公开(公告)号：US20180272648A1

公开(公告)日：2018-09-27

申请号：US15469098

申请日：2017-03-24

Applicant: GOODRICH CORPORATION

Inventor： Zhongfen Ding ,  Scott Alan Eastman ,  Michael Paul Humbert ,  Steven W. Gronda ,  Jacquelynn KM Garofano ,  Brian St. Rock ,  Christopher L. Chapman ,  Farzana Hussain

IPC: B32B3/26 ,  B32B7/12 ,  B32B15/04 ,  B32B9/00 ,  B32B27/06 ,  B32B21/14

CPC classification number: B32B3/266 ,  B32B7/12 ,  B32B9/007 ,  B32B15/04 ,  B32B21/14 ,  B32B27/06 ,  B32B2307/302 ,  B32B2307/3065 ,  B32B2607/00

Abstract: A veneer panel may comprise a face veneer, a thermally conductive layer, and a backing layer bonded to the thermally conductive layer. The thermally conductive layer may comprise a chemically treated thermally conductive layer. The chemically treated thermally conductive layer may comprise a plurality of first vinyl groups chemically bonded to a first surface of the chemically treated thermally conductive layer.

公开(公告)号：US20180186460A1

公开(公告)日：2018-07-05

申请号：US15397552

申请日：2017-01-03

Applicant: Goodrich Corporation

Inventor： Sameh Dardona ,  Marcin Piech ,  Jacquelynn KM Garofano ,  Ray-Sing Lin ,  Paul Sheedy ,  Wayde R. Schmidt

IPC: B64D15/12 ,  B33Y10/00 ,  B33Y80/00 ,  B33Y70/00 ,  C23C24/04 ,  C23C4/12

CPC classification number: B64D15/12 ,  B33Y10/00 ,  B33Y70/00 ,  B33Y80/00 ,  C23C4/12 ,  C23C24/04 ,  H05B3/12 ,  H05B3/262 ,  H05B3/265 ,  H05B3/267 ,  H05B2203/004 ,  H05B2203/013 ,  H05B2203/017 ,  H05B2214/02

Abstract: A multilayer structure for deicing an aircraft airfoil component includes an electrically and thermally insulating bottom layer formed in a defined pattern directly on the aircraft airfoil component, an electrothermal middle layer of electrically resistant heater element arrays formed in the defined pattern on the electrically and thermally insulating bottom layer, and a thermally conductive and electrically insulating top layer encapsulating the electrically and thermally insulating bottom layer and the electrothermal middle layer of electrically resistant heater element arrays. The multilayer structure may be directly applied to the airfoil component by direct writing/additive manufacturing, and may be done with the assistance of a multi-axis robot.