Aircraft throttle control device including an engaging roller coupling

Patent metadata

Field	Value
Publication number	US-9598177-B2
Application number	US-201013500861-A
Country	US
Kind code	B2
Filing date	Oct 5, 2010
Priority date	Oct 6, 2009
Publication date	Mar 21, 2017
Grant date	Mar 21, 2017

Abstract

An aeroengine control device comprising a mount, having pivotally mounted thereon a code wheel together with a main lever and a secondary lever, both for turning the code wheel, each lever being movable between a rest position and a maximum actuation position, the secondary lever being mounted to pivot on the main lever. A connecting rod connects the secondary lever in permanent manner to the code wheel and the main lever is provided with a connection member arranged to co-operate with a portion in relief secured to the code wheel and with a portion in relief secured to the mount in such a manner that the connection member attaches to the code wheel when the main lever is moved while the secondary lever is in its rest position and attaches to the mount, thereby releasing the code wheel to turn, when the secondary lever is moved while the main lever is in its rest position, while movement of either lever is prevented when the other lever is away from its rest position.

First claim

What is claimed is:

1. An aeroengine control device comprising both a mount, having pivotally mounted thereon a code wheel together with a main lever and a secondary lever, both for turning the code wheel, each lever being movable between a rest position and a maximum actuation position, the secondary lever being mounted to pivot on the main lever, wherein a connecting rod connects the secondary lever to the code wheel in permanent manner, and wherein the main lever is provided with a connection member arranged to co-operate with a notch secured to the code wheel and a notch secured to the mount in such a manner that the connection member attaches to the code wheel when the main lever is moved while the secondary lever is in the rest position and attaches to the mount while releasing rotation of the code wheel when the secondary lever is moved while the main lever is in the rest position, with movement of either lever being prevented when the other lever is away from its rest position.

2. The device according to claim 1 , wherein the connection member comprises an arm having one end hinged to the main lever and a free end arranged to co-operate with the notches.

3. The device according to claim 1 , wherein the connection member is received between two walls that extend in circular arcs about the axis of the code wheel, one of them being secured to the code wheel and the other to the mount, the walls being spaced apart from each other and each including one of the notches for receiving a portion of the connection member in such a manner that turning of the code wheel relative to the mount is possible only when the connection member is received in one of the notches, the notches facing each other when the code wheel is in its position that is common to both of the levers being in their rest positions.

4. The device according to claim 3 , wherein the connection member is urged resiliently against the wall secured to the code wheel.

5. The device according to claim 3 , wherein the connection member is provided with at least one wheel mounted to rotate about an axis parallel to the axis of rotation of the code wheel.

6. The device according to claim 5 , wherein the connection member is provided with two wheels mounted to pivot about respective axes parallel to the axis of rotation of the code wheel and in alignment in a direction that is substantially radial relative to the code wheel.

7. The device according to claim 6 , wherein the wheels are movable relative to each other parallel to the substantially radial direction and are urged resiliently towards a position in which they are spaced apart from each other.

8. The device according to claim 3 , wherein the notches include ramps defining transition zones in the vicinity of the rest position such that when a first one of the levers is in the transition zone, movement of the other lever towards its maximum actuation position causes the first lever to return to its rest position.

9. The device according to claim 1 , wherein the connection member includes at least one element that is movable in translation in a direction that is substantially radial relative to the code wheel.

10. The device according to claim 1 , wherein the main lever is mounted to pivot about the axis of the code wheel.

11. The device according to claim 1 , wherein the connection member comprises at least a ring segment surrounding the code wheel and being received between a peripheral surface of the code wheel and a wall of the mount surrounding the ring segment, the ring segment slidably receiving at least one pin having ends arranged to co-operate with the notches formed in the code wheel and with the wall of the mount in order to secure the ring segment in rotation selectively with the code wheel or with the wall of the mount.

12. The device according to claim 11 , having two pins, one performing a locking function and the other performing a function of returning to the rest position when in the transition zone in co-operation with the corresponding notches.

13. The device according to claim 11 , wherein the notches include ramps defining transition zones in the vicinity of the rest position such that when a first one of the levers is in the transition zone, movement of the other lever towards its maximum actuation position causes the first lever to return to its rest position.

14. The device according to claim 1 , including definition means for defining controlled force relationships and/or movement relationships for automatically returning at least one of the levers to its rest position.

15. The device according to claim 14 , wherein said definition means comprise profiles of the notches.

16. The device according to claim 1 , wherein the main lever has two plates with the secondary lever and the connecting rod being mounted between them.

17. The device according to claim 1 , wherein the assembly comprising the code wheel and the levers is associated with friction means acting in the vicinity of the axis or in the vicinity of the outer periphery of the code wheel.

18. The device according to claim 1 , wherein the connection member is urged resiliently against a wall secured to the code wheel and provided with one of the notches.

19. The device according to claim 1 , wherein the connection member is provided with at least one wheel mounted to rotate about an axis parallel to the axis of rotation of the code wheel.

Assignees

• Elabellaoui Hafid
• Besold Jean-Eric
• Besold Marie-Noël
• Besold Aurélie
• Besold Stéphanie
• Besold Antoine
• Pautard Sébasiten
• Engler David
• Merlet Etienne
• Sagem Defense Securite

Inventors

• Elabellaoui Hafid
• Besold Jean-Eric
• Pautard Sébasiten
• Engler David
• Merlet Etienne

Classifications

• B64D31/06 Primary

  actuated automatically · CPC title

• B64D31/04 Primary

  actuated personally · CPC title

• Y10T74/20238

  Interlocked · CPC title