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公开(公告)号：US20230170702A1
公开(公告)日：2023-06-01
申请号：US17916039
申请日：2021-03-17
IPC分类号： H02J3/32 , H02J3/38 , H02J3/00 , B64C39/02 , B64D9/00 , B64U50/30 , B64U20/87 , B60L50/00 , B60L3/00 , G05D1/10
CPC分类号： H02J3/322 , H02J3/381 , H02J3/004 , H02J3/003 , B64C39/024 , B64D9/00 , B64U50/30 , B64U20/87 , B60L50/00 , B60L3/0023 , G05D1/101 , B64U2101/60
摘要： An energy supply system, which is a system constituting a regional power system in a target region, includes a power transmission system including a first power generation facility and a second power generation facility, a power transmission and distribution system that supplies power to each consumer, a management system, and an unmanned flying object. The unmanned flying object has a transport function of transporting a cargo and a power supply function of supplying power to an outside. When the amount of power supplied by the power transmission system is less than the amount of power required by the power transmission and distribution system, the management system performs a power adjustment process of supplying power from the unmanned flying object to the power transmission and distribution system by using the power supply function of the unmanned flying object.
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公开(公告)号：US20190390577A1
公开(公告)日：2019-12-26
申请号：US16527649
申请日：2019-07-31
发明人： Kazuhiko TANIMURA , Hikaru SANO , Satoshi NAKAYAMA , Naoki MIYAKE , Akihisa OKA
摘要： A hydrogen/oxygen stoichiometric combustion turbine system includes: a high-pressure steam turbine (2); a low-pressure steam turbine (3); and a heater (5) disposed between the high-pressure and low-pressure steam turbines. The heater (5) has a combustion portion (53) in which stoichiometric combustion of hydrogen and oxygen is caused, and a mixing portion (55) configured to mix discharged steam (S4) from the high-pressure steam turbine (2) with combustion gas (R) from the combustion portion (53) and to supply the obtained product to the low-pressure steam turbine (3).
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3.发明申请SUNLIGHT-UTILIZING GAS TURBINE POWER GENERATION SYSTEM PROVIDED WITH HYDROGEN-GENERATING UNIT 审中-公开用氢气发电机组提供的天然气涡轮发电系统公开(公告)号：US20150226119A1
公开(公告)日：2015-08-13
申请号：US14695192
申请日：2015-04-24
CPC分类号： F02C3/22 , F02C1/05 , F02C3/04 , F02C6/00 , F02C6/10 , F02C6/18 , F02C7/08 , F02C7/22 , F02C7/32 , F03G6/04 , F05D2220/32 , F05D2220/60 , F05D2260/20 , F24S90/00 , Y02E10/46
摘要： A power generation system having a gas turbine engine that utilizes sunlight, includes a compressor configured to compress an air which is a working medium, a solar heater configured to heat the air compressed by the compressor, utilizing sunlight as a heat source, a hydrogen combustor configured to burn the air compressed by the compressor utilizing hydrogen as a fuel, a turbine configured to output a motive power from a high-temperature gas heated by at least one of the solar heater and the hydrogen combustor, a power generator configured to be driven by the turbine, and at least one hydrogen-generating unit configured to generate hydrogen by utilizing an output of the turbine or exhaust heat from the turbine to decompose a water, and supply the hydrogen so generated to the hydrogen combustor.
摘要翻译： 具有利用太阳光的燃气涡轮发动机的发电系统包括压缩构造成压缩作为工作介质的空气的压缩机，被配置为加热由压缩机压缩的空气的太阳能加热器，利用太阳光作为热源，氢燃烧器 被配置为燃烧利用氢气作为燃料而被压缩机压缩的空气，所述涡轮机构造成从由所述太阳能加热器和所述氢燃烧器中的至少一个加热的高温气体输出动力;被配置为被驱动的发电机 以及至少一个氢气发生单元，其被配置为通过利用涡轮机的输出或者来自涡轮机的排气来产生氢，以分解水，并且将如此产生的氢气供应给氢燃烧器。
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公开(公告)号：US20180328229A1
公开(公告)日：2018-11-15
申请号：US15580923
申请日：2016-06-09
CPC分类号： F01D25/30 , F01D25/162 , F01D25/24 , F05D2220/32 , F05D2230/232
摘要： An exhaust diffuser includes: a plurality of struts, each of which penetrates an internal cylinder and an external cylinder and couples a bearing support and a structural body together, the bearing support disposed inside the internal cylinder, the structural body disposed outside the external cylinder, each strut inclined rearward from the bearing support toward the structural body; and a plurality of strut covers that surround the plurality of struts, respectively, between the internal cylinder and the external cylinder. The external cylinder includes a tapered first stepped portion that expands a diameter of the external cylinder and that overlaps leading edges of the plurality of strut covers in an axial direction of the external cylinder. The internal cylinder includes a tapered second stepped portion that expands a diameter of the internal cylinder and that overlaps trailing edges of the plurality of strut covers in an axial direction of the internal cylinder.
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公开(公告)号：US20180298919A1
公开(公告)日：2018-10-18
申请号：US15767419
申请日：2016-10-07
发明人： Takuya IKEGUCHI , Koji TERAUCHI , Keiji OIKAZE , Naoto SAKAI , Kazuhiko TANIMURA
IPC分类号： F04D29/54
摘要： An intake structure of a compressor includes an intake duct forming an intake port opening in a direction away from a central axis of the compressor and a bellmouth forming an annular channel expanding from an inlet of the compressor toward an inner space of the intake duct. The bellmouth includes a plurality of struts connecting an inner casing positioned inside the annular channel and an outer casing positioned outside the annular channel. At least one of a plurality of transverse struts, of the plurality of struts, which are located on both sides of a center plane passing through the central axis of the compressor and the center of the intake port has a trailing edge positioned on a virtual plane passing through the central axis of the compressor and a leading edge positioned on a side of the intake port with respect to the virtual plane.
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公开(公告)号：US20170022843A1
公开(公告)日：2017-01-26
申请号：US15285910
申请日：2016-10-05
摘要： A turbine ventilation structure includes: an exhaust diffuser including inner and outer tubes to form an exhaust passage for exhaust gas; a strut extending across the exhaust diffuser from a housing to support a bearing inside the inner tube; a strut cover in the exhaust passage that covers the strut; and a connecting member disposed downstream of the strut cover and including a hollow portion to connect the housing and the inner tube. The housing includes a first intake port to introduce an air from outside. The strut cover has a discharge hole at a rear edge portion thereof. The turbine ventilation structure includes a first ventilation passage extending from the first intake port through the hollow portion, then extending from an inner end portion of the strut through between the strut and the strut cover, and the discharge hole, into the exhaust passage.
摘要翻译： 涡轮机通风结构包括：排气扩散器，其包括内管和外管，以形成废气排气通道; 从壳体延伸穿过排气扩散器的支柱，以支撑内管内的轴承; 覆盖支柱的排气通道中的支柱盖; 以及连接构件，其设置在支柱盖的下游，并且包括中空部分以连接壳体和内管。 壳体包括从外部引入空气的第一进气口。 支柱盖在其后边缘部分具有排放孔。 涡轮机通风结构包括从第一进气口延伸穿过中空部分的第一通风通道，然后从支柱的内端部分延伸穿过支柱和支柱盖之间以及排出孔进入排气通道。
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公开(公告)号：US20160047310A1
公开(公告)日：2016-02-18
申请号：US14926721
申请日：2015-10-29
发明人： Kazuhiko TANIMURA
摘要： A heat storage mechanism, of a heat exchanger, which does not shorten the service life of the heat exchanger even when a facility using the heat exchanger is intermittently operated and which suppresses a decrease in efficiency at the time of restart of the facility, is provided. The heat storage mechanism for storing heat of a heat exchanger during stop of operation of a facility provided with the heat exchanger includes an outflow prevention unit configured to prevent outflow of an exhaust gas to the outside, which is a heating medium of the heat exchanger, during stop of operation of the facility is provided in an exhaust passage through which the exhaust gas is discharged to the outside.
摘要翻译： 即使使用热交换器的设备间歇地操作并且抑制了设备重启时的效率降低，热交换器的蓄热机构也不会缩短热交换器的使用寿命 。 用于在设置有热交换器的设备的运行停止期间存储热交换器的热量的储热机构包括：流出防止单元，其被构造成防止作为热交换器的加热介质的排出气体流到外部; 在设备的停止操作期间，排气通过排气通道排出到外部。
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