This invention relates to the production of metals and alloys using the Armstrong Process.
The present invention relates to the production of metals and alloys using the general method disclosed in U.S. Pat. Nos. 6,409,797; 5,958,106; and 5,779,761, all of which are incorporated herein, and preferably a method wherein titanium or an alloy thereof is made by the reduction of halides in a stream of reducing metal. Although the method disclosed herein is applicable to any of the hereinafter disclosed elements or alloys thereof, the invention will be described with respect to titanium and its alloys, simply because the available supply of titanium in the United States is now insufficient to meet the demand. Moreover, as the cost of titanium and its alloys is reduced by the use of the foregoing method, the demand will increase even beyond that already estimated by the aerospace companies and the Department of Defense.
Titanium is a very plentiful element distributed throughout the world, but it is very costly because of the antiquated methods by which it is produced. As is well known in the art, the Kroll and Hunter processes are the principal processes by which titanium is produced worldwide. Both of these processes are batch processes which produce in the first instance, a fused material of titanium and salt and excess reducing metal, magnesium for the Kroll process and sodium for the Hunter process. This fused material (known as sponge) then must be removed from the containers in which it was made, crushed and thereafter electrolytically purified in repeated steps.
The invention hereinafter described is a refinement of the Armstrong Process disclosed in the above incorporated U.S. patents.
Because titanium is an extremely reactive metal and is produced by the Armstrong Process as a very fine powder, generally with average diameters in the 0.1 to 1 micron range as calculated from BET surface area measurements, it is thereafter maintained at elevated temperature in order to increase the average particle diameter to greater than 1 micron. But, even at the large diameters, the powder is difficult to handle unless it has been passivated. By passivation, it is meant that a small amount of oxygen is introduced to the powder to form titanium dioxide on the surface so that the powder is not incendiary when exposed to air. Too much oxygen will increase the oxygen content beyond the ASTM specification for CP titanium grade 2 or for ASTM grade 5 titanium, that is 6/4 alloy (6% Al, 4% V by weight with the balance Ti). Heretofore, it was believed that the only practical way to passivate titanium powder was to bleed an inert gas such as argon with a very small percentage of oxygen for a time sufficient to increase the oxygen content on the surface of the powder to prevent spontaneous combustion when exposed to air. The times for passivation were measured in hours and was a design issue for large scale commercial plants based on a continuous process.
However, it has been unexpectedly and surprisingly found that passivation of titanium powder and/or titanium alloy powder can be accomplished by direct exposure to air and/or water and/or brine under certain conditions, which not only decrease the passivation time but also simplifies equipment design, thereby making the process simpler, more efficient and less expensive.
Accordingly, it is a principal object of the present invention to provide a method of producing passivated friable metal powder without the previous requirements for long periods of passivation.
Another object of the present invention is to provide a method of producing passivated metal powder, comprising introducing a metal halide vapor into a stream of liquid alkali or liquid alkaline earth metal or mixtures thereof forming a reaction zone in which the halide vapor is reduced by the liquid metal present in sufficient excess of stoichiometric such that the metal powder from the reduction of the halide vapor by the liquid metal is friable, separating at least most of the excess liquid metal from the reaction products, growing the metal powder until the particles forming the metal powder have average diameters calculated from BET surface area measurement greater than about one micron, cooling the metal powder, and contacting the cooled metal powder directly with air and/or water and/or brine to passivate and produce friable metal powder.
Another object of the invention to provide a method of producing passivated metal powder, comprising introducing a halide vapor of the metal into a stream of liquid sodium or liquid magnesium metal forming a reaction zone in which the halide is reduced by the liquid sodium or magnesium metal present in sufficient excess of stoichiometric such that the metal powder formed by the reduction of the halide vapor by the liquid sodium or magnesium metal is friable, separating reaction products from at least most of the excess sodium or magnesium metal, maintaining the metal powder at elevated temperature for a time sufficient to grow the powder until the particles forming the powder have average diameters calculated from BET surface area measurement greater than about one micron, cooling the metal powder to less than about 100° C., and contacting the cooled metal powder with air and/or water and/or brine to passivate and produce friable metal powder.
Yet another object of the invention is to provide a method of producing passivated Ti or Ti alloy powder with oxygen concentrations of less than about 1800 parts per million (ppm), comprising introducing a halide vapor of Ti or the metal constituents of the alloy into a stream of a liquid alkali or a liquid alkaline earth metal or mixtures thereof forming a reaction zone in which the halide is reduced by the liquid metal present in sufficient excess of stoichiometric such that Ti or Ti alloy powder from the reduction of the halide by the liquid metal is friable, separating Ti or Ti alloy powder reaction products from at least most of the excess liquid metal, maintaining the Ti or Ti alloy powder at elevated temperature for a time sufficient to grow the particles forming the Ti or Ti alloy powder to average diameters calculated from BET surface area measurement greater than about one micron, cooling the Ti or Ti alloy powder, and directly contacting the cooled Ti or Ti alloy powder with one or more of air and water and brine to passivate and produce friable powder while maintaining the oxygen concentration below about 1800 ppm.
Still a further object of the invention is to provide a method of producing passivated Ti or Ti alloy particles with oxygen concentrations of less than about 900 parts per million (ppm), comprising introducing a halide vapor of Ti or the metal constituents of the alloy at sonic velocity or greater into a stream of liquid alkali or liquid alkaline earth metal or mixtures thereof forming a reaction zone in which the halide is reduced by the liquid metal present in sufficient excess of stoichiometric such that Ti or Ti alloy powder from the reduction of the halide by the liquid metal is friable, separating by filtration and distillation excess liquid metal from the Ti or Ti alloy powder at least in part under vacuum, maintaining the Ti or Ti alloy powder at elevated temperature in a vacuum or an inert atmosphere or a combination thereof for a time sufficient to grow the particles forming the powder to average diameters calculated from BET surface area measurement greater than about one micron, cooling the Ti or Ti alloy powder to temperature of about 70° C. or less, and contacting the cooled Ti or Ti alloy powder with air to passivate the particles while maintaining the oxygen concentration of the powder below about 900 ppm, and washing the passivated powder to produce friable metal powder and to remove other reaction products.
A final object of the invention is to provide a system producing passivated and friable metal particles, comprising a storage container holding a supply of halide of the metal or alloys to be produced, a storage container holding a supply of reducing metal, pump mechanism establishing a flowing stream of liquid reducing metal, mechanism including nozzles for introducing halide vapor into the flowing stream of liquid reducing metal forming a reaction zone and producing reaction products of metal powder and a halide salt, wherein the liquid metal is present in a stoichiometric excess sufficient to maintain the temperature of the reaction products away from the reaction zone below the sintering temperature of the metal powder, separation equipment including one or more of filtration mechanism, distillation mechanism, mechanism for contacting reaction products with hot and/or cold gas for heating and/or cooling reaction products and for separating reducing metal from the metal powder while growing the particles forming the metal powder to have average diameters calculated from BET surface area measurement greater than about one micron, and mechanism contacting cooled metal powder with air and/or water and/or brine to passivate and produce friable metal powder and to separate the salt from the friable metal powder.
The invention consists of certain novel features and a combination of parts hereinafter fully described, illustrated in the accompanying drawings, and particularly pointed out in the appended claims, it being understood that various changes in the details may be made without departing from the spirit, or sacrificing any of the advantages of the present invention.
For the purpose of facilitating an understanding of the invention, there is illustrated in the accompanying drawings a preferred embodiment thereof, from an inspection of which, when considered in connection with the following description, the invention, its construction and operation, and many of its advantages should be readily understood and appreciated.
Referring to the drawings, there is disclosed a system 10 from which is produced friable and passivated metal powder. The metals and the alloys of which may be made according to the system hereinafter described are Ti, Al, Sn, Sb, Be, B, Ta, Zr, V, Nb, Mo, Ga, U, Re, Si or alloys thereof, all as previously disclosed in the above referenced and incorporated patents. The system 10 includes a sodium supply system 11, a chloride supply system 12, a reactor 15, a distillation system 16, a growing system 17, a cooling system 18, a washing system 19 and a drying system 21.
Although described herein with respect to chlorides and sodium reducing metal, it is clear that any halide may be used and a wide variety of alkali and alkaline earth metals or mixtures may be used. Commercially, sodium and magnesium are the most common reducing metals in the reduction of, for instance, titanium. Calcium has been used as a reducing metal in Russia. Although the system hereinafter described is specific to the chloride and to sodium, it is specifically intended that the invention is not so limited.
The sodium system 11 includes a sodium source 30 such as a common rail car, which is in communication with a heater 31 in order to liquify the sodium. The sodium heating system includes filters 32 with the requisite pumps 33 necessary to liquify sodium in a rail car 30 for transfer to sodium storage or an intermediate tank 35. The storage or intermediate tank 35 is provided with an inert atmosphere such as argon and is connected to a sodium substorage tank 40 which is provided with a pressure transmitter 41. Because the sodium in sodium storage tank 35 is liquid, there is a recirculation loop provided through filter 37 and a pump 38 which simply circulate sodium while it remains in the sodium storage tank and of course, there is provided the usual temperature sensors, pressure sensors and other engineering devices, not shown for purposes of clarity and brevity.
As used in the drawings, PT is a pressure transmitter, PSV is a relief valve; PSE is a rupture disc; PSH is a pressure switch; FT is a flow transmitter and CV is a flow control valve. These standard engineering sensors and controls will not be further described.
The sodium supply system 11 further includes a cooling fan 42 in conjunction with a series of sodium transfer pumps 43 which may be electromagnetic and filters 44 for pumping sodium from the storage tanks 35 and 40 to a sodium make-up 45 for loop one, and sodium make-up 46 for loop 2.
The system 10 is configured for two reactor modules as each reactor module can produce 2 million pounds of titanium or titanium alloy, or other metal alloys as previously set out, per year, so that a 4 million pound a year plant would have two operational reactors 15, whereas a 40 million pound plant would have 20 operational reactors 15.
As seen particularly in
Referring to
For an alloy such as the most commonly used 6/4 titanium alloy consisting essentially of 6% aluminum and 4% percent vanadium and described as ASTM B 265, grade 5, Ti 5 alloy, there has to be provided a vanadium chloride boiler 83 and a vanadium chloride boiler 84 connected by pumps 81 to a vanadium chloride day tank 80. Each of the vanadium chloride boilers 83 and 84 is provided with its own heater 86 and is connected by various piping manifolds to the reactors 15 as hereinafter will be set forth. Similarly, a aluminum chloride day tank 90 is provided and is connected by a series of valves 91 to aluminum chloride boilers 93 and 94. Each of the boilers 93 and 94 is provided with a heater 96 and unloading tank 97 and scales 98 in order to weigh the amount of aluminum chloride which is used in the production of the alloy. The difference between the system for aluminum chloride and vanadium chloride is that aluminum chloride is a solid at room temperature and may be transmitted as a solid through the valves 91 from the day tank 90 to the boilers 93. The scales 98 are used to ensure the correct amount of aluminum chloride is thereafter provided to the boilers 93 and 94. As indicated, the various halides or chlorides of the alloy constituents are fed from the boilers via pipes, valves and the like to a common pipe or manifold prior to the entry into the associated reactor 15 with the liquid reducing metal such as, but not limited to liquid sodium or liquid magnesium flowing there through.
Referring now to
The reactor 15 is operated in a protective atmosphere and preferably in an argon atmosphere. Alternative inert gases such as helium may be used. The reaction products from the reactor are connected to a filter 110 which permits liquid reducing metal to be drawn therefrom into the head tank 52 and then back into the sodium supply system 11.
The filter 110 is provided with a valve 111 and is connected to a vacuum system 112 so that a collection pipe 115 surrounded on one side by valve 111 and on the other side by valve 114 is under vacuum and sodium draining from the reaction products slurry of metal powder and salt is directed through a filter (not shown) to a line to condenser drain 53 and hence back to the sodium supply system 11.
From the collection pipe 115 the material, now free of most of the sodium or liquid reducing metal, is introduced into a distillation screw conveyor 120, the screw conveyor being provided with an outlet 125 or collection pipe and two valves 121 and 123, so as to connect the distillation screw conveyor to a vacuum system 122 and insulate the distillation conveyor from the heat treatment calciner 130, as will be explained.
As material is moved by the distillation conveyor 120 in the form of an auger, sodium drained from the distillation conveyor 120 is conducted via a line to condenser drain 54 and returned to the sodium supply 11. Since the distillation screw conveyor 120 is connected by a header 56 to the condenser 55, cooling fan 54 and condensate reservoir 58, the reducing metal vapor is removed in the distillation screw conveyor and again returned as previously described by the pumps 62 to the sodium supply system 11.
It is clear that the majority of the excess sodium in this system is removed from the product and returned to the sodium supply system leaving only entrained sodium and sodium used in the production of the salt which is lost. The salt may or may not be split electrolytically to recirculate the sodium, depending on economics.
The growing station 17 is illustrated particularly in
The cooling and passivation conveyor 135 reduces the temperature of the material therein from the temperature in the calciner 130 which preferably is somewhat in the excess of 700° C. preferably about 750° C., down to less than 100° C. at the outlet 136 and preferably about 80° C. or less. At this point in the process, almost all of the sodium except for that entrained within the particles has been removed, and the remaining reaction products, that is a mixture of salt and metal powder, are conveyed to the cake silo diverter valve 139 and hence through outlets 141 and 142 to the cake storage silo 151 and 152, as best seen in
The cake silos 151, 152 are at temperatures less than 100° C. preferably 80° C. or less, and most preferably 40°-80° C. The washed powder outlet chute 177 connected to the vacuum belt filter 170 directs powder which has been passivated and washed with water and/or brine to an inerted turbo dryer 180. A fines collection filter press 179 is in communication with the powder conveyor housing 171 near the outlet chute 177 to collect fines from the conveyor 170.
The inerted turbo dryer 180 is connected to a condenser 181, a condenser fan 182 and condensate return pump 183 through which the moisture is removed from the passivated and now friable powder, the moisture being returned or disposed of as economics dictate. The inerted turbo dryer 180, as previously stated, is under a protective atmosphere such as argon or nitrogen, and therefore, an argon or nitrogen inlet 185 is connected to protection to the powder after passivation while it is at elevated temperatures.
Finally, a product outlet 190 leads from the turbo dryer 180 to a series of drums 192 which may be stationed beneath the outlet 190 and filled at a rate according to the system design.
Operationally, and by way of example only, without limiting the invention, the sodium storage tank is preferably maintained at an elevated temperature so that the sodium therein is liquid. The melting point of sodium is about 98° C. so that the sodium storage tanks 35 and 40 are maintained about 105° C. whereas the sodium head tank 52 is maintained at about 125-300° C., preferably about 125° C. Exact temperatures and/or pressures hereinafter set forth are subject to engineering considerations so the ranges are by way of example only and are not intended to limit the invention.
The titanium tetrachloride boilers 73, 74 are maintained at about 220° C. resulting in pressures of about 500 kPa but may be at pressures up to about 800 kPa. Both the vanadium chloride boilers 83, 84 as well as aluminum chloride boilers 93, 94 are maintained at pressures greater than the titanium tetrachloride boilers because the vapors from each of the alloy constituent boilers have to be at pressures greater than the titanium chloride boilers so as to prevent titanium chloride from backing up into the alloy constituent boilers. For instance, if the titanium tetrachloride boilers 73, 74 are at 500 kPa, then the VCl4, AlC4 boilers are maintained at about 800 kPa.
The reactor 15 may be operated with an inlet temperature of about 260° C. with the outlet temperature about 100° C. greater, or about 360° C. Higher or lower inlet temperatures are possible. The distillation conveyor 120 is preferably, but not necessarily, operated at about 538° C. but may be operated from about 450° C. up to about 550° C. depending on the vacuum value of the system, the better the vacuum the lower the distillation temperature can be. The calciner 130 is preferably operated at about 750° C. for approximately 6 hours in order to grow the metal particles forming the powder. Again, engineering considerations are taken into account between the equipment size, residence time and the temperature at which the particle growth is maintained. Temperatures of 700° or above are practical, but again, the lower the temperature, the longer the residence time in order to achieve the same particle growth. The cooling passivation conveyor 135 preferably has an inlet temperature which is generally equal to the outlet temperature of the calciner 130 such as about 750° and an outlet temperature preferably in the range of between about 40° C. to 80° C. The higher the outlet temperature the greater the oxygen pick-up of the metal powder, but temperatures in the range of from about 40° C. to about 80° C. are preferred with 40° C. providing better results than the 80° C. temperature.
The cooling and heating in the system 10 is by means of heat transfer through coils in which oil is used as a heat transfer medium for safety considerations. The silos 151 and 152 are generally operated at ambient temperatures in air and stay principally at the temperatures in which the powder is introduced from the conveyor 135, that is in the range between about 40° C. and 80° C. Washing after air passivation or directly without air passivation is done at ambient temperature and the last wash, that is water from the fresh water tank 165 may be warmed to facilitate dissolving salt and warming the powder for entry into the inerted turbo dryer 180.
Generally, the powder entering the turbo dryer 180 is at a temperature in the range of from ambient water tap temperature to about 70° C.
Finally, the powder leaving the inerted turbo dryer 180 at the outlet 190 is preferably at a temperature of about 60° C. at which the powder is not too reactive, it being understood that at higher temperatures, powder is more reactive than at lower temperatures, particularly powder in the 1-10 micron range, which is the preferred particle size as determined by BET measurement after the particles forming the powder exit the calciner 130. As understood from the incorporated patents, metal particles coming out of the reactor 15 generally have average diameters in the range of from about 0.1 to about 1 micron as calculated from BET surface area measurement. However, these particles are too small for many powder metallurgy usages and therefore, need to be grown which is the purpose of the calciner 130. Although maintaining the powder at elevated temperatures causes the particles to grow so that some growth takes place in the filter 115, the distillation conveyor 120 and thereafter during transfer to the heat calciner 130, the majority of the particle growth occurs in the calciner 130, with temperatures for CP titanium or titanium 6/4 alloy of about 750° C. and a residence time of about 6 hours. The system 10, can be designed for various production rates and the equipment dimensions and operating conditions will change as will be understood by an engineer of ordinary skill in this art. Although argon has been indicated as the preferred inert gas, if the temperatures are maintained low enough, nitrogen can be used without deleteriously affecting the powder as well as neon or other inert gases. Although designed herein without blowers, the cake silos 151 and 152 may need blowers in order to circulate additional air to passivated the cake produced from the cooling and passivation conveyor 135. Moreover, passivation could take place by means of contacting the powder after cooling with a mixture of an inert gas and up to about 20% oxygen in countercurrent relationship, but the method before described is preferred.
It should be understood that material entering the cooling and passivation conveyor 135 is under a protective atmosphere from the heat treatment calciner 130 but exits through the conveyor exit 136 at lower temperatures and with some air being present. An alternative method for passivation is to introduce the powder directly into the washing and drying system 19 rather than using first air passivation and thereafter washing. It is preferred to use air passivation first and then washing after passivation, but it may be preferable for reasons of cost and economy, immediately to wash after the powder comes out of the cooling passivation conveyor 135. Although air passivation followed by washing provides a lower oxygen concentration, for instance 900 ppm for CP titanium, that corresponds to ASTM B265 grade 1 titanium, whereas direct water washing (water and/or brine) without air passivation has provided oxygen concentrations of about 1800 ppm. The lower oxygen content may not always be required, depending upon the end use of the powder. Therefore, either water and/or brine passivation directly or air passivation directly may be employed or a combination thereof, that is air passivation followed by washing in which some passivation be used.
While the invention has been particularly shown and described with reference to a preferred embodiment hereof, it will be understood by those skilled in the art that several changes in form and detail may be made without departing from the spirit and scope of the invention.
Number | Name | Date | Kind |
---|---|---|---|
1771928 | Jung | Jul 1930 | A |
2205854 | Kroll | Jun 1940 | A |
2607675 | Gross | Aug 1952 | A |
2647826 | Jordan | Aug 1953 | A |
2816828 | Benedict et al. | Dec 1957 | A |
2823991 | Kamlet | Feb 1958 | A |
2827371 | Quin | Mar 1958 | A |
2835567 | Willcox | May 1958 | A |
2846303 | Keller et al. | Aug 1958 | A |
2846304 | Keller et al. | Aug 1958 | A |
2882143 | Schmidt | Apr 1959 | A |
2882144 | Follows et al. | Apr 1959 | A |
2890112 | Winter | Jun 1959 | A |
2895823 | Lynskey | Jul 1959 | A |
2915382 | Hellier et al. | Dec 1959 | A |
2941867 | Maurer | Jun 1960 | A |
2944888 | Quin | Jul 1960 | A |
3058820 | Whitehurst | Oct 1962 | A |
3067025 | Chisholm | Dec 1962 | A |
3085871 | Griffiths | Apr 1963 | A |
3085872 | Kenneth | Apr 1963 | A |
3113017 | Homme | Dec 1963 | A |
3331666 | Robinson et al. | Jul 1967 | A |
3519258 | Ishizuka | Jul 1970 | A |
3535109 | Ingersoll | Oct 1970 | A |
3650681 | Sugahara et al. | Mar 1972 | A |
3825415 | Johnston et al. | Jul 1974 | A |
3836302 | Kaukeinen | Sep 1974 | A |
3847596 | Holland et al. | Nov 1974 | A |
3867515 | Bohl et al. | Feb 1975 | A |
3919087 | Brumagim | Nov 1975 | A |
3927993 | Griffin | Dec 1975 | A |
3943751 | Akiyama et al. | Mar 1976 | A |
3966460 | Spink | Jun 1976 | A |
4007055 | Whittingham | Feb 1977 | A |
4009007 | Fry | Feb 1977 | A |
4017302 | Bates et al. | Apr 1977 | A |
4070252 | Bonsack | Jan 1978 | A |
4128421 | Marsh et al. | Dec 1978 | A |
4141719 | Hakko | Feb 1979 | A |
4149876 | Rerat | Apr 1979 | A |
4190442 | Patel | Feb 1980 | A |
4331477 | Kubo et al. | May 1982 | A |
4379718 | Grantham et al. | Apr 1983 | A |
4401467 | Jordan | Aug 1983 | A |
4402741 | Pollet et al. | Sep 1983 | A |
4414188 | Becker | Nov 1983 | A |
4423004 | Ross | Dec 1983 | A |
4425217 | Beer | Jan 1984 | A |
4432813 | Williams | Feb 1984 | A |
4445931 | Worthington | May 1984 | A |
4454169 | Hinden et al. | Jun 1984 | A |
4518426 | Murphy | May 1985 | A |
4519837 | Down | May 1985 | A |
4521281 | Kadija | Jun 1985 | A |
4555268 | Getz | Nov 1985 | A |
4556420 | Evans et al. | Dec 1985 | A |
4604368 | Reeve | Aug 1986 | A |
4606902 | Ritter | Aug 1986 | A |
RE32260 | Fry | Oct 1986 | E |
4687632 | Hurd | Aug 1987 | A |
4689129 | Knudsen | Aug 1987 | A |
4725312 | Seon et al. | Feb 1988 | A |
4828008 | White et al. | May 1989 | A |
4830665 | Winand | May 1989 | A |
4839120 | Baba et al. | Jun 1989 | A |
4877445 | Okudaira et al. | Oct 1989 | A |
4897116 | Scheel | Jan 1990 | A |
4902341 | Okudaira et al. | Feb 1990 | A |
4915729 | Boswell et al. | Apr 1990 | A |
4923577 | McLaughlin et al. | May 1990 | A |
4940490 | Fife et al. | Jul 1990 | A |
4941646 | Stelts et al. | Jul 1990 | A |
4985069 | Traut | Jan 1991 | A |
5028491 | Huang et al. | Jul 1991 | A |
5032176 | Kametani et al. | Jul 1991 | A |
5055280 | Nakatani et al. | Oct 1991 | A |
5064463 | Ciomek | Nov 1991 | A |
5082491 | Rerat | Jan 1992 | A |
5147451 | Leland | Sep 1992 | A |
5149497 | McKee et al. | Sep 1992 | A |
5160428 | Kuri | Nov 1992 | A |
5164346 | Giunchi et al. | Nov 1992 | A |
5167271 | Lange et al. | Dec 1992 | A |
5176741 | Bartlett et al. | Jan 1993 | A |
5176810 | Volotinen et al. | Jan 1993 | A |
5211741 | Fife | May 1993 | A |
5259862 | White et al. | Nov 1993 | A |
5338379 | Kelly | Aug 1994 | A |
5356120 | König et al. | Oct 1994 | A |
5427602 | DeYoung et al. | Jun 1995 | A |
5437854 | Walker et al. | Aug 1995 | A |
5439750 | Ravenhall et al. | Aug 1995 | A |
5448447 | Chang | Sep 1995 | A |
5460642 | Leland | Oct 1995 | A |
5498446 | Axelbaum et al. | Mar 1996 | A |
5580516 | Kumar | Dec 1996 | A |
H1642 | Jenkins | Apr 1997 | H |
5637816 | Schneibel | Jun 1997 | A |
5779761 | Armstrong et al. | Jul 1998 | A |
5897830 | Abkowitz et al. | Apr 1999 | A |
5914440 | Celik et al. | Jun 1999 | A |
5948495 | Stanish et al. | Sep 1999 | A |
5951822 | Knapick et al. | Sep 1999 | A |
5954856 | Pathare et al. | Sep 1999 | A |
5958106 | Armstrong et al. | Sep 1999 | A |
5986877 | Pathare et al. | Nov 1999 | A |
5993512 | Pargeter et al. | Nov 1999 | A |
6010661 | Abe et al. | Jan 2000 | A |
6027585 | Patterson et al. | Feb 2000 | A |
6040975 | Mimura | Mar 2000 | A |
6099664 | Davies | Aug 2000 | A |
6103651 | Leitzel | Aug 2000 | A |
6136062 | Loffeholz et al. | Oct 2000 | A |
6180258 | Klier | Jan 2001 | B1 |
6193779 | Reichert et al. | Feb 2001 | B1 |
6210461 | Elliott | Apr 2001 | B1 |
6238456 | Wolf et al. | May 2001 | B1 |
6309570 | Fellabaum | Oct 2001 | B1 |
6309595 | Rosenberg et al. | Oct 2001 | B1 |
6409797 | Armstrong et al. | Jun 2002 | B2 |
6432161 | Oda et al. | Aug 2002 | B1 |
6488073 | Blenkinsop et al. | Dec 2002 | B1 |
6502623 | Schmitt | Jan 2003 | B1 |
6602482 | Kohler et al. | Aug 2003 | B2 |
6689187 | Oda | Feb 2004 | B2 |
6727005 | Gimondo et al. | Apr 2004 | B2 |
6745930 | Schmitt | Jun 2004 | B2 |
6824585 | Joseph et al. | Nov 2004 | B2 |
6861038 | Armstrong et al. | Mar 2005 | B2 |
6884522 | Adams et al. | Apr 2005 | B2 |
6902601 | Nie et al. | Jun 2005 | B2 |
6921510 | Ott et al. | Jul 2005 | B2 |
6955703 | Zhou et al. | Oct 2005 | B2 |
7041150 | Armstrong et al. | May 2006 | B2 |
7351272 | Armstrong et al. | Apr 2008 | B2 |
7410610 | Woodfield et al. | Aug 2008 | B2 |
7435282 | Armstrong et al. | Oct 2008 | B2 |
7445658 | Armstrong et al. | Nov 2008 | B2 |
7501007 | Anderson et al. | Mar 2009 | B2 |
7501089 | Armstrong et al. | Mar 2009 | B2 |
7621977 | Anderson et al. | Nov 2009 | B2 |
20020050185 | Oda | May 2002 | A1 |
20020152844 | Armstrong et al. | Oct 2002 | A1 |
20030061907 | Armstrong et al. | Apr 2003 | A1 |
20030145682 | Anderson et al. | Aug 2003 | A1 |
20040123700 | Zhou et al. | Jul 2004 | A1 |
20050025699 | Reed et al. | Feb 2005 | A1 |
20050081682 | Armstrong et al. | Apr 2005 | A1 |
20050150576 | Venigalla | Jul 2005 | A1 |
20050225014 | Armstrong et al. | Oct 2005 | A1 |
20050284824 | Anderson et al. | Dec 2005 | A1 |
20060086435 | Anderson et al. | Apr 2006 | A1 |
20060102255 | Woodfield et al. | May 2006 | A1 |
20060107790 | Anderson et al. | May 2006 | A1 |
20060123950 | Anderson et al. | Jun 2006 | A1 |
20060150769 | Armstrong et al. | Jul 2006 | A1 |
20060230878 | Anderson et al. | Oct 2006 | A1 |
20070017319 | Jacobsen et al. | Jan 2007 | A1 |
20070079908 | Jacobsen et al. | Apr 2007 | A1 |
20070180951 | Armstrong et al. | Aug 2007 | A1 |
20070180952 | Lanin et al. | Aug 2007 | A1 |
20080031766 | Ernst et al. | Feb 2008 | A1 |
20080152533 | Ernst et al. | Jun 2008 | A1 |
20080187455 | Armstrong et al. | Aug 2008 | A1 |
20080199348 | Armstrong et al. | Aug 2008 | A1 |
Number | Date | Country |
---|---|---|
587782 | Nov 1985 | AU |
2003263081 | Jun 2004 | AU |
2196534 | Feb 1996 | CA |
006615 | Feb 2006 | EA |
007634 | Dec 2006 | EA |
0298698 | Jan 1989 | EP |
0299791 | Jan 1989 | EP |
1441039 | Jul 2004 | EP |
1657317 | May 2006 | EP |
722184 | Jan 1955 | GB |
778021 | Jul 1957 | GB |
31007808 | Sep 1956 | JP |
49042518 | Apr 1974 | JP |
51010803 | Apr 1976 | JP |
60255300 | Dec 1985 | JP |
6112837 | Jan 1986 | JP |
62065921 | Mar 1987 | JP |
64047823 | Feb 1989 | JP |
4116161 | Apr 1992 | JP |
05078762 | Mar 1993 | JP |
10502418 | Mar 1998 | JP |
11090692 | Apr 1999 | JP |
2001279345 | Oct 2001 | JP |
90840 | Jan 1958 | NO |
411962 | Jan 1974 | SU |
WO9604407 | Feb 1996 | WO |
WO9824575 | Jun 1998 | WO |
WO2004022269 | Mar 2004 | WO |
WO2004022797 | Mar 2004 | WO |
WO2004022798 | Mar 2004 | WO |
WO2004022799 | Mar 2004 | WO |
WO2004022800 | Mar 2004 | WO |
WO2004026511 | Apr 2004 | WO |
WO2004028655 | Apr 2004 | WO |
WO2004033736 | Apr 2004 | WO |
WO2004033737 | Apr 2004 | WO |
WO2004048622 | Oct 2004 | WO |
WO2005019485 | Mar 2005 | WO |
WO2005021807 | Mar 2005 | WO |
WO2005023725 | Mar 2005 | WO |
WO2005042792 | May 2005 | WO |
WO2007044635 | Apr 2007 | WO |
WO2007089400 | Aug 2007 | WO |
WO2008013518 | Jan 2008 | WO |
WO2008079115 | Jul 2008 | WO |
Number | Date | Country | |
---|---|---|---|
20080152533 A1 | Jun 2008 | US |