-
1.发明申请公开(公告)号：US20110297485A1
公开(公告)日：2011-12-08
申请号：US13213048
申请日：2011-08-18
IPC分类号： F16H57/04
CPC分类号： F01M11/067 , F01D25/18 , F02C7/36 , F05D2260/40311 , F16H57/0423 , F16H57/0443 , F16H57/045 , F16H57/0486 , F16N17/06
摘要： A lubrication system, includes an auxiliary lubricant tank 48 and a supply conduit 58 extending from a source of lubricant 26 and through the auxiliary lubricant tank. A portion of the conduit resides within the tank and has an opening 136 for allowing lubricant transfer between the tank and the conduit.
摘要翻译： 润滑系统包括辅助润滑剂罐48和从润滑剂源26延伸并通过辅助润滑剂罐的供应管道58。 导管的一部分位于罐内，并且具有开口136，用于允许罐与导管之间的润滑剂转移。
-
公开(公告)号：US08020665B2
公开(公告)日：2011-09-20
申请号：US11603393
申请日：2006-11-22
CPC分类号： F01M11/067 , F01D25/18 , F02C7/36 , F05D2260/40311 , F16H57/0423 , F16H57/0443 , F16H57/045 , F16H57/0486 , F16N17/06
摘要： A lubrication system, includes an auxiliary lubricant tank 48 and a supply conduit 58 extending from a source of lubricant 26 and through the auxiliary lubricant tank. A portion of the conduit resides within the tank and has an opening 136 for allowing lubricant transfer between the tank and the conduit.
摘要翻译： 润滑系统包括辅助润滑剂罐48和从润滑剂源26延伸并通过辅助润滑剂罐的供应管道58。 导管的一部分位于罐内，并且具有开口136，用于允许罐与导管之间的润滑剂转移。
-
公开(公告)号：US09995174B2
公开(公告)日：2018-06-12
申请号：US13428491
申请日：2012-03-23
CPC分类号： F01N3/208 , F01D25/16 , F01D25/18 , F01N3/2066 , F01N11/00 , F01N2610/01 , F01N2610/02 , F01N2610/1406 , F01N2610/142 , F01N2610/148 , F01N2900/1814 , F02C3/10 , F02C7/06 , F02C7/10 , F02C7/36 , F02K3/06 , F05D2260/40311 , F16N7/34 , Y02T10/24 , Y02T50/671 , Y10T29/4932 , Y10T137/0324 , Y10T137/7297
摘要： A gas turbine engine has a fan, first and second compressor stages, first and second turbine stages. The first turbine stage drives the second compressor stage as a high spool. The second turbine stage drives the first compressor stage as part of a low spool. A gear train drives the fan with the low spool, such that the fan and first compressor stage rotate in the same direction. The high spool operates at higher pressures than the low spool. A lubrication system is also disclosed.
-
公开(公告)号：US08484942B1
公开(公告)日：2013-07-16
申请号：US13483657
申请日：2012-05-30
CPC分类号： F01D25/18 , F02C3/107 , F02K3/06 , F16H57/0471 , F16H57/0479 , F16H57/0486 , Y02T50/671
摘要： A gas turbine engine has a fan, first and second compressor stages, first and second turbine stages. The first turbine stage drives the second compressor stage as a high spool. The second turbine stage drives the first compressor stage as part of a low spool. A gear train drives the fan with the low spool, such that the fan and first compressor stage rotate in the same direction. The high spool operates at higher pressures than the low spool. A lubrication system is also disclosed.
摘要翻译： 燃气涡轮发动机具有风扇，第一和第二压缩机级，第一和第二涡轮级。 第一涡轮级将第二压缩机级驱动为高阀芯。 第二涡轮级驱动第一压缩机级作为低阀芯的一部分。 齿轮系用低阀芯驱动风扇，使得风扇和第一压缩机级沿相同的方向旋转。 高阀芯在比低阀芯更高的压力下运行。 还公开了润滑系统。
-
公开(公告)号：US20120192570A1
公开(公告)日：2012-08-02
申请号：US13428491
申请日：2012-03-23
IPC分类号： F02C3/10
CPC分类号： F01N3/208 , F01D25/16 , F01D25/18 , F01N3/2066 , F01N11/00 , F01N2610/01 , F01N2610/02 , F01N2610/1406 , F01N2610/142 , F01N2610/148 , F01N2900/1814 , F02C3/10 , F02C7/06 , F02C7/10 , F02C7/36 , F02K3/06 , F05D2260/40311 , F16N7/34 , Y02T10/24 , Y02T50/671 , Y10T29/4932 , Y10T137/0324 , Y10T137/7297
摘要： A gas turbine engine has a fan, first and second compressor stages, first and second turbine stages. The first turbine stage drives the second compressor stage as a high spool. The second turbine stage drives the first compressor stage as part of a low spool. A gear train drives the fan with the low spool, such that the fan and first compressor stage rotate in the same direction. The high spool operates at higher pressures than the low spool. A lubrication system is also disclosed.
摘要翻译： 燃气涡轮发动机具有风扇，第一和第二压缩机级，第一和第二涡轮级。 第一涡轮级将第二压缩机级驱动为高阀芯。 第二涡轮级驱动第一压缩机级作为低阀芯的一部分。 齿轮系用低阀芯驱动风扇，使得风扇和第一压缩机级沿相同的方向旋转。 高阀芯在比低阀芯更高的压力下运行。 还公开了润滑系统。
-
公开(公告)号：US20180347428A1
公开(公告)日：2018-12-06
申请号：US16006327
申请日：2018-06-12
IPC分类号： F01N3/20 , F02C7/10 , F02C7/36 , F01D25/16 , F01D25/18 , F02C7/06 , F01N11/00 , F02K3/06 , F02C3/10 , F16N7/34
CPC分类号： F01N3/208 , F01D25/16 , F01D25/18 , F01N3/2066 , F01N11/00 , F01N2610/01 , F01N2610/02 , F01N2610/1406 , F01N2610/142 , F01N2610/148 , F01N2900/1814 , F02C3/10 , F02C7/06 , F02C7/10 , F02C7/36 , F02K3/06 , F05D2260/40311 , F16N7/34 , Y02T10/24 , Y02T50/671 , Y10T29/4932 , Y10T137/0324 , Y10T137/7297
摘要： In an embodiment of the present disclosure, a gas turbine engine includes a fan, a first compressor stage and a second compressor stage, a first turbine stage and a second turbine stage, and wherein said first turbine stage drives said second compressor stage as a high spool, and wherein said second turbine stage drives said first compressor stage as part of a low spool, and a gear train driving said fan with said low spool, and such that said fan and said first compressor stage rotate in the same direction, and wherein said high spool operates at higher pressures than said low spool.
-
公开(公告)号：US08511435B2
公开(公告)日：2013-08-20
申请号：US13213048
申请日：2011-08-18
CPC分类号： F01M11/067 , F01D25/18 , F02C7/36 , F05D2260/40311 , F16H57/0423 , F16H57/0443 , F16H57/045 , F16H57/0486 , F16N17/06
摘要： A lubrication system, includes an auxiliary lubricant tank 48 and a supply conduit 58 extending from a source of lubricant 26 and through the auxiliary lubricant tank. A portion of the conduit resides within the tank and has an opening 136 for allowing lubricant transfer between the tank and the conduit.
摘要翻译： 润滑系统包括辅助润滑剂罐48和从润滑剂源26延伸并通过辅助润滑剂罐的供应管道58。 导管的一部分位于罐内，并且具有开口136，用于允许罐与导管之间的润滑剂转移。
-
公开(公告)号：US20080116009A1
公开(公告)日：2008-05-22
申请号：US11603393
申请日：2006-11-22
CPC分类号： F01M11/067 , F01D25/18 , F02C7/36 , F05D2260/40311 , F16H57/0423 , F16H57/0443 , F16H57/045 , F16H57/0486 , F16N17/06
摘要： A lubrication system, includes an auxiliary lubricant tank 48 and a supply conduit 58 extending from a source of lubricant 26 and through the auxiliary lubricant tank. A portion of the conduit resides within the tank and has an opening 136 for allowing lubricant transfer between the tank and the conduit.
摘要翻译： 润滑系统包括辅助润滑剂罐48和从润滑剂源26延伸并通过辅助润滑剂罐的供应管道58。 导管的一部分位于罐内，并且具有开口136，用于允许罐与导管之间的润滑剂转移。
-
公开(公告)号：US08267826B2
公开(公告)日：2012-09-18
申请号：US11080175
申请日：2005-03-15
CPC分类号： F16H57/042 , F16H57/045 , F16H57/0471 , F16H57/0479 , F16H57/0482 , F16H57/082
摘要： A planetary carrier includes a journal bearing for supporting a planetary gear. The journal bearing receives lubricant to produce a lubricant film to support gear loads. A torque frame is attached to the carrier housing to transmit torque and to prevent twisting of the carrier housing. The torque frame includes several lubricant communication passages to provide lubricant to each of the separate journal bearings. Each of the lubricant communication passages includes an accumulator for storing lubricant during normal operation. The accumulator stores a desired amount of lubricant to provide lubricant to the adjacent journal bearing for the interim period between primary system stoppage and reestablishment of lubricant flow by a secondary system.
摘要翻译： 行星架包括用于支撑行星齿轮的轴颈轴承。 轴颈轴承接收润滑剂以产生润滑剂膜以支撑齿轮负载。 扭矩框架附接到承载壳体以传递扭矩并且防止承载壳体的扭转。 扭矩框架包括若干润滑剂连通通道，以向每个单独的轴颈轴承提供润滑剂。 每个润滑剂连通通道包括用于在正常操作期间储存润滑剂的储液器。 蓄能器存储所需量的润滑剂，以在主系统停止和辅助系统重新建立润滑剂流动之间的临时期间向邻近的轴颈轴承提供润滑剂。
-
公开(公告)号：US20120189430A1
公开(公告)日：2012-07-26
申请号：US13437442
申请日：2012-04-02
CPC分类号： F16H57/0424 , F01D5/027 , F01D25/18 , F02C7/28 , F02C7/36 , F05D2240/55 , F05D2240/70 , F05D2260/34 , F05D2260/40311 , F05D2260/98 , F16D1/076 , F16H1/28 , F16H57/0402 , F16H57/042 , F16H57/0421 , F16H57/043 , F16H57/0458 , F16H57/0482 , F16H57/0486 , F16H57/08 , Y10T29/49462
摘要： A turbine engine includes an input shaft and a fan shaft rotatable about an axis. The fan shaft supports fan blades. An epicyclic gear train is connected between the input shaft and the fan shaft. The epicyclic gear train includes a plurality of star gears, a carrier supporting the plurality of star gears, a sun gear that meshes with the plurality of star gears and a ring gear surrounding and meshing with the plurality of star gears such that the sun gear is rotatable in a first direction and the ring gear is rotatable in a second, opposite direction. The ring gear includes first and second portions that each have an inner periphery with teeth. The first and second portions include respective recesses facing one another to provide an internal annular cavity.
摘要翻译： 涡轮发动机包括输入轴和可绕轴线旋转的风扇轴。 风扇轴支持风扇叶片。 行星齿轮系连接在输入轴和风扇轴之间。 行星齿轮系包括多个星形齿轮，支撑多个星形齿轮的载体，与多个星形齿轮啮合的太阳齿轮和围绕并与多个星形齿轮啮合的齿圈，使得太阳轮是 可沿第一方向旋转，并且所述环形齿轮可沿第二相反方向旋转。 齿圈包括第一和第二部分，每个部分具有带齿的内周边。 第一和第二部分包括彼此面对的相应的凹部以提供内部环形空腔。
-
-
-
-
-
-
-
-
-
搜索结果
112 条记录 (耗时 0.024 秒)
