公开(公告)号：US10279886B2

公开(公告)日：2019-05-07

申请号：US15149966

申请日：2016-05-09

Applicant: Goodrich Corporation

Inventor： George Owens ,  Kevin E. Roach ,  Kurt M. Tauscher

IPC: B64D11/00 ,  B64C1/18 ,  B64C1/40 ,  B64D13/08 ,  F24D13/02 ,  B64C1/00

Abstract: An aircraft heated floor panel includes a first support layer, a second support layer, and a heating layer located between the first support layer and the second support layer. An aircraft floor panel includes a floor panel body and a removal feature that provides a mechanism for the aircraft floor panel to be removed from an attached aircraft structure.

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.

公开(公告)号：US20160340020A1

公开(公告)日：2016-11-24

申请号：US15149966

申请日：2016-05-09

Applicant: Goodrich Corporation

Inventor： George Owens ,  Kevin E. Roach ,  Kurt M. Tauscher

IPC: B64C1/18 ,  B64D13/08

CPC classification number: B64C1/18 ,  B64C1/40 ,  B64C2001/0072 ,  B64D13/08 ,  F24D13/024 ,  Y02B30/26

Abstract: An aircraft heated floor panel includes a first support layer, a second support layer, and a heating layer located between the first support layer and the second support layer. An aircraft floor panel includes a floor panel body and a removal feature that provides a mechanism for the aircraft floor panel to be removed from an attached aircraft structure.

Abstract translation: 飞机加热地板镶板包括第一支撑层，第二支撑层和位于第一支撑层和第二支撑层之间的加热层。 飞机地板镶板包括地板面板主体和移除特征，其提供用于飞行器地板面板从附接的飞行器结构中移除的机构。

公开(公告)号：US09623951B2

公开(公告)日：2017-04-18

申请号：US14179281

申请日：2014-02-12

Applicant: Goodrich Corporation

Inventor： Jin Hu ,  Richard R. Hamm ,  Kevin E. Roach

IPC: B60L1/02 ,  B64C1/18 ,  B64D13/00 ,  F24D13/02 ,  H05B3/16 ,  H05K3/38 ,  H05B3/26 ,  H05K3/12 ,  H05K1/16

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 of forming a heating element includes depositing a conductive ink of silver particles in an epoxy resin on a dielectric film to create a conductive circuit, and heat curing the conductive circuit to achieve a resistivity of the heating element less than 1.68×10−6 ohm·meter. An aircraft heated floor panel includes at least one floor panel of an aircraft includes a conductive circuit positioned within the floor panel having a conductive ink of silver particles in an epoxy resin on a dielectric film.

公开(公告)号：US20150053662A1

公开(公告)日：2015-02-26

申请号：US14179281

申请日：2014-02-12

Applicant: Goodrich Corporation

Inventor： Jin Hu ,  Richard R. Hamm ,  Kevin E. Roach

IPC: B64C1/18 ,  H05K3/12 ,  B64D13/00

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 of forming a heating element includes depositing a conductive ink of silver particles in an epoxy resin on a dielectric film to create a conductive circuit, and heat curing the conductive circuit to achieve a resistivity of the heating element less than 1.68×10−6 ohm·meter. An aircraft heated floor panel includes at least one floor panel of an aircraft includes a conductive circuit positioned within the floor panel having a conductive ink of silver particles in an epoxy resin on a dielectric film.

Abstract translation: 一种形成加热元件的方法包括在电介质膜上沉积环氧树脂中的银颗粒的导电油墨以产生导电电路，并对该导电电路进行加热固化，以达到加热元件的电阻率小于1.68×10-6 欧姆·米。 飞机加热地板镶板包括飞机的至少一个地板镶板，其包括位于地板镶板内的导电电路，其具有介电膜上的环氧树脂中的银颗粒的导电油墨。