Hydraulic thrust reverser actuation system

US11136940B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-11136940-B2
Application numberUS-201916711897-A
CountryUS
Kind codeB2
Filing dateDec 12, 2019
Priority dateMay 31, 2019
Publication dateOct 5, 2021
Grant dateOct 5, 2021

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

A hydraulic thrust reverser system (TRAS) including a first return line having a first check valve therein, and a second return line having a second check valve therein, wherein the first return line and the second return line are in fluid communication with each other via a fluid restrictor located upstream of the first and second check valves, wherein the first return line extends from a piston system of the TRAS, the piston system being for moving at least one thrust reverser door, and wherein the second return line extends from a lock system of the TRAS, the lock system being for controlling locks to selectively prevent the movement of the at least one thrust reverser door.

First claim

Opening claim text (preview).

The invention claimed is: 1. A hydraulic thrust reverser system (TRAS) including: a first return line having a first check valve therein; and a second return line having a second check valve therein; wherein the first return line and the second return line are in fluid communication with each other via a fluid restrictor located upstream of the first and second check valves; wherein the first return line extends from a piston system of the TRAS, the piston system being for moving at least one thrust reverser door; and wherein the second return line extends from a lock system of the TRAS, the lock system being for controlling locks to selectively prevent the movement of the at least one thrust reverser door. 2. The TRAS of claim 1 , wherein the fluid restrictor is a fluid line having a bore therethrough for transmitting fluid between the first and second return lines, wherein at least a portion of a length of said bore has a smaller diameter than: a minimum diameter of a bore through the first return line; and/or a minimum diameter of a bore through the second return line. 3. The TRAS of claim 1 , wherein the first return line and the second return line are additionally in fluid communication downstream of the first and second return line check valves. 4. The TRAS of claim 3 , wherein the first return line and the second return line converge to an outlet. 5. The TRAS of claim 1 , configured so that, in use, the first return line is at a first return line pressure and the second return line is at a second return line pressure, and the first and second return line pressures are greater than ambient pressure. 6. The TRAS of claim 1 , wherein the TRAS includes a supply of hydraulic fluid at a supply pressure, and an isolation control valve, wherein the isolation control valve is configured to selectively isolate the supply pressure from both the piston system and the lock system of the TRAS. 7. The TRAS of claim 1 , further comprising: a restrictor line for allowing fluid to flow between the first and second return lines, wherein a first end of the restrictor line is interconnected with the first return line at a location between ends of the first return line, and a second end of the restrictor line is interconnected with the second return line at a location between ends of the second return line, and wherein the restrictor is located in the restrictor line. 8. The TRAS of claim 1 , wherein said at least one thrust reverser door controlled by the piston system, and wherein said one lock system is configured to control a lock to selectively prevent the movement of the at least one thrust reverser door. 9. An aircraft including the TRAS of claim 8 , wherein the aircraft further comprises: an engine and a nacelle, wherein the at least one thrust reverser door forms a section of the nacelle.

Assignees

Inventors

Classifications

  • with blocking systems or locking devices; Arrangement of locking devices for thrust reversers · CPC title

  • F02K1/763Primary

    with actuating systems or actuating devices; Arrangement of actuators for thrust reversers · CPC title

  • with only one servomotor · CPC title

  • Hydraulic actuators · CPC title

  • Locking mechanisms · CPC title

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Frequently asked questions

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What does patent US11136940B2 cover?
A hydraulic thrust reverser system (TRAS) including a first return line having a first check valve therein, and a second return line having a second check valve therein, wherein the first return line and the second return line are in fluid communication with each other via a fluid restrictor located upstream of the first and second check valves, wherein the first return line extends from a pist…
Who is the assignee on this patent?
Goodrich Actuation Systems Ltd
What technology area does this patent fall under?
Primary CPC classification F02K1/763. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Oct 05 2021 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 3 related publications on this page (citations in our corpus or others sharing the same primary CPC).