公开(公告)号：US20220295601A1

公开(公告)日：2022-09-15

申请号：US17752806

申请日：2022-05-24

Applicant: Goodrich Corporation

Inventor： George F. Owens ,  Kevin Edward Roach ,  James A. Mullen ,  Michael John 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 ,  B64D13/08 ,  F24D13/02 ,  B32B3/12 ,  B32B7/12 ,  B32B15/20 ,  B64C1/18 ,  H01C17/06

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：US11274853B2

公开(公告)日：2022-03-15

申请号：US16160417

申请日：2018-10-15

Applicant: Goodrich Corporation

Inventor： Kevin Edward Roach ,  Maureen Elkins ,  Joseph Winesdoerffer

IPC: H05B3/06 ,  H05B3/16 ,  H05B3/46 ,  H05B3/58 ,  F24H1/14 ,  F24H9/06 ,  B33Y80/00 ,  F24H9/00 ,  H05B3/12

Abstract: A heater for an aircraft component includes a plurality of layers of an additively manufactured conductive ink. The conductive ink is printed on the heater surface, either on a substrate or directly. The heater is protected by a closeout material.

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.