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81. 发明申请

US20130259643A1 GEARED TURBOFAN WITH THREE TURBINES WITH FIRST TWO COUNTER-ROTATING, AND THIRD CO-ROTATING WITH THE SECOND TURBINE 审中-公开
标题翻译：具有第三次涡轮机的三轮涡轮机，第二次涡轮机的第三次旋转
公开(公告)号：US20130259643A1
公开(公告)日：2013-10-03
申请号：US13437270
申请日：2012-04-02
申请人： Frederick M. Schwarz , Daniel Bernard Kupratis
发明人： Frederick M. Schwarz , Daniel Bernard Kupratis
IPC分类号： F01D1/26
CPC分类号： F02C3/067 , F01D9/041
摘要： A gas turbine engine has a fan rotor, a first compressor rotor and a second compressor rotor. The second compressor rotor compresses air to a higher pressure than the first compressor rotor. A first turbine rotor drives the second compressor rotor and a second turbine rotor. The second turbine drives the compressor rotor. A fan drive turbine is positioned downstream of the second turbine rotor. The fan drive turbine drives the fan through a gear reduction. The first compressor rotor and second turbine rotor rotate as an intermediate speed spool. The second compressor rotor and first turbine rotor together as a high speed spool, with the high speed spool rotating in an opposed direction to the intermediate speed spool. The fan drive turbine rotates in the same direction as the intermediate speed spool.
摘要翻译：燃气涡轮发动机具有风扇转子，第一压缩机转子和第二压缩机转子。第二压缩机转子将空气压缩到比第一压缩机转子更高的压力。第一涡轮转子驱动第二压缩机转子和第二涡轮转子。第二涡轮驱动压缩机转子。风扇驱动涡轮机位于第二涡轮转子的下游。风扇驱动涡轮驱动风扇通过齿轮减速。第一压缩机转子和第二涡轮机转子作为中间速度卷轴旋转。第二压缩机转子和第一涡轮机转子一起作为高速线轴，高速线轴与中间转速线轴相反地转动。风扇驱动涡轮机沿与中速卷轴相同的方向旋转。

82. 发明申请

US20130255219A1 GEARED TURBOFAN WITH THREE CO-ROTATING TURBINES 审中-公开
标题翻译：具有三个旋转涡轮的齿轮涡轮机
公开(公告)号：US20130255219A1
公开(公告)日：2013-10-03
申请号：US13437304
申请日：2012-04-02
申请人： Frederick M. Schwarz , Daniel Bernard Kupratis
发明人： Frederick M. Schwarz , Daniel Bernard Kupratis
IPC分类号： F02C3/13
CPC分类号： F02K3/075 , F02C3/107 , F02C7/36 , F02K3/06 , F05D2220/36 , F05D2260/40311
摘要： A gas turbine engine has a fan rotor, a first compressor rotor and a second compressor rotor. The second compressor rotor compresses air to a higher pressure than the first compressor rotor. A first turbine rotor drives the second compressor rotor and a second turbine rotor. The second turbine drives the compressor rotor. A fan drive turbine is positioned downstream of the second turbine rotor. The fan drive turbine drives the fan rotor through a gear reduction. The first compressor rotor and second turbine rotor rotate as an intermediate speed spool. The second compressor rotor and first turbine rotor together as a high speed spool. The high speed spool, the intermediate speed spool, and the fan drive turbine rotate in the same direction.
摘要翻译：燃气涡轮发动机具有风扇转子，第一压缩机转子和第二压缩机转子。第二压缩机转子将空气压缩到比第一压缩机转子更高的压力。第一涡轮转子驱动第二压缩机转子和第二涡轮转子。第二涡轮驱动压缩机转子。风扇驱动涡轮机位于第二涡轮转子的下游。风扇驱动涡轮通过齿轮减速器驱动风扇转子。第一压缩机转子和第二涡轮机转子作为中间速度卷轴旋转。第二压缩机转子和第一涡轮转子一起作为高速滑阀。高速卷轴，中速卷轴和风扇驱动涡轮机沿相同方向旋转。

83. 发明授权

US08534043B2 Air-oil heat exchanger 有权
标题翻译：空气 - 油热交换器
公开(公告)号：US08534043B2
公开(公告)日：2013-09-17
申请号：US13301100
申请日：2011-11-21
申请人： Frederick M. Schwarz , Frederick L. Elsaesser
发明人： Frederick M. Schwarz , Frederick L. Elsaesser
IPC分类号： F02K3/02
CPC分类号： F01D25/08 , F01D5/046 , F01D25/12 , F01D25/18 , F01D25/24 , F02C7/06 , F02C7/12 , F02C7/14 , F02C7/16 , F05D2260/20 , F05D2260/211 , F05D2260/232 , F28D2021/0026 , F28D2021/0049 , F28F9/0246 , F28F2280/10 , Y02T50/675
摘要： A heat exchange system for use in fluid operated equipment to provide air and working fluid heat exchanges to cool the working fluid in airstreams on a stream side of a wall. An actuator is mounted to be substantially located on a side of the wall opposite the stream side thereof having a positionable motion effector. A heat exchanger core having a plurality of passageway structures therein to enable providing the working fluid to, and removal therefrom. The heat exchanger core is mounted on the motion effector so as to be extendable and retractable thereby through the opening for selected distances into that region to be occupied by the airstreams.
摘要翻译：一种用于流体操作设备的热交换系统，用于提供空气和工作流体热交换，以在壁的流动侧的气流中冷却工作流体。致动器被安装成基本上位于与其具有可定位的运动执行器的其流侧相对的一侧上。一种热交换器芯，其中具有多个通道结构，以能够提供工作流体并从其中移除。热交换器芯安装在运动执行器上，从而可延伸和缩回，从而通过开口移动到要被空气流占据的区域中的选定距离。

84. 发明申请

US20130167555A1 ALUMINUM FAN BLADE CONSTRUCTION WITH WELDED COVER 有权
标题翻译：铝合金风扇叶片结构与焊接盖
公开(公告)号：US20130167555A1
公开(公告)日：2013-07-04
申请号：US13343025
申请日：2012-01-04
申请人： Frederick M. Schwarz , Michael A. Weisse
发明人： Frederick M. Schwarz , Michael A. Weisse
IPC分类号： F01D5/14 , B23K20/12 , B23K31/02 , F02C3/04 , F01D5/28
CPC分类号： B23K20/1265 , B23K2101/001 , F01D5/147 , F01D5/28 , F05D2220/36 , F05D2230/232 , F05D2300/121
摘要： An airfoil includes, among other possible things, a main body extending between a leading edge and a trailing edge. Channels are formed into the main body, with a plurality of ribs extending intermediate the channels. A cover skin is attached to the main body. The cover skin is welded to the main body at outer edges. An adhesive is placed between inner surfaces of the cover skin and the main body. The adhesive is deposited inwardly of the outer edges of the cover skin.
摘要翻译：除了其他可能的事情之外，翼型件还包括在前缘和后缘之间延伸的主体。通道形成在主体中，多个肋在通道之间延伸。覆盖皮肤附着在主体上。覆盖皮肤在外边缘焊接到主体。将粘合剂放置在覆盖皮肤和主体的内表面之间。粘合剂沉积在覆盖皮肤的外边缘的内侧。

85. 发明申请

US20130149099A1 GAS TURBINE ENGINE WITH FAN VARIABLE AREA NOZZLE TO REDUCE FAN INSTABILITY 审中-公开
标题翻译：具有风扇变化范围的喷气发动机减少风扇不稳定性
公开(公告)号：US20130149099A1
公开(公告)日：2013-06-13
申请号：US13340787
申请日：2011-12-30
申请人： Gregory A. Kohlenberg , Sean P. Zamora , Frederick M. Schwarz
发明人： Gregory A. Kohlenberg , Sean P. Zamora , Frederick M. Schwarz
IPC分类号： F01D17/00 , F01D15/12
CPC分类号： F02K1/15 , B64D33/04 , F01D17/105 , F01D17/14 , F01D25/24 , F02C3/04 , F02C7/36 , F02K1/30 , F02K1/72 , F02K3/02 , F05D2220/32 , F05D2220/36 , F05D2240/128 , F05D2240/35 , F05D2270/3015 , Y02T50/671
摘要： A nacelle assembly for a high-bypass gas turbine engine includes a fan variable area nozzle movable relative a fan nacelle to vary a fan nozzle exit area to reduce a fan instability.
摘要翻译：用于高旁路燃气涡轮发动机的机舱组件包括可相对于风扇机舱移动的风扇可变区域喷嘴，以改变风扇喷嘴出口区域以减少风扇不稳定性。

86. 发明申请

US20130145745A1 GAS TURBINE ENGINE WITH FAN VARIABLE AREA NOZZLE FOR LOW FAN PRESSURE RATIO 有权
公开(公告)号：US20130145745A1
公开(公告)日：2013-06-13
申请号：US13340810
申请日：2011-12-30
申请人： Gregory A. Kohlenberg , Sean P. Zamora , Frederick M. Schwarz
发明人： Gregory A. Kohlenberg , Sean P. Zamora , Frederick M. Schwarz
IPC分类号： F02K3/075
CPC分类号： F01D17/14 , B64D33/04 , F01D5/02 , F01D15/12 , F01D25/24 , F02C3/04 , F02C7/36 , F02C9/18 , F02C9/20 , F02K1/30 , F02K1/72 , F02K3/06 , F04D29/522 , F05D2220/32 , F05D2240/128 , F05D2270/3015
摘要： A gas turbine engine includes a fan section with twenty (20) or less fan blades and a fan pressure ratio less than about 1.45.

87. 发明申请

US20130094937A1 GAS TURBINE ENGINE OIL BUFFERING 有权
标题翻译：气体涡轮发动机油缓冲
公开(公告)号：US20130094937A1
公开(公告)日：2013-04-18
申请号：US13340871
申请日：2011-12-30
申请人： Jorn A. Glahn , Frederick M. Schwarz
发明人： Jorn A. Glahn , Frederick M. Schwarz
IPC分类号： F01D15/12
CPC分类号： F01D15/12 , F01D25/183 , F02C6/08 , F02C7/32 , Y02T50/671
摘要： A turbine engine includes a shaft, a fan, at least one bearing mounted on the shaft and rotationally supporting the fan, a fan drive gear system coupled to drive the fan, a bearing compartment around the at least one bearing and a source of pressurized air in communication with a region outside of the bearing compartment.
摘要翻译：涡轮发动机包括轴，风扇，安装在轴上的至少一个轴承和旋转地支撑风扇，联接以驱动风扇的风扇驱动齿轮系统，围绕至少一个轴承的轴承室和加压空气源与轴承室外部的区域连通。

88. 发明申请

US20120237335A1 GAS TURBINE ENGINE WITH GEARED ARCHITECTURE 有权
标题翻译：具有齿轮架构的气体涡轮发动机
公开(公告)号：US20120237335A1
公开(公告)日：2012-09-20
申请号：US13484722
申请日：2012-05-31
申请人： Michael E. McCune , Lawrence E. Portlock , Frederick M. Schwarz
发明人： Michael E. McCune , Lawrence E. Portlock , Frederick M. Schwarz
IPC分类号： F01D15/12
CPC分类号： F01D5/027 , F02C7/36 , F05D2220/323 , F05D2220/36 , F05D2240/70 , F05D2260/34 , F05D2260/4031 , F05D2260/40311
摘要： A geared architecture with a flex mount for a fan drive gear system.
摘要翻译：具有用于风扇驱动齿轮系统的柔性安装座的齿轮架构。

89. 发明申请

US20120237334A1 GAS TURBINE ENGINE GEAR TRAIN 有权
标题翻译：气体涡轮发动机齿轮火车
公开(公告)号：US20120237334A1
公开(公告)日：2012-09-20
申请号：US13340737
申请日：2011-12-30
申请人： Michael E. McCune , Lawrence E. Portlock , Frederick M. Schwarz
发明人： Michael E. McCune , Lawrence E. Portlock , Frederick M. Schwarz
IPC分类号： F01D15/12 , F16H57/08
CPC分类号： F02C7/36 , F01D5/027 , F02C3/107 , F02K3/06 , F05D2220/36 , F05D2240/70 , F05D2260/34 , F05D2260/4031 , F05D2260/40311 , F16H1/28 , F16H57/0423 , F16H57/0486 , F16H2057/085
摘要： An epicyclic gear train includes a carrier that supports star gears that mesh with a sun gear. A ring gear surrounds and meshes with the star gears. The star gears are supported on respective journal bearings. Each of the journal bearings includes a peripheral journal surface and each of the star gears includes a radially inner journal surface that is in contact with the peripheral journal surface of the respective journal bearing. The epicyclic gear train has a gear reduction ratio of greater than or equal to about 2.3
摘要翻译：行星齿轮系包括支撑与太阳齿轮啮合的星形齿轮的载体。环形齿轮围绕并与星形齿轮啮合。星形齿轮支撑在相应的轴颈轴承上。每个轴颈轴承包括周向轴颈表面，并且每个星形齿轮包括与相应的轴颈轴承的周向轴颈表面接触的径向内部轴颈表面。行星齿轮系具有大于或等于约2.3的齿轮减速比

90. 发明申请

US20120222398A1 GAS TURBINE ENGINE WITH GEARED ARCHITECTURE 审中-公开
标题翻译：具有齿轮架构的气体涡轮发动机
公开(公告)号：US20120222398A1
公开(公告)日：2012-09-06
申请号：US13346100
申请日：2012-01-09
申请人： Peter G. Smith , Stuart S. Ochs , Frederick M. Schwarz
发明人： Peter G. Smith , Stuart S. Ochs , Frederick M. Schwarz
IPC分类号： F02K3/04
CPC分类号： F01D17/162 , F04D29/563 , F05D2220/36
摘要： A turbofan engine includes a geared architecture and a fan variable area nozzle axially movable relative to a fan nacelle to vary a fan nozzle exit area and adjust a pressure ratio of the fan bypass airflow during engine operation.
摘要翻译：涡轮风扇发动机包括齿轮架构和相对于风扇机舱可轴向移动的风扇可变区喷嘴，以改变风扇喷嘴出口区域，并在发动机运行期间调节风扇旁路气流的压力比。

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