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1. 发明申请

WO2006057653A3 INTEGRATED AIR INLET SYSTEM FOR MULTI-PROPULSION AIRCRAFT ENGINES 审中-公开
标题翻译：用于多推进飞机发动机的集成空气入口系统
公开(公告)号：WO2006057653A3
公开(公告)日：2007-10-18
申请号：PCT/US2005004893
申请日：2005-02-16
申请人： AEROJET GENERAL CO , BULMAN MELVIN J , BILLIG FREDERICK S
发明人： BULMAN MELVIN J , BILLIG FREDERICK S
IPC分类号： B64D33/02 , F02K99/00
CPC分类号： F02K7/10 , B64C30/00 , B64D33/02 , F02C7/042 , F02K7/14 , F02K7/16 , F02K9/18 , F05D2220/34 , Y10T137/0536
摘要： An air inlet duct for an air-breathing combined-cycle aircraft engines is internally divided into separate channels for low-speed and high-speed components of the engine, and contains one or more movable panels that are fully contained within the duct and pivotal between an open position in which incoming air is directed to both channels and a closed position in which all incoming air is directed to the channel leading to the high-speed engine. This integrated duct utilizes all incoming air at all stages of flight with no change in either the geometry of the air capture portion of the engine or the engine itself, and no exposure of movable leading edges. The result is a minimum of shock waves and a high degree of efficiency in operation of the engine.
摘要翻译：用于空气呼吸联合循环飞机发动机的空气入口管道被内部分成用于发动机的低速和高速部件的单独的通道，并且包含一个或多个完全容纳在管道内的可移动的面板，并且枢转地在进入的空气被引导到两个通道的打开位置和其中所有进入的空气被引导到通向高速发动机的通道的关闭位置。这种集成的管道在飞行的所有阶段都使用所有进入的空气，而不改变发动机或发动机本身的空气捕获部分的几何形状，也不会使可动的前缘暴露。结果是最小的冲击波和发动机运转的高效率。

2. 发明申请

WO2007035298A2 ADVANCED HYPERSONIC MAGNETIC JET/ELECTRIC TURBINE ENGINE 审中-公开
标题翻译：先进的超声波喷射/电动涡轮发动机
公开(公告)号：WO2007035298A2
公开(公告)日：2007-03-29
申请号：PCT/US2006/035253
申请日：2006-09-11
申请人： LUGG, Richard, H.
发明人： LUGG, Richard, H.
IPC分类号： F02C9/16
CPC分类号： F02K7/10 , F01D5/03 , F02K3/00 , F02K3/08 , F02K5/00 , F03H1/0081 , F03H99/00 , F05D2220/34 , F05D2240/515 , Y02T50/67 , Y02T50/672 , Y02T50/673
摘要： With turbine segments controlled electrically in a shaftless design, the turbine of the present invention creates high propulsion efficiencies over a broader range of operating conditions through the integration of gas turbine, electric and magnetic power systems, advanced materials and alternative petroleum-based combustion c cles,
摘要翻译：涡轮机段在无轴设计中被电气控制，本发明的涡轮通过燃气轮机，电力和磁力系统，先进材料和替代的石油基燃烧气体的集成，在更宽的操作条件范围内产生高推进效率，

3. 发明申请

WO1993010401A1 ARRANGEMENT FOR SUPPRESSING COMBUSTION-CAUSED VIBRATIONS IN THE COMBUSTION CHAMBER OF A GAS TURBINE SYSTEM 审中-公开
标题翻译：用于抑制燃气涡轮机系统燃烧室内燃烧引起的振动的装置
公开(公告)号：WO1993010401A1
公开(公告)日：1993-05-27
申请号：PCT/DE1992000926
申请日：1992-11-06
申请人： SIEMENS AKTIENGESELLSCHAFT , SCHETTER, Bernhard
发明人： SIEMENS AKTIENGESELLSCHAFT
IPC分类号： F23M13/00
CPC分类号： F23R3/28 , F05D2220/32 , F05D2220/34 , F05D2260/96 , F05D2260/962 , F05D2270/14 , F23M20/005 , F23N5/16 , F23R2900/00013 , F23R2900/00014
摘要： An arrangement is disclosed for suppressing the combustion-caused vibrations in a gas turbine system combustion chamber (1) capable of vibrating acoustically. Said combustion chamber (1) has a burner (2) for burning a fuel-carrying fluid that may be supplied to the burner (2) through a supply line (3) capable of acoustically vibrating and acoustically coupled to the combustion chamber (1). In a first embodiment, the arrangement has an acoustically-active element (4, 5; 6; 7; 19) coupled to the supply line (3) that acoustically tunes-in the supply line (3) so that an unsteady combustion caused by acoustic vibrations in the supply line (3) is essentially excluded. In a second embodiment of the invention, the acoustic vibrations in the supply line (3) react by means of the acoustically-active element (4, 5; 6; 7; 19) on the acoustic vibrations in the combustion chamber (1). This feedback is conditioned by an unsteady combustion caused by the acoustic vibrations in the supply line (3) and is set in such a manner that it counteracts the generation of combustion-caused vibrations. The invention may be advantageously used in stationary gas turbine systems with 100 MW and higher electric rated power.
摘要翻译：公开了一种用于抑制能够在声学上振动的燃气轮机系统燃烧室（1）中的燃烧引起的振动的装置。所述燃烧室（1）具有用于燃烧燃料输送流体的燃烧器（2），所述燃料输送流体可以通过能够声学振动和声学耦合到燃烧室（1）的供应管线（3）供应到燃烧器（2）。在第一实施例中，该装置具有耦合到供应管线（3）的声学有效元件（4,5; 6; 7; 19），其在供应管线（3）中声学调谐，使得由电源线（3）中的声音振动基本上被排除。在本发明的第二实施例中，供应管线（3）中的声振动通过声学活动元件（4,5; 6; 7; 19）在燃烧室（1）中的声振动上作用。这种反馈受到由供应管线（3）中的声音振动引起的不稳定燃烧的影响，并且被设置为使得其抵消燃烧引起的振动的产生。本发明可有利地用于具有100MW和更高电额定功率的固定式燃气轮机系统中。

4. 发明申请

WO2012166271A2 ADJUSTABLE EXHAUST APPARATUS FOR A RAM AIR TURBINE GENERATING SYSTEM 审中-公开
标题翻译：可调式排气装置，用于RAM空气涡轮发电系统
公开(公告)号：WO2012166271A2
公开(公告)日：2012-12-06
申请号：PCT/US2012/035771
申请日：2012-04-30
申请人： ADVANCED TECHNOLOGIES GROUP, INC. , JUSTAK, John, F.
发明人： JUSTAK, John, F.
IPC分类号： F03D7/02 , F01D9/04
CPC分类号： B64D41/007 , F01D17/14 , F03D1/04 , F03D9/00 , F03D9/25 , F03D9/32 , F03D15/20 , F03D80/70 , F03D80/82 , F05D2220/34 , Y02E10/72
摘要： An adjustable exhaust apparatus for use with a pod having a pod housing formed with at least one exhaust opening comprises a number of exhaust panels each hinged to the pod housing in position to move between a closed position in which the at least one exhaust opening is sealed, and an open position in which the exhaust panels are oriented at up to about a 30° angle relative to the pod housing. The exhaust panels, when in the open position, are effective to create a negative pressure within at least the aft portion of the pod housing to draw air into the pod and to assists in maintaining or at least avoiding an appreciable drop in the kinetic energy of an air stream moving through the pod interior.
摘要翻译：一种与可拆卸的排气装置一起使用，其具有形成有至少一个排气口的荚壳体，所述荚壳包括形成有至少一个排气口的多个排气板，每个排气板各自铰接到所述荚壳体的适当位置，以在所述至少一个排气口被密封的关闭位置之间移动，以及打开位置，其中排气板相对于荚壳体定向成高达约30°的角度。当排气板处于打开位置时，有效地在荚壳体的至少后部部分内产生负压，以将空气吸入荚中并帮助维持或至少避免动能的明显下降通过荚内部移动的气流。

5. 发明申请

WO99014116A1 RAM AIR TURBINE SYSTEM 审中-公开
标题翻译： RAM空气涡轮机系统
公开(公告)号：WO99014116A1
公开(公告)日：1999-03-25
申请号：PCT/US1998/019413
申请日：1998-09-17
IPC分类号： B64D41/00 , F01D15/08 , F01D15/10
CPC分类号： B64D41/007 , F01D15/08 , F01D15/10 , F05D2220/34 , F05D2270/03
摘要： A ram air turbine includes a reaction turbine and an electrical generator that is driven by shaft power of the reaction turbine. A scoop directs a flow of ram air to an inlet of the reaction turbine and creates a pressure head for the reaction turbine. The reaction turbine and the scoop are contained entirely within a pod. The ram air turbine further includes a turbocompressor, including a turbine stage and a compressor stage, which provides a stream of cooled air to equipment inside the pod. The turbocompressor also reacts loads shed by the electrical generator.
摘要翻译：压头空气涡轮机包括由反应涡轮机的轴功率驱动的反应涡轮机和发电机。勺子将冲压空气流引导到反应涡轮机的入口并产生用于反应涡轮机的压力头。反应涡轮机和勺子完全包含在荚内。压头空气涡轮机还包括涡轮压缩机，其包括涡轮级和压缩机级，其向冷却器内的设备提供冷却空气流。涡轮压缩机还对由发电机排出的负载作出反应。

6. 发明申请

WO1998027330A1 RAMJET ENGINE FOR POWER GENERATION 审中-公开
标题翻译：用于发电的RAMJET发动机
公开(公告)号：WO1998027330A1
公开(公告)日：1998-06-25
申请号：PCT/US1997023351
申请日：1997-12-16
申请人： LAWLOR, Shawn, P.
IPC分类号： F02K07/10
CPC分类号： F01D1/34 , F02C3/14 , F02C3/16 , F02C7/04 , F02K1/827 , F02K7/005 , F05D2220/10 , F05D2220/34 , F05D2270/082 , Y02E20/16 , Y02T50/672 , Y02T50/677
摘要： A ramjet engine power generator (100) having supersonic ramjets (U) has partially shrouded ramjet inlets. Fuel is oxidized in the ramjets to produce thrust and rotate a shaft (110). Efficient mixing of the oxidant and fuel prior to entry into the ramjet combustor, and the short residence times in the combustion chamber minimize the formation of NOx.
摘要翻译：具有超音速冲击弹（U）的冲压式发动机发电机（100）具有部分覆盖的冲压式进气口。燃料在冲击器中被氧化以产生推力并旋转轴（110）。氧化剂和燃料在进入冲压式喷气式燃烧器之前的有效混合以及在燃烧室中的短停留时间使得NOx的形成最小化。

7. 发明申请

WO2007035298A3 ADVANCED HYPERSONIC MAGNETIC JET/ELECTRIC TURBINE ENGINE 审中-公开
标题翻译：先进的超音速磁力喷射/电动涡轮发动机
公开(公告)号：WO2007035298A3
公开(公告)日：2007-12-27
申请号：PCT/US2006035253
申请日：2006-09-11
申请人： LUGG RICHARD H
发明人： LUGG RICHARD H
IPC分类号： F02K3/00 , F02K7/00 , F02K9/00
CPC分类号： F02K7/10 , F01D5/03 , F02K3/00 , F02K3/08 , F02K5/00 , F03H1/0081 , F03H99/00 , F05D2220/34 , F05D2240/515 , Y02T50/67 , Y02T50/672 , Y02T50/673
摘要： With turbine segments controlled electrically in a shaftless design, the turbine of the present invention creates high propulsion efficiencies over a broader range of operating conditions through the integration of gas turbine, electric and magnetic power systems, advanced materials and alternative petroleum-based combustion c cles,
摘要翻译：对于以无轴设计电控制的涡轮扇形段，本发明的涡轮通过集成燃气涡轮，电动和磁力动力系统，先进材料和替代石油基燃烧循环，在更广泛的操作条件范围内产生高推进效率，

8. 发明申请

WO2003010432A1 ROTARY RAMJET ENGINE WITH FLAMEHOLDER EXTENDING TO RUNNING CLEARANCE AT ENGINE CASING INTERIOR WALL 审中-公开
标题翻译：旋转式拉杆发动机，具有扩展到发动机外壳内部空间的运行间隙
公开(公告)号：WO2003010432A1
公开(公告)日：2003-02-06
申请号：PCT/US2002/023318
申请日：2002-07-23
申请人： RAMGEN POWER SYSTEMS, INC.
发明人： LAWLOR, Shawn, P. , STEELE, Robert, C. , KENDRICK, Donald
IPC分类号： F02K7/10
CPC分类号： F02K7/10 , F05D2220/10 , F05D2220/34 , F05D2250/25 , F05D2270/082
摘要： A rotary ramjet engine (E) is provided operating with a very low axial flow component. The engine has a rotor (210), shaft (204), a plurality of ramjet combustors mounted on the periphery of the rotor (210). A set of spaced helical strakes extend from the outside surface of the rotor toward the interior wall of the engine case, less a running clearance therefrom. A centerbody (36) is provided for each ramjet engine. The centerbody is disposed parallelto the strakes and includes leading edge structure (34), opposing sidewalls, a shaped cavity, and a rear end wall.
摘要翻译：提供旋转冲压喷气发动机（E），其操作具有非常低的轴向流动分量。发动机具有转子（210），轴（204），安装在转子（210）周边上的多个冲压喷气燃烧器。一组间隔开的螺旋形斜架从转子的外表面朝向发动机机壳的内壁延伸，减少了与其的运行间隙。为每个冲压喷气发动机提供中心体（36）。所述中心体平行于所述横梁设置并包括前缘结构（34），相对侧壁，成形腔和后端壁。

9. 发明申请

WO0038985A9 LOW DRAG DUCTED RAM AIR TURBINE GENERATOR AND COOLING SYSTEM 审中-公开
标题翻译：低牵引RAM空气涡轮发电机和冷却系统
公开(公告)号：WO0038985A9
公开(公告)日：2001-08-02
申请号：PCT/US9929671
申请日：1999-12-14
申请人： GHETZLER AERO POWER CORP , GHETZLER RICHARD , WOJTALIK JEROME , KRUSE NEILS , STEPHENS KENDAL R , SCHMULENSON HAROLD
发明人： GHETZLER RICHARD , WOJTALIK JEROME , KRUSE NEILS , STEPHENS KENDAL R , SCHMULENSON HAROLD
IPC分类号： F02C7/04 , F01D15/10 , F01D17/06 , F01D17/14 , F01D25/12 , F02C7/042 , H02K7/18
CPC分类号： F01D25/12 , B64D41/007 , F01D15/10 , F01D17/06 , F01D17/14 , F02C7/042 , F05D2220/34 , Y02T50/671 , Y02T50/675 , Y10T137/0536 , Y10T137/0645
摘要： A low drag ducted ram air turbine generator and cooling system is provided. The ducted ram air turbine generator and cooling system has reduced drag while extracting dynamic energy from the air stream during the complete range of intended flight operating regimes. A centerbody/valve tube (57) having an aerodynamically shaped nose (76) is slidably received in a fairing (30) and primary structure (50) to provide a variable inlet area. An internal nozzle control mechanism (115) attached to the valve tube positions nozzle control doors (70) to provide variable area nozzles directing air flow to the turbine stator (80) and rotor blades (62) to maintain optimum generator efficiency.
摘要翻译：提供了一种低阻力管道式冲压式空气涡轮发电机和冷却系统。管道式冲压式空气涡轮发电机和冷却系统在预期的飞行运行状态的完整范围内从空气流中提取动态能量减少了阻力。具有空气动力学形状的鼻部（76）的中心体/阀管（57）可滑动地容纳在整流罩（30）和主结构（50）中以提供可变的入口区域。附接到阀管的内部喷嘴控制机构（115）定位喷嘴控制门（70），以提供将空气流引导到涡轮定子（80）和转子叶片（62）的可变区域喷嘴，以保持最佳发电机效率。

10. 发明申请

WO2014140449A1 SOUFFLANTE DE TURBOMOTEUR A FLUX MULTIPLE, ET TURBOMOTEUR EQUIPE D'UNE TELLE SOUFFLANTE 审中-公开
标题翻译：多风扇涡轮发动机风扇和涡轮发动机配有风扇
公开(公告)号：WO2014140449A1
公开(公告)日：2014-09-18
申请号：PCT/FR2014/050472
申请日：2014-03-04
申请人： SNECMA
发明人： DELAPIERRE, Michaël , REGHEZZA, Patrick, Jean-Louis
IPC分类号： F01D5/22 , F01D5/30 , F01D5/32 , F01D11/00 , F04D29/66
CPC分类号： F01D5/26 , F01D1/06 , F01D5/22 , F01D5/3007 , F01D5/323 , F01D9/041 , F01D11/008 , F02K1/00 , F02K3/00 , F04D29/322 , F04D29/668 , F05D2220/34 , F05D2220/36 , F05D2230/644 , F05D2240/35 , F05D2260/30 , F05D2260/96
摘要： La soufflante (3) comporte un disque de soufflante (8) apte à être entraîné en rotation autour d'un axe longitudinal et pourvu, en périphérie, d'aubes radiales (10) comprenant chacune un pied (12) s'engageant par coulisse- ment dans une rainure (18) du disque, et, extérieurement à celle-ci, une pale (11), des plateformes (14) entourant le disque en étant intercalées entre les aubes radiales. Avantageusement, la soufflante comporte de plus des cales d'amortissement (31) qui sont agencées tangentiellement en périphérie extérieure (19) dudit disque (8), sous les plateformes (14) et entre deux pieds (12) d'aubes radiales adjacentes, chaque cale (31) étant au contact tangentiel des deux aubes adjacentes.
摘要翻译：风扇（3）包括能够围绕纵向轴线旋转地驱动的风扇盘（8），并且在周边处设置有径向叶片（10），每个叶片包括可滑动地接合在盘的凹槽（18）中的根部（12）并且在其外侧具有叶片（11），围绕所述盘的平台（14）插入在所述径向叶片之间。有利地，风扇还包括减震楔（31），它们在平台（14）的下方和相邻的径向叶片的两根（12）之间的切割位置处设置在所述盘（8）的外周（19）处，每个楔形（31）与两个相邻的叶片切向接触。

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