公开(公告)号：US20200215725A1

公开(公告)日：2020-07-09

申请号：US16672667

申请日：2019-11-04

Applicant: Goodrich Corporation

Inventor： Nathaniel Ching ,  Jin Hu ,  Wenping Zhao ,  Casey Slane

IPC: B29C33/00 ,  B29C33/52 ,  B29C70/30

Abstract: A method of making a blind hole in a wall of a multi-section tank during manufacture includes inserting a thin, flexible composite spacer ring in a hole in a composite material between mating parts of a soluble tool. The composite spacer ring is cured to the composite material during curing and maintains the hole between sections of the tank once completed.

公开(公告)号：US20200011543A1

公开(公告)日：2020-01-09

申请号：US16453220

申请日：2019-06-26

Applicant: Goodrich Corporation

Inventor： Jin Hu ,  Nathaniel Ching ,  Casey Slane ,  Galdemir Cezar Botura

IPC: F24D13/02 ,  B64C1/18

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.

公开(公告)号：US20200010168A1

公开(公告)日：2020-01-09

申请号：US16026855

申请日：2018-07-03

Applicant: Goodrich Corporation

Inventor： Jin Hu ,  Nathaniel Ching ,  Wenping Zhao ,  Casey Slane ,  Galdemir Cezar Botura

IPC: B64C1/18 ,  B64C1/00 ,  B32B3/12 ,  B32B5/02 ,  B32B5/18 ,  B32B5/24 ,  B32B5/26 ,  B32B15/14 ,  B32B27/12 ,  B32B37/06 ,  B32B37/14 ,  B32B37/18

Abstract: A heated floor panel assembly for aircraft includes structural layers made of a fiber matrix and a high temperature thermoplastic resin. The structural layers are within the heated floor panel assembly to protect the other assembly components from damage and absorb stress. The heated floor panel assembly further includes a heating layer with a heating element, an impact layer, and a core layer to take shear stress exerted on the assembly.

公开(公告)号：US20180213606A1

公开(公告)日：2018-07-26

申请号：US15416743

申请日：2017-01-26

Applicant: Goodrich Corporation

Inventor： Jin Hu ,  Casey Slane ,  Nathaniel Ching ,  Galdemir Cezar Botura

IPC: H05B3/20

CPC classification number: H05B3/20 ,  B64D15/12 ,  H05B2203/006 ,  H05B2203/013 ,  H05B2203/017 ,  H05B2214/02 ,  H05B2214/04

Abstract: A heating element includes an electrode array having first and second interdigitated electrodes. The first electrode is configured to have a first polarity, and the second electrode is configured to have a second polarity. The electrode array substantially encloses a plurality of regions. The heating element further includes a heating surface including a layer of a carbon allotrope material having a first electrical resistance. The electrode array is in electrical communication with the carbon allotrope material.

公开(公告)号：US20240124146A1

公开(公告)日：2024-04-18

申请号：US18535566

申请日：2023-12-11

Applicant: Goodrich Corporation

Inventor： Casey Slane ,  Jin Hu ,  Nathaniel Ching ,  Galdemir Cezar Botura ,  James A. Mullen ,  Mark James Didyk

IPC: B64D15/12 ,  H05B3/14

CPC classification number: B64D15/12 ,  H05B3/145 ,  B82Y30/00

Abstract: An ice protection system for an aircraft component includes a plurality of heaters. The aircraft component has at least two section and a junction area. At least one of the heaters is an H-shape carbon allotrope heater designed to apply heat to the junction area and prevent ice accumulation in the junction area.

公开(公告)号：US11939105B2

公开(公告)日：2024-03-26

申请号：US15689585

申请日：2017-08-29

Applicant: Goodrich Corporation

Inventor： Casey Slane ,  Jin Hu ,  Nathaniel Ching

IPC: F17C1/08 ,  B64D11/02 ,  B64D11/04 ,  B64D37/04 ,  B64D37/06 ,  B65D1/40 ,  B65D88/02 ,  B65D90/02 ,  F17C1/06 ,  F17C1/16

CPC classification number: B65D1/40 ,  B64D11/02 ,  B64D11/04 ,  B64D37/04 ,  B64D37/06 ,  B65D88/02 ,  B65D90/02 ,  F17C1/06 ,  F17C1/16

Abstract: A conformable tank includes a body with a plurality of walls defining a cavity in the body, and an internal support structure connected to an internal surface of one of the plurality of walls and protruding into the cavity of the body. The plurality of walls are formed of a first 3D woven composite material. The internal support structure is formed of a second composite material.

公开(公告)号：US11910495B2

公开(公告)日：2024-02-20

申请号：US16713475

申请日：2019-12-13

Applicant: GOODRICH CORPORATION

Inventor： Jin Hu ,  Casey Slane ,  Nathaniel Ching

IPC: H05B3/14 ,  B64D15/12 ,  C09D11/037 ,  C09D11/102 ,  C09D11/52 ,  H05B1/02 ,  H05B3/03 ,  H05B3/32

CPC classification number: H05B3/145 ,  B64D15/12 ,  C09D11/037 ,  C09D11/102 ,  C09D11/52 ,  H05B1/0236 ,  H05B3/03 ,  H05B3/32 ,  B64D2221/00 ,  H05B2203/013 ,  H05B2203/017 ,  H05B2203/02

Abstract: A conductive ink may comprise a high temperature thermoplastic polyurethane (TPU) and a plurality of conductive particles disposed in the high temperature TPU. The plurality of conductive particles may comprise between 60% and 95% of the conductive ink by weight. The high temperature TPU may include a melting point between 120° C. and 200° C. The conductive ink may be used for external heated composite structures, such as rotor blades, fixed wings, faring, engine lip electrothermal ice protection, or the like. The conductive ink may have enhanced mechanical fatigue resistance.

公开(公告)号：US11906095B2

公开(公告)日：2024-02-20

申请号：US17135351

申请日：2020-12-28

Applicant: GOODRICH CORPORATION

Inventor： Nathaniel Ching ,  Jin Hu ,  Ramesh Achutha Rao

IPC: F16L47/24

CPC classification number: 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.

公开(公告)号：US20230234712A1

公开(公告)日：2023-07-27

申请号：US18178810

申请日：2023-03-06

Applicant: Goodrich Corporation

Inventor： Nathaniel Ching ,  Jin Hu ,  Peter J. Walsh ,  Casey Slane

IPC: B64D15/12 ,  C09J7/38 ,  C08K3/08 ,  C09J9/02 ,  C09J11/04 ,  B64D15/00 ,  C09J5/06 ,  C08K3/22

CPC classification number: B64D15/12 ,  C09J7/385 ,  C08K3/08 ,  C09J9/02 ,  C09J11/04 ,  B64D15/00 ,  C09J5/06 ,  C08K3/22 ,  B82Y30/00

Abstract: A method of making an adhesive for an ice protection assembly includes mixing ferrous nanoparticles into the adhesive. Removal of the adhesive for ice protection assembly inspection or repair includes heating the ferrous nanoparticles in the adhesive to soften the adhesive and allow for easy removal or repositioning of the ice protection assembly.

公开(公告)号：US11639040B2

公开(公告)日：2023-05-02

申请号：US16796791

申请日：2020-02-20

Applicant: GOODRICH CORPORATION

Inventor： Nathaniel Ching ,  Jin Hu ,  Casey Slane

IPC: B29D22/00 ,  B29C65/00 ,  B29C70/34 ,  B64D11/00 ,  B29C70/72 ,  B29L31/30

Abstract: A method of manufacturing a cured vessel is disclosed herein. The method comprises wrapping a first bladder in a first composite laminate, wrapping a second bladder in a second composite laminate. The method further comprises joining the first composite laminate and the second composite laminate by wrapping them both in a third composite laminate to form an un-cured vessel. The un-cured vessel is cured by heating the uncured vessel and pressurizing the bladder while the uncured vessel is in a vessel mold.