IP Library Granted Patent US 10,651,364
Granted Patent B2
US 10,651,364 · App. 15/585,825 · Granted May 12, 2020

Servo valve with asymmetrical redundant piezoelectric actuator

Inventors: Jean-Luc Bertrand (Orleans, FR); Catherine Mailhan (Vendome, FR)
Assignee: ZODIAC HYDRAULICS
H01L41/0906B60W30/18F02D29/04F15B11/05F15B13/0436F15B15/02F16H61/421F16K31/004
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 10,651,364
App. No.
15/585,825
Granted
May 12, 2020
Kind
B2
Abstract

A driving stage of a servo valve, including a hydraulic ejector and a hydraulic receiver able to be moved relative to each other, one of the two hydraulic units being integral with a mobile unit, movable relative to a body of the servo valve through actuation means, characterized in that the actuation means comprise two piezoelectric actuators connected in series. Control device comprising a servo valve comprising such a driving stage.

Claims (14)

1. A driving stage of a servo valve, the driving stage including a hydraulic unit for ejecting a jet of fluid and a hydraulic unit for receiving the jet of fluid, the hydraulic units being able to be moved relative to each other so as to change their relative position and thereby to generate a pressure differential, one of the two hydraulic units being fixedly mounted on a body of the servo valve and the other hydraulic unit being integral with a mobile unit of the driving stage, movable relative to a body of the servo valve through actuating means, the actuating means comprising a first piezoelectric actuator and a second piezoelectric actuator connected in series, the maximum elongation (Amax 41 ) of the first piezoelectric actuator being substantially equal to half the maximum elongation (Amax 42 ) of the second piezoelectric actuator.

2. The driving stage according to claim 1 , in which the fixed hydraulic unit is a fluid receiver and the hydraulic unit integral with the mobile unit is a fluid ejector.

3. The driving stage according to claim 1 , in which the actuating means comprise a cowling extending around the first and second piezoelectric actuators, the cowling comprising means for pre-charging the first and the second piezoelectric actuators.

4. The driving stage according to claim 3 , in which the pre-charging means comprise an elastic bellows.

5. A device for controlling a hydraulic actuator comprising a servo valve including a driving stage according to claim 1 and a control unit, the control unit selectively adopting one control configuration among a plurality of control configurations, the plurality of control configurations comprising a first control configuration called normal and a second control configuration called degraded,

in the normal configuration, the control unit powers at least the first piezoelectric actuator;

in the degraded configuration, the control unit powers at least the second piezoelectric actuator.

6. The device according to claim 5 , in which, in the normal configuration, the control unit powers the first and the second piezoelectric actuator.

7. The device according to claim 5 , in which, in the degraded configuration, the control unit only powers the second piezoelectric actuator.

8. The device according to claim 5 , in which the plurality of control configurations comprises a third control configuration called safety, in which only one of the piezoelectric actuators is powered.

9. The device according to claim 8 , in which, in the safety configuration, only the first piezoelectric actuator is powered.

10. The device according to claim 5 , in which:

in the normal configuration, the control unit powers the second piezoelectric actuator so that the latter extends to half its maximum elongation (Amax 42 ) whatever the power supply voltage of the first piezoelectric actuator;

in the degraded configuration, the control unit powers the second piezoelectric actuator so that the latter extends beyond half its maximum elongation (Amax 42 ).

Assignments (4)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Dec 17, 2024
From: SAFRAN AEROTECHNICS
To: SAFRAN AEROSYSTEMS
Reel/Frame 069715/0156 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Dec 6, 2024
From: SAFRAN AEROSYSTEMS HYDRAULICS
To: SAFRAN AEROTECHNICS
Reel/Frame 069504/0161 →
CHANGE OF NAME Recorded Jun 4, 2021
From: ZODIAC HYDRAULICS
To: SAFRAN AEROSYSTEMS HYDRAULICS
Reel/Frame 056488/0187 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded May 4, 2017
From: BERTRAND, JEAN-LUC; MAILHAN, CATHERINE
To: ZODIAC HYDRAULICS
Reel/Frame 042238/0332 →
Priority Claims (1)
FR 16 53985 · May 3, 2016 · national
Continuity (1)
Related Publication 20170324021A1 · Nov 9, 2017