公开(公告)号：US09963241B2

公开(公告)日：2018-05-08

申请号：US15034708

申请日：2014-10-29

Applicant: Airbus Defence and Space GmbH

Inventor： Gerrit Schramm ,  Renè Langermann ,  Richard Trott ,  Arnd Schirrmann

IPC: B64D41/00 ,  F17C9/04 ,  F02C1/00 ,  H01M16/00 ,  H01M8/04007 ,  H01M8/04082

CPC classification number: B64D41/00 ,  B64D2041/005 ,  F02C1/002 ,  F17C9/04 ,  H01M8/04007 ,  H01M8/04208 ,  H01M16/003 ,  H01M2250/20 ,  H01M2250/402 ,  Y02B90/12 ,  Y02T90/32 ,  Y02T90/36

Abstract: An aircraft includes a fuel cell device which can be operated with hydrogen from a hydrogen tank and with oxygen drawn from the surrounding air, and further includes a superconducting magnetic energy storage unit (SMES unit) which is disposed, together with the hydrogen tank, in a cryogenic container, wherein the cryogenic container does not have an active cooling system or a liquid hydrogen generating device, and has a volume for holding a maximum of 40 kg liquid hydrogen.

公开(公告)号：US20170098977A1

公开(公告)日：2017-04-06

申请号：US15282435

申请日：2016-09-30

Applicant: AIR LIQUIDE INDUSTRIAL U.S. LLP

Inventor： Charles L. CARISTAN

IPC: H02K7/18 ,  F17C9/04 ,  F17C7/02 ,  F01D15/10 ,  F02C1/00

CPC classification number: H02K7/1823 ,  F01D15/10 ,  F02C1/002 ,  F05D2210/12 ,  F05D2220/32 ,  F17C7/02 ,  F17C7/04 ,  F17C9/04 ,  F17C2221/011 ,  F17C2221/012 ,  F17C2221/013 ,  F17C2221/014 ,  F17C2221/032 ,  F17C2223/0161 ,  F17C2223/033 ,  F17C2223/035 ,  F17C2225/0123 ,  F17C2225/03 ,  F17C2225/035 ,  F17C2225/036 ,  F17C2227/0311 ,  F17C2227/0316 ,  F17C2227/0393 ,  F17C2265/05 ,  F17C2265/07 ,  F17C2270/0168 ,  F17C2270/0581 ,  Y02E60/321

Abstract: Liquid cryogen from a tank having a head space pressure P1 is vaporized with a pressure building vaporizer to gaseous cryogen and the pressure of the gaseous cryogen is built to a pressure P2. The pressurized gaseous cryogen at pressure P2 is expanded across an expander to decrease its pressure and fed to a point of use at an installation including the vaporizer at a pressure P3. P2≧2×P3. Energy from the expanded gas may be recovered in the form of mechanical energy, electrical energy.

公开(公告)号：US20070220896A1

公开(公告)日：2007-09-27

申请号：US11388466

申请日：2006-03-24

Applicant: Balachandar Varatharajan ,  Chellappa Balan ,  Michael Bowman

Inventor： Balachandar Varatharajan ,  Chellappa Balan ,  Michael Bowman

IPC: F02C1/00

CPC classification number: F02C1/002 ,  F02C3/20 ,  F05D2270/082 ,  Y02T50/677

Abstract: A gas turbine systems of reducing NOx emissions and enhancing operability comprises a compressor; a combustor disposed downstream of and in fluid communication with the compressor; a turbine assembly disposed down stream of and in fluid communication with the combustor; an oxygen-enriched gas source disposed in selective fluid communication with the compressor, the combustor, or a combination of the foregoing, wherein the oxygen-enriched gas source is a pressure swing absorption system, an electrolyzer, or a membrane reactor.

Abstract translation: 一种减少NO x排放和提高可操作性的燃气轮机系统包括压缩机; 设置在压缩机下游并与压缩机流体连通的燃烧器; 涡轮组件，其布置在燃烧器的下游并与燃烧器流体连通; 设置成与压缩机，燃烧器或前述的组合选择性流体连通的富氧气体源，其中富氧气体源是变压吸收系统，电解器或膜反应器。

公开(公告)号：US4201049A

公开(公告)日：1980-05-06

申请号：US964810

申请日：1978-11-29

Applicant: Arno W. Tobber

Inventor： Arno W. Tobber

IPC: F02C1/00 ,  F02C3/30 ,  F03B13/00 ,  F16D33/00

CPC classification number: F03B13/00 ,  F02C1/002 ,  F02C3/30

Abstract: A turbine power plant of particularly inexpensive construction and using static expansion of the combustion gas to accelerate slugs of liquid used as the motive power for a Pelton wheel. The turbine power plant comprises a fuel combustion unit producing combustion gas which serves to impart speed to slugs of an auxiliary liquid, like water, in output pipes; this auxiliary liquid acts on a Pelton wheel to produce rotary drive. A part of the auxiliary liquid is reconverted as slugs to compress the air supplied to the fuel combustion unit. The turbine power plant also includes a second Pelton wheel driving a common shaft for an air fan, and a pair of rotating nozzles arranged to produce the said slugs of auxiliary liquid. The second Pelton wheel is driven by part of the auxiliary liquid.

Abstract translation: 一种涡轮发电厂，其特别廉价的结构，并且使用燃烧气体的静态膨胀来加速用作佩尔顿轮的动力的液体。 涡轮发电厂包括燃料燃烧单元，其产生燃烧气体，其用于将诸如水之类的辅助液体的lug塞速度输送到输出管中; 该辅助液体作用在佩尔顿轮上以产生旋转驱动。 辅助液体的一部分被重新转换为s塞，以压缩供应到燃料燃烧单元的空气。 涡轮动力装置还包括驱动用于空气风扇的公共轴的第二佩尔顿轮和布置成产生所述辅助液体的一群的旋转喷嘴。 第二个Pelton轮由辅助液体的一部分驱动。

公开(公告)号：US08186169B2

公开(公告)日：2012-05-29

申请号：US12910033

申请日：2010-10-22

Applicant: Barrett David Gardiner

Inventor： Barrett David Gardiner

IPC: F02C7/18

CPC classification number: F02C1/002 ,  F02C3/30 ,  F02C7/18 ,  F05D2260/205 ,  F05D2270/082 ,  F25J3/04545 ,  F25J3/04563 ,  F25J3/04575 ,  F25J3/04593 ,  F25J3/04612 ,  F25J2245/42 ,  F25J2260/44 ,  Y02E20/16 ,  Y02E20/18

Abstract: A nitrogen source supplies a flow of nitrogen to a cooling circuit in the turbine section of a gas turbine. The nitrogen in the cooling circuit absorbs heat from the turbine section and flows to a flow divider where the heated nitrogen is split into a combustor flow and a return flow. The combustor nitrogen flow is injected into the gas turbine combustor. The return nitrogen flow is returned to the flow of nitrogen supplied to the gas turbine cooling circuit.

Abstract translation: 氮源将氮气流提供给燃气轮机的涡轮部分中的冷却回路。 冷却回路中的氮吸收来自涡轮机部分的热量并且流到分流器，在该分流器中加热的氮被分成燃烧室流和回流。 将燃烧器氮气流注入燃气轮机燃烧器。 返回的氮气流返回到供应到燃气轮机冷却回路的氮气流中。

公开(公告)号：US20080289335A1

公开(公告)日：2008-11-27

申请号：US11794086

申请日：2005-12-23

Applicant: Kenneth William Patterson Drysdale

Inventor： Kenneth William Patterson Drysdale

IPC: F01K25/06

CPC classification number: H02K7/1823 ,  F01D15/005 ,  F01K21/005 ,  F02C1/002 ,  F02C1/007 ,  F05D2210/13 ,  F25B11/02 ,  F25B29/003 ,  F25B2339/047 ,  F25B2400/14 ,  F28C3/08 ,  H02M7/10

Abstract: A refrigeration apparatus (7200) includes a heat pump circuit (7201) and a power generation circuit (7100). The power generation circuit (7100) includes an evaporator (701) including a first and a second heat exchanger (710a, 710b), a turbine (702), a condenser (703) and a pump (704). The first heat exchanger (710a) absorbs heat rejected from the heat pump circuit (7201) into a power generation circuit (7100) while the second heat exchanger (710b) further heats the fluid. The power generation circuit (7100) includes a bypass (707) which allows a portion of working liquid to enter the turbine (702) without passing through the evaporator (701). A heat pump (704) with similar bypass is also disclosed. Also disclosed are dual stage turbine design and a nozzle (10300) for a turbine which includes two fluid paths (1011, 1014) that adapted to receive and mix the liquid and vapour streams of working fluid, so that the liquid working fluid is vaporized by the heat from the vapour working fluid.

Abstract translation: 制冷装置（7200）包括热泵回路（7201）和发电回路（7100）。 发电电路（7100）包括包括第一和第二热交换器（710a，710b）的蒸发器（701），涡轮机（702），冷凝器（703）和泵（704）。 第一热交换器（710a）将从热泵回路（7201）排出的热量吸收到发电回路（7100），而第二热交换器（710b）进一步加热流体。 发电电路（7100）包括旁路（707），其允许一部分工作液体进入涡轮机（702）而不通过蒸发器（701）。 还公开了具有类似旁路的热泵（704）。 还公开了双级涡轮机设计和用于涡轮机的喷嘴（10300），其包括适于接收和混合工作流体的液体和蒸气流的两个流体路径（1011,1014），使得液体工作流体被 来自蒸汽工作流体的热量。

公开(公告)号：US5308366A

公开(公告)日：1994-05-03

申请号：US973455

申请日：1992-11-09

Applicant: David Stelman

Inventor： David Stelman

IPC: B01J7/00 ,  B64G1/42 ,  C01B3/00 ,  F02C1/00

CPC classification number: C01B3/00 ,  B01J7/00 ,  B64G1/421 ,  F02C1/002

Abstract: A reactor for producing hot hydrogen in vacuo which in turn drives a power-generating device such as a turbine is disclosed. Within the reactor are injected heat-generating reactants such as beryllium and oxygen. The reactants heat hydrogen which in turn is delivered to a power-generating device such as a turbine.

Abstract translation: 公开了一种用于在真空中产生热氢的反应器，其又驱动诸如涡轮机之类的发电装置。 在反应器内注入发热反应物如铍和氧。 反应物加热氢气，氢气又被输送到诸如涡轮机的发电装置。

公开(公告)号：US20160178129A1

公开(公告)日：2016-06-23

申请号：US15053840

申请日：2016-02-25

Applicant: Highview Enterprises Limited

Inventor： Haisheng Chen ,  Yulong Ding ,  Toby Peters ,  Ferdinand Berger

IPC: F17C9/04 ,  F02C6/14 ,  F03G7/04 ,  F02C1/00

CPC classification number: F17C9/04 ,  F01D15/005 ,  F01D15/04 ,  F01K3/00 ,  F01K13/00 ,  F01K15/04 ,  F02C1/002 ,  F02C1/05 ,  F02C6/14 ,  F03D9/17 ,  F03D9/25 ,  F05B2210/12 ,  F05D2210/12 ,  F25J1/0012 ,  F25J1/004 ,  F25J1/0045 ,  F25J1/0221 ,  F25J1/0228 ,  F25J1/0234 ,  F25J1/0242 ,  F25J1/0251 ,  F25J1/0281 ,  F25J3/04018 ,  F25J3/04078 ,  F25J3/04115 ,  F25J3/04169 ,  F25J3/04224 ,  F25J3/04496 ,  F25J3/04533 ,  F25J3/04593 ,  F25J3/04612 ,  F25J3/04618 ,  F25J3/04836 ,  F25J2205/62 ,  F25J2210/40 ,  F25J2215/40 ,  F25J2230/06 ,  F25J2230/20 ,  F25J2230/30 ,  F25J2235/02 ,  F25J2240/10 ,  F25J2240/90 ,  F25J2245/40 ,  F25J2260/20 ,  Y02E10/72 ,  Y02E60/15 ,  Y02T50/672

Abstract: The present invention concerns systems for storing energy and using the stored energy to generate electrical energy or drive a propeller (505). In particular, the present invention provides a method of storing energy comprising: providing a gaseous input, producing a cryogen from the gaseous input; storing the cryogen; expanding the cryogen; using the expanded cryogen to drive a turbine (320) and recovering cold energy from the expansion of the cryogen. The present invention also provides a cryogenic energy storage system comprising: a source of cryogen; a cryogen storage facility (370); means for expanding the cryogen; a turbine (320) capable of being driven by the expanding cryogen; and means (340, 350) for recovering cold energy released during expansion of the cryogen.

Abstract translation: 本发明涉及用于存储能量和使用所存储的能量以产生电能或驱动螺旋桨（505）的系统。 特别地，本发明提供一种储存能量的方法，包括：提供气体输入，从气体输入产生冷冻剂; 储存冷冻剂; 扩大制冷剂; 使用膨胀的冷冻剂驱动涡轮机（320）并从冷冻剂的膨胀中回收冷能。 本发明还提供了一种低温储能系统，包括：冷冻源; 冷冻剂储存设施（370）; 用于扩大冷冻剂的手段; 能够被膨胀的冷冻剂驱动的涡轮机（320）; 以及用于回收在冷冻剂膨胀期间释放的冷能的装置（340,350）。

公开(公告)号：US08616005B1

公开(公告)日：2013-12-31

申请号：US12556063

申请日：2009-09-09

Applicant: Dennis James Cousino, Sr.

Inventor： Dennis James Cousino, Sr.

IPC: F02C1/00

CPC classification number: F02C1/002

Abstract: A method and apparatus for boosting the performance of gas turbine engines, pipelines, and other applications using gas turbine engine systems. A pressurizing device or other source is preferably used to deliver an intake air stream to the gas turbine engine at at least 2% above atmospheric pressure. The pressurizing device of other source is preferably not mechanically driven by the gas turbine engine itself.

Abstract translation: 一种用于使用燃气涡轮发动机系统来提高燃气轮机发动机，管道和其它应用的性能的方法和装置。 优选地使用加压装置或其它源，以将进气流以大气压以上2％的速度输送到燃气涡轮发动机。 其他源的加压装置优选地不由燃气涡轮发动机本身机械驱动。

公开(公告)号：US20120096868A1

公开(公告)日：2012-04-26

申请号：US12910033

申请日：2010-10-22

Applicant: Barrett David Gardiner

Inventor： Barrett David Gardiner

IPC: F02C1/00

CPC classification number: F02C1/002 ,  F02C3/30 ,  F02C7/18 ,  F05D2260/205 ,  F05D2270/082 ,  F25J3/04545 ,  F25J3/04563 ,  F25J3/04575 ,  F25J3/04593 ,  F25J3/04612 ,  F25J2245/42 ,  F25J2260/44 ,  Y02E20/16 ,  Y02E20/18

Abstract: The present application provides an integrated gasification combined cycle system. The integrated gasification combined cycle system may include a nitrogen source, a combustor, and a turbine. A flow of nitrogen from the nitrogen source passes through and cools the turbine and then flows into the combustor.

Abstract translation: 本申请提供了一种综合气化联合循环系统。 一体化气化联合循环系统可以包括氮源，燃烧器和涡轮机。 来自氮源的氮气流通过并冷却涡轮，然后流入燃烧器。