公开(公告)号：US20180176989A1

公开(公告)日：2018-06-21

申请号：US15385494

申请日：2016-12-20

Applicant: Goodrich Corporation

Inventor： Jin Hu ,  Galdemir Cezar Botura

IPC: H05B1/02 ,  B32B37/16 ,  B32B5/02 ,  B32B15/14 ,  B32B5/26 ,  B32B3/12 ,  B32B7/12 ,  B32B37/12 ,  H05B3/16 ,  B64C1/18

Abstract: A floor panel assembly includes an insulating layer which protects a sheet heater, first and second structural layers, and a honeycomb layer for support. The floor panel assembly allows for heating of the cabin of an aircraft without mechanical damage to the sheet heater.

公开(公告)号：US20180168003A1

公开(公告)日：2018-06-14

申请号：US15373372

申请日：2016-12-08

Applicant: Goodrich Corporation

Inventor： James A. Mullen ,  Jin Hu ,  Galdemir Cezar Botura ,  Zaffir A. Chaudhry ,  Wenping Zhao

IPC: H05B3/14 ,  B64D15/12

CPC classification number: H05B3/145 ,  B64D15/12 ,  H05B3/262 ,  H05B2203/013 ,  H05B2214/02 ,  H05B2214/04 ,  Y02T50/54

Abstract: A carbon allotrope heating element includes an electrical resistivity between 0.005 ohms per square (Ω/sq) and 3.0 Ω/sq. A heating system includes a component and a carbon allotrope heating element having an electrical resistivity between 0.005 Ω/sq and 3.0 Ω/sq. A method includes modifying a carbon allotrope heating element to have an electrical resistivity between 0.005 Ω/sq and 3.0 Ω/sq and applying the carbon allotrope heating element to a component of an aircraft.

公开(公告)号：US09994325B2

公开(公告)日：2018-06-12

申请号：US15140075

申请日：2016-04-27

Applicant: Goodrich Corporation

Inventor： Jin Hu

IPC: B64D15/16 ,  C08J5/18 ,  D01F6/70

CPC classification number: B64D15/16 ,  B64D15/166 ,  C08J5/18 ,  C08J2375/06 ,  C08J2375/08 ,  D01F6/70 ,  D10B2401/061 ,  D10B2505/20

Abstract: A deicer includes an aircraft structure and an outer layer with a sheet having a brittle point lower than −40° C. (−40° F.). The sheet includes a polyether urethane elastomer. A deicer includes an aircraft structure and an outer elastomer layer. The outer elastomer layer includes a non-woven fabric having polyether urethane fibers and one of (1) a carbon allotrope material aligned with at least one of the polyether urethane fibers and (2) a polyester urethane composition located on a portion of the non-woven fabric. A method of forming a layer of a deicer boot includes forming a polyether urethane elastomer sheet having a brittle point lower than −40° C. (−40° F.) and incorporating the polyether urethane elastomer sheet onto an aircraft structure.

公开(公告)号：US20160007474A1

公开(公告)日：2016-01-07

申请号：US14790886

申请日：2015-07-02

Applicant: United Technologies Corporation ,  Goodrich Corporation

Inventor： Sameh Dardona ,  Michael P. Humbert ,  John P. Wesson ,  Wayde R. Schmidt ,  Daniel V. Viens ,  Jin Hu

IPC: H05K3/00 ,  H05B3/06 ,  H05B3/02 ,  H05K3/30 ,  H05B3/12 ,  H05B3/26 ,  H05K3/12 ,  H05B3/00 ,  H05B3/16

CPC classification number: H05K3/0014 ,  B33Y80/00 ,  H05B3/0014 ,  H05B3/06 ,  H05B3/12 ,  H05B3/145 ,  H05B3/16 ,  H05B3/265 ,  H05B3/267 ,  H05B3/34 ,  H05B3/84 ,  H05B2203/003 ,  H05B2203/013 ,  H05B2203/017 ,  H05B2214/02 ,  H05B2214/04 ,  H05K3/12 ,  H05K3/30

Abstract: A heating circuit assembly and method of manufacture includes an electrically conductive heating element having a pattern. An electrically non-conductive substrate is additive manufactured and secured to the element for structural support. The substrate has a topology that generally aligns with the pattern of the element thereby reducing the assembly weight and minimizing substrate material waste.

Abstract translation: 加热电路组件及其制造方法包括具有图案的导电加热元件。 非导电基材是制造并固定到用于结构支撑的元件的添加剂。 衬底具有通常与元件的图案对准的拓扑，从而减少组件重量并使衬底材料浪费最小化。

公开(公告)号：US20140353238A1

公开(公告)日：2014-12-04

申请号：US13907264

申请日：2013-05-31

Applicant: Goodrich Corporation

Inventor： Jin Hu

IPC: B01D71/02 ,  B01D67/00 ,  C02F1/50

CPC classification number: B01D71/022 ,  B01D39/1623 ,  B01D69/105 ,  B01D69/12 ,  B01D2239/0442 ,  B01D2239/0668 ,  B01D2325/48 ,  C02F1/001 ,  C02F1/505 ,  C02F2201/006

Abstract: The invention provides a method of preparing a filter medium by thermally bonding silver-coated spunbonded nonwoven fabrics to a dirt-retaining membrane, a chemical-retaining membrane, a pathogen-retaining membrane, or a combination thereof. The invention also relates to the use of one or more silver-coated spunbonded nonwoven fabric layers as a component of a microorganism-killing membrane in filter media for a fluid filtration system. The filter media of the invention offers efficient disinfection effects, maintaining a low pressure drop and a high flow rate when in use. Further, the filter media is adhesive free and contains at least one thermal binding layer made of spunbonded nonwoven polymeric fabrics. The invention also features a water-purification cartridge and the use thereof in a potable water system.

Abstract translation: 本发明提供了一种通过将银涂布的纺粘非织造织物热粘合到污垢保持膜，化学保持膜，病原体保持膜或其组合来制备过滤介质的方法。 本发明还涉及一种或多种银涂布的纺粘非织造织物层作为微生物杀伤膜的组分在用于流体过滤系统的过滤介质中的用途。 本发明的过滤介质在使用时提供有效的消毒效果，保持低压降和高流速。 此外，过滤介质是无粘性的并且包含至少一个由纺粘非织造聚合物织物制成的热粘合层。 本发明还具有一种净水筒及其在饮用水系统中的应用。

公开(公告)号：US12195183B2

公开(公告)日：2025-01-14

申请号：US17530180

申请日：2021-11-18

Applicant: GOODRICH CORPORATION

Inventor： Jin Hu ,  Phi Doan

IPC: B64D11/02 ,  A01N33/12 ,  B05D3/02 ,  B05D3/10 ,  C09D5/14 ,  C23G1/08 ,  E03C1/04 ,  E03C1/10

Abstract: A method of manufacturing an aircraft metallic faucet with an anti-microbial coating may comprise: disposing the aircraft metallic faucet in a piranha solution; washing the aircraft metallic faucet; and coating a surface of the aircraft metallic faucet with a Si-Quat based coating. A method of manufacturing an aircraft metallic faucet with a hybrid anti-microbial coating with cross-linkers may comprise: disposing the aircraft metallic faucet in a piranha solution; washing the aircraft metallic faucet; coating a surface of the aircraft metallic faucet with a hybrid Si-Quat coating with crosslinkers; and curing the hybrid Si-Quat coating at a temperature between 60° C. (140° F.) and 100° C. (212° F.).

公开(公告)号：US20240417081A1

公开(公告)日：2024-12-19

申请号：US18336446

申请日：2023-06-16

Applicant: Goodrich Corporation

Inventor： Nathaniel Ching ,  Jin Hu ,  Galdemir C. Botura ,  Steven Kestler

IPC: B64D15/12 ,  H05B1/02

Abstract: The present disclosure provides for ice protection heater assemblies, and related methods of fabrication and use. More particularly, the present disclosure provides for chordwise ice protection heater assemblies for aircraft or the like. The heater assemblies provide that the heater zones for the ice protection heater assembly are designed such that the electricity mainly flows along the chord of the aircraft component (e.g., wing). This puts the electrical connection points above and below as well as behind the stagnation point of the aircraft component. The electrical connection points are thus behind the area to be protected from icing via the heater assembly.

公开(公告)号：US12104090B2

公开(公告)日：2024-10-01

申请号：US18178810

申请日：2023-03-06

Applicant: Goodrich Corporation

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

IPC: C09J11/04 ,  B64D15/00 ,  B64D15/12 ,  C08K3/08 ,  C08K3/22 ,  C09J5/06 ,  C09J7/38 ,  C09J9/02 ,  B64D33/02 ,  B82Y30/00 ,  C08K7/04 ,  C09J9/00 ,  C09J109/02 ,  C09J123/08 ,  C09J175/04

CPC classification number: C09J11/04 ,  B64D15/00 ,  B64D15/12 ,  C08K3/08 ,  C08K3/22 ,  C09J5/06 ,  C09J7/385 ,  C09J9/02 ,  B64D2033/0233 ,  B82Y30/00 ,  C08K2003/0856 ,  C08K2003/2265 ,  C08K7/04 ,  C08K2201/001 ,  C08K2201/011 ,  C09J7/38 ,  C09J9/00 ,  C09J109/02 ,  C09J123/0853 ,  C09J175/04 ,  C09J2203/35 ,  C09J2301/502

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：US20230322409A1

公开(公告)日：2023-10-12

申请号：US18332641

申请日：2023-06-09

Applicant: GOODRICH CORPORATION

Inventor： Casey M Slane ,  Jin Hu ,  Nathaniel Ching

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

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

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：US20230203666A1

公开(公告)日：2023-06-29

申请号：US17562194

申请日：2021-12-27

Applicant: Goodrich Corporation

Inventor： Jin Hu

IPC: C23C22/06 ,  C23C22/78 ,  C22C38/18

CPC classification number: C23C22/06 ,  C23C22/78 ,  C22C38/18

Abstract: Disclosed is a method of manufacturing a stainless steel component, the method including texturizing a stainless steel substrate by bead blasting to provide a texturized stainless steel. The stainless steel substrate includes grade 316 austenitic stainless steel. The method also includes treating the texturized stainless steel with a passivation solution to provide a passivated stainless steel. The method further includes treating the passivated stainless steel with an oxidizing solution including sulfuric acid and hydrogen peroxide at a temperature of about 130 to about 200 degrees Fahrenheit for at least 50 minutes to provide an antimicrobial stainless steel surface that is free of a separate coating. The method includes obtaining at least 99.9% E. coli reduction as measured by JIS Z 2801:2010 test on the antimicrobial stainless steel without a separate coating.