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1. 发明申请

US20030074883A1 Method and apparatus for total energy fuel conversion systems 失效
标题翻译：总能量燃料转换系统的方法和装置
公开(公告)号：US20030074883A1
公开(公告)日：2003-04-24
申请号：US10193068
申请日：2002-07-11
申请人： EGT DEVELOPMENTS, LLC
发明人： Anthony Cirrito , Bernard P. Ennis
IPC分类号： F02C003/14 , F02C005/02 , C07C027/06
CPC分类号： F02K9/00 , C06D5/00 , C10G2400/20 , F02C3/00 , F02C3/36 , F02G5/00 , Y02E20/16 , Y02E20/18 , Y02P20/128 , Y02P20/582 , Y02T10/166
摘要： Process of producing power comprising: providing a turbine adapted to generate shaft work, said turbine having a combustor; and a rocket engine having a nozzle and a compressor means; feeding fuel and oxidant to the rocket engine and the rocket engine compressor means; feeding carbonaceous matter and steam into the rocket engine nozzle; processing the output of the rocket engine nozzle into fuel for the turbine; introducing said fuel and oxidant for the turbine to the turbine combustor; and recycling a substantial portion of the hot exhaust from the turbine to the rocket engine compressor means; and controlling the inlet temperature to the turbine. Apparatus for producing power comprising a rocket engine and a turbine adapted to generate shaft work is also disclosed. An alternative process comprises providing a steam turbine adapted to generate shaft work; and a rocket engine having a nozzle and a rocket engine compressor means; feeding fuel and oxidant to the rocket engine; feeding carbonaceous matter and water, steam or water-steam mixture to the rocket engine nozzle; processing the output of the rocket engine nozzle into fuel for a boiler and a heat source for a second rocket engine; boiling water in said boiler to produce water vapor; using the resultant water vapor to power said steam turbine; transforming the output of the second rocket engine into a fuel product is also disclosed.
摘要翻译：生产动力的过程包括：提供适于产生轴作用的涡轮，所述涡轮具有燃烧器; 和具有喷嘴和压缩机装置的火箭发动机; 向火箭发动机和火箭发动机压缩机装置供给燃料和氧化剂; 将碳质物质和蒸汽送入火箭发动机喷嘴; 将火箭发动机喷嘴的输出处理为涡轮机的燃料; 将所述涡轮机的燃料和氧化剂引入到涡轮机燃烧器; 并将来自涡轮机的大部分热排气回收到火箭发动机压缩机装置; 并控制到涡轮机的入口温度。还公开了用于产生动力的装置，其包括适于产生轴功的火箭发动机和涡轮。替代方法包括提供适于产生轴作用的蒸汽轮机; 和具有喷嘴和火箭发动机压缩机装置的火箭发动机; 将燃料和氧化剂供给火箭发动机; 将含碳物质和水，蒸汽或水蒸汽混合物送入火箭发动机喷嘴; 将火箭发动机喷嘴的输出处理成用于锅炉的燃料和用于第二火箭发动机的热源; 锅炉内的沸水产生水汽; 使用所得的水蒸气来对所述蒸汽轮机供电; 还公开了将第二火箭发动机的输出转换成燃料产物。

2. 发明申请

US20040154306A1 Compound gas turbine engines and methods of operation thereof 失效
标题翻译：复合燃气涡轮发动机及其操作方法
公开(公告)号：US20040154306A1
公开(公告)日：2004-08-12
申请号：US10482604
申请日：2003-12-26
发明人： Hubert Michael Benians
IPC分类号： F02C005/02
CPC分类号： F02C5/12 , F02C5/02
摘要： The engine (10) has a compressor (12) for compressing air, a plurality of combustion chambers (22a-f) in which fuel mixed with the compressed air combusts, and a turbine (16) which is driven by the products of combustion. Each combustion chamber operates in a cycle comprising the phases of: A. charging the combustion chamber with a charge of compressed air from the compressor while preventing air from escaping from the combustion chamber, B. then compounding by charging with a compounding charge of gas to form a compounded charge; C. then injecting fuel into the combustion chamber so that there is spontaneous ignition and combustion of the fuel with the compounded charge; and D. then exhausting the products of combustion to the turbine. The cycles of the combustion chambers are out of phase in a sequence, and part of the compounded charge (and/or the products of combustion thereof) in each combustion chamber during the combustion phase thereof is transferred to the next combustion chamber in the sequence to provide the compounding charge for that next combustion chamber.
摘要翻译：发动机（10）具有用于压缩空气的压缩机（12），与压缩空气混合的燃料燃烧的多个燃烧室（22a-f）和由燃烧产物驱动的涡轮机（16）。每个燃烧室在一个包括以下各个阶段的循环中操作：A.用来自压缩机的压缩空气的加压给燃烧室充电，同时防止空气从燃烧室B逸出，然后通过用气体的混合装料形成复合费用; 然后将燃料喷射到燃烧室中，使得燃料与复合装料自发点燃和燃烧; 然后将燃烧产物排出到涡轮机。燃烧室的循环在一个顺序上是异相的，并且在其燃烧阶段期间，每个燃烧室中的一部分复合装料（和/或其燃烧产物）按顺序转移到下一个燃烧室为下一个燃烧室提供配料。

3. 发明申请

US20020046560A1 High pressure gas cycle and power plant 失效
标题翻译：高压气体循环和发电厂
公开(公告)号：US20020046560A1
公开(公告)日：2002-04-25
申请号：US09935748
申请日：2001-08-24
发明人： J. Hilbert Anderson
IPC分类号： F02C005/02
CPC分类号： F02C3/02 , F02C5/10 , F02C5/12 , F02G1/00 , F02G2243/52
摘要： Provided is a combustion chamber for producing a pressurized gas containing: a wall structure defining an interior chamber; a first reflecting surface for reflecting a pressure wave within said interior chamber; a second reflecting surface for reflecting said pressure wave within said interior chamber, wherein said first and second reflecting surfaces being constructed and arranged to resonate said pressure wave in said interior chamber; at least one first inlet for introducing a first gas into said interior chamber; and at least one outlet from said interior chamber for drawing off a pressurized gas from said interior chamber. Also provided is a turbine engine containing the combustion chamber, and an electrical generating power plant containing the turbine engine.
摘要翻译：提供一种用于生产加压气体的燃烧室，包括：限定内部室的壁结构; 用于在所述内部室内反射压力波的第一反射表面; 用于将所述压力波反射在所述内部室内的第二反射表面，其中所述第一和第二反射表面被构造和布置成使所述内部腔室中的所述压力波谐振; 用于将第一气体引入所述内部室的至少一个第一入口; 以及来自所述内部室的至少一个出口，用于从所述内部室抽出加压气体。还提供了包含燃烧室的涡轮发动机和包含涡轮发动机的发电厂。

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