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公开(公告)号:US20250074008A1
公开(公告)日:2025-03-06
申请号:US18494003
申请日:2023-10-25
Applicant: Goodrich Corporation
Abstract: The present disclosure provides for composite tank assemblies and related methods of fabrication and use. More particularly, the present disclosure provides for linerless composite tank assemblies for aircraft or fuel or the like, and related modular manufacturing methods. The present disclosure uses a multi-section manufacturing method and carbon fiber or equivalent material with epoxy or the like to fabricate the linerless composite tank assemblies (e.g., thermosetting epoxy; thermoplastic).
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公开(公告)号:US20240428398A1
公开(公告)日:2024-12-26
申请号:US18337815
申请日:2023-06-20
Applicant: Goodrich Corporation
Inventor: Nathaniel Ching , Galdemir C. Botura , Jin Hu
Abstract: The present disclosure provides for heater failure detection assemblies/systems and related methods of fabrication and use. More particularly, the present disclosure provides for heater failure detection assemblies/systems for aircraft or the like, with the heater failure detection assemblies/systems utilizing thermal images to detect the operation or failure of an aircraft heater.
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13.
公开(公告)号:US11878500B2
公开(公告)日:2024-01-23
申请号:US17804436
申请日:2022-05-27
Applicant: Goodrich Corporation
Inventor: Daniel Waina , Jin Hu , Casey Slane , Nathaniel Ching , Galdemir Cezar Botura
CPC classification number: B32B5/024 , B32B3/12 , B32B15/14 , B32B27/08 , B64C1/18 , B32B2260/021 , B32B2260/046 , B32B2262/101 , B32B2262/106 , B32B2305/024 , B32B2305/07 , B32B2307/558 , B32B2307/581 , B32B2605/18
Abstract: A heated floor panel assembly for aircraft includes an impact layer made from a 2-D or 3-D woven high temperature thermoplastic fiber matrix impregnated with a resin. The impact layer can further include woven metallic fibers. The assembly also includes a stack of structural layers, a heating layer, and a core layer for absorbing shear stress.
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公开(公告)号:US11639051B2
公开(公告)日:2023-05-02
申请号:US17087972
申请日:2020-11-03
Applicant: Goodrich Corporation
Inventor: Jin Hu , Galdemir Cezar Botura , Casey Slane , Nathaniel Ching
Abstract: A method for reducing the resistivity of a carbon nanotube nonwoven sheet includes providing a carbon nanotube nonwoven sheet comprising a plurality of carbon nanotubes and applying pressure to the carbon nanotube nonwoven sheet to reduce air voids between carbon nanotubes within the carbon nanotube nonwoven sheet.
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公开(公告)号:US20230077788A1
公开(公告)日:2023-03-16
申请号:US17471425
申请日:2021-09-10
Applicant: Goodrich Corporation
Inventor: Nathaniel Ching , Jin Hu , Galdemir Cezar Botura
Abstract: A carbon nano tube (CNT) conduit heater system includes a CNT sheet having a first surface and a second surface. A first busbar is electrically coupled to the CNT sheet. A second busbar is electrically coupled to the CNT sheet. The second busbar is arranged substantially parallel to the first busbar. A first protective layer is disposed on the first surface and a second protective layer is disposed on the second surface, wherein the second protective layer is joined to the first protective layer encapsulating the CNT sheet the first busbar and the second busbar forming a heater assembly having a first side and a second side.
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公开(公告)号:US11542019B2
公开(公告)日:2023-01-03
申请号:US16578731
申请日:2019-09-23
Applicant: Goodrich Corporation
Inventor: Casey Slane , Peter J. Walsh , Jin Hu , Nathaniel Ching
IPC: B64D15/12 , C08K3/04 , C09J7/38 , C09J9/02 , C09J125/06 , C09J183/04 , B82Y30/00 , B82Y40/00
Abstract: A method of making an adhesive for an ice protection assembly includes transferring Z-CNTs from a substrate carrier into the adhesive. De-bonding of the adhesive for ice protection assembly inspection or repair or repositioning at initial installation includes heating the Z-CNTs in the adhesive to soften the adhesive and allow for easy removal.
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17.
公开(公告)号:US11376811B2
公开(公告)日:2022-07-05
申请号:US16411561
申请日:2019-05-14
Applicant: Goodrich Corporation
Inventor: Daniel Waina , Jin Hu , Casey Slane , Nathaniel Ching , Galdemir Cezar Botura
Abstract: A heated floor panel assembly for aircraft includes an impact layer made from a 2-D or 3-D woven high temperature thermoplastic fiber matrix impregnated with a resin. The impact layer can further include woven metallic fibers. The assembly also includes a stack of structural layers, a heating layer, and a core layer for absorbing shear stress.
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公开(公告)号:US20220205573A1
公开(公告)日:2022-06-30
申请号:US17135351
申请日:2020-12-28
Applicant: GOODRICH CORPORATION
Inventor: Nathaniel Ching , Jin Hu , Ramesh Achutha Rao
IPC: F16L47/24
Abstract: An apparatus may comprise: a metal pipe portion extending from a first end to a first transition end and defining a first radially outer surface and a first radially inner surface, the first transition end comprising a first tooth element and a second tooth element disposed circumferentially adjacent to the first tooth element; and a polymeric pipe portion having a second transition end and defining a second radially outer surface and a second radially inner surface, the second transition end having a complimentary shape to the first transition end, the second transition end coupled to the first transition end.
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公开(公告)号:US20210122096A1
公开(公告)日:2021-04-29
申请号:US16664162
申请日:2019-10-25
Applicant: GOODRICH CORPORATION
Inventor: Jin Hu , Casey Slane , Nathaniel Ching
Abstract: A method for forming a deicer includes forming a body of the deicer. The method further includes forming an outer layer of the deicer through extrusion of an elastomeric material. The method further includes coupling the outer layer of the deicer to the body of the deicer.
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公开(公告)号:US10920994B2
公开(公告)日:2021-02-16
申请号:US16026336
申请日:2018-07-03
Applicant: Goodrich Corporation
Inventor: Nathaniel Ching , Jin Hu , Casey Slane
Abstract: A heater panel includes a core and a heater/dielectric layer including a positive thermal coefficient (PTC) heater layer between a pair of dielectric layers. A structural facing is included, wherein the heater/dielectric layer is bonded directly between the core and the structural facing. A second structural facing can be bonded to the core opposite the heater/dielectric layer. An impact layer can be bonded to the structural facing, e.g., the first structural facing described above, opposite the heater/dielectric layer.
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