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公开(公告)号：US20210095728A1
公开(公告)日：2021-04-01
申请号：US16588186
申请日：2019-09-30
Applicant: GOODRICH CORPORATION
Inventor： Richard A. Kipp
Abstract: A brake stack is disclosed. The brake stack comprises a first stator, a second stator, and a first rotor disposed between the first stator and the second stator. The brake stack further comprises a first spring disposed between the first stator and the second stator. The first spring is disposed radially inward of the first rotor. The first spring is disposed axially between the first stator and the second stator. The first spring is configured to partially compress when a force applied to a pressure plate of the brake stack is less than a threshold force.
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公开(公告)号：US20190077500A1
公开(公告)日：2019-03-14
申请号：US15701075
申请日：2017-09-11
Applicant: Goodrich Corporation
Inventor： Richard A. Kipp , Steven T. Keller
CPC classification number: B64C25/426 , B60T8/1703 , B60T8/171 , B60T8/172 , B60T17/22 , B60T2270/60 , B64C25/405 , G05D1/0202
Abstract: Systems and methods for aircraft electric taxi brake optimization are provided. The system may comprise an aircraft having a landing gear comprising a wheel, a friction brake having a brake material coupled to the wheel, a regenerative brake comprising a reversible taxi motor coupled to the wheel, a sensor configured to measure a wheel parameter of the wheel and a temperature of the friction brake, a tangible, non-transitory memory configured to communicate with a controller, the tangible, non-transitory memory having instructions stored thereon that, in response to execution by the controller, cause the controller to perform operations comprising: receiving, by the controller, a command signal and the friction brake temperature and calculating, by the controller, a brake material temperature based on the wheel parameter, the friction brake temperature, and the command signal.
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公开(公告)号：US11226019B2
公开(公告)日：2022-01-18
申请号：US16588186
申请日：2019-09-30
Applicant: GOODRICH CORPORATION
Inventor： Richard A. Kipp
IPC: F16D55/36 , B64C25/42 , F16D125/58
Abstract: A brake stack is disclosed. The brake stack comprises a first stator, a second stator, and a first rotor disposed between the first stator and the second stator. The brake stack further comprises a first spring disposed between the first stator and the second stator. The first spring is disposed radially inward of the first rotor. The first spring is disposed axially between the first stator and the second stator. The first spring is configured to partially compress when a force applied to a pressure plate of the brake stack is less than a threshold force.
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公开(公告)号：US20200173489A1
公开(公告)日：2020-06-04
申请号：US16786854
申请日：2020-02-10
Applicant: Goodrich Corporation
Inventor： Scott Whittle , Richard A. Kipp , Nathaniel J. Herrmann
Abstract: An aircraft landing gear arrangement may comprise a landing gear bogie having an axle, a torque tube surrounding the axle and mechanically coupled to the landing gear bogie. A brake stack may surround the torque tube. The torque tube may comprise a cylindrical body extending between a first end and a second end. A flange may be disposed at the first end. A mating surface may be disposed on the first end or the second end of the torque tube for mating the torque tube to the landing gear bogie. A bogie flange may extend from the landing gear bogie whereby the torque tube may be mounted to the landing gear bogie.
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公开(公告)号：US11118620B2
公开(公告)日：2021-09-14
申请号：US16786854
申请日：2020-02-10
Applicant: Goodrich Corporation
Inventor： Scott Whittle , Richard A. Kipp , Nathaniel J Herrmann
Abstract: An aircraft landing gear arrangement may comprise a landing gear bogie having an axle, a torque tube surrounding the axle and mechanically coupled to the landing gear bogie. A brake stack may surround the torque tube. The torque tube may comprise a cylindrical body extending between a first end and a second end. A flange may be disposed at the first end. A mating surface may be disposed on the first end or the second end of the torque tube for mating the torque tube to the landing gear bogie. A bogie flange may extend from the landing gear bogie whereby the torque tube may be mounted to the landing gear bogie.
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Patent Agency Ranking
公开(公告)号：US10598209B2
公开(公告)日：2020-03-24
申请号：US15699682
申请日：2017-09-08
Applicant: Goodrich Corporation
Inventor： Scott Whittle , Richard A. Kipp , Nathaniel J Herrmann
Abstract: An aircraft landing gear arrangement may comprise a landing gear bogie having an axle, a torque tube surrounding the axle and mechanically coupled to the landing gear bogie. A brake stack may surround the torque tube. The torque tube may comprise a cylindrical body extending between a first end and a second end. A flange may be disposed at the first end. A mating surface may be disposed on the first end or the second end of the torque tube for mating the torque tube to the landing gear bogie. A bogie flange may extend from the landing gear bogie whereby the torque tube may be mounted to the landing gear bogie.
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公开(公告)号：US10543909B2
公开(公告)日：2020-01-28
申请号：US15701075
申请日：2017-09-11
Applicant: Goodrich Corporation
Inventor： Richard A. Kipp , Steven T. Keller
Abstract: Systems and methods for aircraft electric taxi brake optimization are provided. The system may comprise an aircraft having a landing gear comprising a wheel, a friction brake having a brake material coupled to the wheel, a regenerative brake comprising a reversible taxi motor coupled to the wheel, a sensor configured to measure a wheel parameter of the wheel and a temperature of the friction brake, a tangible, non-transitory memory configured to communicate with a controller, the tangible, non-transitory memory having instructions stored thereon that, in response to execution by the controller, cause the controller to perform operations comprising: receiving, by the controller, a command signal and the friction brake temperature and calculating, by the controller, a brake material temperature based on the wheel parameter, the friction brake temperature, and the command signal.
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公开(公告)号：US20190078608A1
公开(公告)日：2019-03-14
申请号：US15699682
申请日：2017-09-08
Applicant: Goodrich Corporation
Inventor： Scott Whittle , Richard A. Kipp , Nathaniel J. Herrmann
CPC classification number: F16C3/02 , B64C25/34 , B64C25/42 , F16C2326/43 , F16C2361/45 , F16D55/24 , F16D55/40 , F16D65/02 , F16D2065/1388
Abstract: An aircraft landing gear arrangement may comprise a landing gear bogie having an axle, a torque tube surrounding the axle and mechanically coupled to the landing gear bogie. A brake stack may surround the torque tube. The torque tube may comprise a cylindrical body extending between a first end and a second end. A flange may be disposed at the first end. A mating surface may be disposed on the first end or the second end of the torque tube for mating the torque tube to the landing gear bogie. A bogie flange may extend from the landing gear bogie whereby the torque tube may be mounted to the landing gear bogie.
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公开(公告)号：US10093298B2
公开(公告)日：2018-10-09
申请号：US14991290
申请日：2016-01-08
Applicant: Goodrich Corporation
Inventor： Richard A. Kipp
IPC: G01C23/00 , G05D3/00 , G06F17/00 , B60T17/22 , B60T8/17 , B60T8/88 , B60T13/74 , B64C25/44 , G01L5/28 , B60T8/32
Abstract: The present disclosure relates to brake control and monitoring, and more particularly, to a brake control and monitoring system that monitors brake actuation force.
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公开(公告)号：US20170197606A1
公开(公告)日：2017-07-13
申请号：US14991290
申请日：2016-01-08
Applicant: Goodrich Corporation
Inventor： Richard A. Kipp
CPC classification number: B60T17/221 , B60T8/1703 , B60T8/325 , B60T8/885 , B60T13/741 , B60T2270/406 , B64C25/44 , G01L5/28
Abstract: The present disclosure relates to brake control and monitoring, and more particularly, to a brake control and monitoring system that monitors brake actuation force.
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