Patent · US Active

Metallic lined trunnion bearing for aircraft landing gear

US10724575B2 · kind B2 · utility

4Cited by
48References
15Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJun 22, 2018
Grant dateJul 28, 2020
Priority date
Expiry dateJun 22, 2038

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF16C2326/43
  • WIPO fieldMechanical elements
  • WIPO sectorMechanical engineering

Abstract

A trunnion bearing includes an inner ring that has a first exterior surface and a first interior surface. The first exterior surface has a spherical contour. The trunnion bearing includes an outer ring that has a second interior surface and a second exterior surface. The second interior surface has a spherical contour. The inner ring is disposed at least partially in the outer ring. A metallic liner made of a copper based alloy is disposed between the first exterior surface of the inner ring and the second interior surface of the outer ring. The inner ring and/or the outer ring are made from a titanium based alloy.

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