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公开(公告)号:US09470302B1
公开(公告)日:2016-10-18
申请号:US14678307
申请日:2015-04-03
Applicant: Hamilton Sundstrand Corporation
Inventor: Glenn C. Lemmers, Jr. , Aaron M. Finke , Doren C. Smith , Andrew P. Grosskopf , David S. Behling
Abstract: Embodiments herein relate to piece-part, sub-assembly, assembly, and component levels of a differential composed of a sun gear configuration and utilized in an integrated drive generator. An integrated drive generator is a hydro-mechanical transmission that drives a synchronous salient pole generator. The integrated drive generator is a constant speed output, variable speed input transmission that includes the differential and a hydraulic unit. In general, the integrated drive generator utilizes the variable speed input from an accessory gear box of an engine to drive or control a hydraulic unit, which in turn drives or controls a churn leg member of the differential. As the differential is driven, speeds of each speed member of the differential are then summed to generate the constant speed output to drive the synchronous salient pole generator.
Abstract translation: 本文的实施例涉及由太阳齿轮构造并用于集成驱动发电机的差速器的零件,子组件,组件和部件水平。 集成驱动发电机是驱动同步凸极发电机的水力机械变速器。 集成驱动发电机是恒速输出,变速输入变速器,包括差速器和液压单元。 通常,集成驱动发电机利用来自发动机的附件齿轮箱的可变速度输入来驱动或控制液压单元,液压单元又驱动或控制差速器的流道支腿构件。 当差速器被驱动时,差速器的每个速度部件的速度被相加以产生恒速输出以驱动同步凸极发生器。
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公开(公告)号:US20160290467A1
公开(公告)日:2016-10-06
申请号:US14677631
申请日:2015-04-02
Applicant: Hamilton Sundstrand Corporation
Inventor: Glenn C. Lemmers, JR. , Aaron M. Finke , Doren C. Smith , Andrew P. Grosskopf , David S. Behling
Abstract: A planet gear for an integrated drive generator (IDG) includes a planet gear body having an outer diametric surface provided with 15 gear teeth.
Abstract translation: 用于集成驱动发电机(IDG)的行星齿轮包括具有设置有15个齿轮齿的外径表面的行星齿轮体。
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公开(公告)号:US20230324002A1
公开(公告)日:2023-10-12
申请号:US17717458
申请日:2022-04-11
Applicant: Hamilton Sundstrand Corporation
Inventor: Dhaval S. Patel , Aaron M. Finke , Glenn C. Lemmers, JR. , Andreas C. Koenig
CPC classification number: F01D25/20 , F01D15/10 , F05D2220/768 , F05D2270/708 , F05D2260/98 , F05D2270/02 , F05D2260/60
Abstract: An aircraft oil management system includes a generator, pump, and pump control system. The generator is mechanically coupled to a prime mover via a the rotor shaft and is configured to output three-phase power. The pump is mechanically decoupled from the rotor shaft and delivers oil to the generator. The pump control system drives the pump independent of a rotational speed of the rotor shaft.
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公开(公告)号:US20230184306A1
公开(公告)日:2023-06-15
申请号:US18103308
申请日:2023-01-30
Applicant: Hamilton Sundstrand Corporation
Inventor: Aaron M. Finke , Andreas C. Koenig , Tyler W. Hayes , Mustansir H. Kheraluwala
CPC classification number: F16D67/02 , F16D13/40 , F16D23/12 , F16D2500/10406 , F16D2125/36
Abstract: A disconnect mechanism comprises an input shaft defining a drive axis, a disconnect shaft selectively engaged with the input shaft to be driven about the drive axis by the input shaft, and a disconnect ramp operatively connected to the disconnect shaft to axially move the disconnect shaft between at least a first axial position and a second axial position. A disconnect pawl is selectively engaged with the disconnect ramp shaft, and a brake is selectively engaged with the disconnect shaft in the second axial position.
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公开(公告)号:US11598384B2
公开(公告)日:2023-03-07
申请号:US17393349
申请日:2021-08-03
Applicant: Hamilton Sundstrand Corporation
Inventor: Aaron M. Finke , Andreas C. Koenig , Tyler W. Hayes , Mustansir Kheraluwala
IPC: F16D13/40 , F16D67/02 , F16D23/12 , F16D125/36
Abstract: A disconnect mechanism comprises an input shaft defining a drive axis, a disconnect shaft selectively engaged with the input shaft to be driven about the drive axis by the input shaft, and a disconnect ramp operatively connected to the disconnect shaft to axially move the disconnect shaft between at least a first axial position and a second axial position. A disconnect pawl is selectively engaged with the disconnect ramp shaft, and a brake is selectively engaged with the disconnect shaft in the second axial position.
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公开(公告)号:US11226026B2
公开(公告)日:2022-01-18
申请号:US16387961
申请日:2019-04-18
Applicant: Hamilton Sundstrand Corporation
Inventor: Stephen Michael Bortoli , Aaron M. Finke , Mark J. Franklin , Glenn C. Lemmers, Jr.
Abstract: A multispeed turbomachine transmission can include an input shaft and a plurality of input shaft gears disposed on the input shaft. The transmission can include one or more clutch shafts, one or more clutch shaft input gears disposed on the one or more clutch shafts, each meshed with at least one of the plurality of input shaft gears, at least one clutch shaft output gear mounted to each clutch shaft, a clutch connected to each clutch shaft and configured to selectively connect the one or more clutch shaft input gears to the at least one clutch shaft output gear. The transmission can include an output shaft and at least one output shaft gear connected to the output shaft and meshed with the at least one clutch shaft output gear.
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公开(公告)号:US11226014B2
公开(公告)日:2022-01-18
申请号:US16388254
申请日:2019-04-18
Applicant: Hamilton Sundstrand Corporation
Inventor: Stephen Michael Bortoli , Aaron M. Finke , Mark J. Franklin
Abstract: A hydraulic clutch assembly can include a shaft defining a shaft channel, one or more hydraulic ports defined through the shaft, and one or more lubrication holes defined through the shaft. A porting manifold can be disposed at least partially within the shaft channel. The porting manifold can include a control pressure path in fluid communication with the one or more hydraulic ports and a lubrication flow path in fluid communication with the one or more lubrication holes. The control pressure path and the lubrication path can be fluidly isolated in the porting manifold.
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公开(公告)号:US11118514B2
公开(公告)日:2021-09-14
申请号:US16536960
申请日:2019-08-09
Applicant: Hamilton Sundstrand Corporation
Inventor: Aaron M. Finke , Stephen Michael Bortoli , Jonathan C. Dell
Abstract: A turbomachine dual spool transmission system can include a transmission assembly configured to connect to a combination output of a dual spool differential at a transmission input to be driven by the combination output to turn a transmission output. The transmission assembly can be configured to provide a first output gear ratio in a first state and a second output gear ratio in a second state. The system can include the dual spool differential. The dual spool differential can include a gear assembly configured to combine a low pressure spool input and a high pressure spool input into a combination output to provide an output speed range smaller than a low pressure speed range alone.
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公开(公告)号:US20210040895A1
公开(公告)日:2021-02-11
申请号:US16536974
申请日:2019-08-09
Applicant: Hamilton Sundstrand Corporation
Inventor: Aaron M. Finke , Stephen Michael Bortoli , Jonathan C. Dell
Abstract: A turbomachine dual spool differential can include a gear assembly configured to combine a low pressure spool input and a high pressure spool input into a combination output to provide an output speed range smaller than a low pressure spool speed range alone. The gear assembly can include a ring gear, a sun gear, and a plurality of planetary gears disposed between the sun gear and the ring gear and meshed with the sun gear and the ring gear. The planetary gears can be rotationally connected to a carrier.
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公开(公告)号:US20210040893A1
公开(公告)日:2021-02-11
申请号:US16536938
申请日:2019-08-09
Applicant: Hamilton Sundstrand Corporation
Inventor: Aaron M. Finke , Stephen Michael Bortoli , Jonathan C. Dell
Abstract: A turbomachine dual spool transmission system can include a direct drive assembly configured to selectively allow bypassing of a dual spool differential combination output to allow selective direct engagement of a low pressure spool to directly drive a rotational member or to be directly driven by the rotational member. The system can include the dual spool differential. The dual spool differential can include a gear assembly configured to combine a low pressure spool input and a high pressure spool input into a combination output to provide an output speed range smaller than a low pressure speed range alone.
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