公开(公告)号：US20240300653A1

公开(公告)日：2024-09-12

申请号：US18323630

申请日：2023-05-25

Applicant: Goodrich Corporation

Inventor： Anvith BG Gopinath Gowda ,  Shyam Kumar Dattatri ,  Rhushikesh Patil

IPC: B64D15/16 ,  B64F5/10

CPC classification number: B64D15/166 ,  B64F5/10

Abstract: The present disclosure provides for pneumatic deicer boot assemblies, and related methods of fabrication and use. More particularly, the present disclosure provides for bartack stitched pneumatic deicer boot assemblies for aircraft or the like, with the bartack stitched pneumatic deicer boot assemblies having an inflatable carcass formed by two layers (e.g., a stretchable layer and a non-stretchable layer) stitched together using bartack stitches.

公开(公告)号：US12110118B2

公开(公告)日：2024-10-08

申请号：US17859416

申请日：2022-07-07

Applicant: GOODRICH CORPORATION

Inventor： Shyam Kumar Dattatri ,  Harish Venkateshaiah ,  Rhushikesh Patil ,  Harshavardhana Nanjundegowda

IPC: B64D15/16 ,  B29C65/14 ,  B32B3/08 ,  B32B7/12 ,  B32B27/12 ,  B32B27/34 ,  B29L22/02

CPC classification number: B64D15/166 ,  B29C65/1412 ,  B29C65/1432 ,  B29C65/1438 ,  B32B3/08 ,  B32B7/12 ,  B32B27/12 ,  B32B27/34 ,  B29L2022/02 ,  B32B2250/04 ,  B32B2255/02 ,  B32B2255/26 ,  B32B2255/28 ,  B32B2307/51 ,  B32B2605/18

Abstract: Ice may form along the leading edge of an aircraft wing or horizontal and vertical stabilizers. A pneumatic deicer system may be configured to inflate and dislodge ice along the leading edge of lift and control surfaces. The pneumatic deicer system may comprise a laser welded deicing boot attached to the leading edge. The compressed air can be directed to the deicing boot, inflating the deicing boot along inflatable tubes formed by laser welds, which can crack and dislodge the ice. A method of manufacturing a laser welded pneumatic deicer boot is also disclosed.

公开(公告)号：US20230312112A1

公开(公告)日：2023-10-05

申请号：US17859416

申请日：2022-07-07

Applicant: GOODRICH CORPORATION

Inventor： Shyam Kumar Dattatri ,  Harish Venkateshaiah ,  Rhushikesh Patil ,  Harshavardhana Nanjundegowda

IPC: B64D15/16 ,  B32B27/12 ,  B32B27/34 ,  B32B3/08 ,  B32B7/12 ,  B29C65/14

CPC classification number: B64D15/166 ,  B32B27/12 ,  B32B27/34 ,  B32B3/08 ,  B32B7/12 ,  B29C65/1412 ,  B29C65/1438 ,  B29C65/1432 ,  B32B2255/02 ,  B32B2255/28 ,  B32B2255/26 ,  B29L2022/02

Abstract: Ice may form along the leading edge of an aircraft wing or horizontal and vertical stabilizers. A pneumatic deicer system may be configured to inflate and dislodge ice along the leading edge of lift and control surfaces. The pneumatic deicer system may comprise a laser welded deicing boot attached to the leading edge. The compressed air can be directed to the deicing boot, inflating the deicing boot along inflatable tubes formed by laser welds, which can crack and dislodge the ice. A method of manufacturing a laser welded pneumatic deicer boot is also disclosed.

公开(公告)号：US20250042556A1

公开(公告)日：2025-02-06

申请号：US18788756

申请日：2024-07-30

Applicant: Goodrich Corporation

Inventor： Sugumaran Selvaraj ,  Shyam Kumar Dattatri ,  Manjunath Hiremath ,  Rhushikesh Patil

IPC: B64D15/12 ,  B64D15/16 ,  B64D15/22

Abstract: A target material removal (TMR) element is provided and includes a body region; thermal elements within the body region; and vibration elements within the body region. The TMR element is controlled to perform TMR operations that include one or more of the thermal elements generating heat that is transmitted through the body region to a target material in a manner that defines one or more zones of the target material. The TMR operations further include, subsequent to the one or more of the thermal elements beginning generating the heat that is transmitted through the body region to the target material, the one or more of the vibration elements generating vibrations that are transmitted through the body region to the one or more zones of the target material.