geometry is of primary importance, junction depth control is the first thing to consider. Recent years, people have started to use carbon implant to suppress boron TED. The reason is that when carbon concentration is high enough (above 1×1019cm-3), it would create an interstitial “under-saturation” region (Carroll, 1998) (Moroz, 2005). Therefore, boron dopant atoms would less likely to be “kicked-out” by the excessive interstitials in the lattice, and implant profile remains stable during annealing. In order to incorporate carbon into silicon, the implant layer needs to be fully amorphized before annealing. Therefore, germanium pre-amorphization implant (Ge-PAI) was inserted in the process flow. Although it is a common practice to use Ge-PAI now, we all know that Ge-PAI is problematic due to it results in elevated end-of-range (EOR) defect damages, which have been identified as the leakage source for the devices. In the light of this concern, we put the constraints on Ge-PAI usage, so that it would not impact the junction quality. However, the trade-off between limiting Ge-PAI dosage and excessive residual implant damage may lead to an insufficient amorphous layer for carbon incorporation.
\n\t\t\t\tThe other way to get around of this problem would be to increase the carbon implant dose, so that it reaches the critical dose for the formation of amorphous layer. However, carbon also leaves behind point defects (Mirabella, 2002), and causes device leakage. Although the effect of these point defects left behind by carbon implant are still under investigation, the increase in sheet resistance is observable. This is due to carbon diffuses predominantly by a “kick-out” mechanism. If carbon concentration is too high, it would unavoidably compete with boron dopant atoms for occupying lattice sites, and kick the already electrically active boron atoms out of the lattice sites. Therefore, the use of carbon should be evaluated of its pro’s and con’s. If we go beyond a certain dosage of carbon, the benefits of activation improvement and diffusion suppression would be compromised by the excessive implant damage and dopant deactivation.
\n\t\t\t\tSince High Mass Molecular (HMM) implants have been known to create an amorphous layer as effectively as the heavy ion species (Krull, 2006), implanting molecular carbon is a potential technique to replace the process steps of Ge PAI plus monomer carbon implant. C16H10 is shown to be a consistently self-amorphizing method for introducing carbon into the extension region.
\n\t\t\t\tIn a preliminary study, we used Axcelis’ OptimaHD Imax implanter for molecular carbon implants. We proved that a single implant of C16H10 can effectively replace a two step Ge + C implant sequence. As logic device technologies advanced into the 40nm node, USJ requirements became very stringent. The xj target of p-MOSFET SDE implant is very aggressive, less than 20nm per ITRS roadmap (ITRS 2005). In order to meet these requirements, both the implant and anneal of p-type species need to be considered simultaneously because their interaction is essential to the desired outcome. The process of record (POR) for Ge +C in this case is a Ge/12keV/1×1015cm-2+ C/2.5keV/1×1015cm-2 implant sequence. We compared the B/400eV/1×1015cm-2 implant Rs-Xj results with the presence of the Ge + C, against C16H10 implant of the equivalent carbon dose and energy. Figure 18 shows an XTEM image of a C16H10 implant at 2.5keV per carbon atom, with1×1015 cm-2 dose. The amorphous layer is around 12.9nm, whereas, the projected range of this carbon implant is at 10.2nm, according to SRIM. This result is in line with the data previously published (Mirabella, 2002), and sufficient for the purposes of this study.
\n\t\t\t\tXTEM image of a C16H10 implant at 2.5keV per carbon atom, with 1×1015cm-2 dose
For the case of laser spike annealing (LSA) only, a comparison of POR co-implant against C16H10 implant effect on the boron SDE implant is made in figure 19. The Rs vs. Xj of the two implants indicate that if LSA only was used, it is easy to achieve the advanced logic process target. The Rs of the boron SDE implant with the one step C16H10 implant is comparable to that of the Ge + C co-implant’s. However, one can see that monatomic co-implants may still be insufficient for suppressing the boron diffusion above 15nm deep in the substrate. Although the amorphous layer created by Ge/12keV/1×1015cm-2 is around 20nm, the total defects it creates could provide a lot of interstitials in the deeper region. If one pays attention to the boron profile, one can see the characteristic signal of the amorphous layer and crystalline layer interface at around 20nm deep. The carbon atoms would segregate at this interface, and influence the subsequent boron diffusion. However, one can argue that the tail region of the annealed boron profile for the Ge + C co-implanted case, being slightly higher at around 15nm is beyond the p-n junction. No matter how the defect damage is distributed, we would still expect that the one step C16H10 implant should cause much less implant damage and easier to be annealed. Frontier Semiconductor provides a metrology system that measures the non-contact sheet resistance, and leakage current, called RsL. The RsL leakage current measurement for Ge + C co-implanted USJ shows an average of 28 uA/cm2 in this case. And the RsL leakage current measurement for Ge + C co-implanted USJ shows an average of 0.7 uA/cm2 in this case. This is only one fourth of the leakage current from POR.
\n\t\t\t\tComparison of the B/400eV/1×1015cm-2 LSA annealed dopant profile with the presence of the Ge + C, and C16H10 implant. The POR is a Ge/12keV/1×1015cm-2+ C/2.5keV/1×1015cm-2 implant sequence, and C16H10 implant is of the equivalent carbon dose and energy.
RsL leakage current measurement for Ge + C co-implanted USJ shows an average of 28 uA/cm2 in this case.
RsL leakage current measurement for C16H10 co-implanted USJ shows an average of 0.7 uA/cm2 in this case.
We also investigated the combination of C16H10, and B18H22 implants for USJ formation in a p-MOSFET SDE doping process for a 40nm logic device. We studied the split condition of various energies, beam currents, and different advanced annealing schemes. The objective of this study is to use molecular carbon implant technology to supersede monomer carbon implants as a new process step in advanced CMOS device manufacturing. There are several reasons for the industry to consider molecular carbon instead of monomer carbon. First, conventional monomer carbon implant has poor implanter productivity. Secondly, carbon implants may have side effects (Mirabella, 2002), such as their competition with electrical dopant for substitutional silicon lattice sites and formation of excessive point defects, and incur penalties as well as benefits. Therefore, its adoption requires complicated integration schemes.
\n\t\t\t\tThe purpose of this study was on developing the future USJF. Since the annealing program could be altered and the thermal budget be reduced, the focus was put on the interaction between implant and anneal. There are three different annealing programs involved in this study. The first one is a millisecond laser anneal. The second and the third programs are with spike RTP with the peak temperatures at <1000ºC and >1000ºC, and followed by laser anneal. We denote them as anneal “A” and anneal “B” respectively. In the blanket wafer test part, an implant and anneal matrix was designed to study the possibility of using C16H10, to replace the 2-step Ge-PAI + carbon co-implant sequence. In the device wafer test, we use the p-MOSFET of 40nm node logic, which requires high dose and low energy BF2 implant, along with three other co-implants for the SDE doping process. In this study, the productivity of B18H22 for low energy boron implant was also evaluated. We first focus on the process matching of B18H22 to the recipe of 3keV BF2\n\t\t\t\t\t+ in the process of record (POR). There is also a 2-step Ge-PAI + carbon co-implant sequence precedes the BF2 SDE implant. In the subsequent annealing process, both RTP spike and LSA annealing are applied in this case. Since there is fluorine in the BF2 implant, which is known to affect the boron doping profile during anneal, the B18H22\n\t\t\t\t\t+ energy may need some adjustment to reflect the difference in the boron diffusion profile from the influence of fluorine.
\n\t\t\t\tIf the conventional co-implants were replaced by C16H10, the Rs could be further improved when millisecond laser anneal was applied. This offers the process solution to the LSA only scheme. We expect lower device leakage since Ge-PAI was eliminated. In this case, a light RTP spike anneal was applied to remove the implant damage. Although the molecular carbon implant appears to have the process equivalency as the conventional co-implants, it has lost the process advantages in Rs reduction as shown in the LSA only case. Figure 22 shows the 350eV boron post anneal dopant profile of different annealing schemes. As expected, the xj increases in accordance to RTP temperatures. LSA offers diffusionless anneal, and it only shifts the profile for no more than 2nm deeper, and gets the best sheet resistance. If the spike RTP was added prior to LSA, the profile would shift from 5 to 7nm for “A” annealing scheme and “B” annealing scheme respectively. In figure 23, the 350eV boron implant of the 2-step co-implant is compared against the C16H10 co-implant. The xj of these two implant schemes all shift 5nm after “A” annealing scheme. We can conclude that, even with the light spike RTP added in the annealing scheme, molecular carbon co-implant would behave the same as the monatomic co-implants. The reason is that millisecond anneal, although can activate boron dopant atoms effectively, it doesn’t remove the excessive interstitials resulted from implant damage due to limited thermal annealing. When a spike RTP in the 1000。C regime was applied, the implant induced EOR defect damage would resolve and release the interstitials, which allows the boron TED to run out its course, due to sufficient thermal energy. Therefore, the self-amorphization property of the molecular C16H10 implant may not bring process benefits to p-type USJ formation, unless a diffusionless annealing scheme is employed.
\n\t\t\t\tThe 350eV boron post anneal dopant profile of different annealing schemes. LSA is a millisecond laser anneal. Anneal “A” is a <1000ºC spike RTP followed by a millisecond anneal; and anneal “B” is a >1000ºC spike RTP followed by a millisecond anneal.
The 350eV boron post anneal dopant profile of different annealing schemes, and of the Ge-PAI plus mono-atomic carbon 2-step co-implant versus the C16H10 co-implant.
\n\t\t\t\t\tFigure 24 shows the overlap capacitance of C16H10 plus B18H22 implanting into the SDE region of a 40nm logic device. In comparison to the POR implant matrix shown on the left side, B18H22 direct replacement of BF2 as the boron dopant in the POR appears to have a much higher Cov. This indicates that B18H22 diffuses faster than BF2 in the RTP plus LSA annealing scheme. The main reason should be due to the presence of fluorine in the BF2 implant, which also plays a role in boron TED suppression. However, if the C16H10 implant is employed instead of the conventional co-implants, the Cov is restored. In short, molecular implants can at least be shown to have process equivalency even if the annealing scheme is not in favor of molecular implants. On the other hand, C16H10 has been shown as a valid replacement for current POR co-implants for PMOS SDE. It not only can be easily integrated into the existing process nodes for Ge-PAI replacement, but also allows a smooth transition to a smaller thermal-budget or diffusionless annealing scheme in the future.
\n\t\t\t\tOverlap capacitance of C16H10 plus B18H22. implanting into the SDE region of a 40nm logic device, where the POR is mono-atomic Ge-PAI plus C, followed by a BF2 SDE implant.
The 2keV equivalent boron energy beams of BF2, B10H14, and B18H22, could be extracted from the source and travel in the ion implanter beam line at an energy of 5keV, 20keV and ~40keV respectively.
Owing to the advent of High Mass Molecular implant technology, semiconductor manufacturing fabs now have an opportunity to leap forward in making great productivity and process improvement by utilizing its unique properties of effective beam transportation in the ion implanter beam line, and self-amorphization during process. The amorphous layer could be formed at a relatively lower dose for the HMM implant to avoid the side effects of excessive implant damage. By proper tuning the molecular carbon implant, we can show process equivalency to conventional co-implant scheme, and utilize it for the 40nm p-MOSFET device. Should the annealing scheme be flexible, and the carbon implant only sees the LSA as the post-implant anneal, the adverse effects of carbon implant, such as its competition against boron dopant for activation, etc, can be nullified. Figure 25 shows the industrial trend in the past 40 years for choosing the primary p-type dopant. This trend is in response to the demand for low energy boron implant. Fortunately, people always find a production worthy solution when the request becomes imminent. Even though using BF3 as the source material is problematic, the industrial people are still clinging to it due to the benefit of higher productivity than monatomic boron for low energy operation. It is authors’ believe that as long as Moore’s law still holds, both productivity and process issues will compel fab engineers to migrate to the next generation of p-type dopants. It would be only natural for such evolution to take place. Just as sometimes in the past, we migrated from monatomic boron to small molecular BF2. This time we are just going from BF2, the smaller molecule to B10H14 or B18H22, bigger molecules. For the last transition, the productivity improvement was noticeable, but not awesome, due to either boron or BF2, only has one dopant atom in it. But for this transition, the productivity would get improved from ten to twenty times, due to the HMM B10H14 or B18H22 ions contain that many more dopant atoms. This would be more than just an evolutionary change. It is so significant a leap for the ion implantation technology so that it should to be deemed as a revolutionary change for the silicon manufacturers to make.
\n\t\tThe author would like to thank Hans Cheng of TSMC, Phoenix Kuo of UMC, and Jay Huang of Rexchip for their many years of collaboration with us in the field of HMM ion implantation for DRAM and advanced logic device manufacturing. Most of all, I would like to extend my appreciation to P.S. Chen and S.H. Yang of NTC, who actually adopted B18H22 ion implantation in their 70nm DRAM production for the P+ poly implant process.
\n\t\tNon-contact dry gas seals with a grooved pattern on a seal face can maintain a film thickness of just a few micrometers. Therefore, these seals have better sealing performance when compared to typical labyrinth seals [X]. Dry gas seals are used in many turbomachinery, such as in gas and steam turbines, turbochargers, and compressors. Moreover, they are applied to high-speed operation and under high-pressure differences.
Recently, to reduce energy consumption, more enhancements toward efficient turbomachinery are required. To solve this problem, one effective way is by enhancing the sealing characteristics of seals. Many types of grooved dry gas seals have been developed [1]. Spiral grooved seals are widely used because of their good sealing ability. Lately, a significant amount of research on spiral grooved dry gas seals focused on analytical methods [2, 3, 4, 5, 6, 7, 8], dynamic force characteristics [9, 10, 11], thermal effects considerations [12], and CFD analysis considering the turbulent flow [13] have been performed.
On the other hand, the optimum design of the grooves is one of the effective ways to enhance the seal characteristics. The optimum design methods have been also applied to gas film bearings. Lin and Satomi [14] and Hashimoto and Ochiai [15, 16] applied an optimum design method to spiral groove thrust bearing towards enhancing performance characteristics from variations in groove depth, groove angle, and so on. Moreover, an experimental verification was conducted comparing the novel configuration against a conventional designed spiral groove bearing. However, it was found that the effectiveness of the optimization is limited because these studies have not been changed the groove shapes which were based on a spiral path.
Under this circumstance, Hashimoto and Ochiai [17] proposed a topological optimum design method for a grooved thrust gas bearing. In this method, the groove shape could be changed freely using a cubic spline function. Novel groove shapes were found in this study. The effectiveness and the applicability of the method were verified theoretically and experimentally. Moreover, Hashimoto and Namba [18] found the best groove shapes against various objective functions such as film thickness, friction torque, and dynamic axial stiffness. Also, the effect of the new groove shape on sealing characteristics of FDB(Fluid dynamic bearing) was studied previously and discussed by authors [19].
To date, many researchers have treated spirally grooved shape dry gas seals. On the other hand, recently, the optimum design of groove shape on the dry gas seal was proposed by authors, and comparison of the flow visualization was presented [21]. However, the process of the optimum design has not been mentioned and also it has not been studied for a wide range of operation conditions. Therefore, in this study, the application of the topological optimum design to the dry gas seal instead of the thrust bearings to find an optimum groove shape that enhances the seal leakage restriction and its dynamic stiffness is presented. Moreover, it is important to know the optimum groove shapes under various conditions, therefore, in this study, we tried to make a categorization map of the seal’s optimum shape based on the results of the optimum design calculations under a wide range of operating conditions. Furthermore, CFD analysis is conducted and compared with the experimental flow visualizations for verification, while the rationale for reducing the gas leakage with an optimized seal is presented.
Figure 1 shows the typical structure of a dry gas seal cartridge. It consists of a rotating shaft, a ring with grooves on its face, a stationary ring, support springs, and housing. The gas film is generated by the hydrodynamic effect induced on the grooves of the face. The film thickness is determined by the force balance between the support springs and the hydrodynamic gas film force. The film thickness can be changed by changing the support springs. The seal leakage is a function of the film thickness, the gas pressure differential between the inner side and outer side of the seal chamber, the viscosity of the gas, and the groove shape mounted on the face.
Components of a non-contacting dry gas seal.
In the design of dry gas seals, it is important to minimize the gas leakage towards enhancing the efficiency of turbomachinery. Simultaneously, enhancing the dynamic stiffness of a gas film is an important factor for its safe operation, at high speed in particular. Because turbomachinery is likely to be exposed to some outer disturbance such as earthquakes, a hard contact of the rotor on the seal surface leads to serious damage to the mechanical system.
Both a low gas leakage and a high gas film stiffness are trade-off relations, being difficult to optimize both parameters at the same time. Therefore, in this study, sufficient stiffness is selected for safety. The whole structure of the dry gas seal with the gas film is modeled as spring and damper as shown later. Therefore, from the calculation of a linear vibration waveform, the minimum film thickness is obtained. Under the conditions presented in Table 1, Ref. [19], the required gas lubricated film stiffness is defined. Because the leakage rate is strongly affected by film thickness, the value is fixed as 5 μm in this optimization as shown in Table 1.
Parameter | Values |
---|---|
Stator mass | 1.0 kg |
Support spring | 5.0 × 105 N/m |
Steady-state clearance | 5 μm |
Assumed disturbance | 5 G |
Viscosity of the air | 1.82 × 10−5 Pa·s |
Compressibility number | 100–750 |
Outer side pressure | 0.5–10 MPa |
Inner side pressure | 0.1 MPa |
Dry gas seal physical parameters.
The optimization method in this study is based on Hashimoto and Ochiai’s topological optimum design theory [17]. The outline of the method is as follows. The initial groove geometry is the usual spiral groove shape, and then, cubic spline interpolation functions are applied to the initial geometry with 4 grids. Moving the grids on the same circumferences changes the groove shape. Applying the optimum design method, an optimized seal groove shape is obtained. Simultaneously, the number of grooves
where, the
Geometry of a seal and optimum design variables.
In the optimum design, the objective functions should be defined. Obviously, the most important one is to minimize the leakage
Moreover, even if a lesser leakage design is available, it is impractical to have a lesser dynamic stiffness simultaneously. Since dry gas seals are usually used under high speed and high-pressure differential conditions, sudden contact on the seal faces may lead to serious accidents. Therefore, the dynamic stiffness
The constraint relationships in this optimization are
where
The
The optimum design problem is formulated as
The analysis method to calculate the seal characteristics is shown below. During the optimum design calculations, the groove shape should be changed continuously from its original spiral groove shape into other shapes. Therefore, a boundary-fitted coordinate system is adopted as the numerical calculation method [15]. Moreover, a divergence formulation method is implemented. A Reynolds equivalent equation obtained from flow balance as shown in Figure 3 is used to obtain the pressure distributions on the seal face. This is because the geometry has a step over which there is a discontinuous pressure gradient between the groove and the land areas.
Control volume and flow rates.
The Reynolds equivalent equation [16] is
Subscripts 1, 2, and
where the mass flow rates through the various boundaries are
The coefficients of
Assuming a small amplitude vibration of the seal with frequency
where,
Substituting Eq. (12) into Eq. (7) and neglecting seconds terms of
Discretizing Eqs. (13) and (14), and then solving the equations numerically, the static and dynamic components of the gas pressure fields are obtained. Finally, the gas leakage rate
Moreover, assuming the simple vibration model of a dry gas seal shown in Figure 4, the dynamic stiffness
Simple vibration model of the dry gas seal.
Using the method mentioned above, topological optimum calculations were conducted. The calculation conditions are shown in Tables 1 and 2, and Figure 2. As shown in Table 1, the mass of stator
Parameters | Values |
---|---|
Groove number | 6,8,10,12,14,16,18,20,22,24 |
Minimum groove depth | |
Maximum groove depth | |
Minimum angle amount | |
Maximum angle amount | |
Minimum groove width | |
Maximum groove width | |
Minimum seal radius to outer radius ratio | |
Maximum seal radius to outer radius ratio |
Parameters for optimum design study.
By solving the above optimum design problem, a multi objective genetic algorithm is used as this in a multi objective optimization [20].
Figure 5 shows the optimization results for operation with a compressibility number
The case of Pareto optimum solutions (Pi = 2.5 MPa, Λ = 500).
Seal shapes | Leakage flow rate | Dynamic stiffness |
---|---|---|
Spiral groove | 24.9 × 10−5 | 177 |
Maximum stiffness | 26.9 × 10−5 | 286 |
Minimum leakage | 18.8 × 10−5 | 28.9 |
Optimized geometry | 18.9 × 10−5 | 30.5 |
Characteristic values.
The initial shape of the spiral groove seal labeled (A) does not have the desired characteristics of both low gas leakage and high dynamic stiffness. Comparing the shapes of (A) through (D), from the point of view of minimizing the gas leakage, the shape of the groove is quite different from the initial spiral groove as shown in Figure 5B. The optimized shape has a bending curve in the vicinity of the outer diameter of the seal face. On the other hand, from the viewpoint of maximizing the dynamic stiffness, the shape of the groove, as shown in Figure 5C is similar to the spiral groove shape in Figure 5A. This is because a high positive dynamic pressure is required. It is well known that the spiral groove shape can effectively generate high positive pressure.
Thus, considering an allowable dynamic stiffness, the optimized shape as shown in Figure 5D is similar to the shape that minimizes gas leakage with a bending curve. However, the length of the bending curve is no longer that of the leakage minimized seal. This is due to gas flow around the outer vicinity of the gas seal face. The gas flow from the outer high pressure is retarded by the effect of the curved shape of the grooves. From these results, the most interesting thing is that quite a different shape is obtained for the case reducing gas leakage only. However, the results are valid only for the case of
Figure 6 depicts the tendency of change in the shape of the dry gas seal face on the Pareto optimum solution. Orienting the low leakage design, the strong bending shape in the outer vicinity and the wide plane region in the inner side are obtained. This bending shape reduces the leakage to the inner side of the seal by pump-out effect from the inner to the outer circumference side. On the other hand, emphasizing the stiffness design, it is found that the bending tendency goes weak and finally the shape goes to the spiral shape gradually.
Change in optimum shape tendency of the dry gas seal face.
From the point of view of the actual seal design, a wider range of operations is required. Therefore, the optimum design calculations were conducted over a wide range of conditions
Figure 7 depicts the optimized shape map for a wide range of inner static pressure at the outside diameter and compressibility numbers. There are three types of shapes, one is quite similar to the spiral groove shape and applicable to a low inlet pressure range of
Optimal design map under a wide range of conditions.
From the results, in the case of low inner static pressure conditions and a low compressibility number (
On the other hand, for a high inlet pressure or a high compressibility number condition, shown in the red area, the allowable film stiffness could be obtained easily as its basic ability. Because the high inlet pressure condition is expected to deliver a hydrostatic effect and the high compressibility number leads to an enhancement of the hydrodynamic effect. Hence, the main object of topological optimization is to reduce gas leakage. However, for a low inner static pressure condition, the hydrostatic effect is not expected. Therefore, the bending curve shape is weak. In other words, it is found that the topological optimization for reducing gas leakage is effective in the case of a high inner static pressure condition.
In order to consider the mechanism for reducing the gas leakage of the optimized shape, which is the interesting bending shape, a CFD analysis of the gas flow was conducted using commercial software (ANSYS FLUENT) which can solve the Navier-Stokes equation including the flow of outer side area of dry gas seal and considered to be obtained more accurate solution compared to usually used Reynolds equation, which is neglecting the outer side flow of seals. In the past work of Hashimoto[18], a similar bending shape is obtained in the case of maximizing the bearing stiffness on a high-speed air bearing. However, as mentioned in the previous sections, another tendency is obtained in this case. That is, the bending shape is obtained in the case of minimizing the air leakage instead of maximizing the stiffness. Therefore, the reason why this shape is obtained is unclear.
Figure 8 and Table 4 report the CFD calculation model and the specifications respectively. The inner and outer radii are same as our experimental equipment [21], Moreover, the groove depths and seal clearance of the seals are 60 μm and 30 μm respectively because of their mesh size limitations. The seal radius ratio (Rs/Ro) and Groove width ratios are chosen by representative values for each seal. In addition, Table 4 indicates the calculation conditions of CFD analysis. The inlet pressure, it means the outer side of the dry gas seal, is set as 0.11 MPa, and the rotational speed is set as 5000 rpm. These values are the same as the previous experiment. The calculations are conducted under the area of one groove pattern by using a periodic boundary condition. In addition, the calculation does not use the turbulent model and concludes choked flow. Because the Reynolds number of the gas seal flow is approximately
CFD analysis model.
Spiral groove | Optimized groove | |
---|---|---|
Outer radius | 32.0 mm | |
Inner radius | 25.6 mm | |
Groove depth | 60 μm | |
Seal Clearance | 30 μm | |
Seal radius ratio Seal radius ratio ( | 0.5 | 0.4 |
Groove width ratio | 0.86 μm | 0.93 μm |
Number of groove | 10 | 24 |
Seal specifications of CFD analysis.
Operating conditions | |
---|---|
Inlet pressure | 0.11 MPa |
Outlet pressure | 0.1 MPa |
Rotational speed | 5000 rpm |
Air temperature | 300 K |
Dynamic viscosity of air | 1.85 × 10−5 Pa·s |
Calculation conditions of CFD analysis.
Figure 9 shows the predicted (I) pressure distribution and (II) velocity distribution from the CFD analysis on the middle plane of gas film thickness comparing the conventional spiral grooved seal(a) versus the optimized seal(b). In this study, the film thicknesses are common. Therefore, the closing forces are different. In addition, the visualization areas are different in the two seals because the calculation area depends on the groove shape intervals.
CDF analysis results of pressure and velocity distributions on grooved seals.
From the results in Figure 9(I), high pressure is generated on the outer region of the seal caused by the hydrostatic effect. However, the high-pressure area in the optimized seal is narrow compared with that of the spiral grooved seal. Moreover, the velocities on the flow in the optimized seal are faster than those in the spiral grooved seal. This is due to groove shape in the outer radius vicinity. The groove shape of the spiral groove is formed along the rotational direction. Consequently, outer air is drawn into the seal and the air velocity is fast. On the other hand, with the optimized seal face, the gas flow velocity in the outer vicinity reduces because the inflow is suppressed by the pump effect of the bending shape groove. As mentioned earlier, reducing the gas inlet flow velocity on the optimized seal face leads to reduce the gas overall leakage.
Moreover, comparing both the Reynolds equation and the CFD results of load-carrying capacity and amount of leakage, are shown in Table 6. As shown in the Table, the load-carrying capacity is in very good agreement with both results. On the other hand, the amount of leakage, there is a little difference in both analytical solutions. This is because the amount of leakage is calculated using pressure difference and it is easy to include the numerical error. Besides, the load-carrying capacity is calculated by the integration of pressure distribution. Therefore, it is considered that the numerical error is very small. However, the difference in the amount of leakages is acceptable.
Reynolds Eq. | CFD | ||
---|---|---|---|
Load carrying capacity (kg) | Spiral | 0.79 | 0.76 |
Optimized | 0.76 | 0.71 | |
Amount of leakage (10−5 kg/s) | Spiral | 7.87 | 8.19 |
Optimized | 5.70 | 5.81 |
Comparison of Reynolds equation to CFD.
Finally, the experimental verification of flow visualization is mentioned. The experimental visualization results are picked up from our past research work [21, 22].
The experimental conditions are same as Tables 4 and 5, except the groove depth of 70μm and the seal clearance of 50μm. Here, the main purpose of the verification is to confirm the qualitative flow difference, therefore we think the comparison is meaningful even if the values between the CFD and experimental visualization are not the same. The specific visualization setup and spec are shown in the previous studies.
Figure 10 depicts the experimental visualization results of our previous study [21]. The velocity distributions are shown as color arrows. The outer side gas flows strongly into the spiral groove seal face through the boundary as shown in Figure 10a. On the other hand, in the case of optimized seal, the flows are very weak compared to that of spiral groove seal. The same tendencies are shown in the CFD analysis results, and the applicability of the optimization was verified experimentally.
Experimental visualization results [
In this study, a topological optimization of the groove shape on a dry gas seal is conducted to improve its sealing characteristics. The main conclusions are as follows:
The groove shape of the topological optimum design to minimize gas leakage has a bending curve near the outer radius of the rotating seal face. On the other hand, the optimum groove shape when maximizing the gas film stiffness becomes quite similar to that of a spiral grooved shape.
For the purpose of obtaining a workable solution over a wide range of operating conditions, an allowable gas film stiffness is adopted. As a result, the optimum shape pattern is similar to that of the spiral groove under conditions of low inner static pressure and low compressibility number. For high inner static pressure and high compressibility number conditions, the outer groove shape bends. The tendency of bending becomes stronger with an increase in the inner static pressure at the outside diameter and the compressibility number.
CFD analysis reveals that the inflow velocity in the optimized seal is low compared with that in a conventional spiral groove seal. The newly found outer bending curve shape of the groove leads to suppress the inflow. Moreover, the same tendency is shown in experimental visualization.
We would like to express our sincere gratitude to Professor Hiromu Hashimoto for his appropriate suggestions, Professor Luis San Andres for his polite advice, and all the students who have supported this research.
a | a parameter related to the inflow angle β used to define a spiral curvature |
b1 | width of groove [m] |
b2 | width of land [m] |
c | damping coefficient of gas film [N·s/m] |
f(X) | objective function [N/m] |
gi(X) (i =1∼2n+2) | constraint function |
hg | groove depth [m] |
hr | gas film thickness [m] |
k | spring coefficient of gas film |
k1 | spring coefficient of support spring |
N | number of grooves |
ns | shaft angular speed [rpm] |
p0 | static component of gas film pressure (absolute pressure) [Pa] |
pa | atmospheric pressure at inside diameter[Pa] |
PI | inner side pressure [Pa] |
PO | outer side pressure [Pa] |
pt | dynamic component of gas film pressure [Pa] |
q | leakage gas mass flow rate [kg/s] |
r | coordinate of radial direction [m] |
ri | inside radius of seal [m] |
ro | outside radius of seal [m] |
rs | inner radius of the grooves [m] |
Rs | seal diameter ratio (= rs /ro) |
Rr | ratio between inside radius and outside radius of seal (=r i /r o) |
X | vector of variables used in calculations |
α | groove width ratio =b1 /(b1+ b2 ) |
β | inflow angle [rad] |
Δr | equipartition space of r[m] |
θ | coordinate of circumferential direction [rad] |
Θi | angle of basic geometry (spiral curvature) at the ith nodal point [rad] |
ϕi | extent of angle change from basic geometry (spiral curvature) at the ith nodal point [rad] |
δϕI | extent of angle change during optimization at the ith nodal point [rad] |
Λ | compressibility number = 6μω s /Pa)*(r1/hr)2 |
μ | viscosity of gas [Pa·s] |
ρ | density of gas [kg/m3] |
ξ | coordinates of change based on boundary fitted coordinate system [m] |
η | coordinates of change based on boundary fitted coordinate system [rad] |
ωf | angular velocity of squeeze motion [rad/s] |
ωs | angular velocity of shaft rotation [rad/s] |
max | maximum value of state variables |
min | minimum value of state variables |
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