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21. 发明授权

US4712371A Process and device for starting a gas turbine 失效
标题翻译：用于启动燃气轮机的过程和装置
公开(公告)号：US4712371A
公开(公告)日：1987-12-15
申请号：US797903
申请日：1985-11-14
申请人： Thomas Weber
发明人： Thomas Weber
IPC分类号： F02C7/272 , F02C7/27
CPC分类号： F02C7/272 , Y02T50/671
摘要： A process and a device for starting a gas turbine such as a jet engine which contains a compressor, a turbine and a combustion chamber by means of hot exhaust gases from an exhaust gas source, wherein the energy of the exhaust gases is transferred at least partially to the gas turbine for the starting process. For this purpose the hot exhaust gases are used for simultaneously driving the turbine and for igniting the combustion in the combustion chamber. A single exhaust gas source can be used. In this manner, a large number of component parts are eliminated and the reliability of the starting process is considerably increased overall.
摘要翻译：一种用于启动诸如喷气发动机的燃气轮机的方法和装置，其包含来自废气源的热废气的压缩机，涡轮机和燃烧室，其中废气的能量至少部分地转移到燃气轮机进行起动过程。为此，热废气用于同时驱动涡轮并用于点燃燃烧室中的燃烧。可以使用单个废气源。以这种方式，消除了大量的部件，并且总体上大大提高了起动过程的可靠性。

22. 发明授权

US3066487A Combustion starter having overspeed safety 失效
标题翻译：燃油起动器具有超速安全
公开(公告)号：US3066487A
公开(公告)日：1962-12-04
申请号：US73468458
申请日：1958-05-12
申请人： BENDIX CORP
发明人： FERGUSON JR JOHN H
IPC分类号： F02C7/272
CPC分类号： F02C7/272 , F05D2270/021

23. 发明授权

US2986005A Engine starting system 失效
标题翻译：发动机启动系统
公开(公告)号：US2986005A
公开(公告)日：1961-05-30
申请号：US80871459
申请日：1959-04-24
申请人： BOEING CO
发明人： DUDLEY JACK D
IPC分类号： F02C7/272
CPC分类号： F02C7/272

24. 发明授权

US2985104A Improved cartridge for producing gas 失效
标题翻译：改进的气瓶生产气瓶
公开(公告)号：US2985104A
公开(公告)日：1961-05-23
申请号：US47932155
申请日：1955-01-03
申请人： PHILLIPS PETROLEUM CO
发明人： FOX HOMER M
IPC分类号： C06B45/10 , F02C7/224 , F02C7/272 , F02C7/277 , F42B3/04 , F42B19/20
CPC分类号： F42B3/04 , C06B45/10 , F02C7/224 , F02C7/272 , F02C7/277 , F42B19/20

25. 发明授权

US2913872A Speed limiting arrangement for turbine rotors 失效
标题翻译：涡轮转子的限速装置
公开(公告)号：US2913872A
公开(公告)日：1959-11-24
申请号：US46164354
申请日：1954-10-11
申请人： GEN ELECTRIC
发明人： BLOOMBERG DAVID J
IPC分类号： F01D21/02 , F02C7/272 , F02C7/277
CPC分类号： F02C7/277 , F01D21/02 , F02C7/272 , Y02T50/671

26. 发明授权

US11512645B2 Solid-propellant gas generator assemblies and methods 有权
公开(公告)号：US11512645B2
公开(公告)日：2022-11-29
申请号：US16811673
申请日：2020-03-06
申请人： GOODRICH CORPORATION
发明人： Brian Wilson , Kevin Mueller
IPC分类号： F15B15/19 , F02C7/272 , F02K9/95 , F42B3/04 , F02C7/32
摘要： A solid-propellant gas generator assembly may comprise a bulkhead having an orifice disposed in a housing. The bulkhead may be disposed between a first end and a second end of the housing. The bulkhead and the first end may define a propellant cavity. The bulkhead and the second end may define a pressure chamber. A fast burning solid-propellant may be disposed in the propellant cavity. The solid-propellant gas generator assembly may be configured to replace a slow burning solid-propellant gas generator system in a solid-propellent gas generator system.

27. 发明申请

US20210277831A1 SOLID-PROPELLANT GAS GENERATOR ASSEMBLIES AND METHODS 有权
公开(公告)号：US20210277831A1
公开(公告)日：2021-09-09
申请号：US16811673
申请日：2020-03-06
申请人： GOODRICH CORPORATION
发明人： Brian Wilson , Kevin Mueller
IPC分类号： F02C7/272 , F02K9/95
摘要： A solid-propellant gas generator assembly may comprise a bulkhead having an orifice disposed in a housing. The bulkhead may be disposed between a first end and a second end of the housing. The bulkhead and the first end may define a propellant cavity. The bulkhead and the second end may define a pressure chamber. A fast burning solid-propellant may be disposed in the propellant cavity. The solid-propellant gas generator assembly may be configured to replace a slow burning solid-propellant gas generator system in a solid-propellent gas generator system.

28. 发明授权

US09951694B2 System and method for emergency starting of an aircraft turbomachine 有权
公开(公告)号：US09951694B2
公开(公告)日：2018-04-24
申请号：US15022101
申请日：2014-09-12
申请人： SNECMA , TURBOMECA , HERAKLES
发明人： Romain Thiriet , Patrick Marconi , Camel Serghine , Antoine Marie Georges Caratge , Francois Danguy , Laurent Fabbri , Pierre Yvart , Laurent Soulie , Philippe Barrat
IPC分类号： F02C7/27 , F01D19/00 , B64D27/10 , F02C7/277 , F02C7/272 , F02C6/20
CPC分类号： F02C7/277 , B64D27/10 , F01D19/00 , F02C6/206 , F02C7/272 , F05D2260/85 , Y02T50/672
摘要： An emergency start system for a turbine engine of an aircraft including at least one solid propellant gas generator, an electrically controlled ignition device, a computer connected to the ignition device, and at least one starter motor comprising a turbine for driving a shaft which is for coupling to a shaft of the turbine engine The outlet of the gases from the generator are connected to the inlet of the turbine of the starter motor.

29. 发明申请

US20050188701A1 Solid propellant gas generators in power systems 失效
标题翻译：电力系统中固体推进剂气体发生器
公开(公告)号：US20050188701A1
公开(公告)日：2005-09-01
申请号：US10789177
申请日：2004-02-26
申请人： Ru-Li Kung , Scott Goldberg , Alex Morando , Tom Iles
发明人： Ru-Li Kung , Scott Goldberg , Alex Morando , Tom Iles
IPC分类号： F02C1/00 , F02C3/26 , F02C7/272 , F02C7/32
CPC分类号： F02C7/272 , F02C1/00 , F02C7/32 , F05D2220/50 , Y02T50/671
摘要： An emergency power system comprising a plurality of solid propellant gas generators each having a gas outlet in fluid communication with a turbine wheel rotationally disposed within a gas turbine housing, the turbine wheel being in rotational communication with an electric generator input shaft, a fluid pump input shaft, or both. A method of producing power from such an emergency power system is also disclosed.
摘要翻译：一种应急动力系统，包括多个固体推进剂气体发生器，每个固体推进剂气体发生器具有与旋转地设置在燃气涡轮机壳体内的涡轮机叶轮流体连通的气体出口，所述涡轮机叶轮与发电机输入轴旋转连通，轴或两者。还公开了一种从这样的应急电力系统产生电力的方法。

30. 发明授权

US5184458A Power unit fuel pressurization system 失效
标题翻译：动力装置燃油加压系统
公开(公告)号：US5184458A
公开(公告)日：1993-02-09
申请号：US439684
申请日：1989-11-21
申请人： Steven W. Lampe , Malcolm J. McArthur
发明人： Steven W. Lampe , Malcolm J. McArthur
IPC分类号： B64D41/00 , F02C7/272 , F02C7/277 , F02C7/32
CPC分类号： F02C7/32 , B64D41/00 , F02C7/272 , F02C7/277 , F05D2220/50 , F05D2260/4023 , Y02T50/44 , Y02T50/671
摘要： A power generating unit in accordance with the present invention comprises a pressurized gas source (44) providing pressurized gas containing oxygen to be used in combustion of a fuel; a combustor (42) for providing pressurized gas produced by combustion of a mixture of the pressurized gas provided to the combustor by the pressurized gas source and fuel provided to the combustor by a fuel supply (48); a first turbine (68) driven by pressurized gas produced by the combustor; a gear box (70) driven by the turbine having an output shaft (72); a fuel pump (46) disposed within the fuel supply having a pair of input shafts (64 and 76) for providing pressurized fuel to the combustor in response to rotation of either of the input shafts; a motor (58) coupled to the pressurized gas source having a drive shaft (60) which rotates in response to the pressurized gas applied from the gas source; and a coupling mechanism (62 and 74), coupled to the shafts, for applying driving torque to the fuel pump during rotation of the pressurized gas to the combustor from the input shaft which is rotating at a higher velocity.
摘要翻译：根据本发明的发电单元包括加压气体源（44），其提供用于燃料燃烧的含氧的加压气体; 燃烧器（42），用于通过由加压气体源提供给燃烧器的加压气体的混合物燃烧产生的加压气体和通过燃料供给装置（48）提供给燃烧器的燃料; 由燃烧器产生的加压气体驱动的第一涡轮机（68）; 由所述涡轮机驱动的齿轮箱（70）具有输出轴（72）; 设置在燃料供给装置内的燃料泵（46）具有一对输入轴（64和76），用于响应于任一个输入轴的转动而向燃烧器提供加压燃料; 耦合到加压气体源的马达（58）具有响应于从气体源施加的加压气体而旋转的驱动轴（60）; 以及联接到所述轴的联接机构（62和74），用于在从所述输入轴以更高速度旋转的状态下将所述加压气体旋转到所述燃烧器期间向所述燃料泵施加驱动扭矩。

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