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公开(公告)号:US20220411076A1
公开(公告)日:2022-12-29
申请号:US17357676
申请日:2021-06-24
Applicant: Goodrich Corporation
Inventor: Nathaniel Ching , Jin Hu , Casey Slane , Galdemir Cezar Botura , Wenping Zhao
IPC: B64D15/12 , B23K26/00 , B23K26/352 , B23K26/70 , B32B5/18 , B32B3/12 , B32B5/02 , B32B7/12 , B32B9/04 , B32B25/20 , B32B27/34 , B32B27/28
Abstract: Disclosed is a first method of providing a heating system to an outer skin of an aircraft, that has the steps of forming laser-induced graphene (LIG) on a polymer sheet by directing laser energy towards the polymer sheet; coupling electrical leads to the LIG; and bonding the polymer sheet against the outer skin or erosion protection layer secured to the outer skin so that to the polymer sheet conforms with a shape of the outer skin.
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公开(公告)号:US20220397207A1
公开(公告)日:2022-12-15
申请号:US17348385
申请日:2021-06-15
Applicant: Goodrich Corporation
Inventor: Nathaniel Ching , Jin Hu , Kevin Edward Roach
IPC: F16K17/06 , F16K17/196
Abstract: A container assembly includes a container body having a housing defining an internal compartment and an opening connected to the internal compartment. A cap having an engagement feature is mounted to the housing about the opening. A pressure relief valve is operably coupled with the internal compartment to vent fluid from the internal compartment. The pressure relief valve has a movable member movable between a first position and a second position. When the movable member is in the first position, the movable member is configured to cooperate with the engagement feature to restrict movement of the cap relative to the opening.
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公开(公告)号:US11499724B2
公开(公告)日:2022-11-15
申请号:US16453220
申请日:2019-06-26
Applicant: Goodrich Corporation
Inventor: Jin Hu , Nathaniel Ching , Casey Slane , Galdemir Cezar Botura
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. The heater layer can be formed by direct writing a heating element pattern onto a dielectric layer bonded to the core.
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公开(公告)号:US11477856B2
公开(公告)日:2022-10-18
申请号:US16748325
申请日:2020-01-21
Applicant: Goodrich Corporation
Inventor: Nathaniel Ching , Casey Slane , Jin Hu
IPC: H05B3/14 , C01B32/168 , C01B32/194 , C01B32/21
Abstract: A carbon allotrope element includes a carbon allotrope layer formed from a carbon allotrope material impregnated with a dielectric resin and having a first surface. The carbon allotrope element further includes a first bus bar in communication with the first surface, and a second bus bar in communication with the first surface and non-adjacent to the first bus bar. The first surface includes a layer of the dielectric resin and a plurality of abraded regions, and each of the first and second bus bars is in communication with one of the plurality of abraded regions of the first surface.
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65.
公开(公告)号:US20220288887A1
公开(公告)日:2022-09-15
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
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:US11122650B2
公开(公告)日:2021-09-14
申请号:US16032793
申请日:2018-07-11
Applicant: Goodrich Corporation
Inventor: Nathaniel Ching , Jin Hu , Casey Slane , Galdemir Cezar Botura
Abstract: A heating element includes a first bus bar disposed to receive current from a power source, and a second bus bar non-adjacent to the first bus bar. The heating element further includes a polymer ink section extending between the first and second bus bars, and the section includes a plurality of PTC polymer inks each different from one another. The second bus bar is electrically connected to the first bus bar via the polymer ink section.
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公开(公告)号:US11091266B2
公开(公告)日:2021-08-17
申请号:US15689599
申请日:2017-08-29
Applicant: Goodrich Corporation
Inventor: Nathaniel Ching , Casey Slane , Jin Hu
IPC: B65D1/16 , B65D90/02 , B60K15/03 , B60K15/073 , B64D37/02 , B64D11/00 , B29C64/393 , B33Y50/02 , B29C64/118 , B33Y10/00 , B33Y80/00 , B64C3/34 , B64D37/06 , B64D37/04 , B64D11/02 , B29L31/00 , B29K105/08
Abstract: A conformable tank includes a body with a plurality of walls defining a cavity in the body, and an internal support connected to an internal surface of one of the plurality of wall of the body and protruding into the cavity of the body. The body and the internal support are an additively manufactured integral structure formed by a fiber filament reinforced composite material.
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公开(公告)号:US20210185771A1
公开(公告)日:2021-06-17
申请号:US16713442
申请日:2019-12-13
Applicant: GOODRICH CORPORATION
Inventor: Nathaniel Ching , Jin Hu , Casey Slane
Abstract: An internal heating trace assembly may include a first bus bar, a second bus bar, a plurality of ceramic positive temperature coefficient (PTC) elements, and an insulator. The ceramic PTC elements may be disposed in parallel between the first bus bar and the second bus bar. The insulator may include a heat-shrink tubing. The ceramic PTC element may include a PTC strip or a PTC bead.
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公开(公告)号:US10785831B2
公开(公告)日:2020-09-22
申请号:US15789632
申请日:2017-10-20
Applicant: Goodrich Corporation
Inventor: Casey Slane , Jin Hu , Galdemir Cezar Botura , Nathaniel Ching
IPC: H05B3/14 , C01B32/158 , C01B32/168 , B64D15/12 , C01B32/194
Abstract: An ice protection heater element includes a carbon allotrope heater with micro-perforations across up to about sixty percent of the carbon allotrope heater's surface. The micro-perforations allow uniform heating across the heating element and tailored electrical resistances for ice protection.
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70.
公开(公告)号:US20200009825A1
公开(公告)日:2020-01-09
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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