公开(公告)号：US20200331616A1

公开(公告)日：2020-10-22

申请号：US16389313

申请日：2019-04-19

Applicant: GOODRICH CORPORATION

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

IPC: B64D15/12 ,  B64C3/18 ,  B64F5/10

Abstract: An aircraft may include a fuselage and a wing extending away from the fuselage to a wing tip. The wing may have a leading edge portion, a suction side portion, and a pressure side portion. A thermoelectric element may be coupled to an inner surface of the wing. A chemical adhesive may be disposed on a thermoelectric inner surface. A structural rib may be adhesively bonded to the thermoelectric element by curing the chemical adhesive. The structural rib may be mechanically fastened to a suction side of the wing and to a pressure side of the wing.

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.

公开(公告)号：US10660160B2

公开(公告)日：2020-05-19

申请号：US15271009

申请日：2016-09-20

Applicant: Goodrich Corporation

Inventor： Jin Hu ,  Galdemir Cezar Botura

IPC: H05B3/34 ,  H05B3/14 ,  B64D15/12

Abstract: A nano alumina fabric protects heaters used for de-icing aircraft or other vehicles. This allows heaters to withstand mechanical foreign object damage (FOD), is environmentally safe, and is a cost-efficient alternative to other protection fabrics.

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

IPC: B32B5/02 ,  B64C1/18 ,  B32B3/12 ,  B32B27/08 ,  B32B15/14

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.

公开(公告)号：US20190152613A1

公开(公告)日：2019-05-23

申请号：US15816785

申请日：2017-11-17

Applicant: Goodrich Corporation

Inventor： Jin Hu ,  Casey Slane ,  Nathaniel Ching

IPC: B64D15/16 ,  B32B5/26 ,  B32B7/08 ,  B32B25/10

Abstract: A pneumatic de-icer includes an externally facing weathering surface that includes a low-friction additive in the rubber mixture. The low-friction additive has a coefficient of friction of 0.10 or less, and promotes ice shedding because the additive has low ice adhesion compared to typical rubber materials used for pneumatic de-icer assemblies.

公开(公告)号：US20190124724A1

公开(公告)日：2019-04-25

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

CPC classification number: H05B3/145 ,  B64D15/12 ,  C01B32/158 ,  C01B32/168 ,  C01B32/194 ,  H05B2203/007 ,  H05B2203/017 ,  H05B2214/04

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.

公开(公告)号：US20190061986A1

公开(公告)日：2019-02-28

申请号：US15689585

申请日：2017-08-29

Applicant: Goodrich Corporation

Inventor： Casey Slane ,  Jin Hu ,  Nathaniel Ching

IPC: B65D1/40

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：US20180168002A1

公开(公告)日：2018-06-14

申请号：US15373368

申请日：2016-12-08

Applicant: Goodrich Corporation

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

IPC: H05B3/14 ,  H05B3/34

Abstract: A heating element includes a bottom layer, a web consisting of a carbon nanotube (CNT) yarn wherein the web is affixed to a first side of the bottom layer, and an encapsulating layer positioned on the web and the first side of the bottom layer. A method for making a heating element includes providing a bottom layer, inserting a plurality of pegs into the bottom layer such that a portion of each peg protrudes from the bottom layer, weaving a CNT yarn around the protruding portions of the plurality of pegs to form a CNT web, affixing the CNT web to the bottom layer, and encapsulating the CNT web and the bottom layer to form the heating element

公开(公告)号：US09994326B2

公开(公告)日：2018-06-12

申请号：US15140024

申请日：2016-04-27

Applicant: Goodrich Corporation

Inventor： Jin Hu

IPC: B29C70/14 ,  B64D15/16 ,  B29C70/18 ,  B29C70/42 ,  D01D5/00 ,  B29K75/00 ,  B29K105/08 ,  B29K105/16 ,  B29K505/02 ,  B29K507/04 ,  B29L31/30

CPC classification number: B64D15/166 ,  B29C70/14 ,  B29C70/18 ,  B29C70/42 ,  B29K2075/00 ,  B29K2105/0863 ,  B29K2105/16 ,  B29K2505/02 ,  B29K2507/04 ,  B29L2031/3085 ,  D01D5/003

Abstract: A deicer boot includes an aircraft structure and an outer layer. The outer layer includes a plurality of elastomer fibers and a carbon allotrope material. The carbon allotrope material is aligned with at least one elastomer fiber belonging to the plurality of elastomer fibers. A method of forming a layer of a deicer boot includes aligning a carbon allotrope material with a first elastomer fiber, joining the first elastomer fiber with a plurality of additional elastomer fibers to form a non-woven fiber fabric, and incorporating the non-woven fiber fabric into a sheet.

公开(公告)号：US20170238369A1

公开(公告)日：2017-08-17

申请号：US15428072

申请日：2017-02-08

Applicant: Goodrich Corporation

Inventor： George F. Owens ,  Kevin E. Roach ,  James Mullen ,  Michael J. 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 ,  B64C1/18 ,  B32B15/20 ,  H01C17/06 ,  B32B3/12 ,  B32B7/12

CPC classification number: H05B3/26 ,  B32B3/12 ,  B32B7/12 ,  B32B15/20 ,  B32B2255/00 ,  B32B2307/202 ,  B32B2605/18 ,  B64C1/18 ,  B64D13/08 ,  F24D13/024 ,  H01C17/06 ,  Y02B30/26

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.