Manually actuated hydraulic circuit for ram air turbine (RAT) restow

Patent metadata

Field	Value
Publication number	US-11858650-B2
Application number	US-202016791139-A
Country	US
Kind code	B2
Filing date	Feb 14, 2020
Priority date	Feb 14, 2020
Publication date	Jan 2, 2024
Grant date	Jan 2, 2024

Abstract

A ram air turbine (RAT) restow system includes an actuator assembly with a piston interposed between an upper fluid compartment and a lower fluid compartment. The actuator assembly is configured to selectively move the piston between a deployed position and a stowed position. A hydraulic restow circuit is interposed between the actuator assembly and a hydraulic fluid system that is configured to output fluid. The hydraulic restow circuit includes a restow valve configured to operate in a first position that establishes a first fluid path to deliver the fluid to the upper fluid compartment and a second position that establishes a second fluid path to deliver the fluid to the lower fluid compartment.

First claim

What is claimed is:

1. A ram air turbine (RAT) restow system comprising:
an actuator assembly including a piston interposed between an upper fluid compartment and a lower fluid compartment, the actuator assembly configured to selectively move the piston between a deployed position and a stowed position; and
a hydraulic restow circuit configured to receive fluid, the hydraulic restow circuit including a manually actuated restow valve configured to operate in a first position that establishes a first fluid path to deliver the fluid to the upper fluid compartment to effect the deployed position and a second position that establishes a second fluid path to deliver the fluid to the lower fluid compartment to transition from the deployed position to the stowed position,
wherein the manually actuated restow valve rotates about a center axis in a first direction in response to receiving a rotational force manually applied to the manually actuated restow valve, and rotates about the center axis in a second direction opposite the first direction in response to manually removing the rotational force,
wherein the hydraulic restow circuit further comprises:
an actuator supply line including a first end in fluid communication with the actuator assembly and a second end in fluid communication with a third fluid path of the restow valve;
a aircraft return line including a first end in fluid communication with the third fluid path;
an aircraft supply line in fluid communication with the restow valve; and
an actuator return line including a first end in fluid communication with the actuator assembly and a second end in fluid communication with one of a first valve fluid path of the restow valve when the restow valve is in the first position or a second valve fluid path of the restow valve when the restow valve is in the second position,
wherein the actuator return line is in fluid communication with both the actuator supply line and the aircraft return line via the first valve fluid path when the restow valve operates in the first position, and
wherein the actuator return line is disconnected from the both the actuator supply line and the aircraft supply line, and is in fluid communication with the aircraft return line via the second valve fluid path when the restow valve is in the second position.

2. The RAT restow system of claim 1 , wherein the second fluid path delivers the fluid to the lower fluid compartment such that the piston is forced into the upper fluid compartment to invoke the stowed position.

3. The RAT restow system of claim 1 , wherein the hydraulic restow circuit is interposed between the actuator assembly and a hydraulic fluid system integrated with an aircraft and is configured to output the fluid.

4. The RAT restow system of claim 2 , wherein the manually actuated restow valve includes:
a grip configured to receive the rotational force manually applied thereto; and
a valve spring that is elastically biased according to the first position.

5. The RAT restow system of claim 4 , wherein the valve spring is elastically loaded in response to transitioning the manually actuated restow valve from the first position to the second position, and the valve spring automatically returns the manually actuated restow valve to the first operating position in response to manually releasing the grip such that the manually actuated restow valve is forced from the second position.

6. The RAT restow system of claim 1 , wherein the aircraft supply line is completely disconnected from the actuator supply line, the actuator return line, and the aircraft return line when the restow valve is in the first position.

Assignees

• Hamilton Sundstrand Corp

Inventors

• Konicek Timothy Scott
• Gerger Stuart T
• Bortoli Stephen Michael

Classifications

• B64D41/007 Primary

  Ram air turbines · CPC title

• F01D15/10

  Adaptations for driving, or combinations with, electric generators · CPC title

• F02C7/32

  Arrangement, mounting, or driving, of auxiliaries · CPC title

• F15B15/1476

  Special return means · CPC title

• F15B15/202

  Externally-operated valves mounted in or on the actuator · CPC title