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公开(公告)号：US12221388B2
公开(公告)日：2025-02-11
申请号：US17407024
申请日：2021-08-19
Applicant: Honeywell International Inc.
Inventor： Stefan Glen , David Lane Charles , Long Gui Tang , Yanmei Piao , Neil Murdie , Mark C. James
Abstract: An example method includes combining an interlayer and a carbon fiber fabric, wherein the interlayer comprises a highly oriented milled carbon fiber ply comprising a plurality of out-of-plane carbon fibers. The method further includes winding the interlayer and the carbon fiber fabric around a core to form a composite fiber preform comprising a plurality of layers defining an annulus extending along a central axis. The method further includes densifying the composite fiber preform.
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公开(公告)号：US10094439B2
公开(公告)日：2018-10-09
申请号：US15447960
申请日：2017-03-02
Applicant: Honeywell International Inc.
Inventor： David Lane Charles , Amanda Childers , J. Robert Sutton, II
Abstract: In some examples, a disc brake assembly and methods of forming and assembling said brake disc assembly. The brake disc assembly including a core structure and a plurality of wear pads. The core structure having a first major surface comprising at least one curved ridge or curved channel that extends in a radial direction along the first major surface between an inner and outer diameter of the core structure. Each wear pad defining a friction surface and a mounting surface such that the mounting surfaces of the plurality of wear pads are positioned adjacent to, and in contact with, the first major surface of the core structure, where at least one of the mounting surfaces of the plurality of wear pads includes a corresponding curved ridge or curved channel configured to interlink with the at least one curved ridge or curved channel of the core structure.
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公开(公告)号：US20180252284A1
公开(公告)日：2018-09-06
申请号：US15447960
申请日：2017-03-02
Applicant: Honeywell International Inc.
Inventor： David Lane Charles , Amanda Childers , J. Robert Sutton, II
CPC classification number: F16D69/0408 , B64C25/42 , F16D65/122 , F16D65/125 , F16D65/126 , F16D65/127 , F16D65/186 , F16D69/023 , F16D2065/1312 , F16D2065/1316 , F16D2065/132 , F16D2065/1324 , F16D2065/1344 , F16D2065/1356 , F16D2069/004 , F16D2069/009 , F16D2069/0433 , F16D2069/0441 , F16D2069/0491 , F16D2200/0052 , F16D2200/006 , F16D2200/0082 , F16D2250/0084
Abstract: In some examples, a disc brake assembly and methods of forming and assembling said brake disc assembly. The brake disc assembly including a core structure and a plurality of wear pads. The core structure having a first major surface comprising at least one curved ridge or curved channel that extends in a radial direction along the first major surface between an inner and outer diameter of the core structure. Each wear pad defining a friction surface and a mounting surface such that the mounting surfaces of the plurality of wear pads are positioned adjacent to, and in contact with, the first major surface of the core structure, where at least one of the mounting surfaces of the plurality of wear pads includes a corresponding curved ridge or curved channel configured to interlink with the at least one curved ridge or curved channel of the core structure.
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Patent Agency Ranking
公开(公告)号：US09290264B2
公开(公告)日：2016-03-22
申请号：US14099162
申请日：2013-12-06
Applicant: HONEYWELL INTERNATIONAL INC.
Inventor： David Lane Charles , Donald Jeffrey Christensen
CPC classification number: B64C25/405 , Y02T50/823
Abstract: An electric taxi system (ETS) for an aircraft may include an annular output gearbox positioned between a wheel and a main strut of a main landing gear of the aircraft. The output gearbox may surround a brake piston assembly of the wheel of the aircraft. One or more selectively operable engaging assemblies, for selectively coupling the ETS with the wheel of the aircraft, may be positioned between the output gearbox and the wheel of the aircraft. The one or more selectively operable engaging assemblies may be coupled with an output gear of the output gearbox to rotate with the output gear.
Abstract translation: 用于飞机的电动出租车系统（ETS）可以包括定位在飞行器的主起落架的车轮和主支柱之间的环形输出齿轮箱。 输出齿轮箱可以围绕飞行器的车轮的制动器活塞组件。 用于选择性地将ETS与飞行器的车轮联接的一个或多个可选择性操作的接合组件可以位于输出齿轮箱和飞行器的车轮之间。 一个或多个可选择性操作的接合组件可以与输出齿轮箱的输出齿轮联接以与输出齿轮一起旋转。
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5.发明授权Aircraft electric taxi system with friction actuated, bi-directional clutch 有权具有摩擦致动，双向离合器的飞机电动出租车系统公开(公告)号：US08702550B1
公开(公告)日：2014-04-22
申请号：US13945828
申请日：2013-07-18
Applicant: Honeywell International, Inc.
Inventor： Donald J. Christensen , Todd Langston , David Lane Charles , Rudy Velasquez
IPC: F16H48/06
CPC classification number: B64C25/405 , F16D41/125 , Y02T50/823
Abstract: An electric taxi system (ETS) for an aircraft may comprise drive motors mounted coaxially with wheels of the aircraft. A clutch assembly may be interposed between the drive motor the wheel. The clutch assembly may transmit torque from the motor to the wheel when the wheel and a rotor of the motor rotate at the same rotational speed. The clutch assembly may self-disengage a rotor of the motor from the wheel when the wheel rotates faster than the rotor.
Abstract translation: 用于飞机的电动出租车系统（ETS）可以包括与飞机的车轮同轴安装的驱动马达。 离合器组件可以介于驱动马达轮之间。 当车轮和电机的转子以相同的转速旋转时，离合器组件可以将扭矩从电动机传递到车轮。 当轮子转动比转子更快时，离合器组件可以使电动机的转子与车轮脱离接合。
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公开(公告)号：US08702032B2
公开(公告)日：2014-04-22
申请号：US13929204
申请日：2013-06-27
Applicant: Honeywell International, Inc.
IPC: B64C25/50
CPC classification number: B64C25/405 , Y02T10/7258 , Y02T50/823
Abstract: A method of taxing an aircraft with an electric taxi system (ETS) comprising of drive units producing airflow through rotors to pre-cool drive motors and produce rotation of aircraft wheels. The drive motors may be used to produce reverse motion of the aircraft and of operating the drive motors independently of one another so one can operate at a rate of speed and/or direction that is different from the second one of the drive units which may provide enhanced maneuverability of the aircraft during taxing. The drive motors may be controlled to produce regenerative power producing a deceleration of the aircraft that does not shift a center of gravity of the aircraft.
Abstract translation: 一种用电动出租车系统（ETS）对飞机征税的方法，该电动出租车系统包括通过转子产生气流的驱动单元，以预冷却驱动马达并产生飞行器轮的旋转。 驱动马达可以用于产生飞行器的反向运动并且彼此独立地操作驱动马达，因此可以以与可提供的驱动单元的第二驱动单元不同的速度和/或方向的速度操作 提高飞机在征税时的机动性。 可以控制驱动马达以产生再生能量，从而产生不会使飞行器重心偏移的飞行器的减速。
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公开(公告)号：US20230057890A1
公开(公告)日：2023-02-23
申请号：US17407024
申请日：2021-08-19
Applicant: Honeywell International Inc.
Inventor： Stefan Glen , David Lane Charles , Long Gui Tang , Yanmei Piao , Neil Murdie , Mark C. James
Abstract: An example method includes combining an interlayer and a carbon fiber fabric, wherein the interlayer comprises a highly oriented milled carbon fiber ply comprising a plurality of out-of-plane carbon fibers. The method further includes winding the interlayer and the carbon fiber fabric around a core to form a composite fiber preform comprising a plurality of layers defining an annulus extending along a central axis. The method further includes densifying the composite fiber preform.
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8.发明申请公开(公告)号：US20140124617A1
公开(公告)日：2014-05-08
申请号：US13945828
申请日：2013-07-18
Applicant: HONEYWELL INTERNATIONAL, INC.
Inventor： DONALD J. CHRISTENSEN , Todd Langston , David Lane Charles , Rudy Velasquez
IPC: B64C25/40
CPC classification number: B64C25/405 , F16D41/125 , Y02T50/823
Abstract: An electric taxi system (ETS) for an aircraft may comprise drive motors mounted coaxially with wheels of the aircraft. A clutch assembly may be interposed between the drive motor the wheel. The clutch assembly may transmit torque from the motor to the wheel when the wheel and a rotor of the motor rotate at the same rotational speed. The clutch assembly may self-disengage a rotor of the motor from the wheel when the wheel rotates faster than the rotor.
Abstract translation: 用于飞机的电动出租车系统（ETS）可以包括与飞机的车轮同轴安装的驱动马达。 离合器组件可以介于驱动马达轮之间。 当车轮和电机的转子以相同的转速旋转时，离合器组件可以将扭矩从电动机传递到车轮。 当轮子转动比转子更快时，离合器组件可以使电动机的转子与车轮脱离接合。
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