公开(公告)号：US20190061948A1

公开(公告)日：2019-02-28

申请号：US15689599

申请日：2017-08-29

Applicant: Goodrich Corporation

Inventor： Nathaniel Ching ,  Casey Slane ,  Jin Hu

IPC: B64D11/00 ,  B29C64/393 ,  B33Y50/02 ,  B29C64/118 ,  B33Y10/00 ,  B33Y80/00

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.

公开(公告)号：US20190061947A1

公开(公告)日：2019-02-28

申请号：US15689570

申请日：2017-08-29

Applicant: Goodrich Corporation

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

IPC: B64D11/00 ,  E03B11/00

CPC classification number: B64D11/00 ,  B64D11/0007 ,  B64D37/04 ,  B64D37/06 ,  E03B11/00

Abstract: A conformable tank includes a body with a plurality of composite walls formed around a cavity, and an internal support connected to one of the plurality of composite walls and positioned in the cavity. The plurality of composite walls includes a flat side wall disposed opposite a curved side wall. A first section of one of the plurality of composite walls includes an exterior facing, an interior facing, and a core positioned between the exterior facing and the interior facing.

公开(公告)号：US20180162114A1

公开(公告)日：2018-06-14

申请号：US15373370

申请日：2016-12-08

Applicant: Goodrich Corporation

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

IPC: B32B37/16 ,  B32B5/26 ,  B32B15/14 ,  B32B5/02 ,  B32B15/20 ,  B32B27/12 ,  B32B27/32 ,  B32B37/10 ,  D06C15/00

CPC classification number: B32B37/16 ,  B32B5/022 ,  B32B5/26 ,  B32B15/14 ,  B32B15/20 ,  B32B27/12 ,  B32B27/322 ,  B32B37/10 ,  B32B2262/101 ,  B32B2262/106 ,  B32B2307/202 ,  B32B2311/24 ,  B32B2313/04 ,  B32B2327/18 ,  B32B2605/18 ,  B64D15/12 ,  B82Y30/00 ,  D04H1/4242 ,  D06C15/00

Abstract: A method for reducing the resistivity of a carbon nanotube nonwoven sheet includes providing a carbon nanotube nonwoven sheet comprising a plurality of carbon nanotubes and applying pressure to the carbon nanotube nonwoven sheet to reduce air voids between carbon nanotubes within the carbon nanotube nonwoven sheet.

公开(公告)号：US12145733B2

公开(公告)日：2024-11-19

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 ,  B82Y30/00 ,  F02C7/047 ,  H05B3/14

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：US11919648B2

公开(公告)日：2024-03-05

申请号：US18059745

申请日：2022-11-29

Applicant: Goodrich Corporation

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

IPC: B64D15/12 ,  C08K3/04 ,  C09J7/38 ,  C09J9/02 ,  C09J125/06 ,  C09J183/04 ,  B82Y30/00 ,  B82Y40/00

CPC classification number: B64D15/12 ,  C08K3/041 ,  C09J7/385 ,  C09J9/02 ,  C09J125/06 ,  C09J183/04 ,  B82Y30/00 ,  B82Y40/00

Abstract: A method of making an adhesive for an ice protection assembly includes transferring Z-CNTs from a substrate carrier into the adhesive. De-bonding of the adhesive for ice protection assembly inspection or repair or repositioning at initial installation includes heating the Z-CNTs in the adhesive to soften the adhesive and allow for easy removal.

公开(公告)号：US11826776B2

公开(公告)日：2023-11-28

申请号：US16934700

申请日：2020-07-21

Applicant: GOODRICH CORPORATION

Inventor： Jin Hu ,  Nathaniel Ching ,  Phi Doan ,  Casey Slane

IPC: B05D1/18 ,  B05D7/22 ,  F17C1/10

CPC classification number: B05D1/18 ,  B05D7/227 ,  F17C1/10 ,  B05D2259/00 ,  F17C2203/0604 ,  F17C2203/0607 ,  F17C2203/0648

Abstract: A method of coating a high-pressure fluid vessel comprises filling a high-pressure fluid vessel with a coating solution, draining the coating solution, and drying a remainder of the coating solution in the high-pressure fluid vessel. The coating solution may include a thermoplastic elastomer that is hard with a low glass transition temperature and a high melting temperature. Drying the remainder of the coating solution may form a food grade coating within the high-pressure fluid vessel.

公开(公告)号：US11713137B2

公开(公告)日：2023-08-01

申请号：US16663989

申请日：2019-10-25

Applicant: GOODRICH CORPORATION

Inventor： Casey Slane ,  Jin Hu ,  Nathaniel Ching

IPC: B64F5/10 ,  B32B5/02 ,  B32B7/12 ,  B32B15/08 ,  B32B25/08 ,  B32B27/08 ,  B32B27/12 ,  B32B37/12 ,  B32B37/18

CPC classification number: B64F5/10 ,  B32B5/024 ,  B32B7/12 ,  B32B15/08 ,  B32B25/08 ,  B32B27/08 ,  B32B27/12 ,  B32B37/12 ,  B32B37/182 ,  B32B2037/1253 ,  B32B2307/734 ,  B32B2309/105 ,  B32B2605/18

Abstract: A method for forming an aircraft component includes forming an inner portion of the aircraft component. The method further includes forming an outer layer of the aircraft component using extrusion of an elastomeric material. The method further includes coupling the outer layer of the aircraft component to the inner portion of the aircraft component.

公开(公告)号：US20230124999A1

公开(公告)日：2023-04-20

申请号：US17548910

申请日：2021-12-13

Applicant: Goodrich Corporation

Inventor： Adam George ,  Alex Zadell ,  Galdemir Cezar Botura ,  Casey Slane ,  Sugumaran Selvaraj ,  Andrew Taylor

IPC: B64D15/12

Abstract: A system for heating an aircraft surface having a thermally disadvantaged zone includes a carbon nano-tube (CNT) sheet heating element having a power inlet configured to receive power from an external electrical power source and provide it to the CNT sheet heating element that extends across the thermally disadvantaged zone. The CNT sheet heating element is configured and arranged such upon application of power from the external electrical power source to the CNT sheet heating element, the CNT sheet heating element produces a first heat output in a first zone and a second heat output in the thermally disadvantaged zone with the second heat output being greater than the first heat output.

公开(公告)号：US20230123677A1

公开(公告)日：2023-04-20

申请号：US17568402

申请日：2022-01-04

Applicant: Goodrich Corporation

Inventor： Brandon Hein ,  Casey Slane ,  Jeffrey Martin Werbelow ,  Galdemir Cezar Botura ,  Matthew Hamman

IPC: B64D15/12 ,  H05B3/28 ,  H05B3/14 ,  B32B9/00 ,  B32B9/04 ,  B32B15/08 ,  B32B27/08 ,  B32B37/06 ,  B32B37/04

Abstract: A multilayer heating structure for controlling ice accumulation on a surface of an aircraft includes a carbon nano-tube (CNT) heater. The heater includes: a CNT layer; a first encapsulation layer disposed on a first side of the CNT layer formed of a first encapsulation layer thermoplastic material; and a second encapsulation layer disposed on a second side of the CNT layer formed of a second encapsulation layer thermoplastic material.

公开(公告)号：US20230085454A1

公开(公告)日：2023-03-16

申请号：US17473493

申请日：2021-09-13

Applicant: Goodrich Corporation

Inventor： Casey Slane ,  Galdemir Cezar Botura

IPC: C09K3/18 ,  B05D5/08 ,  F03D80/40

Abstract: The present invention is directed to a coated substrate including a substrate that is part of an aerospace, a wind turbine, or a marine structure; and an exterior coating on the substrate, the exterior coating including an icephobic or a low ice adhesion composition including an indicator that is an additive that is detectable or measurable as the exterior coating wears; wherein the indicator provides indicia of wear of the exterior coating; and a method of inspecting the exterior coating on the substrate.