公开(公告)号：US09789974B2

公开(公告)日：2017-10-17

申请号：US14887069

申请日：2015-10-19

Applicant: Goodrich Corporation

Inventor： Paul R. Burte ,  Andrew Walsh ,  Todd Rook

IPC: G01M17/00 ,  B64D45/00 ,  B60T17/22 ,  F16D66/00

CPC classification number: B64D45/00 ,  B60T17/221 ,  B64C25/42 ,  B64D2045/0085 ,  F16D66/00 ,  F16D2066/001

Abstract: In accordance with various embodiments, disclosed is a brake monitoring system for monitoring the health status of the brakes of an aircraft, the aircraft comprising a plurality of brakes, the brake monitoring system comprising conducting a statistical comparison of a brake temperature against a temperature data centrality value based on the temperature values of the plurality of brakes.

公开(公告)号：US20140187370A1

公开(公告)日：2014-07-03

申请号：US13731142

申请日：2012-12-31

Applicant: GOODRICH CORPORATION

Inventor： Andrew Walsh

IPC: F16H7/02

CPC classification number: F16H7/023 ,  B64C25/405 ,  F16H7/0827 ,  Y02T50/823

Abstract: A landing gear wheel drive system includes a landing gear strut, a wheel, a drive loop carrier assembly, a drive loop, and a displacement system. The wheel is rotatably attached to the landing gear strut and includes a ring gear mounted to the wheel. The drive loop carrier assembly includes a plurality of toothed pulleys. The drive loop extends around the toothed pulleys to form a continuous loop. The displacement system is connected to the drive loop carrier assembly to selectively engage with the ring gear.

Abstract translation: 起落架轮驱动系统包括起落架支柱，轮，驱动环承载组件，驱动环和排量系统。 车轮可旋转地附接到起落架支柱并且包括安装到车轮的齿圈。 驱动环承载器组件包括多个带齿的滑轮。 驱动环绕着带齿的滑轮延伸以形成连续的环。 位移系统连接到驱动环支架组件以选择性地与环形齿轮啮合。

公开(公告)号：US20170106995A1

公开(公告)日：2017-04-20

申请号：US14887069

申请日：2015-10-19

Applicant: Goodrich Corporation

Inventor： Paul R. Burte ,  Andrew Walsh ,  Todd Rook

IPC: B64D45/00 ,  B60T17/22 ,  F16D66/00

CPC classification number: B64D45/00 ,  B60T17/221 ,  B64C25/42 ,  B64D2045/0085 ,  F16D66/00 ,  F16D2066/001

Abstract: In accordance with various embodiments, disclosed is a brake monitoring system for monitoring the health status of the brakes of an aircraft, the aircraft comprising a plurality of brakes, the brake monitoring system comprising conducting a statistical comparison of a brake temperature against a temperature data centrality value based on the temperature values of the plurality of brakes.