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公开(公告)号：EP3199840A1
公开(公告)日：2017-08-02
申请号：EP17152876.3
申请日：2017-01-24
发明人： NIERGARTH, Daniel Alan , MILLER, Brandon Wayne , ERTAS, Bugra Han , BRADLEY, Donald Albert , DICKMAN, Joseph Robert
CPC分类号： F16H57/0006 , F02C7/36 , F05D2260/40311 , F05D2260/96 , F16C19/28 , F16H1/28 , F16H57/0471 , F16H57/082 , F16H2057/0012
摘要： An epicyclic gearing arrangement includes a planet gear 84 rotatable on a planet bearing that is mounted via a support pin 96 to a carrier 90, 92, 94 of the epicyclic gearing arrangement. A spring film damper 101 is disposed between the outer surface of the bearing's outer ring and the opposing inner surface of the planet gear and includes an annular gap. The support pin and/or outer ring include oil feed holes that open into the respective annular gap(s).
摘要翻译： 行星齿轮装置包括可在行星轴承上旋转的行星齿轮84，行星齿轮84经由支撑销96安装到行星齿轮装置的行星架90,92,94。 弹簧薄膜阻尼器101设置在轴承外圈的外表面和行星齿轮的相对内表面之间并且包括环形间隙。 支撑销和/或外环包括通向相应的环形间隙的供油孔。
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公开(公告)号：EP3199768A1
公开(公告)日：2017-08-02
申请号：EP17153200.5
申请日：2017-01-26
发明人： NIERGARTH, Daniel Alan , MILLER, Brandon Wayne , ERTAS, Bugra Han , BRADLEY, Donald Albert , DICKMAN, Joseph Robert
IPC分类号： F01D25/16 , F02K3/06 , F02C7/36 , F16H1/28 , F16H57/028
摘要： An epicyclic gearing arrangement includes a planet gear (842) rotatable on a planet bearing that is mounted via a support pin (96) to a carrier (90, 92, 94) of the epicyclic gearing arrangement. An attenuation spring is disposed between the outer surface (843) of the bearing's outer ring (841) and the opposing inner surface (844) of the planet gear (842) and includes an annular gap. A spring film damper is disposed between the cylindrical outer surface (105) of the support pin (96) and the opposing inner surface of the inner ring (102) of the planet bearing and includes an annular gap. The support pin (96) and/or outer ring (842) include oil feed holes (961, 82) that open into the respective annular gap(s). A gas turbine engine (10) includes an epicyclic gearing arrangement having such a planet bearing.
摘要翻译： 行星齿轮装置包括可在行星轴承上旋转的行星齿轮（842），该行星齿轮经由支撑销（96）安装到行星齿轮装置的行星架（90,92,94）上。 衰减弹簧布置在轴承外圈（841）的外表面（843）和行星齿轮（842）的相对内表面（844）之间并且包括环形间隙。 弹簧薄膜阻尼器设置在支撑销（96）的圆柱形外表面（105）和行星轴承的内环（102）的相对内表面之间并且包括环形间隙。 支撑销（96）和/或外环（842）包括通向相应的环形间隙的供油孔（961,82）。 燃气涡轮发动机（10）包括具有这种行星轴承的行星齿轮装置。
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3.发明公开PLANET GEARBOX WITH CYLINDRICAL ROLLER BEARING WITH HIGH DENSITY ROLLER PACKING 审中-公开PLANETEN-GETRIEBE MIT ZYLINDERROLLENLAGER MIT HOHER ROLLENDICHTE
公开(公告)号：EP3147482A1
公开(公告)日：2017-03-29
申请号：EP16190098.0
申请日：2016-09-22
IPC分类号： F02C7/36 , F16C43/06 , F16H57/025
CPC分类号： F01D25/16 , F01D5/06 , F01D15/12 , F02C7/36 , F04D29/321 , F04D29/325 , F05D2220/32 , F05D2240/50 , F05D2260/40311 , F05D2300/20 , F16C19/28 , F16C33/34 , F16C33/485 , F16C2206/40 , F16C2240/46 , F16C2240/60 , F16C2360/23 , F16C2361/65 , F16H1/28 , F16H57/08 , F16H2057/085 , Y02T50/671
摘要： A planet gearbox is provided for connection to a carrier of an epicyclic gearing arrangement with a single input and single output and including a sun gear 80, a ring gear 86 and at least one double helix planet gear rotatable on a cylindrical roller bearing with a cage 118 having a cross-web thickness of 15% to 25% of the diameter of the cylindrical rollers 104 and an L/D ratio exceeding 1.0. A gas turbine engine 10 includes a fan 38 and LP shaft 36, which couples a compressor 22 to a turbine 30. An epicyclic gearing arrangement has a single input from the LP shaft coupled to a sun gear 80, a single output coupled to the fan's shaft, and a planet bearing cage 118 having a cross-web thickness measuring 15% to 25% of the roller's diameter.
摘要翻译： 行星齿轮箱被提供用于连接到具有单个输入和单个输出的行星齿轮传动装置的载体，并且包括太阳齿轮80，齿圈86和至少一个双螺旋行星齿轮，其可旋转在具有保持架的圆柱滚子轴承 118，横板厚度为圆筒形辊104的直径的15％至25％，L / D比超过1.0。 燃气涡轮发动机10包括风扇38和LP轴36，其将压缩机22联接到涡轮机30.行星齿轮传动装置具有联接到太阳齿轮80的LP轴的单个输入，与风扇 轴和行星轴承保持架118，其具有测量辊直径的15％至25％的横向卷材厚度。
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公开(公告)号：EP3095974B1
公开(公告)日：2020-04-08
申请号：EP16170161.0
申请日：2016-05-18
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公开(公告)号：EP3159578B1
公开(公告)日：2020-02-19
申请号：EP16193771.9
申请日：2016-10-13
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公开(公告)号：EP3165739B1
公开(公告)日：2018-09-19
申请号：EP16196830.0
申请日：2016-11-02
CPC分类号： F16H57/0006 , F02C3/107 , F02C7/36 , F02K3/06 , F05D2260/40311 , F05D2260/96 , F16H1/28 , F16H57/082
摘要： A planet gear train 200 for an engine casing 226 includes a sun gear 204 rotatable by a shaft 202, a ring gear 208, a plurality of planet gears 206 rotatably mounted in a planet carrier 210 and meshing with the sun gear 204 and the ring gear 208, and a damping system. The damping system includes a soft mount 212 disposed about the shaft 202 and coupling the planet carrier 210 the engine casing 226. The soft mount 212 includes a flexible inner sleeve 214 and a flexible outer sleeve 216. The flexible inner sleeve 214 and the flexible outer sleeve 216 are fixedly coupled together at respective central portions thereof near the shaft 202. The damping system further includes a plurality of damping couplers 218 disposed about an outer flange 232 of the planet carrier 210. The plurality of damping couplers is configured to flexibly couple the flexible inner sleeve 214 to the flexible outer sleeve 216.
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公开(公告)号：EP2949870B1
公开(公告)日：2017-10-18
申请号：EP15168754.8
申请日：2015-05-21
CPC分类号： F01D7/02 , F01D5/02 , F01D21/08 , F02C3/04 , F05D2220/32 , F05D2220/36 , F05D2240/30 , F05D2260/53 , F05D2260/77 , F05D2260/79 , F05D2270/021 , F05D2270/09 , F05D2270/58 , Y02T50/673
摘要： A pitch control mechanism (100, 200, 300, 400, 500, 600) includes: a rotor structure configured for rotation about a longitudinal axis; a row of blades (28) carried by the rotor structure, each blade having an airfoil and a trunnion (120) mounted for pivoting movement relative to the rotor structure, about a trunnion axis which is perpendicular to the longitudinal axis; a unison ring (108, 208, 308, 408, 508, 608) interconnecting the blades (28); an actuator (106, 206, 306, 406, 506, 606) connected to the unison ring (108, 208, 308, 408, 508, 608) and the rotor structure, operable to move the unison ring (108, 208, 308, 408, 508, 608) relative to the rotor structure; at least one moveable counterweight (138, 238, 338, 438, 538, 638) carried by the rotor structure, remote from the blades (28); and an interconnection between the blades (28) and the counterweight, such that movement of the counterweight (138, 238, 338, 438, 538, 638) causes a change in the pitch angle of the blades (28).
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8.发明公开MULTI-DIRECTIONAL GEARBOX DEFLECTION LIMITER FOR A GAS TURBINE ENGINE 审中-公开多功能食品加拿大瑞士啤酒酿酒师FÜREINEN GASTURBINENMOTOR
公开(公告)号：EP3144498A1
公开(公告)日：2017-03-22
申请号：EP16188622.1
申请日：2016-09-13
IPC分类号： F02C3/107 , F02C7/36 , F02C7/20 , F01D25/04 , F16H57/028
CPC分类号： F02C7/36 , F01D25/04 , F01D25/28 , F02C3/04 , F02C3/107 , F02C7/20 , F05D2240/91 , F05D2250/43 , F05D2260/30 , F05D2260/40311 , F05D2260/96 , F05D2300/501 , F16H1/28 , F16H57/0006 , F16H57/028
摘要： A gas turbine engine including a fan 38, a core 16 including at least one rotatable shaft, and a gearbox 100 mechanically coupling at least one rotatable shaft of the core to the fan is provided. The gas turbine engine also includes a coupling system 132 for mounting the gearbox within the gas turbine engine. The coupling system includes a flexible coupling 152 connected to at least one of a fan frame 144 or a core frame 134, as well as a torque frame connected to the flexible coupling and the gearbox. Moreover, a deflection limiter 174 is provided, loosely attaching the flexible coupling to the gearbox to provide a predetermined axial range of motion, radial range of motion, and circumferential range of motion between the gearbox and the frame to which the flexible coupling is attached.
摘要翻译： 提供一种燃气涡轮发动机，其包括风扇38，包括至少一个可旋转轴的铁心16和将机芯的至少一个可旋转轴机械连接到风扇的齿轮箱100。 燃气涡轮发动机还包括用于将齿轮箱安装在燃气涡轮发动机内的联接系统132。 联接系统包括连接到风扇框架144或芯框架134中的至少一个的柔性联接器152以及连接到柔性联轴器和变速箱的扭矩框架。 此外，提供了一个偏转限制器174，其将柔性联接器松散地附接到齿轮箱，以提供预定的轴向运动范围，径向运动范围以及齿轮箱与柔性联轴器所附接的框架之间的周向运动范围。
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公开(公告)号：EP3144498B1
公开(公告)日：2018-12-12
申请号：EP16188622.1
申请日：2016-09-13
IPC分类号： F02C3/107 , F02C7/36 , F02C7/20 , F01D25/04 , F16H57/028
CPC分类号： F02C7/36 , F01D25/04 , F01D25/28 , F02C3/04 , F02C3/107 , F02C7/20 , F05D2240/91 , F05D2250/43 , F05D2260/30 , F05D2260/40311 , F05D2260/96 , F05D2300/501 , F16H1/28 , F16H57/0006 , F16H57/028
摘要： A gas turbine engine including a fan 38, a core 16 including at least one rotatable shaft, and a gearbox 100 mechanically coupling at least one rotatable shaft of the core to the fan is provided. The gas turbine engine also includes a coupling system 132 for mounting the gearbox within the gas turbine engine. The coupling system includes a flexible coupling 152 connected to at least one of a fan frame 144 or a core frame 134, as well as a torque frame connected to the flexible coupling and the gearbox. Moreover, a deflection limiter 174 is provided, loosely attaching the flexible coupling to the gearbox to provide a predetermined axial range of motion, radial range of motion, and circumferential range of motion between the gearbox and the frame to which the flexible coupling is attached.
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公开(公告)号：EP3199839A1
公开(公告)日：2017-08-02
申请号：EP17152870.6
申请日：2017-01-24
发明人： NIERGARTH, Daniel Alan , MILLER, Brandon Wayne , ERTAS, Bugra Han , BRADLEY, Donald Albert , DICKMAN, Joseph Robert
摘要： An epicyclic gearing arrangement includes a planet gear (84, 841, 842) rotatable on a planet bearing that is mounted via a support pin (96) to a carrier (90, 92, 94) of the epicyclic gearing arrangement. A spring film damper is disposed between the cylindrical outer surface (105) of the support pin (96) and the opposing inner surface of the inner ring (102) of the planet bearing and includes a radial gap. The support pin (96) includes oil feed holes 961 that open into the respective radial gap. A gas turbine engine (10) includes an epicyclic gearing arrangement having such a planet bearing.
摘要翻译： 行星齿轮装置包括行星齿轮（84,841,842），所述行星齿轮在行星轴承上可旋转，所述行星齿轮经由支撑销（96）安装到所述行星齿轮装置的行星架（90,92,94）上。 弹簧薄膜阻尼器设置在支撑销（96）的圆柱形外表面（105）和行星轴承的内环（102）的相对内表面之间并且包括径向间隙。 支撑销（96）包括通向相应径向间隙的供油孔961。 燃气涡轮发动机（10）包括具有这种行星轴承的行星齿轮装置。
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