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公开(公告)号:US20230332627A1
公开(公告)日:2023-10-19
申请号:US17723891
申请日:2022-04-19
Applicant: GOODRICH CORPORATION
Inventor: HARALD KLODE , JASON BRADLEY ALLEN
CPC classification number: F04C15/0084 , F04C15/0061 , F16D57/002 , F03C2/08 , F04C2240/81 , F04C2270/0525
Abstract: A hydraulic fluid system is disclosed herein. The hydraulic fluid system includes a hydraulic motor including an output shaft, a reduction gear box having a first side and an opposing second side, the reduction gear box being coupled to the output shaft at the first side and coupled to a reduction shaft at the second side, and a magneto-rheological fluid brake (MRF) brake coupled to the reduction shaft.
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公开(公告)号:US20230358290A1
公开(公告)日:2023-11-09
申请号:US17848164
申请日:2022-06-23
Applicant: GOODRICH CORPORATION
Inventor: VISHAL SREEKUMAR MENON , BASAVARAJ BODKI , JASON BRADLEY ALLEN , ADAM J. DITZLER
CPC classification number: F16F9/3264 , F16F9/38 , B64C25/60
Abstract: A temperature compensating shock strut health indicator system for use with a shock strut comprises a visual indicator comprising a plurality of sectors and a pointer configured to rotate with respect to the visual indicator to point to one of the plurality of sectors. The sector to which the pointer points to is dependent on the shock strut stroke (i.e., the position of the piston with respect to the cylinder). In various embodiments, the visual indicator includes various rings that correspond to a different temperature compensated ideal stroke whereby a crew member can correspond the pointer to the appropriate ring depending on ambient temperature. In various embodiments, the pointer comprises a temperature sensitive material configured to cause the pointer to rotate with respect to the visual indicator to actively compensate for temperature.
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公开(公告)号:US20240336353A1
公开(公告)日:2024-10-10
申请号:US18745279
申请日:2024-06-17
Applicant: GOODRICH CORPORATION
Inventor: JASON BRADLEY ALLEN
Abstract: An aircraft landing gear actuation system which uses two separate actuation forces to retract aircraft landing gear is disclosed. One of the actuation forces may be provided by an actuator, such as a hydraulic actuator. Another of these actuation forces may be provided by a pressurized fluid that is directed into the actuator through a conduit that extends into a hollow interior of an actuator rod of the actuator. The pressurized fluid may be provided from a pressurized fluid source that contains a fixed volume of pressurized fluid. This pressurized fluid may exert a force on an actuator piston of the actuator or the actuator rod. The pressurized fluid may also be used to dampen the deployment of the landing gear.
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公开(公告)号:US20230182891A1
公开(公告)日:2023-06-15
申请号:US17549144
申请日:2021-12-13
Applicant: GOODRICH CORPORATION
Inventor: JASON BRADLEY ALLEN
Abstract: A rack assembly for a rack and pinion gear system may comprise: a rack housing; and a rack disposed within the rack housing, the rack and the rack housing at least partially defining a first hydraulic chamber disposed between a first side of the rack and the rack housing, a second hydraulic chamber disposed between a second side of the rack and the rack housing, a third hydraulic chamber disposed within the rack proximal the first hydraulic chamber, and a fourth hydraulic chamber disposed within the rack proximal the second hydraulic chamber.
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公开(公告)号:US20240317390A1
公开(公告)日:2024-09-26
申请号:US18187416
申请日:2023-03-21
Applicant: GOODRICH CORPORATION
Inventor: JASON BRADLEY ALLEN
CPC classification number: B64C25/50 , B64C25/58 , F15B13/0401 , F15B2211/40553 , F15B2211/40576 , F15B2211/7058
Abstract: A nose-wheel steering system is provided. The nose-wheel steering system includes a hydraulic motor including a drive shaft configured to rotate about a first axis; and a hydraulic motor start assist mechanism coupled to the hydraulic motor and configured to provide a temporary boost of hydraulic fluid pressure supplied to the hydraulic motor.
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公开(公告)号:US20230257109A1
公开(公告)日:2023-08-17
申请号:US17673521
申请日:2022-02-16
Applicant: GOODRICH CORPORATION
Inventor: JASON BRADLEY ALLEN
Abstract: An aircraft landing gear actuation system which uses two separate actuation forces to retract aircraft landing gear is disclosed. One of the actuation forces may be provided by an actuator, such as a hydraulic actuator. Another of these actuation forces may be provided by a pressurized fluid that is directed into the actuator through a conduit that extends into a hollow interior of an actuator rod of the actuator. The pressurized fluid may be provided from a pressurized fluid source that contains a fixed volume of pressurized fluid. This pressurized fluid may exert a force on an actuator piston of the actuator or the actuator rod. The pressurized fluid may also be used to dampen the deployment of the landing gear.
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公开(公告)号:US20230150052A1
公开(公告)日:2023-05-18
申请号:US17528999
申请日:2021-11-17
Applicant: GOODRICH CORPORATION
Inventor: NOEL C. HAYNES , JASON BRADLEY ALLEN
CPC classification number: B23K20/122 , B22F10/28 , B22F3/12 , B22F12/226 , B23K3/063 , B23K35/0227 , B33Y10/00 , B22F2301/205 , B22F2301/35 , B22F2301/052 , B22F2201/20
Abstract: A method of forming a rod feedstock for titanium stir friction welding additive manufacturing may comprise: mixing a plurality of powdered metals comprising titanium, iron, vanadium, and aluminum to produce a powder blend; at least one of die pressing the powder blend to form a die pressed powder or continuously powder rolling the powder blend to form a die pressed powder; and sintering the powder blend to form a rod feedstock having a cross-sectional profile.
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