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61. 发明公开

EP3149309A1 COMBUSTION ENGINE 有权
标题翻译：内燃机
公开(公告)号：EP3149309A1
公开(公告)日：2017-04-05
申请号：EP15721795.1
申请日：2015-04-30
申请人： Gabrielle Engine Limited
发明人： WILLIAMS, Clive Propert
IPC分类号： F02C3/16
CPC分类号： F02C3/14 , F02C3/165 , F02C7/06 , F02C7/22 , F04D29/284 , F05D2240/35
摘要： A combustion engine comprising a radial compressor in flow communication via a flow passage with an annular compressor-combustor array radially outward of the radial compressor. Both the radial compressor and compressor-combustor are co-axial with, and rotatable around, a central axis.
摘要翻译：一种内燃机，包括径流式压缩机，所述径流式压缩机经由流动通道与径向压缩机的径向外部的环形压缩机 - 燃烧器阵列流动连通。径向压缩机和压缩机 - 燃烧器都与中心轴线共轴并且可围绕中心轴线旋转。

62. 发明公开

EP1627185A4 TRAPPED VORTEX COMBUSTOR 审中-公开
标题翻译： BRENNKAMMER MIT EINGESCHLOSSENEM WIRBEL
公开(公告)号：EP1627185A4
公开(公告)日：2017-01-11
申请号：EP04785836
申请日：2004-02-04
申请人： DRESSER-RAND COMPANY
发明人： KENDRICK DONALD , LAWLOR SHAWN P , STEELE ROBERT C
IPC分类号： F23R3/58 , F01D1/02 , F01D1/32 , F02C3/16 , F02K7/00 , F02K7/10 , F23R20060101 , F23R3/18 , F23R3/20 , F23R3/28 , F23R3/50
CPC分类号： F23R3/50 , F01D1/026 , F01D1/32 , F02C3/165 , F02K7/005 , F02K7/10 , F05D2220/60 , F05D2250/25 , F23R3/18 , F23R3/28

63. 发明公开

EP3019703A2 ENGINE PROPULSION SYSTEM 有权
标题翻译： MOTORANTRIEBSSYSTEM
公开(公告)号：EP3019703A2
公开(公告)日：2016-05-18
申请号：EP14823797.7
申请日：2014-07-10
申请人： Miller, Derrick
发明人： Miller, Derrick
IPC分类号： F01D1/32
CPC分类号： F02K9/95 , F02C3/14 , F02C3/165 , F02C5/02 , F02C5/04 , F02C5/12 , F02K9/00 , F05D2220/32 , F41A19/13 , H02K7/1823
摘要： This invention relates to devices that convert hydraulic pressure and flow into torque and angular displacement. Previously, engines utilized a large number of moving parts that reduced system efficiency instead of concentrating on turning a shaft. Embodiments of the present invention use at least one cannon (10) wherein each cannon is configured to displace the media. Each cannon contains a firing pin outer casing (11) configured to accommodate a firing pin (12). The firing pin is configured to create the mechanical energy when moved thus allowing the media to exit the cannon

64. 发明公开

EP2990729A1 COMBUSTION SYSTEM 审中-公开
标题翻译： VERBRENNUNGSSYSTEM
公开(公告)号：EP2990729A1
公开(公告)日：2016-03-02
申请号：EP15180309.5
申请日：2015-08-07
申请人： Rolls-Royce North American Technologies, Inc.
发明人： RESS, Jr, Robert A. , HOLDCRAFT, John D.
IPC分类号： F23R3/56
CPC分类号： F02C3/165 , B23P15/00 , F02C5/04 , F02C7/222 , F23R3/56
摘要： A combustion system for gas turbine engine is disclosed. The combustion system includes a wave rotor drum and a drive coupled to the wave rotor drum. The wave rotor drum is mounted for rotation about an axis and is formed to include a plurality of combustion channels that extend along the axis to conduct transient waves along the axis during operation of the combustion system. The drive is coupled to the wave rotor drum and is adapted to drive rotation of the wave rotor drum about the axis.
摘要翻译：公开了一种燃气轮机的燃烧系统。燃烧系统包括波转子鼓和耦合到波转子鼓的驱动器。波转子鼓安装成围绕轴线旋转，并且形成为包括沿着轴线延伸的多个燃烧通道，以在燃烧系统的操作期间沿轴线传导瞬态波。驱动器耦合到波转子鼓并且适于驱动波转子鼓绕轴线的旋转。

65. 发明公开

EP2721273A1 COMBUSTION SYSTEMS AND COMBUSTION SYSTEM COMPONENTS FOR ROTARY RAMJET ENGINES 审中-公开
标题翻译：燃烧系统和燃烧系统部件的转子发动机冲压发动机引擎
公开(公告)号：EP2721273A1
公开(公告)日：2014-04-23
申请号：EP12800390.2
申请日：2012-05-25
申请人： Socpra-Sciences Et Génie S.E.C.
发明人： PLANTE, Jean-Sébastien , PICARD, Mathieu , RANCOURT, David
IPC分类号： F02C7/264 , F02C3/14 , F02K7/10 , F23R3/28
CPC分类号： F23R3/28 , F02C3/165 , F02C7/264 , F02K7/10 , F23R3/18 , F23R3/286 , F23R3/343 , F23R2900/00012 , F23R2900/03343 , Y02T50/672
摘要： The present disclosure relates to combustion systems and components for rotary ramjet engines. An injection system, optionally stratified for ease of engine startup, provides an air and fuel mixture to a combustion chamber. An ignition system ignites the mixture. A flameholding system may be positioned for communication with the combustion chamber to force an ignited flow of the air and fuel mixture toward a center of rotation within the ramjet engine. The ramjet engine may comprise a diverging stator for improved exhaust efficiency. Ignition may take place in the engine air intake. Alternatively, ignition may take place within the combustion chamber using a dual-hub electrically charged system. An impulse turbine may use recirculation of injected fuel to cool a rim-rotor and/or to reduce windage on the rim-rotor. A sealing system may reduce gas leaks from a fuel conduit into the engine air intake.

66. 发明公开

EP2598736A2 TURBINENRADANORDNUNG FÜR EINE GASTURBINE 审中-公开
标题翻译：涡轮的燃气轮机
公开(公告)号：EP2598736A2
公开(公告)日：2013-06-05
申请号：EP11817300.4
申请日：2011-10-14
申请人： Baltico GmbH
发明人： BÜCHLER, Dirk , BUTTKEWITZ, Gerhard
IPC分类号： F02C3/16 , F01D1/24 , F01D15/10 , F02C3/04 , F02C3/067 , F02C3/08 , F02C3/09 , F02C3/14
CPC分类号： F01D1/04 , F01D1/24 , F01D15/10 , F02C3/04 , F02C3/067 , F02C3/08 , F02C3/09 , F02C3/14 , F02C3/16 , F02C3/165
摘要： The invention relates to a turbine wheel arrangement for a gas turbine comprising two successive turbine wheels (18, 20) rotating in opposite directions, wherein the first turbine wheel (18) comprises flow channels (42) of a Laval cross-sectional shape, distributed over the circumference and having radially inner gas inlets (43) and radially further out gas outlets (45), in each case with a substantially tangential flow direction component, wherein the gas outlets (45) act on the second axially or radially acting turbine wheel (20) in the direction of flow. This has the effect that the thermal energy and compressive energy of the gas at the nozzle inlet is largely converted into flow energy at the outlet of the turbine stage. The rotational speeds of the two rotors coupled to the turbine wheels can be set as desired, allowing the operational states of the two systems to be optimally set without adjusting systems.

67. 发明公开

EP2340357A1 INDEXED POSITIVE DISPLACEMENT ROTARY MOTION DEVICE 审中-公开
标题翻译：指数正位移旋转运动装置
公开(公告)号：EP2340357A1
公开(公告)日：2011-07-06
申请号：EP09813935.5
申请日：2009-09-17
申请人： Exponential Technologies, Inc.
发明人： JUAN, Alejandro , PATTERSON, Curtis , GOTTFRIED, Kristjan , FARSHCHIAN, Soheil
IPC分类号： F01C3/08 , F01C3/06
CPC分类号： F01C3/085 , F01C1/10 , F01C1/107 , F01C1/20 , F01C21/08 , F01C21/10 , F02B53/04 , F02B53/10 , F02B53/12 , F02C3/165 , F02C5/00 , F04C3/085 , F04C18/48 , F04C2250/201 , F05D2250/232
摘要： An indexing system for a rotor assembly where the indexing system can regulate the rotational location of drive rotors that are configured to rotate about a shaft in one form.
摘要翻译：一种用于转子组件的分度系统，其中分度系统可以调节构造成以一种形式围绕轴旋转的驱动转子的旋转位置。

68. 发明公开

EP1627185A2 TRAPPED VORTEX COMBUSTOR 审中-公开
标题翻译：燃烧被困EDDY
公开(公告)号：EP1627185A2
公开(公告)日：2006-02-22
申请号：EP04785836.0
申请日：2004-02-04
申请人： Ramgen Power Systems, Inc.
发明人： KENDRICK, Donald , LAWLOR, Shawn, P. , STEELE, Robert, C.
IPC分类号： F23R3/58
CPC分类号： F23R3/50 , F01D1/026 , F01D1/32 , F02C3/165 , F02K7/005 , F02K7/10 , F05D2220/60 , F05D2250/25 , F23R3/18 , F23R3/28
摘要： A trapped vortex combustor for gas turbine engines. An annular combustor housing is provided having a plurality of inlet centerbodies disposed along a helical axis. The inlet centerbodies include a leading edge structure, opposing sidewalls, a pressurizable cavity, and a rear wall. Inlet centerbodies cooperate with adjacent structure and an aft bluff body to define a trapped vortex cavity combustion chamber for mixing an inlet fluid and burning fuel to form hot combustion gases. Mixing is enhanced by utilizing struts adjacent to the rear wall to create eddies in the fluid flow, and by injecting fuel and/or air in opposition to swirl created by the bulk fluid flow. Hot combustion gases are utilized in a turbine for extraction of kinetic energy, or in heat exchange equipment for recovery of thermal energy. High combustion efficiencies and less than 10 ppm emissions of oxides of nitrogen and of carbon monoxide are achieved.

69. 发明公开

EP1548364A3 A rotary combustor, and electrical generator comprising a combustor of this type 审中-公开
标题翻译：旋转式燃烧器和包括这种燃烧器的发电机
公开(公告)号：EP1548364A3
公开(公告)日：2005-09-28
申请号：EP04030125.1
申请日：2004-12-20
申请人： C.R.F. Società Consortile per Azioni
发明人： Perlo, Pietro , Innocenti, Gianfranco , Repetto, Piermario , Sgroi, Mauro , Bollito, Gianluca , Pairetti, Bartolo , Monferino, Rossella , Finizio, Roberto , Carvignese, Cosimo
IPC分类号： F23R3/56 , F23C11/04 , F02C3/16 , H02K7/18 , F16C39/06 , F23R3/50 , B81B7/00 , F02K7/00
CPC分类号： H02K7/1823 , F01D1/32 , F02C3/16 , F02C3/165 , F02K7/005 , F16C32/0427 , F16C32/0429 , F16C39/063 , F23C15/00 , F23R3/52 , F23R3/56
摘要： The combustor (1) comprises a stationary structure (2; 102) and at least one tubular rotor (3; 3', 3") supported rotatably about an axis (4) by the structure (2; 102) by means of contactless suspension devices (5-8; 5', 5", 6', 6") there being formed within this rotor at least one combustion chamber (20; 20', 20") having at least one orientated lateral outflow aperture (21; 22; 23, 24) for the ejection of the combustion gases. The rotor (3; 3', 3") has a narrow circumferential slot (30; 30', 30") through which there extend at least one controlled stationary injector (31; 31', 31") of fuel and combustion agent and an associated igniter (32; 32', 32") which is also stationary.
A control unit (ECU; 35) operates the injector (31; 31', 31") and the igniter (32; 32', 32") according to predetermined procedures, in such a way as to generate a detonation wave which is propagated in the chamber (20; 20', 20"), and to cause the rotor (3; 3', 32) to rotate as a result of the thrust due to the combustion gases emitted through the lateral outflow aperture (21, 22; 23, 24).
摘要翻译：所述燃烧器（1）包括静止结构（2; 102）和至少一个管状转子（3; 3'，3“），所述管状转子通过所述结构（2; 102）围绕轴线（4）在该转子内形成至少一个燃烧室（20; 20'，20“）的装置（5-8; 5'，5”，6'，6“），该燃烧室具有至少一个定向的横向流出孔（21; 22 ; 23,24），用于喷射燃烧气体。转子（3; 3'，3“）具有狭窄的圆周槽（30; 30'，30”），通过该狭槽延伸至少一个燃料和燃烧剂的受控制的固定喷射器（31; 31'，31“）和一个相关的点火器（32; 32'，32“），它也是静止的。控制单元（ECU; 35）根据预定程序操作喷射器（31; 31'，31“）和点火器（32; 32'，32”），以产生传播的爆震波在所述腔室（20; 20'，20“）中，并且由于通过所述侧向流出孔（21,22; 20）发射的燃烧气体的推力而使所述转子（3; 3'，32） 23，24）。

70. 发明公开

EP1455065A3 Pulse detonation system for a gas turbine engine 有权
标题翻译：燃气涡轮发动机的脉冲爆震系统
公开(公告)号：EP1455065A3
公开(公告)日：2004-12-22
申请号：EP04251220.2
申请日：2004-03-03
申请人： GENERAL ELECTRIC COMPANY
发明人： Venkataramani, Kattalaicheri Srinivasan , Butler, Lawrence , Bailey, William Andrew
IPC分类号： F02C5/06 , F02K7/02
CPC分类号： F02C3/165 , F02K3/06 , F02K7/02 , Y02T50/671
摘要： A pulse detonation system for a gas turbine engine having a longitudinal centerline axis (12) extending therethrough, where the pulse detonation system includes an air inlet duct (48) in flow communication with a source of compressed air, the air inlet duct (48) including at least one port (50) formed therein for permitting compressed air to flow therethrough, a fuel injector (52) mounted to the air inlet duct (48) in circumferentially spaced relation to each port (50), and a device mounted to the air inlet duct (48) in circumferentially spaced relation to each fuel injector (52) for initiating a detonation wave. A rotatable ring member (56) is also positioned in coaxial relation around a portion of the air inlet duct (48), with the ring member (56) including at least one stage of detonation (58/60) disposed therein. Accordingly, a detonation wave is produced in each detonation stage (58,60) and combustion gases following each detonation wave create a torque which causes the ring member (56) to rotate. Each detonation stage (58,60) in the ring member (56) further includes a plurality of circumferentially spaced detonation ducts (66) extending tangentially from an inner surface (74) of the ring member (56), wherein the detonation ducts (66) are aligned with each port (50), the fuel injector (52) and the initiation device (54) in a predetermined timing and sequence so that detonation waves are produced therein.
摘要翻译：一种用于燃气涡轮发动机的脉冲爆震系统，其具有延伸穿过其中的纵向中心线轴线（12），其中脉冲爆震系统包括与压缩空气源流动连通的进气管道（48）包括至少一个形成在其中的用于允许压缩空气流过其中的端口（50），安装到进气管道（48）上的燃料喷射器（52），其与每个端口（50）周向间隔开，以及安装到与每个燃料喷射器（52）周向间隔开的空气入口导管（48），用于启动爆轰波。一个可转动的环形件（56）也以同轴的关系设置在进气管（48）的一部分周围，环形件（56）至少包括一个设置在其中的爆炸阶段（58/60）。因此，在每个爆轰阶段（58,60）中产生爆轰波，并且在每个爆轰波之后的燃烧气体产生导致环部件（56）旋转的扭矩。环形部件（56）中的每个爆震阶段（58,60）还包括从环形部件（56）的内表面（74）切向延伸的多个周向间隔的爆震导管（66），其中爆震导管）以预定的时间和顺序与每个端口（50），燃料喷射器（52）和启动装置（54）对齐，从而在其中产生爆轰波。

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