COUPLED PLANETARY GEARBOX
    11.
    发明申请

    公开(公告)号:US20200292074A1

    公开(公告)日:2020-09-17

    申请号:US16353444

    申请日:2019-03-14

    Abstract: Disclosed is a transmission having: an input shaft configured to rotationally communicate with a gas turbine engine; an output shaft configured to rotationally communicate with an aircraft accessory; and a gear system connected between the input shaft and the output shaft, the gear system including: a plurality of clutches that are axially aligned and radially offset, the plurality of clutches configured to engage in parallel the output shaft and shift the transmission to generate a plurality gear speeds; and a plurality of pistons that are configured to engage the respective plurality of clutches, the plurality of pistons being hydraulically controlled and adapted to receive fluid from a respective plurality of ports in the output shaft.

    Input driven gear for a differential

    公开(公告)号:US10024413B2

    公开(公告)日:2018-07-17

    申请号:US14678259

    申请日:2015-04-03

    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.

    Disconnect shaft for an integrated drive generator (IDG)

    公开(公告)号:US09732804B2

    公开(公告)日:2017-08-15

    申请号:US14685957

    申请日:2015-04-14

    CPC classification number: F16D11/14 F16C3/02 F16D1/02 F16D2011/008

    Abstract: A disconnect shaft of an integrated drive generator is provided including a body configured to rotate about an axis of rotation. The body has a first end, a second opposite end, and a plurality of teeth formed adjacent the first end and configured to engage a complementary portion of an adjacent component. A relief is formed in the body such that a first portion is defined between the relief and the plurality of teeth. The first portion includes a plurality of threads having at least one of a major diameter between about 1.3044 and about 1.3125 inches (3.313-3.334 centimeters), a minor diameter between about 1.2482 and about 1.2547 inches (3.170-3.187 centimeters), a pitch diameter between about 1.2765 and about 1.2800 inches (3.242-3.251 centimeters), and a root radius between about 0.0075 and 0.0090 inches (0.0190-0.0029 centimeters).

    DISCONNECT SHAFT FOR AN INTEGRATED DRIVE GENERATOR (IDG)
    14.
    发明申请
    DISCONNECT SHAFT FOR AN INTEGRATED DRIVE GENERATOR (IDG) 有权
    用于集成驱动发电机(IDG)的断开轴

    公开(公告)号:US20160305491A1

    公开(公告)日:2016-10-20

    申请号:US14685957

    申请日:2015-04-14

    CPC classification number: F16D11/14 F16C3/02 F16D1/02 F16D2011/008

    Abstract: A disconnect shaft of an integrated drive generator is provided including a body configured to rotate about an axis of rotation. The body has a first end, a second opposite end, and a plurality of teeth formed adjacent the first end and configured to engage a complementary portion of an adjacent component. A relief is formed in the body such that a first portion is defined between the relief and the plurality of teeth. The first portion includes a plurality of threads having at least one of a major diameter between about 1.3044 and about 1.3125 inches (3.313-3.334 centimeters), a minor diameter between about 1.2482 and about 1.2547 inches (3.170-3.187 centimeters), a pitch diameter between about 1.2765 and about 1.2800 inches (3.242-3.251 centimeters), and a root radius between about 0.0075 and 0.0090 inches (0.0190-0.0029 centimeters).

    Abstract translation: 提供集成驱动发生器的断开轴,包括构造成围绕旋转轴线旋转的主体。 主体具有第一端部,第二相对端部以及与第一端部相邻形成并且被配置为接合相邻部件的互补部分的多个齿部。 在本体中形成浮雕,使得第一部分被限定在浮雕和多个齿之间。 第一部分包括多个螺纹,其具有大直径在大约1.3044和大约1.3125英寸(3.313-3.334厘米)之间,小直径在大约1.2482和大约1.2547英寸(3.170-3.187厘米)之间的至少一个,螺距直径 约1.2765至约1.2800英寸(3.242-3.251厘米),根部半径在约0.0075至0.0090英寸(0.0190-0.0029厘米)之间。

    Turbomachine dual spool transmission systems

    公开(公告)号:US11713720B2

    公开(公告)日:2023-08-01

    申请号:US17473530

    申请日:2021-09-13

    CPC classification number: F02C7/32 F05D2260/4023 F05D2260/40311

    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.

    DUAL DRIVE, DUAL CLUTCH DRIVE SYSTEM FOR AN AIRCRAFT ACCESSORY

    公开(公告)号:US20220348347A1

    公开(公告)日:2022-11-03

    申请号:US17377551

    申请日:2021-07-16

    Abstract: A dual drive, dual clutch accessory drive system for an aircraft including a first input shaft connected to a first pressure spool of a turbine engine. The first input shaft rotates at a first speed. A second input shaft is connected to a second spool of the turbine engine that is distinct from the first spool. The second input shaft rotates at a second speed. An output shaft operatively connected to an aircraft accessory. A first drive path selectively operatively connects the first input shaft with the output shaft. The first drive path includes a first clutch. The first drive path being operable to rotate the output shaft at the first speed. A second drive path operatively connects the second input shaft with the output shaft. The second drive path includes a second clutch. The second drive path is operable to rotate the output shaft at the second speed.

    Turbomachine dual spool transmission systems

    公开(公告)号:US11255273B2

    公开(公告)日:2022-02-22

    申请号:US16536974

    申请日:2019-08-09

    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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