Patent · US Active

Yoke installation protection assembly with integrated inclinometer portion

US10875629B2 · kind B2 · utility

0Cited by
5References
20Claims
0Family size

Assignee

Inventors

Key dates

Filing dateApr 2, 2018
Grant dateDec 29, 2020
Priority date
Expiry dateMar 21, 2039

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB64F5/10
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

Yoke alignment assemblies, aircraft, and rigid covers are provided. An aircraft includes a yoke alignment assembly. A yoke alignment assembly is provided for aligning an aircraft yoke with a column. The yoke alignment assembly includes a rigid cover and a flexible cover. The rigid cover defines a protective portion configured to protect the yoke. The inclinometer portion is configured to hold an inclinometer. The flexible cover is secured to an upper part of the protective portion and is configured to protect the yoke.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.