Rotary piston type actuator with a central actuation assembly

US9816537B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9816537-B2
Application numberUS-201313921904-A
CountryUS
Kind codeB2
Filing dateJun 19, 2013
Priority dateFeb 27, 2013
Publication dateNov 14, 2017
Grant dateNov 14, 2017

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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 rotary actuator includes a housing, a rotor assembly rotatably journaled in said housing and including a rotary output shaft, a central actuation assembly including a central mounting point formed in an external surface of the rotary output shaft, said central mounting point proximal to the longitudinal midpoint of the rotary output shaft, a mounting assembly adapted for attachment to an external mounting connector of a mounting surface of an aircraft structural member, and an actuation arm removably attached at a proximal end to the central mounting point, said actuation arm adapted at a distal end for attachment to an external mounting feature of an aircraft assembly to be actuated.

First claim

Opening claim text (preview).

What is claimed is: 1. A rotary actuator comprising: a housing; a rotor assembly rotatably journaled in said housing and including a rotary output shaft; a central actuation assembly including a central mounting point formed in an external surface of the rotary output shaft, said central mounting point proximal to the longitudinal midpoint of the rotary output shaft, and a radial recess formed in an external peripheral surface of the housing proximal to the central mounting point of the rotary output shaft; a mounting assembly adapted for attachment to an external mounting connector of a mounting surface of an aircraft structural member; and an actuation arm extending through the radial recess and removably attached at a proximal end to the central mounting point, said actuation arm adapted at a distal end for attachment to an external mounting feature of an aircraft assembly to be actuated. 2. The rotary actuator of claim 1 wherein the mounting assembly comprises a radially projecting portion of the housing disposed at a midpoint of the housing, said mounting assembly disposed about 180 degrees from the radial recess of the central actuation assembly. 3. The rotary actuator of claim 1 , wherein: the housing defines a first arcuate chamber including a first cavity, a first fluid port in fluid communication with the first cavity, and an open end; the rotor assembly further includes a first rotor arm extending radially outward from the rotary output shaft; and the rotary actuator further comprises an arcuate-shaped first piston disposed in said housing for reciprocal movement in the first arcuate chamber through the open end, wherein a first seal, the first cavity, and the first piston define a first pressure chamber, and a first portion of the first piston contacts the first rotor arm. 4. The rotary actuator of claim 3 , wherein the housing further defines a second arcuate chamber comprising a second cavity, and a second fluid port in fluid communication with the second cavity; the rotor assembly further comprises a second rotor arm; and the rotary actuator further comprises an arcuate-shaped second piston disposed in said housing for reciprocal movement in the second arcuate chamber, wherein a second seal, the second cavity, and the second piston define a second pressure chamber, and a first portion of the second piston contacts the second rotor arm. 5. The rotary actuator of claim 4 wherein the central actuation assembly further includes a radial recess formed in an external peripheral surface of the housing proximal to the central mounting point of the rotary output shaft, and wherein said actuation arm extends through the radial recess. 6. The rotary actuator of claim 1 , further comprising a rotary actuator comprising a stator mounted to the housing and a rotor coupled to the rotary output shaft. 7. The rotary actuator of claim 6 , wherein the rotary actuator is one of a rotary piston type actuator, a rotary vane type actuator, or a rotary fluid type actuator. 8. The rotary actuator of claim 6 , wherein the rotary actuator is an electromechanical actuator. 9. A rotary actuator comprising: a housing comprising a mounting assembly; a rotor assembly rotatably journaled in said housing and including a rotary output shaft, and a radial recess formed in an external peripheral surface of the housing proximal to the central mounting point of the rotary output shaft; a central actuation assembly including a central mounting point formed in an external surface of the rotary output shaft, said central mounting point proximal to the longitudinal midpoint of the rotary output shaft; and an actuation arm extending through the radial recess and removably attached at a proximal end to the central mounting point, said actuation arm adapted at a distal end for attachment to an external mounting feature of a member to be actuated. 10. The rotary actuator of claim 9 wherein the mounting assembly comprises a radially projecting portion of the housing, said mounting assembly disposed about 180 degrees from the radial recess of the central actuation assembly, said mounting assembly adapted for attachment to an external mounting connector of a mounting surface. 11. The rotary actuator of claim 10 , wherein the radially projecting portion of the housing is a radially projecting central portion of the housing. 12. The rotary actuator of claim 9 , wherein: the housing defines a first arcuate chamber including a first cavity, a first fluid port in fluid communication with the first cavity, and an open end; the rotor assembly further includes a first rotor arm extending radially outward from the rotary output shaft; and the rotary actuator further comprises an arcuate-shaped first piston disposed in said housing for reciprocal movement in the first arcuate chamber through the open end, wherein a first seal, the first cavity, and the first piston define a first pressure chamber, and a first portion of the first piston contacts the first rotor arm. 13. The rotary actuator of claim 12 , wherein the housing further defines a second arcuate chamber comprising a second cavity, and a second fluid port in fluid communication with the second cavity; the rotor assembly further comprises a second rotor arm; and the rotary actuator further comprises an arcuate-shaped second piston disposed in said housing for reciprocal movement in the second arcuate chamber, wherein a second seal, the second cavity, and the second piston define a second pressure chamber, and a first portion of the second piston contacts the second rotor arm. 14. The rotary actuator of claim 13 wherein the central actuation assembly further includes a radial recess formed in an external peripheral surface of the housing proximal to the central mounting point of the rotary output shaft, and wherein said actuation arm extends through the radial recess. 15. The rotary actuator of claim 9 , further comprising a rotary actuator comprising a stator mounted to the housing and a rotor coupled to the rotary output shaft. 16. The rotary actuator of claim 15 , wherein the rotary actuator is one of a rotary piston type actuator, a rotary vane type actuator, or a rotary fluid type actuator. 17. The rotary actuator of claim 15 , wherein the rotary actuator is an electromechanical actuator. 18. The rotary actuator of claim 15 , wherein the rotary actuator comprises a linear actuator and a linear-to-rotary motion conversion assembly coupled to the rotor. 19. The rotary actuator of claim 9 , wherein the housing is formed as a unitary one-piece housing. 20. The rotary actuator of claim 9 , wherein the external mounting feature is attached to one of an aircraft structural member or an external mounting connector of an external surface, and the mounting assembly is attached to the other of the aircraft structural member or the external mounting connector. 21. A method of rotary actuation comprising: providing a rotary actuator comprising: a housing; a rotor assembly rotatably journaled in said housing and including a rotary output shaft; a central actuation assembly including a central mounting point formed in an external surface of the rotary output shaft, said central mounting point proximal to the longitudinal midpoint of the rotary output shaft, and a radial recess formed in an external peripheral surface of the housing proximal to the central mounting point of the rotary output shaft; and an actuation arm extending through the radial recess and remova

Assignees

Inventors

Classifications

  • using fluid pressure · CPC title

  • F15B15/125Primary

    of the curved-cylinder type · CPC title

  • F15B15/02Primary

    Mechanical layout characterised by the means for converting the movement of the fluid-actuated element into movement of the finally-operated member · CPC title

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What does patent US9816537B2 cover?
A rotary actuator includes a housing, a rotor assembly rotatably journaled in said housing and including a rotary output shaft, a central actuation assembly including a central mounting point formed in an external surface of the rotary output shaft, said central mounting point proximal to the longitudinal midpoint of the rotary output shaft, a mounting assembly adapted for attachment to an exte…
Who is the assignee on this patent?
Woodward Inc
What technology area does this patent fall under?
Primary CPC classification F15B15/125. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Nov 14 2017 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 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).