公开(公告)号：US20200010169A1

公开(公告)日：2020-01-09

申请号：US16026899

申请日：2018-07-03

Applicant: Goodrich Corporation

Inventor： Casey Slane ,  Nathaniel Ching ,  Wenping Zhao ,  Daniel Waina ,  Jin Hu ,  Brandon Hein ,  George F. Owens ,  James A. Mullen

IPC: B64C1/18 ,  H05B3/28 ,  B64C1/00 ,  B32B3/12 ,  B32B15/20 ,  B32B15/18 ,  B32B15/14 ,  B32B5/18 ,  B32B5/02

Abstract: A heated floor panel assembly with an impact layer is made to absorb blunt force and protect a heating element inside the assembly. The assembly further includes a plurality of structural layer made of a reinforced polymer matrix, one or more core layer with a honeycomb or foam structure for absorbing shear stress, and a heating layer containing the heating element. The impact layer is a composite layer with a resin impregnated fiber matrix.

公开(公告)号：US20220022286A1

公开(公告)日：2022-01-20

申请号：US16933833

申请日：2020-07-20

Applicant: GOODRICH CORPORATION

Inventor： Jin Hu ,  Casey Slane ,  Daniel Waina ,  Nathaniel Ching ,  Brandon Hein

IPC: H05B3/14 ,  B64D15/12 ,  B64C27/46 ,  H05B3/34

Abstract: An ice protection system may include a blade and an electrothermal heater including a carbon nanotube (CNT) element and a metal element. The CNT element may be a CNT fabric or a CNT yarn. The metal element may be coupled to the CNT element via a metallization process, or the like. The electrothermal heater element may include an electric sheet resistivity between 0.01 and 0.5 ohms/square.

公开(公告)号：US20220396360A1

公开(公告)日：2022-12-15

申请号：US17346731

申请日：2021-06-14

Applicant: Goodrich Corporation

Inventor： Casey Slane ,  Daniel Waina ,  Galdemir Cezar Botura

IPC: B64D15/16 ,  D02G3/02 ,  C01B32/158

Abstract: A de-icing assembly for a surface of an aircraft includes: a carcass with a first layer, a second layer, and a carcass centerline and a plurality of seams sewn into the carcass, wherein the plurality of seams join the first and second layers of the carcass together. The assembly includes a plurality of inflation passages formed by the plurality of seams and disposed between the first and second layers of the carcass. The system also includes a manifold fluidly connected to and disposed beneath the carcass, the manifold comprising a width and a manifold centerline oriented approximately perpendicular or parallel to the carcass centerline. The seams are sown by a stitchline formed of carbon nanotube yarn

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

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

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.

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：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

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

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.

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

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

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.

公开(公告)号：US11975849B2

公开(公告)日：2024-05-07

申请号：US17346731

申请日：2021-06-14

Applicant: Goodrich Corporation

Inventor： Casey Slane ,  Daniel Waina ,  Galdemir Cezar Botura

IPC: B32B9/00 ,  B64D15/16 ,  C01B32/158 ,  D02G3/02

CPC classification number: B64D15/166 ,  C01B32/158 ,  D02G3/02 ,  C01B2202/22 ,  D10B2101/122

Abstract: A de-icing assembly for a surface of an aircraft includes: a carcass with a first layer, a second layer, and a carcass centerline and a plurality of seams sewn into the carcass, wherein the plurality of seams join the first and second layers of the carcass together. The assembly includes a plurality of inflation passages formed by the plurality of seams and disposed between the first and second layers of the carcass. The system also includes a manifold fluidly connected to and disposed beneath the carcass, the manifold comprising a width and a manifold centerline oriented approximately perpendicular or parallel to the carcass centerline. The seams are sown by a stitchline formed of carbon nanotube yarn.

公开(公告)号：US11044789B2

公开(公告)日：2021-06-22

申请号：US16157775

申请日：2018-10-11

Applicant: Goodrich Corporation

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

IPC: H05B3/48 ,  H05B3/03 ,  H05B3/18

Abstract: Additively manufactured heating elements for tubes are made from a positive temperature coefficient heater ink printed on the tube. A bus bar is likewise printed onto the tube using a conductive ink. The positive temperature coefficient heater ink and bust bar conductive ink are encapsulated with a closing adhesive.

公开(公告)号：US10899427B2

公开(公告)日：2021-01-26

申请号：US16026899

申请日：2018-07-03

Applicant: Goodrich Corporation

Inventor： Casey Slane ,  Nathaniel Ching ,  Wenping Zhao ,  Daniel Waina ,  Jin Hu ,  Brandon Hein ,  George F. Owens ,  James A. Mullen

IPC: H05B3/20 ,  H05B3/28 ,  B64C1/18 ,  B32B3/12 ,  B32B5/02 ,  B32B5/18 ,  B32B15/14 ,  B32B15/18 ,  B32B15/20 ,  B64C1/00

Abstract: A heated floor panel assembly with an impact layer is made to absorb blunt force and protect a heating element inside the assembly. The assembly further includes a plurality of structural layer made of a reinforced polymer matrix, one or more core layer with a honeycomb or foam structure for absorbing shear stress, and a heating layer containing the heating element. The impact layer is a composite layer with a resin impregnated fiber matrix.