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91. 发明授权

US09222416B2 Turbine engine gearbox 有权
标题翻译：涡轮发动机变速箱
公开(公告)号：US09222416B2
公开(公告)日：2015-12-29
申请号：US14470982
申请日：2014-08-28
申请人： UNITED TECHNOLOGIES CORPORATION
发明人： Michael E. McCune
IPC分类号： F16H1/28 , F02C7/36 , F16H1/46 , F01D15/12 , F02K3/072 , F16H57/00
CPC分类号： F02C7/36 , F01D15/12 , F02K3/04 , F02K3/072 , F05D2260/40311 , F16H1/28 , F16H1/46 , F16H57/0006 , Y02T50/671
摘要： A gas turbine engine comprises a fan, a compressor, a combustor, and a fan drive turbine rotor. The fan drive turbine drives the fan through a gear reduction. The gear reduction includes at least two double helical gears in meshed engagement. Each of the at least two double helical gears are disposed to rotate about respective axes, and each have a first plurality of gear teeth axially spaced from a second plurality of gear teeth by a spacer. Each of the first plurality of gear teeth has a first end facing the spacer and each of the second plurality of gear teeth has a first end facing the spacer. Each first end of the first plurality of gear teeth is circumferentially offset from each first end of the second plurality of gear teeth. A method is also disclosed.
摘要翻译：燃气涡轮发动机包括风扇，压缩机，燃烧器和风扇驱动涡轮机转子。风扇驱动涡轮驱动风扇通过齿轮减速。齿轮减速包括至少两个啮合啮合的双斜齿轮。所述至少两个双螺旋齿轮中的每一个设置成围绕相应的轴线旋转，并且每个具有通过间隔件与第二多个齿轮齿轴向间隔开的第一多个齿轮齿。第一多个齿轮齿中的每一个具有面向间隔件的第一端，并且第二多个齿轮齿中的每一个具有面向间隔件的第一端。第一多个齿轮齿的每个第一端从第二多个齿轮齿的每个第一端周向地偏移。还公开了一种方法。

92. 发明授权

US09217391B2 Turbine engine comprising a contrarotating propeller receiver supported by a structural casing attached to the intermediate housing 有权
标题翻译：涡轮发动机包括由连接到中间壳体的结构壳体支撑的对转螺旋桨接收器
公开(公告)号：US09217391B2
公开(公告)日：2015-12-22
申请号：US13654796
申请日：2012-10-18
申请人： SNECMA
发明人： Francois Gallet , Audrey Grede
IPC分类号： F02K3/062 , F02K3/072
CPC分类号： F02K3/072 , F02K3/062 , F05D2220/324 , F05D2220/325 , Y02T50/672
摘要： An open rotor type aircraft turbine engine including a contrarotating propeller receiver and a dual-body gas generator having a low-pressure compressor and a high-pressure compressor separated by an intermediate housing, in which the gas generator is arranged upstream from the receiver is provided. The turbine engine includes a structural casing for supporting the receiver, surrounding the gas generator and having a downstream end attached to the receiver and an upstream end attached to the intermediate housing; and a connection device between the structural supporting casing and the gas generator, arranged between the upstream and downstream ends of the casing.
摘要翻译：提供一种开式转子式飞机涡轮发动机，其包括对转螺旋桨接收器和具有低压压缩机和由其中气体发生器布置在接收器上游的中间壳体分隔的高压压缩机的双体气体发生器。涡轮发动机包括用于支撑接收器的结构壳体，围绕气体发生器并且具有附接到接收器的下游端和附接到中间壳体的上游端; 以及布置在壳体的上游和下游端之间的结构支撑壳体和气体发生器之间的连接装置。

93. 发明申请

US20150308352A1 GAS TURBINE ENGINE WITH FAN-TIED INDUCER SECTION 有权
标题翻译：具有风扇电感器部分的气体涡轮发动机
公开(公告)号：US20150308352A1
公开(公告)日：2015-10-29
申请号：US14788913
申请日：2015-07-01
申请人： United Technologies Corporation
发明人： Daniel Bernard Kupratis , Frederick M. Schwarz
IPC分类号： F02C7/36 , F02C7/042 , F02C7/047 , F02C3/06
CPC分类号： F02C7/36 , F02C7/042 , F02C7/047 , F02K3/072 , F05D2230/51 , F05D2260/40311
摘要： A gas turbine engine includes a shaft, a speed reduction device driven by the shaft, and a fan including a fan rotor driven by the speed reduction device. A compressor section has a plurality of compressor stages driven by the shaft. At least one inducer stage is positioned aft of the fan and coupled for rotation with the fan rotor. The at least one inducer stage is positioned upstream of the compressor section.
摘要翻译：燃气涡轮发动机包括轴，由轴驱动的减速装置和包括由减速装置驱动的风扇转子的风扇。压缩机部具有由轴驱动的多个压缩机级。至少一个诱导器台被定位在风扇的后方并与风扇转子一起旋转。所述至少一个导流段设置在压缩机部分的上游。

94. 发明授权

US09091207B2 Gas turbine engine air intake in a nacelle 有权
标题翻译：燃气轮机在机舱内进气
公开(公告)号：US09091207B2
公开(公告)日：2015-07-28
申请号：US13502294
申请日：2010-10-14
申请人： Philippe Gerard Chanez , Gaetan Jean Mabboux , Philippe Gilles Minot , Thomas Alain Christian Vincent , Didier Jean-Louis Yvon
发明人： Philippe Gerard Chanez , Gaetan Jean Mabboux , Philippe Gilles Minot , Thomas Alain Christian Vincent , Didier Jean-Louis Yvon
IPC分类号： F02C7/052 , B64D33/02 , F02C7/05 , F02C7/20 , F02K3/062 , F02K3/072 , B64D27/00
CPC分类号： F02C7/05 , B64D33/02 , B64D2027/005 , B64D2033/022 , B64D2033/0293 , F02C7/052 , F02C7/20 , F02K3/062 , F02K3/072 , F05D2250/292 , F05D2250/70 , F05D2260/607 , Y02T50/66 , Y02T50/671 , Y02T50/675
摘要： An assembly including a gas turbine engine and a nacelle in which the engine is housed, the nacelle including an air intake fairing that forms an air inlet and includes: a member for deflecting foreign objects, which together with the fairing, forms an air intake duct; and, downstream from the deflecting member, a secondary deflecting channel, and a main channel for supplying air to the engine. The air intake duct is configured to deflect at least some of the foreign objects sucked in through the air inlet towards the secondary deflecting channel. The secondary deflecting channel is shaped such that the flow velocity of the air flowing therethrough increases from upstream to downstream, the secondary channel having an outlet with an opening leading into the outer wall of the nacelle.
摘要翻译：包括燃气涡轮发动机和其中容纳发动机的机舱的组件，所述机舱包括形成空气入口的进气整流装置，并且包括：用于偏转异物的构件，其与整流罩一起形成进气管道 ; 并且在偏转构件的下游具有次级偏转通道和用于向发动机供应空气的主通道。进气管道构造成使通过空气入口吸入的至少一些异物朝向次级偏转通道偏转。二次偏转通道成形为使得流过其中的空气的流速从上游到下游增加，次级通道具有出口，其具有通向机舱的外壁的开口。

95. 发明申请

US20150198065A1 TURBOMACHINE ASSEMBLY COMPRISING TWO BODIES AND MEANS FOR GUIDING A FLUID FLOWING FROM ONE BODY TO THE OTHER 有权
标题翻译：包含两个机构的涡轮组件和用于引导从一个体向其他流体流动的流体的装置
公开(公告)号：US20150198065A1
公开(公告)日：2015-07-16
申请号：US14583910
申请日：2014-12-29
申请人： SNECMA
发明人： Catherine PIKOVSKY , Dominik IGEL , Boris LEMATTRE
IPC分类号： F01D25/18 , F01D11/02
CPC分类号： F01D25/183 , B64D2027/005 , F01D11/02 , F02C7/28 , F02K3/062 , F02K3/072 , F05D2220/325 , Y02T50/66
摘要： The primary subject-matter of the invention is a turbomachine assembly (1), comprising first (2) and second (3) bodies, at least one (2) of which is rotating relative to the other (3) around the axis of rotation (T) of the turbomachine (10), between which a tight zone (EH) is formed comprising a sealing gasket (16), a flowing fluid (H), in particular lubricant oil (H), able to circulate inside the first (2) and second (3) bodies and to be driven toward said at least one rotating body (2) from the other body (3), characterized in that said at least one rotating body (2) comprises means (4a, 4b, 4c; 5a, 5b) for guiding the rotation, in the direction of rotation (F3) of said at least one rotating body (2), of the flow of fluid (H) inside said at least one rotating body (2) so as to drive the flowing fluid (H) away from the tight zone (EH).
摘要翻译：本发明的主要主题是涡轮机组件（1），其包括第一（2）和第二（3）主体，其中至少一个（2）相对于另一个（3）围绕旋转轴线旋转（10），其间形成有紧密区域（EH），其包括密封垫圈（16），流体流体（H），特别是润滑油（H），其能够在第一（ 2）和第二（3）体，并且从另一主体（3）被驱动朝向所述至少一个旋转体（2），其特征在于，所述至少一个旋转体（2）包括装置（4a，4b，4c） ; 5a，5b），用于沿所述至少一个旋转体（2）的旋转方向（F3）引导所述至少一个旋转体（2）内部的流体（H）流动，从而驱动流动的流体（H）远离紧密区域（EH）。

96. 发明授权

US09057325B2 Rotary units, rotary mechanisms, and related applications 有权
标题翻译：旋转单元，旋转机构和相关应用
公开(公告)号：US09057325B2
公开(公告)日：2015-06-16
申请号：US14341804
申请日：2014-07-26
申请人： Christopher C. Sappenfield
发明人： Christopher C. Sappenfield
IPC分类号： F02K3/02 , F02C3/04 , F16H1/28 , F16H37/08 , A61C17/26
CPC分类号： F02K3/072 , A61C17/26 , F02C3/04 , F02C7/36 , F02K3/065 , F16H1/28 , F16H37/0813
摘要： The invention relates to rotary units and rotary mechanisms that are suitable for use in numerous applications. Rotary units typically include rotational components that are configured to rotate. In some embodiments, for example, multiple rotary units are assembled in rotary mechanisms such that neighboring pairs of rotational components counter-rotate or contra-rotate relative to one another during operation of the rotary mechanisms. Rotational components generally include one or more implements that are structured to perform or effect one or more types of work as the rotational components rotate relative to one another in a given rotary mechanism. In certain embodiments, implements are configured to rotate and/or to effect the movement of other components as rotational components rotate. In some embodiments, engines include rotary mechanisms and are used in, for example, ground vehicles, marine vehicles, aircraft, or devices.
摘要翻译：本发明涉及适用于许多应用中的旋转单元和旋转机构。旋转单元通常包括被配置为旋转的旋转部件。在一些实施例中，例如，多个旋转单元组装在旋转机构中，使得相邻的旋转组件对在旋转机构的操作期间相对于彼此反转或相反旋转。旋转部件通常包括一个或多个被构造成执行或实现一种或多种类型的工件的工具，因为旋转部件在给定的旋转机构中相对于彼此旋转。在某些实施例中，器具被配置为在旋转部件旋转时旋转和/或实现其它部件的移动。在一些实施例中，发动机包括旋转机构，并且用于例如地面车辆，船用车辆，飞行器或设备中。

97. 发明授权

US08944765B2 Bellows type sealing device for partition penetration by a connecting rod of a turboprop fan blade orientation control system 有权
标题翻译：涡卷螺旋桨风扇叶片定向控制系统的连杆用于隔板穿透的波纹管式密封装置
公开(公告)号：US08944765B2
公开(公告)日：2015-02-03
申请号：US13236689
申请日：2011-09-20
申请人： Gilles Alain Charier , Francois Gallet
发明人： Gilles Alain Charier , Francois Gallet
IPC分类号： B64C11/06 , F01D7/00 , F01D25/16 , F01D25/18 , F02C7/06 , F02K3/072 , F16J3/04 , F16J15/52
CPC分类号： F01D7/00 , B64C11/308 , B64D2027/005 , F01D25/16 , F01D25/183 , F02C7/06 , F02K3/072 , F05D2220/324 , F05D2220/325 , F05D2240/55 , F05D2250/232 , F05D2260/50 , F05D2260/56 , F05D2260/79 , F16J3/047 , F16J15/52 , Y02T50/66
摘要： The invention relates to a sealing device for the partition penetration of a connecting rod of a turboprop fan blade orientation control system. The device includes a bellows (60) of trunconical shape designed to allow passage of the connecting rod (50a) and having, at its wider end, means (62, 64) of attachment to the partition (58) to be sealed and, at its narrower end, an O-ring through which the connecting rod is free to slide.
摘要翻译：本发明涉及一种用于涡轮螺旋桨叶风扇叶片定向控制系统的连杆的隔板穿透的密封装置。该装置包括一个具有trunconical形状的波纹管（60），其设计成允许连杆（50a）通过，并且在其更宽的端部具有附接到待密封的隔板（58）的装置（62,64），并且在其较窄的端部，连接杆可自由滑动的O形环。

98. 发明授权

US08935913B2 Geared turbofan gas turbine engine architecture 有权
标题翻译：齿轮涡轮风力发电机结构
公开(公告)号：US08935913B2
公开(公告)日：2015-01-20
申请号：US13645606
申请日：2012-10-05
申请人： United Technologies Corporation
发明人： Daniel Bernard Kupratis , Frederick M. Schwarz
IPC分类号： F02K3/06
CPC分类号： F02C7/36 , F01D5/06 , F01D9/02 , F01D9/065 , F02C3/04 , F02C3/107 , F02C3/36 , F02C7/06 , F02C9/18 , F02K1/78 , F02K3/04 , F02K3/06 , F02K3/072 , F04D27/009 , F04D29/325 , F05D2220/32 , F05D2220/323 , F05D2240/12 , F05D2240/35 , F05D2240/60 , F05D2260/4031 , F05D2260/40311 , Y02T50/671
摘要： A gas turbine engine typically includes a fan section, a compressor section, a combustor section and a turbine section. A speed reduction device such as an epicyclical gear assembly may be utilized to drive the fan section such that the fan section may rotate at a speed different than the turbine section so as to increase the overall propulsive efficiency of the engine. In such engine architectures, a shaft driven by one of the turbine sections provides an input to the epicyclical gear assembly that drives the fan section at a speed different than the turbine section such that both the turbine section and the fan section can rotate at closer to optimal speeds providing increased performance attributes and performance by desirable combinations of the disclosed features of the various components of the described and disclosed gas turbine engine.
摘要翻译：燃气涡轮发动机通常包括风扇部分，压缩机部分，燃烧器部分和涡轮部分。可以使用诸如行星齿轮组件的减速装置来驱动风扇部分，使得风扇部分可以以不同于涡轮机部分的速度旋转，从而增加发动机的整体推进效率。在这样的发动机结构中，由一个涡轮机部分驱动的轴为行星齿轮组件提供输入，该输入齿轮组件以不同于涡轮机部分的速度驱动风扇部分，使得涡轮部分和风扇部分可以更接近最佳速度通过所述和所公开的燃气涡轮发动机的各种部件的公开特征的期望组合来提供增加的性能属性和性能。

99. 发明授权

US08894351B2 Retaining ring 有权
标题翻译：保持环
公开(公告)号：US08894351B2
公开(公告)日：2014-11-25
申请号：US13188792
申请日：2011-07-22
申请人： Yolaine Carre , Mathieu Jean Pierre Trohel
发明人： Yolaine Carre , Mathieu Jean Pierre Trohel
IPC分类号： F01D5/08 , B64C11/06 , F02K3/072 , F04D29/34 , B64D27/02
CPC分类号： B64C11/06 , B64D2027/026 , F02K3/072 , Y02T50/66 , Y02T50/672
摘要： A retaining ring presenting, on its periphery, a plurality of radial bores, each of the bores being able to receive a blade root. The retaining ring also includes at least one first radial opening traversed by a compression tube and at least one second radial opening, the at least first radial opening and the at least second radial opening being separated from each other by at least one of the bores of the plurality of radial bores. The ventilation device finds a particularly interesting application in the field of turbine engines including a pusher open rotor.
摘要翻译：保持环在其周边上呈现多个径向孔，每个孔能够接收叶根。保持环还包括由压缩管和至少一个第二径向开口横穿的至少一个第一径向开口，所述至少第一径向开口和至少第二径向开口通过至少一个孔多个径向孔。通风装置在涡轮发动机领域中发现了一个非常有趣的应用，包括推进器开放式转子。

100. 发明授权

US08887485B2 Three spool gas turbine engine having a clutch and compressor bypass 有权
标题翻译：具有离合器和压缩机旁路的三轴式燃气涡轮发动机
公开(公告)号：US08887485B2
公开(公告)日：2014-11-18
申请号：US12582339
申请日：2009-10-20
申请人： Robert A. Ress, Jr.
发明人： Robert A. Ress, Jr.
IPC分类号： F02K3/06 , F02C7/36 , F02K3/072
CPC分类号： F02K3/072 , F02C7/36 , F05D2260/4023 , Y10T403/10
摘要： An adaptive cycle gas turbine engine is disclosed having a number of features. A fan arrangement is provided having counter-rotating fan stages, one fan stage is operable to be clutched and decoupled from the other stage. A high pressure compressor bypass is also provided. A clutch is provided to at least partially drive an intermediate pressure compressor with a high pressure turbine when the high pressure compressor is bypassed. A partial bypass of the high pressure turbine may be provided.
摘要翻译：公开了具有许多特征的自适应循环燃气涡轮发动机。提供具有反向旋转风扇级的风扇装置，一个风扇级可操作以与另一级离合并与其分离。还提供高压压缩机旁路。当旁通高压压缩机时，提供离合器以至少部分驱动具有高压涡轮机的中压压缩机。可以提供高压涡轮机的部分旁路。

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