IP Library › Granted Patent US 10,113,568
Granted Patent B2
US 10,113,568 · App. 15/048,196 · Granted Oct 30, 2018

Ram air turbine hydraulic release mechanism

Inventor: David G. Bannon (Rockford, IL)
Assignee: HAMILTON SUNDSTRAND CORPORATION
F15B15/261B64D41/007F15B1/027F15B15/14
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Quick Facts
Patent No.
US 10,113,568
App. No.
15/048,196
Granted
Oct 30, 2018
Kind
B2
Abstract

A ram air turbine actuator release device to release a ram air turbine actuator includes a lock bolt releasably engaged to the ram air turbine actuator, a toggle comprising a toggle roller to engage the lock bolt, and a toggle pivot to couple the toggle to the ram air turbine actuator, a hydraulic toggle actuator, including a piston defining a first hydraulic chamber and a second hydraulic chamber, a solenoid valve in fluid communication with the first hydraulic chamber, and a plunger coupled to the piston, wherein a pressure differential between the first hydraulic chamber and the second hydraulic chamber displaces the plunger to rotate the toggle to disengage the toggle roller from the lock bolt.

Claims (35)

1. A ram air turbine actuator release device to release a ram air turbine actuator, the ram air turbine actuator release device comprising:

a lock bolt releasably engaged to the ram air turbine actuator;

a toggle comprising a toggle roller to engage the lock bolt, and a toggle pivot to couple the toggle to the ram air turbine actuator;

a hydraulic toggle actuator, comprising:

a housing;

a piston defining a first surface of a first hydraulic chamber and a second hydraulic chamber within the housing;

a solenoid valve disposed immediately adjacent to the housing and the first hydraulic chamber and in fluid communication with the first hydraulic chamber to define a second surface of the first hydraulic chamber, which is opposite the first surface of the first hydraulic chamber; and

a plunger coupled to the piston, wherein a pressure differential between the first hydraulic chamber and the second hydraulic chamber causes the piston to translate within the housing to thereby displace the plunger such that the plunger rotates the toggle to disengage the toggle roller from the lock bolt.

2. The ram air turbine actuator release device of claim 1 , wherein the piston is displaced a desired distance.

3. The ram air turbine actuator release device of claim 1 , wherein the plunger applies a desired force.

4. The ram air turbine actuator release device of claim 1 , wherein the hydraulic toggle actuator further comprises a return orifice in fluid communication with the first hydraulic chamber.

5. The ram air turbine actuator release device of claim 1 , wherein the solenoid valve selectively provides hydraulic pressure to the first hydraulic chamber.

6. The ram air turbine actuator release device of claim 1 , wherein the solenoid valve is in fluid communication with an aircraft hydraulic system.

7. The ram air turbine actuator release device of claim 1 , further comprising a hydraulic accumulator in fluid communication with an aircraft hydraulic system.

8. The ram air turbine actuator release device of claim 7 , wherein the hydraulic accumulator is in fluid communication with the solenoid valve.

9. The ram air turbine actuator release device of claim 1 , further comprising a reset plunger to bias the toggle to an engaged position.

10. A ram air turbine system, comprising:

a ram air turbine;

a deployment actuator to deploy the ram air turbine; and

a ram air turbine actuator release device to release the deployment actuator, the ram air turbine actuator release device comprising:

a lock bolt releasably engaged to the deployment actuator;

a toggle comprising a toggle roller to engage the lock bolt, and a toggle pivot to couple the toggle to the deployment actuator;

a hydraulic toggle actuator, comprising:

a housing

a piston defining a first surface of a first hydraulic chamber and a second hydraulic chamber within the housing;

a solenoid valve disposed immediately adjacent to the housing and the first hydraulic chamber and in fluid communication with the first hydraulic chamber to define a second surface of the first hydraulic chamber, which is opposite the first surface of the first hydraulic chamber; and

a plunger coupled to the piston, wherein a pressure differential between the first hydraulic chamber and the second hydraulic chamber causes the piston to translate within the housing to thereby displace the plunger such that the plunger rotates the toggle to disengage the toggle roller from the lock bolt.

11. The ram air turbine system of claim 10 , wherein the piston is displaced a desired distance.

12. The ram air turbine system of claim 10 , wherein the plunger applies a desired force.

13. The ram air turbine system of claim 10 , wherein the hydraulic toggle actuator further comprises a return orifice in fluid communication with the first hydraulic chamber.

14. The ram air turbine system of claim 10 , wherein the solenoid valve selectively provides hydraulic pressure to the first hydraulic chamber.

15. The ram air turbine system of claim 10 , wherein the solenoid valve is in fluid communication with an aircraft hydraulic system.

16. The ram air turbine system of claim 10 , further comprising a hydraulic accumulator in fluid communication with an aircraft hydraulic system.

17. The ram air turbine system of claim 16 , wherein the hydraulic accumulator is in fluid communication with the solenoid valve.

18. The ram air turbine system of claim 10 , further comprising a reset plunger to bias the toggle to an engaged position.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Feb 19, 2016
From: BANNON, DAVID G.
To: HAMILTON SUNDSTRAND CORPORATION
Reel/Frame 037777/0357 →
Continuity (1)
Related Publication 20170241453A1 · Aug 24, 2017
Cited By (5)
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