IP Library › Granted Patent US 9,845,853
Granted Patent B2
US 9,845,853 · App. 14/601,695 · Granted Dec 19, 2017

Linear electromechanical actuator and anti-jamming device

Inventors: Eduardo Chamorro Gonzalez-Tablas (Getafe, ES); Francisco Jose Aguado Lopez (Getafe, ES); Esteban Morante Lopez (Getafe, ES); Andres Jimenez Olazabal (Getafe, ES)
Assignee: CESA, Compania Espanola de Sistemas Aeronauticos, S.A.
F16H25/205B64C13/28B64C13/42B64C13/50B64C25/20B64C25/24F16H25/20G01L3/26F16H2025/2071Y02T50/44Y10T74/186
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Quick Facts
Patent No.
US 9,845,853
App. No.
14/601,695
Granted
Dec 19, 2017
Kind
B2
Abstract

A linear electromechanical actuator with a main screw-nut assembly driven by a main motion device and having a hollow screw with an abutting surface; an anti-jamming piston arranged coaxially within the screw and shiftable between an engaged position in which locking dogs interfere with the abutting surface and a disengaged position in which the piston is free to slide within the screw; and actuating elements configured to shift the piston from the engaged to the disengaged position upon electrical or mechanical failure of the actuator. The actuating elements include a key axially movable between the engaged and disengaged positions and having a locking section, configured to bias the locking dogs into interference with the abutting surface in the engaged position, and an unlocking section, configured to allow free sliding of the piston within the screw in the disengaged position. An anti-jamming device for operating a critical flight control surface.

Claims (16)

1. A linear electromechanical actuator, comprising:

a main screw-nut assembly driven by a main motion device,

an anti-jamming piston arranged coaxially within a hollow screw of the main screw-nut assembly and shiftable between an engaged position in which a plurality of locking dogs interfere with an abutting surface of the hollow screw and a disengaged position in which the anti-jamming piston is free to slide within the hollow screw; and

actuating elements configured to shift the anti-jamming piston from the engaged position to the disengaged position upon electrical or mechanical failure of the linear electromechanical actuator, the actuating elements comprising a key axially movable between the engaged position and the disengaged position and comprising a locking section, configured to engage and bias the locking dogs into interference with the abutting surface in the engaged position, and an unlocking section, configured to allow the locking dogs to move away from the abutting surface and to allow free sliding of the anti-jamming piston within the hollow screw in the disengaged position.

2. The linear electromechanical actuator according to claim 1 , wherein the anti-jamming piston further comprises guiding elements configured to guide the plurality of locking dogs into and out of interference with the abutting surface of the hollow screw.

3. The linear electromechanical actuator according to claim 2 , wherein the guiding elements comprise a guiding piston detachably coupled to the anti-jamming piston, the guiding piston having a plurality of guiding slots, each guiding slot configured to guide one locking dog into and out of interference with the abutting surface of the hollow screw.

4. The linear electromechanical actuator according to claim 1 , wherein the key further comprises a camming section located between the locking and unlocking sections and configured to guide the locking dogs between the locking and unlocking sections.

5. The linear electromechanical actuator according to claim 1 , wherein the anti-jamming piston includes a groove configured to house a slide ring.

6. The linear electromechanical actuator according to claim 1 , wherein the anti-jamming piston includes a sleeve configured to guide sliding of the anti-jamming piston within the hollow screw and a tubular strut detachably coupled to the sleeve.

7. The linear electromechanical actuator according to claim 6 , where the sleeve comprises a recess configured to house the actuating elements.

8. The linear electromechanical actuator according to claim 1 , wherein the actuating elements comprise a secondary screw-nut assembly driven by a secondary motion device and configured to axially move the key between the engaged position and the disengaged position.

9. The linear electromechanical actuator according to claim 8 , further comprising:

incoming electrical power measuring elements, configured to measure the electrical consumption of the linear electromechanical actuator;

outcoming mechanical power measuring elements, configured to measure the mechanical power provided by the linear electromechanical actuator; and

processing elements, the processing elements configured to calculate the ratio η between the mechanical power provided by the linear electromechanical actuator, measured by the outcoming mechanical power measuring elements, and the electrical power consumption of the linear electromechanical actuator, measured by the incoming electrical power measuring elements, the processing elements configured to compare the calculated ratio to a reference ratio η ref , and the processing elements configured to generate a command signal that activates the secondary motion device that drives the secondary screw-nut assembly in case the calculated ratio η falls behind the reference ratio η ref .

10. The linear electromechanical actuator according to claim 1 , wherein the actuating elements comprise elastic elements having a stiffness configured to axially move the key between the engaged position and the disengaged position through elastic deformation in case the axial component of the load of the main screw-nut assembly transmitted through the locking dogs in the engaged position surpasses the maximum axial load of the main screw-nut assembly.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 21, 2015
From: CHAMORRO GONZALEZ-TABLAS, EDUARADO; AGUADO LOPEZ, FRANCISCO JOSE; JIMENEZ OLAZABAL, ANDRES; MORANTE LOPEZ, ESTEBAN
To: CESA, COMPANIA ESPANOLA DE SISTEMAS AERONAUTICOS S.A.
Reel/Frame 034774/0752 →
Priority Claims (1)
EP 14382016 · Jan 21, 2014 · regional
Continuity (1)
Related Publication 20150204427A1 · Jul 23, 2015