公开(公告)号：US20180305031A1

公开(公告)日：2018-10-25

申请号：US15903656

申请日：2018-02-23

Applicant: Goodrich Corporation

Inventor： Alan J. Fahrner ,  Andrew Taylor ,  James Putt

IPC: B64D15/16 ,  D05B93/00

Abstract: A de-icing assembly for a surface of an aircraft includes a carcass, seams, inflation passages, a manifold, and a reinforcement stitchline. The carcass includes a first layer, a second layer, and a carcass centerline. The seams are sewn into the carcass and join the first and second layers of the carcass together. The inflation passages are formed by the seams and are disposed between the first and second layers of the carcass. The manifold includes a width and a manifold centerline oriented approximately perpendicular to the carcass centerline and is fluidly connected to and is disposed beneath the carcass. The first reinforcement stitchline is sewn into the carcass adjacent to one of the plurality of seams and is disposed at a location on the carcass overlapping with the manifold. The first reinforcement stitchline is disposed approximately perpendicular to the manifold centerline and extends across the width of the manifold.

公开(公告)号：US10780984B2

公开(公告)日：2020-09-22

申请号：US15903656

申请日：2018-02-23

Applicant: Goodrich Corporation

Inventor： Alan J. Fahrner ,  Andrew Taylor ,  James Putt

IPC: B64D15/16 ,  D05B93/00

Abstract: A de-icing assembly for a surface of an aircraft includes a carcass, seams, inflation passages, a manifold, and a reinforcement stitchline. The carcass includes a first layer, a second layer, and a carcass centerline. The seams are sewn into the carcass and join the first and second layers of the carcass together. The inflation passages are formed by the seams and are disposed between the first and second layers of the carcass. The manifold includes a width and a manifold centerline oriented approximately perpendicular to the carcass centerline and is fluidly connected to and is disposed beneath the carcass. The first reinforcement stitchline is sewn into the carcass adjacent to one of the plurality of seams and is disposed at a location on the carcass overlapping with the manifold. The first reinforcement stitchline is disposed approximately perpendicular to the manifold centerline and extends across the width of the manifold.