IP Library › Granted Patent US 10,974,821
Granted Patent B2
US 10,974,821 · App. 15/676,261 · Granted Apr 13, 2021

Aircraft undercarriage fitted with a shimmy-attenuator device

Inventors: Nicolas Nguyen (Velizy Villacoublay, FR); Laurent Mallet (Toulon, FR); Frédéric Ivaldi (Toulon, FR); Thierry Blanpain (Velizy Villacoublay, FR); Philippe Henrion (Velizy Villacoublay, FR)
Assignee: SAFRAN LANDING SYSTEMS
B64C25/505
View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 10,974,821
App. No.
15/676,261
Granted
Apr 13, 2021
Kind
B2
Abstract

An aircraft undercarriage having a sliding rod slidably mounted in a strut-leg, and a scissors linkage ( 4 ) having one branch ( 4 a ) hinged to the strut-leg or to a turning element of a control for steering the sliding rod mounted to turn in the strut-leg, and one branch ( 4 b ) hinged to the sliding rod, the branches being hinged to each other by a pivot pin ( 12 ), the undercarriage being fitted with a shimmy-attenuator device ( 10 a, 10 b ) placed on the pivot pin of the shimmy-attenuator, the attenuator device including threshold resilient return means generating a force returning the branches towards a rest position, and at least damping means generating a damping force when the branches move axially along the pivot pin. The attenuator device comprises two modules ( 10 a, 10 b ) placed on either side of the scissors linkage in order to co-operate with the pivot pin, each of the modules performing at least one of the damping function and the threshold resilient return function.

Claims (11)

1. An aircraft undercarriage comprising:

a sliding rod slidably mounted in a strut-leg,

a scissors linkage having one branch hinged to the strut-leg or to a turning element of a control for steering the sliding rod mounted to turn in the strut-leg, and one branch hinged to the sliding rod, the branches being hinged to each other by a pivot pin, and

a shimmy-attenuator device placed on the pivot pin of the scissors linkage,

wherein the shimmy-attenuator device includes threshold resilient return means generating a force returning the branches towards a rest position, and at least damping means generating a damping force when the branches move axially along the pivot pin, and

wherein the attenuator device comprises two modules placed on either side of the scissors linkage and arranged directly at opposite ends of the pivot pin, each of the modules performing at least one of the damping function and the threshold resilient return function.

2. An undercarriage according to claim 1 , wherein one of the modules performs the threshold resilient return function and the other module performs the damping function.

3. The undercarriage according to claim 2 , wherein the module that performs the threshold resilient return function comprises a cage containing two series of Belleville washers mounted in opposition and held captive on the pivot pin by means of a terminal nut serving to prestress the washers.

4. The undercarriage according to claim 2 , wherein the module that performs the damping function comprises a piston secured to the pivot pin and defining two chambers filled with hydraulic fluid and put into fluid flow communication via a throttling orifice.

5. The undercarriage according to claim 1 , wherein the two modules are identical and both perform the threshold resilient return function and the damping function.

6. The undercarriage according to claim 5 , wherein each of the modules includes a cage fitted with prestress elastomer washers having viscoelastic properties that perform both the threshold resilient return function and also the damping function.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Nov 15, 2017
From: NGUYEN, NICOLAS; MALLET, LAURENT; IVALDI, FREDERIC; BLANPAIN, THIERRY; HENRION, PHILIPPE
To: SAFRAN LANDING SYSTEMS
Reel/Frame 044455/0495 →
Priority Claims (1)
FR 16 59340 · Sep 29, 2016 · national
Continuity (1)
Related Publication 20180086440A1 · Mar 29, 2018
Cited By (1)
US 12,637,205