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1. 发明申请

US20230014316A1 CONTROL DEVICE, CONTROL METHOD, AND PROGRAM 有权
公开(公告)号：US20230014316A1
公开(公告)日：2023-01-19
申请号：US17953704
申请日：2022-09-27
申请人： MITSUBISHI HEAVY INDUSTRIES, LTD.
发明人： Akihiko SAITO , Hidekazu YAMASHITA , Jun SASAHARA , Koichiro YANO , Yosuke KITAUCHI , Mizuhiko TANAKA , Masahiro YOSHIDA
IPC分类号： F02C3/055 , F02C3/16
摘要： A control device for adjusting an amount of fuel to be supplied to a gas turbine based on a rotational speed of the gas turbine, such that a frequency of electric power output by a power generator that generates electric power using the gas turbine is within a given range, includes a load value acquisition unit configured to acquire a load value that is a value of a load applied to the power generator after cutoff of a part of the load applied to the power generator when the part of the load applied to the power generator is cut off, an arithmetic unit configured to calculate an adjusted value that is a value of the load different from the load value by carrying out an arithmetic operation on the load value and a bias, and a command unit configured to adjust the amount of fuel by outputting a first signal for causing the power generator to output electric power corresponding to the adjusted value.

2. 发明授权

US09551353B2 Compressor blade mounting arrangement 有权
标题翻译：压缩机叶片安装布置
公开(公告)号：US09551353B2
公开(公告)日：2017-01-24
申请号：US13963425
申请日：2013-08-09
申请人： General Electric Company
发明人： John Herbert Dimmick, III
IPC分类号： F02C3/04 , F02C3/055 , F02C3/06 , F04D29/32 , F01D5/30
CPC分类号： F04D29/322 , F01D5/303 , F01D5/3038 , F01D5/3046 , F02C3/04 , F02C3/055 , F02C3/06
摘要： A compressor blade mounting arrangement includes a compressor blade having an airfoil, a base attachment and a platform disposed between the airfoil and the base attachment. The base attachment includes a first root portion extending radially inwardly from the platform and a second root portion extending radially inwardly from the platform, the first root portion and the second root portion defining a hollow portion therebetween. The base attachment also includes a compression plate disposed within the hollow portion and in fitted engagement with the first root portion and the second root portion. The base portion further includes at least one tab protruding from at least one of the first root portion and the second root portion. The compressor blade mounting arrangement also includes a wheel including a channel extending from a base wall to a rim of the wheel, the channel having a varying opening width.
摘要翻译：压缩机叶片安装装置包括具有翼型件的压缩机叶片，底座附件和设置在翼型件和底座附件之间的平台。基座附件包括从平台径向向内延伸的第一根部部分和从平台径向向内延伸的第二根部部分，第一根部部分和第二根部部分在其间限定中空部分。基座附件还包括设置在中空部分内并与第一根部部分和第二根部部分配合接合的压缩板。基部还包括从第一根部部分和第二根部部分中的至少一个突出的至少一个突出部。压缩机叶片安装装置还包括轮，该轮包括从底壁延伸到轮的轮缘的通道，该通道具有变化的开口宽度。

3. 发明授权

US07168235B2 Highly supercharged regenerative gas turbine 失效
标题翻译：高增压再生燃气轮机
公开(公告)号：US07168235B2
公开(公告)日：2007-01-30
申请号：US11099218
申请日：2005-04-05
申请人： William L. Kopko
发明人： William L. Kopko
IPC分类号： F02C3/055 , F02C7/10
CPC分类号： F02C7/10 , F02C3/36 , F02C6/12 , F02C6/18 , F02C7/08 , F02C7/143
摘要： The present invention comprises a highly supercharged, regenerative gas-turbine system. The gas turbine comprises a compressor, a regenerator, a combustor, and an expander. A pre-compressor pressurizes air going into the compressor section of the gas turbine. A cooler lowers the temperature of the air going into the compressor. The compressor pressurizes air, which then flows through the regenerator, which heats the air before it enters the combustor. The combustor further heats the air which then flows through the expander and then the regenerator. A post-expander is preferably located downstream of the regenerator. The post-expander is a second expander that receives high-pressure gas exiting the regenerator. The post-expander preferably drives the pre-compressor. The preferred pre-compressor and post-expander are toroidal intersecting vane machines (TIVMs), which are positive-displacement rotary devices. Numerous alternated embodiments of this basic system are described.
摘要翻译：本发明包括高增压，再生式燃气轮机系统。燃气轮机包括压缩机，再生器，燃烧器和膨胀机。预压缩机对进入燃气轮机的压缩机部分的空气加压。冷却器降低进入压缩机的空气的温度。压缩机对空气进行加压，然后空气流过再生器，空气在其进入燃烧器之前加热空气。燃烧器进一步加热然后流过膨胀器然后再生器的空气。后膨胀器优选位于再生器的下游。后膨胀器是接收离开再生器的高压气体的第二膨胀器。后膨胀器优选地驱动预压缩机。优选的预压缩机和后膨胀机是环形交叉叶片机（TIVM），它们是正排量旋转装置。描述了该基本系统的许多替代实施例。

4. 发明申请

US20050126175A1 Integrated microturbine system 失效
标题翻译：集成微型涡轮机系统
公开(公告)号：US20050126175A1
公开(公告)日：2005-06-16
申请号：US10737053
申请日：2003-12-16
申请人： Patrick Badgley
发明人： Patrick Badgley
IPC分类号： F01C11/00 , F02C3/04 , F02C3/055
CPC分类号： F02C3/055 , F01C11/004 , F02C3/04 , F05D2250/82
摘要： A microturbine for the generation of mechanical and electrical power comprising a positive displacement axial vane rotary compressor and an axial vane rotary expander. The compressor and expander are joined by a common shaft. The system further includes at least one combustor for heating a driving fluid prior to its entering the expander. The driving fluid, such as air, enters the compressor at ambient conditions of pressure and temperature and is compressed. The compressed driving fluid is preheated by the exhaust from the expander, then passes through a combustor to bring its temperature to a desired expander inlet temperature and then enters the expander where the expansion force of the hot driving fluid acting against the vanes of the expander is translated into rotation of the common shaft for driving both the compressor and a suitable power device such as an electrical generator.
摘要翻译：一种用于产生机械和电力的微型涡轮机，包括正排量轴向叶片旋转压缩机和轴向叶片旋转式膨胀机。压缩机和膨胀机通过公共轴连接。该系统还包括至少一个用于在驱动流体进入膨胀机之前加热驱动流体的燃烧器。诸如空气的驱动流体在压力和温度的环境条件下进入压缩机并被压缩。压缩的驱动流体由来自膨胀器的排气预热，然后通过燃烧器使其温度达到所需的膨胀机入口温度，然后进入膨胀机，在该膨胀机中，作用于膨胀机叶片的热驱动流体的膨胀力为转换为公共轴的旋转，用于驱动压缩机和诸如发电机的合适的动力装置。

5. 发明授权

US2421518A Jet propulsion 失效
标题翻译：喷气推进
公开(公告)号：US2421518A
公开(公告)日：1947-06-03
申请号：US34399340
申请日：1940-07-05
申请人： UNITED AIRCRAFT CORP
发明人： MOLLOY RICHARD C
IPC分类号： F02C3/055 , F02K7/08
CPC分类号： F02K7/08 , F02C3/055

6. 发明申请

US20190048796A1 TURBINE CLEARANCE CONTROL SYSTEM AND METHOD FOR IMPROVED VARIABLE CYCLE GAS TURBINE ENGINE FUEL BURN 审中-公开
公开(公告)号：US20190048796A1
公开(公告)日：2019-02-14
申请号：US16048738
申请日：2018-07-30
申请人： United Technologies Corporation
发明人： Walter A. Ledwith, Jr. , Scott A. Carr , Christopher J. Hanlon , Peter A. White , Theodore W. Hall , John R. Farris , Andrew S. Miller , Christopher W. Robak , David C. Pimenta , David Richard Griffin
IPC分类号： F02C3/055 , F02C7/18 , F01D11/24
摘要： A method of assembling a gas turbine engine includes setting a build clearance at assembly in response to a running tip clearance defined with a cooled cooling air. A method of operating a gas turbine engine includes supplying a cooled cooling air to a high pressure turbine in response to an engine rotor speed.

7. 发明授权

US5970924A Arc-piston engine 失效
标题翻译：弧形活塞发动机
公开(公告)号：US5970924A
公开(公告)日：1999-10-26
申请号：US579950
申请日：1995-12-28
申请人： Sang-Bok Pyon
发明人： Sang-Bok Pyon
IPC分类号： F02B73/00 , F01C9/00 , F01C11/00 , F02B41/10 , F02B53/04 , F02B75/02 , F02C1/00 , F02C3/055 , F02C5/02 , F02C6/00 , F02F1/18 , F02B53/06
CPC分类号： F01C9/002 , F01C11/006 , F02C3/055 , F02C5/02 , F02C6/00 , F02B2075/027 , F05D2250/71 , Y02T50/671
摘要： An engine having an annular cylinder formed about an opening which utilizes an arc-piston reciprocally positioned in the annular cylinder with a partition secured within the annular cylinder separating the annular cylinder into an air intake compression chamber and a gas combustion chamber such that in use upon reciprocation of the arc-piston one of the chambers is expanding while the remaining of the chambers is contacting is disclosed. Within the opening a conventional gas turbine may be positioned and the rotational power of the arc-piston engine is combined with the rotational power of the gas turbine.
摘要翻译：一种发动机，其具有围绕开口形成的环形圆筒，其利用在环形圆筒中往复定位的弧形活塞，其中固定在环形气缸内的分隔件将环形圆筒分隔成进气压缩室和气体燃烧室，公开了电弧活塞一个室的往复运动，同时其余室接触的是膨胀的。在开口内，常规的燃气轮机可以被定位，并且电弧活塞发动机的旋转动力与燃气轮机的旋转动力相结合。

8. 发明授权

US4261169A Method for converting thermal energy into mechanical energy and a machine for carrying out said method 失效
标题翻译：将热能转换为机械能的方法和用于执行所述方法的机器
公开(公告)号：US4261169A
公开(公告)日：1981-04-14
申请号：US943993
申请日：1978-09-20
申请人： Bernard Zimmern
发明人： Bernard Zimmern
IPC分类号： F01N3/30 , F01K21/04 , F02B3/06 , F02B47/02 , F02C3/055 , F02C3/30 , F02G1/00 , F02G3/00
CPC分类号： F02G1/00 , F02B47/02 , F02C3/055 , F02B3/06 , Y02T10/121
摘要： The method of energy conversion consists in burning a fuel in an oxidizing gas in order to admit the combustion gases into an expansion machine for delivering mechanical energy, in previously compressing the oxidizing gas in a positive-displacement compressor driven by the expansion machine, in injecting into the compressor a sealing and/or lubricating auxiliary liquid which is continuously cooled and separated from the compressed gas, then re-injected into the compressor. The auxiliary liquid is cooled by vaporization of water and the steam produced is entrained in the stream of compressed oxidizing gas.
摘要翻译：能量转换的方法包括在氧化气体中燃烧燃料，以便将燃烧气体进入用于输送机械能的膨胀机，以预先压缩由膨胀机驱动的正排量压缩机中的氧化气体，注入将与压缩气体连续冷却和分离的密封和/或润滑辅助液体输入到压缩机中，然后重新注入压缩机。辅助液体通过水蒸发而冷却，产生的蒸汽被夹带在压缩的氧化气体流中。

9. 发明授权

US3661477A Heat shield 失效
标题翻译：隔热板
公开(公告)号：US3661477A
公开(公告)日：1972-05-09
申请号：US3661477D
申请日：1969-12-15
申请人： KONGSBERG VAPENFAB AS
发明人： WESTRUM THORBJORN
IPC分类号： F02C3/055 , F01D5/08 , F01D25/26 , F02C7/20 , F02C7/24 , F01D25/20 , F03D11/00
CPC分类号： F01D25/26 , F02C7/24 , F05D2230/642
摘要： A segmented annular heat shield for mounting between the turbine blade wheel and the compressor impeller of a radial gas turbine. Each segment is fixedly secured to a stationary structure at one point at its outer edge and also fastened to said structure at two further fastening points at its inner edge in such a manner that at these further fastening points the segment is restrained from movement in the axial direction of the shield but can move freely in the plane of the segment. The segments adjoin along joints of such a design as to admit of relative movement of the segments in the plane thereof due to heat expansion.
摘要翻译：一种用于安装在涡轮叶轮与径向燃气轮机的压缩机叶轮之间的分段式环形隔热罩。每个区段在其外边缘处的一个点处固定地固定到固定结构上，并且在其内边缘处的两个另外的紧固点处固定到所述结构，使得在这些另外的紧固点处，该区段被限制在轴向的运动屏蔽的方向，但可以在片段的平面内自由移动。这些部分沿着这种设计的关节相邻，以便承认由于热膨胀而在其平面中的段的相对运动。

10. 发明授权

US2645898A Combustion chamber having a series of expansion chambers 失效
标题翻译：燃烧室具有一系列膨胀室
公开(公告)号：US2645898A
公开(公告)日：1953-07-21
申请号：US77600747
申请日：1947-09-25
申请人： ROMUALD HURTAJ
发明人： ROMUALD HURTAJ
IPC分类号： F02C3/055
CPC分类号： F02C3/055 , Y02T50/671

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