Aircraft landing gear pitch trimmer actuator with variable damping

Patent metadata

Field	Value
Publication number	US-9994309-B2
Application number	US-201414765448-A
Country	US
Kind code	B2
Filing date	Feb 4, 2014
Priority date	Feb 4, 2013
Publication date	Jun 12, 2018
Grant date	Jun 12, 2018

Abstract

A pitch trimmer assembly for an aircraft landing gear having a damping element arranged to be connected between a first and a second element of an aircraft landing gear and arranged to exert a first damping force when in a first state and a second damping force in a second state, the damping element being switchable between the first and second states in dependence on the relative positions of the first and second landing gear elements.

First claim

The invention claimed is:

1. A pitch trimmer assembly for an aircraft landing gear, the pitch trimmer assembly including a telescopic pitch trimmer actuator arranged to be connected between a first element of the aircraft landing gear and a second element of the aircraft landing gear, the pitch trimmer actuator being arranged to exert a first damping force when in a first state in which the pitch trimmer actuator is not fully retracted and a second damping force greater than the first damping force when in a second state in which the pitch trimmer actuator is fully retracted, the pitch trimmer actuator being switchable between the first state and the second state in dependence on the relative positions of the first element of the landing gear and the second element of the landing gear;
wherein the pitch trimmer assembly includes a valve arranged to modify the flow of a damping fluid within the pitch trimmer actuator to place the pitch trimmer actuator into the second state when a valve actuating element is in a compressed state, and wherein the pitch trimmer assembly further comprises a first articulation link and a second articulation link pivotally connected adjacent an end of the pitch trimmer actuator, the valve actuating element being arranged to be compressed by one of the first articulation link and the second articulation link when first articulation link and the second articulation link are within a predetermined range of relative configurations.

2. The pitch trimmer assembly according to claim 1 , wherein the predetermined range of relative configurations is arranged to occur when the pitch trimmer actuator is retracted and the first articulation link and the second articulation link are at an angle to one another that is less than a predefined value.

3. An aircraft landing gear comprising a telescopic strut and the pitch trimmer assembly according to claim 1 connected to the telescopic strut.

4. The pitch trimmer assembly according to claim 1 , wherein the first element comprises a sliding tube upper portion of the landing gear, and the second element comprises a first articulation link pivotally connected to the sliding tube upper portion.

5. The pitch trimmer assembly according to claim 1 , wherein the first element comprises a sliding tube upper portion of the landing gear, and the second element comprises a bogie beam pivotally mounted to the end of a sliding tube lower portion that is telescopically connected to the sliding tube upper portion.

6. A landing gear comprising: a first element; a second element operatively connected to the first element; and
a pitch trimmer assembly, the pitch trimmer assembly including a telescopic pitch trimmer actuator connected between the first element and the second element, the pitch trimmer actuator being arranged to exert a first damping force when in a first damping state in which the pitch trimmer actuator is not fully retracted and a second damping force greater than the first damping force when in a second damping state in which the pitch trimmer actuator is fully retracted, the pitch trimmer actuator being switchable between the first damping state and the second damping state in dependence on the relative positions of the first element and the second element;
wherein the pitch trimmer assembly includes a valve arranged to modify the flow of a damping fluid within the pitch trimmer actuator to place the pitch trimmer actuator into the second damping state when a valve actuating element is in a compressed state, and wherein the pitch trimmer assembly further comprises a first articulation link and a second articulation link pivotally connected adjacent an end of the pitch trimmer actuator, the valve actuating element being arranged to be compressed by one of the first articulation link and the second articulation link when first articulation link and the second articulation link are within a predetermined range of relative configurations.

7. The landing gear of claim 6 , wherein the first element comprises a sliding tube upper portion and the second element comprises a bogie beam, the bogie beam being pivotally mounted to the end of a sliding tube lower portion that is telescopically connected to the sliding tube upper portion.

8. The landing gear of claim 7 , wherein the first articulation link is pivotally connected to one of the sliding tube upper portion and the bogie beam, and the second articulation link is pivotally connected to the other of the sliding tube upper portion and the bogie beam.

9. The landing gear of claim 8 , wherein the pitch trimmer actuator comprises a telescoping link that is pivotally connected at a first end to the sliding tube upper portion and pivotally connected at a second end to the first articulation link.

10. The landing gear of claim 9 , wherein the pitch trimmer actuator comprises a valve that is operated by contact with an anvil on the second articulation link when the bogie beam reaches a predetermined angle with respect to the sliding tube upper portion.

11. The landing gear of claim 6 , wherein the first element comprises a sliding tube upper portion, and the first articulation link is pivotally connected to the sliding tube upper portion.

12. A landing gear comprising:
a sliding tube upper portion;
a sliding tube lower portion telescopically connected to the sliding tube upper portion;
a bogie beam pivotally mounted to an end of the sliding tube lower portion;
a pitch trimmer assembly comprising:
a first articulation link pivotally connected to a second articulation link, the first articulation link further being pivotally connected to one of the sliding tube upper portion and the bogie beam, and the second articulation link further being pivotally connected to the other of the sliding tube upper portion and the bogie beam,
a telescopic pitch trimmer actuator that is pivotally connected at a first end to the sliding tube upper portion and pivotally connected at a second end to the first articulation link, the pitch trimmer actuator being arranged to exert a first damping force when in a first damping state and a second damping force greater than the first damping force when in a second damping state, the pitch trimmer actuator being switchable between the first damping state and the second damping state in dependence on a state of retraction of the pitch trimmer actuator and the relative positions of the sliding tube upper portion and the bogie beam, and wherein the pitch trimmer actuator comprises a valve that is operated by contact with an anvil on the second articulation link when the bogie beam reaches a predetermined angle with respect to the sliding tube upper portion.

Assignees

• Safran Landing Systems Uk Ltd
• Safran Landing Systems Uk Ltd

Inventors

• Hodgkinson Ben
• Schmidt R Kyle
• Smart David

Classifications

• B64C25/34 Primary

  wheeled type, e.g. multi-wheeled bogies · CPC title

• F16F9/10

  using liquid only; using a fluid of which the nature is immaterial · CPC title

• B64C25/60 Primary

  Oleo legs · CPC title

• F16F9/34

  Special valve constructions ({F16F9/44, F16F9/50 take precedence; filtering details F16F9/3285} ; valves in general F16K); Shape or construction of throttling passages · CPC title

• B64C25/58

  Arrangements or adaptations of shock-absorbers or springs (shimmy-dampers B64C25/50) · CPC title