公开(公告)号：US12188511B2

公开(公告)日：2025-01-07

申请号：US17702612

申请日：2022-03-23

Applicant: THE BOEING COMPANY

Inventor： Samuel L. Block ,  Colin L Farr

IPC: F16B37/14 ,  B64F5/10 ,  F16B43/00 ,  F16B39/28

Abstract: A nut cap assembly for securing an internal component to an external component includes a seal cap having a base and a shroud extending from the base. The base includes a mounting flange configured to be mounted to the internal component. The base includes an opening at a mounting end of the base configured to be mounted to the internal component. The base includes a seal groove surrounding the opening configured to receive a seal. The seal groove is open at the mounting end to interface the seal with the internal component. The shroud includes a nut pocket has a cap anti-rotation feature. The nut cap assembly includes a nut received in the nut pocket. The nut includes a threaded bore configured to threadably receive a threaded fastener used to secure the internal component to the external component. The nut includes a nut anti-rotation feature interfacing with the cap anti-rotation feature.