Pin joint assembly

Patent metadata

Field	Value
Publication number	US-9863455-B2
Application number	US-201414761142-A
Country	US
Kind code	B2
Filing date	Jan 13, 2014
Priority date	Jan 18, 2013
Publication date	Jan 9, 2018
Grant date	Jan 9, 2018

Abstract

A pin joint assembly for an aircraft landing gear having an elongate joint pin; at least one first lug through which the joint pin passes; and at least one second lug through which the joint pin passes. The joint pin assembly includes first and second retaining elements located at opposite ends of the joint pin and arranged to maintain the location of the joint pin relative to the first and second lugs. At least portion of the pin joint assembly is elastically deformable.

First claim

The invention claimed is:

1. A pin joint assembly for an aircraft landing gear comprising:
an elongate joint pin;
at least one first lug through which the joint pin passes, the first lug having a first lug portion bearing on a first part of the joint pin and a second lug portion bearing on a second part of the joint pin, the second part being spaced from the first part;
at least one second lug through which the joint pin passes, the second lug bearing on a third part of the joint pin independently of the first lug, the third part being between and separate from the first part and the second part; and
first and second retaining elements located at opposite ends of the joint pin and arranged to maintain the location of the joint pin relative to the first and second lugs;
wherein at least a portion of the pin joint assembly is elastically deformable.

2. The pin joint assembly according to claim 1 , wherein one or more of the first and second retaining elements is elastically deformable.

3. The pin joint assembly according to claim 2 , at least one of the first and second retaining elements comprises an elastically deformable flat plate.

4. The pin joint assembly according to claim 3 , wherein the elastically deformable flat plate has a thickness along a longitudinal axis of the joint pin of about 3 millimeters.

5. The pin joint assembly according to claim 1 , wherein the first and second retaining elements are secured to the pin joint assembly by one or more retaining bolts extending through the joint pin in a direction parallel to a longitudinal axis of the joint pin.

6. The pin joint assembly according to claim 5 , wherein the one or more retaining bolts are elastically deformable in a direction parallel to their longitudinal axis.

7. The pin joint assembly according to claim 5 , wherein at least one of the first and second retaining elements comprises an end cap secured to one of the one or more retaining bolts.

8. The pin joint assembly according to claim 7 , wherein one or more of the end caps are secured to the joint pin by a retaining nut threaded to a portion of the one or more retaining bolts passing through the or each respective end cap.

9. The pin joint assembly according to claim 1 , wherein one or more of the retaining elements comprise steel, aluminium or titanium.

10. The pin joint assembly according to claim 1 , wherein the elongate joint pin comprises fibre reinforced composite.

11. The pin joint assembly according to claim 1 , wherein one or more of the retaining elements has an axial thickness of less than 5 millimetres.

12. An aircraft landing gear comprising a pin joint assembly according claim 1 .

Assignees

• Safran Landing Systems Uk Ltd

Inventors

• Green Chris

Classifications

• F16C2326/43

  Aeroplanes; Helicopters · CPC title

• F16B19/02 Primary

  Bolts or sleeves for positioning of machine parts, e.g. notched taper pins, fitting pins, sleeves, eccentric positioning rings · CPC title

• Y10T24/4698

  Movably connected to penetrating portion · CPC title

• F16C25/04

  self-adjusting · CPC title

• F16C11/045

  with at least a pair of arms pivoting relatively to at least one other arm, all arms being mounted on one pin (crank-pins F16C11/02) · CPC title