公开(公告)号：US11912415B2

公开(公告)日：2024-02-27

申请号：US17587832

申请日：2022-01-28

Applicant: Textron Aviation Inc.

Inventor： Todd Alan Thisius ,  Tim Todd Razey

IPC: B64D11/06 ,  B60N2/07 ,  B60N2/015 ,  B60N2/005

CPC classification number: B64D11/0696 ,  B60N2/005 ,  B60N2/01516 ,  B60N2/0715 ,  B60N2/0722

Abstract: A vibration-reducing insert is usable to reduce vibration or play between two metal aircraft components. The insert rotates on a fastener, and includes a shelf that projects into the gap and operates as an indexable cam to establish an appropriate compression in an engaged portion of the shelf.

公开(公告)号：US20220242577A1

公开(公告)日：2022-08-04

申请号：US17587832

申请日：2022-01-28

Applicant: Textron Aviation Inc.

Inventor： Todd Alan Thisius ,  Tim Todd Razey

IPC: B64D11/06 ,  B60N2/015 ,  B60N2/07

Abstract: A vibration-reducing insert is usable to reduce vibration or play between two metal aircraft components. The insert rotates on a fastener, and includes a shelf that projects into the gap and operates as an indexable cam to establish an appropriate compression in an engaged portion of the shelf.