公开(公告)号：US20190185168A1

公开(公告)日：2019-06-20

申请号：US15845428

申请日：2017-12-18

Applicant: Goodrich Corporation

Inventor： James R. Hunter ,  Galdemir Cezar Botura ,  Samual Steven Riczo Schomer ,  Alan J. Fahrner ,  Kurt M. Tauscher

IPC: B64D15/16 ,  B32B7/08

CPC classification number: B64D15/166 ,  B32B7/08 ,  B32B2250/02 ,  B32B2605/18

Abstract: A de-icing assembly for a surface of an aircraft includes a carcass with a first layer and a second layer, a plurality of seams sewn into the carcass, and a bonded region. The plurality of seams join the first and second layers of the carcass together. Each of the plurality of seams comprises two or more stitchlines. The bonded region is disposed between the two or more stitchlines and seals a portion of the first layer of the carcass to a portion of the second layer of the carcass.

公开(公告)号：US10780983B2

公开(公告)日：2020-09-22

申请号：US15845428

申请日：2017-12-18

Applicant: Goodrich Corporation

Inventor： James R. Hunter ,  Galdemir Cezar Botura ,  Samual Steven Riczo Schomer ,  Alan J. Fahrner ,  Kurt M. Tauscher

IPC: B64D15/16 ,  B32B7/08

Abstract: A de-icing assembly for a surface of an aircraft includes a carcass with a first layer and a second layer, a plurality of seams sewn into the carcass, and a bonded region. The plurality of seams join the first and second layers of the carcass together. Each of the plurality of seams comprises two or more stitchlines. The bonded region is disposed between the two or more stitchlines and seals a portion of the first layer of the carcass to a portion of the second layer of the carcass.

公开(公告)号：US20170273148A1

公开(公告)日：2017-09-21

申请号：US15442752

申请日：2017-02-27

Applicant: Goodrich Corporation

Inventor： Samual Steven Riczo Schomer ,  Alan J. Fahrner ,  Kurt M. Tauscher ,  Andrew Taylor ,  James R. Hunter ,  David L. Brittingham

IPC: H05B6/62 ,  B64F5/10 ,  B64D15/16 ,  B29C65/04 ,  B29C65/00

CPC classification number: H05B6/62 ,  B29C65/04 ,  B29C65/08 ,  B29C65/1403 ,  B29C65/1467 ,  B29C65/62 ,  B29C66/1122 ,  B29C66/244 ,  B29C66/438 ,  B29C66/439 ,  B29C66/81417 ,  B29C66/81427 ,  B29C66/8322 ,  B29L2022/02 ,  B29L2024/006 ,  B29L2031/3076 ,  B64D15/166 ,  B64D2033/0233 ,  B64F5/10

Abstract: A die-welding system for a de-icer assembly includes a die, a die base, a high energy source, and a de-icer assembly. The de-icer assembly includes a first welded-material layer and a second welded-material layer. At least one of the die and the die base includes a welded-portion pattern thereon configured to weld the first welded-material layer to the second welded-material layer in the pattern of the welded-portion pattern such that inflatable portions are formed within the welded-portion pattern formed in the de-icer assembly between non-welded sections of the first welded-material layer and the second welded-material layer.

公开(公告)号：US20170266869A1

公开(公告)日：2017-09-21

申请号：US15442772

申请日：2017-02-27

Applicant: Goodrich Corporation

Inventor： Samuel Steven Riczo Schomer ,  Alan J. Fahrner ,  Kurt M. Tauscher ,  Andrew Taylor ,  James R. Hunter ,  David L. Brittingham

IPC: B29C65/04 ,  B64D15/16 ,  B29C65/00

CPC classification number: B29C65/04 ,  B29C65/08 ,  B29C65/1403 ,  B29C65/1467 ,  B29C65/62 ,  B29C66/1122 ,  B29C66/244 ,  B29C66/438 ,  B29C66/439 ,  B29C66/71 ,  B29C66/7392 ,  B29C66/81417 ,  B29C66/81427 ,  B29C66/8322 ,  B29L2022/02 ,  B29L2024/006 ,  B29L2031/3076 ,  B64D15/166 ,  B64D2033/0233 ,  B29K2021/00 ,  B29K2011/00 ,  B29K2021/006 ,  B29K2007/00 ,  B29K2075/00

Abstract: A method of manufacturing a de-icer assembly includes positioning a first welded-material layer and a second welded-material layer between a die and a die base of a die-based welding system, wherein at least one of the die and the die base includes a welded-portion pattern configured to weld the first welded-material layer to the second welded-material layer in the pattern such that inflatable portions are formed within the welded-portion pattern formed in the de-icer assembly between non-welded sections of the first welded-material layer and the second welded-material layer, pressing the first welded-material layer and the second welded-material layer together between the die and die base, and applying high energy to the die-based welding system using a high energy source such that the first welded-material layer and the second welded-material layer are welded together at the areas in the shape of the welded-portion pattern to form a welded de-icer assembly.

公开(公告)号：US20170266753A1

公开(公告)日：2017-09-21

申请号：US15442785

申请日：2017-02-27

Applicant: Goodrich Corporation

Inventor： Samual Steven Riczo Schomer ,  Alan J. Fahrner ,  Kurt M. Tauscher ,  Andrew Taylor ,  James R. Hunter ,  David L. Brittingham

IPC: B23K20/10 ,  B64D15/16 ,  B64F5/10

CPC classification number: B23K20/10 ,  B29C65/04 ,  B29C65/08 ,  B29C65/1403 ,  B29C65/1467 ,  B29C65/62 ,  B29C66/1122 ,  B29C66/232 ,  B29C66/244 ,  B29C66/438 ,  B29C66/71 ,  B29C66/7292 ,  B29C66/81417 ,  B29C66/81427 ,  B29C66/8322 ,  B29L2022/02 ,  B29L2024/006 ,  B29L2031/3076 ,  B64D15/166 ,  B64F5/10 ,  B29K2021/00

Abstract: A method of manufacturing a de-icer assembly includes disposing a first welded-material layer and a second welded-material layer beneath a horn of a horn-based welding system, controlling the horn to move along a welded-portion pattern configured to weld the first welded-material layer to the second welded-material layer in the pattern of the welded-portion pattern such that inflatable portions are formed within the welded-portion pattern formed in the de-icer assembly between non-welded sections of the first welded-material layer and the second welded-material layer, and applying high-frequency energy to the first welded-material layer and a second welded-material layer using the horn such that the first welded-material layer and the second welded-material layer are welded together at areas in the shape of the welded-portion pattern to form a welded de-icer assembly.