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11. 发明公开

EP4286673A3 METHOD OF CONTROLLING DEFLAGRATION COMBUSTION PROCESS IN PISTONLESS COMBUSTOR 审中-公开
公开(公告)号：EP4286673A3
公开(公告)日：2024-02-21
申请号：EP23203129.4
申请日：2020-06-08
申请人： Finno Energy Oy
发明人： ERÄMAA, Timo , SALMINEN, Heikki
IPC分类号： F23R7/00 , F23N5/20 , F02C5/12 , F23R3/58
摘要： A pistonless combustor (100) is disclosed. The pistonless combustor comprises at least one input channel (33, 34, 43, 44, 63) for air and fuel, an output channel (15), and a first combustion chamber (10). At least one input channel (33, 34, 43, 44, 63) is controlled with a valve (31, 32, 41, 42, 61). One or more of the at least one input channel (33, 34, 43, 44, 63) has an eccentric alignment configured to produce an eccentric input flow of air creating a self-preserving flow pattern (91, 92) of a fuel-air mixture within the first combustion chamber (10).

12. 发明授权

EP3999779B1 CHAMBRE DE COMBUSTION DE TURBOMACHINE A VOLUME CONSTANT 有权
公开(公告)号：EP3999779B1
公开(公告)日：2023-12-20
申请号：EP20750326.9
申请日：2020-07-08
发明人： ESCURE, Didier René André , TANTOT, Nicolas Jérôme Jean
IPC分类号： F23R7/00 , F02C5/12

13. 发明授权

EP3980693B1 METHOD OF CONTROLLING DEFLAGRATION COMBUSTION PROCESS IN PISTONLESS COMBUSTOR 审中-实审
公开(公告)号：EP3980693B1
公开(公告)日：2023-11-22
申请号：EP20758262.8
申请日：2020-06-08
发明人： ERÄMAA, Timo , SALMINEN, Heikki
IPC分类号： F23R7/00 , F23N5/20 , F02C5/12

14. 发明授权

EP3250859B1 MODULE DE COMBUSTION A VOLUME CONSTANT POUR UNE TURBOMACHINE COMPORTANT UN ALLUMAGE PAR COMMUNICATION 有权
公开(公告)号：EP3250859B1
公开(公告)日：2022-09-14
申请号：EP16705236.4
申请日：2016-01-26
发明人： LEYKO, Matthieu
IPC分类号： F23R7/00 , F02C5/12 , F23R3/48

15. 发明授权

EP3250858B1 MODULE DE COMBUSTION A VOLUME CONSTANT POUR UNE TURBOMACHINE 有权
公开(公告)号：EP3250858B1
公开(公告)日：2021-03-03
申请号：EP16705231.5
申请日：2016-01-25
发明人： LEYKO, Matthieu
IPC分类号： F23R7/00 , F02C5/12

16. 发明公开

EP3611357A1 ENGINE 审中-公开
公开(公告)号：EP3611357A1
公开(公告)日：2020-02-19
申请号：EP18784219.0
申请日：2018-03-30
申请人： Amnext Technology Inc.
发明人： OHISHI, Yasutoshi
IPC分类号： F02B71/04 , F01D13/02 , F01K23/02 , F02B63/04 , F02B71/06 , F02B73/00 , F02C5/02 , F02C5/08 , F02C5/12 , H02K35/02
摘要： An engine (5) with a gas supply unit (10) that supplies combustion gas for driving purposes with linear reciprocal movement of a piston (12) is provided. The gas supply unit (10) includes a first combustion chamber (31) provided on a first side of the piston, a first gas outlet (17) that supplies high pressure combustion gas generated in the first combustion chamber for driving purposes, and a second combustion chamber (32) that is provided on a second side on the other side of the piston and generates a second force that moves the piston toward the first side. The engine (5) further includes a piston control unit (60) that controls the position of the piston against a first force of the piston that moves due to combustion in the first combustion chamber and the second force described above.

17. 发明授权

EP2312126B1 Power generation system and corresponding power generating method 有权
标题翻译：发电系统和用于产生能量的方法相关联的
公开(公告)号：EP2312126B1
公开(公告)日：2015-12-23
申请号：EP09172601.8
申请日：2009-10-08
申请人： General Electric Company
发明人： Joshi, Narendra Digamber , Tangirala, Venkat Eswarlu , Hinckley, Kevin Michael
IPC分类号： F01D19/02 , F02C5/12 , F02C7/08 , F02C7/224 , F23R7/00
CPC分类号： F01D19/02 , F02C5/12 , F02C7/08 , F02C7/224 , F23R7/00

18. 发明授权

EP2326815B1 VERBRENNUNGSTURBINE MIT DISKONTINUIERLICHER VERBRENNUNG 有权
标题翻译：燃烧涡轮不连续燃烧
公开(公告)号：EP2326815B1
公开(公告)日：2015-01-28
申请号：EP09775586.2
申请日：2009-08-05
申请人： Gabl, Helmut , Lorenz, Edmund , Niederl, Franz
发明人： Gabl, Helmut , Lorenz, Edmund , Niederl, Franz
IPC分类号： F02C5/12 , F23R7/00 , F02K7/06
CPC分类号： F02C5/12 , F02C5/02 , F02K7/06 , F23R7/00 , Y02T50/671

19. 发明公开

EP1710417A2 Pulse combustion device 有权
标题翻译： Apparat mit pulsierender Verbrennung
公开(公告)号：EP1710417A2
公开(公告)日：2006-10-11
申请号：EP06251551.5
申请日：2006-03-23
申请人： UNITED TECHNOLOGIES CORPORATION
发明人： Lupkes, Kirk R. , Lidstone, Gary L.
IPC分类号： F02C5/12 , F02K7/06
CPC分类号： F02K7/06 , F02C5/02 , F02C5/12 , F05D2250/323 , F05D2250/324 , F05D2250/52 , F23R7/00
摘要： A pulse combustion device (26) comprises a circular array of conduits (30) each having an inlet (42) and an outlet (43). A valve admits a first gas to the inlets (42). An outlet end member (45) is provided. The array and end member (45) are relatively rotatable and the outlet end member (45) forms a nozzle with a circumferentially varying geometry.
摘要翻译：脉冲燃烧装置（26）包括每个具有入口（42）和出口（43）的导管（30）的圆形阵列。阀门允许第一气体到入口（42）。提供出口端部件（45）。阵列和端部构件（45）相对可旋转，并且出口端构件（45）形成具有周向变化几何形状的喷嘴。

20. 发明公开

EP1483489A1 TURBINE A GAZ AVEC COMBUSTION INTERMITTENTE 有权
标题翻译：涡轮机GAZ AVEC燃烧间隔
公开(公告)号：EP1483489A1
公开(公告)日：2004-12-08
申请号：EP02797995.4
申请日：2002-08-29
申请人： Macarez, Bernard
发明人： Macarez, Bernard
IPC分类号： F02C5/12
CPC分类号： F02C5/02 , F02C5/12 , F23R7/00 , Y02T50/671
摘要： The pulse jet engine is a gas turbine characterized by an intermittent isochore combustion. The permanent flow of compressor output is pumped over in the form of gas bursts (pulses) towards the turbine stages after combustion has taken place in one or several units of three combustion chambers operating according to a three-phase cycle: intake, combustion, expansion. The throttle valves for opening and closing the chambers are controlled by electromagnets monitored by a digital system. The adjustment of the frequency of pulse productions and harmonization of the units enable the operating lines and variable permeability levels in the compressor field. The structural architecture is applicable to any type of aircraft engine, on land or at sea. For the same power level, the pulse jet engine consumes less fuel, and the pumped over air flow is less than that of gas turbines.
摘要翻译：脉冲喷气发动机是一种燃气轮机，其特征在于间歇等时燃烧。在燃烧发生在三个燃烧室的一个或多个单元中，燃烧发生后，压缩机输出的永久流以气体突发（脉冲）的形式被泵送到三个燃烧室，这三个燃烧室按照三相循环进行操作：进气，燃烧，膨胀。用于打开和关闭腔室的节流阀由数字系统监控的电磁铁控制。脉冲产生频率的调整和单元的协调使得压缩机领域的操作线和可变渗透率水平成为可能。该结构体系结构适用于陆地或海上的任何类型的飞机发动机。对于相同的功率水平，脉冲喷气发动机消耗更少的燃料，并且泵送的空气流量小于燃气轮机。

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