公开(公告)号：US20150053664A1

公开(公告)日：2015-02-26

申请号：US14191873

申请日：2014-02-27

Applicant: Goodrich Corporation

Inventor： Jin Hu

IPC: F24D13/02 ,  H05B3/16 ,  B64C1/18 ,  H05K3/12 ,  H05K3/38

CPC classification number: B64C1/18 ,  B64D13/00 ,  F24D13/024 ,  F24D2200/08 ,  F24D2220/2081 ,  H05B3/16 ,  H05B3/26 ,  H05B2203/003 ,  H05B2203/013 ,  H05B2203/017 ,  H05K1/167 ,  H05K3/1216 ,  H05K3/1283 ,  H05K3/38 ,  H05K2201/09263 ,  Y02B30/26 ,  Y10T29/49155 ,  Y10T29/49162

Abstract: A method for providing an electrical connection for conductive ink includes direct writing a bus bar onto areas of a desired electrical connection of the conductive ink. The conductive ink is screen printed onto a dielectric film to create a conductive circuit. An aircraft heated floor panel includes at least one floor panel of an aircraft. The one floor panel includes a conductive circuit having a conductive ink including a bus bar directly written onto areas of a desired electrical connection of the conductive ink. The conductive ink is screen printed onto a dielectric film to create a conductive circuit.

Abstract translation: 用于提供用于导电油墨的电连接的方法包括将母线直接写入导电油墨的期望电连接的区域上。 将导电油墨丝网印刷在电介质膜上以产生导电电路。 飞机加热地板镶板至少包括一架飞机的地板。 一层面板包括具有导电油墨的导电电路，该导电油墨包括直接写入导电油墨的所需电连接区域的母线。 将导电油墨丝网印刷在电介质膜上以产生导电电路。

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.

公开(公告)号：US20220295601A1

公开(公告)日：2022-09-15

申请号：US17752806

申请日：2022-05-24

Applicant: Goodrich Corporation

Inventor： George F. Owens ,  Kevin Edward Roach ,  James A. Mullen ,  Michael John Giamati ,  Jon Shearer ,  James Van Twisk ,  David L. Brittingham ,  Tommy M. Wilson, JR. ,  Jin Hu ,  William A. Veronesi ,  Mark R. Gurvich ,  Joseph Winesdoerffer ,  Jason Gesner

IPC: H05B3/26 ,  B64D13/08 ,  F24D13/02 ,  B32B3/12 ,  B32B7/12 ,  B32B15/20 ,  B64C1/18 ,  H01C17/06

Abstract: An aircraft heated floor panel includes a first face sheet, a second face sheet opposite the first face sheet, and core with an electrically conductive core portion. The electrically conductive core portion supports the first face sheet and the second face sheet, and is electrically insulated from the external environment to receive electrical power, resistively generate heat, and communicate heat to the first face sheet.

公开(公告)号：US20220194588A1

公开(公告)日：2022-06-23

申请号：US17529443

申请日：2021-11-18

Applicant: GOODRICH CORPORATION

Inventor： Jin Hu ,  Phi Doan

IPC: B64D11/02 ,  B05D3/10 ,  C23G1/08 ,  C23C22/50 ,  B05D5/00 ,  B05D3/02 ,  A01N33/12

Abstract: A method of manufacturing a metal component with an anti-microbial molecular layer may comprise: disposing the metal component in a piranha solution; washing the metal component; and grafting a surface of the metal component with a Si-Quat or hybrid Si-Quat molecular layer.

公开(公告)号：US20210291957A1

公开(公告)日：2021-09-23

申请号：US16824984

申请日：2020-03-20

Applicant: GOODRICH CORPORATION

Inventor： Brandon Hein ,  James A. Mullen ,  George F. Owens ,  Nathaniel Ching ,  Jin Hu

IPC: B64C1/18

Abstract: A heated floor panel may comprise a base assembly and a heating element located on a first surface of the base assembly. A panel skin may be located over the heating element and the first surface of the base assembly. The panel skin may extend from the first surface of the base assembly to a second surface of the base assembly opposite the first surface of the base assembly.