Pitch-yaw actuation system and method for actuating a device head

US12017801B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-12017801-B2
Application numberUS-202217660405-A
CountryUS
Kind codeB2
Filing dateApr 23, 2022
Priority dateJun 2, 2021
Publication dateJun 25, 2024
Grant dateJun 25, 2024

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  1. Title

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  2. Abstract

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  4. Key dates

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  5. First independent claim

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

A pitch-yaw actuation system includes a pitch frame, a yaw frame, a pitch actuator, a yaw actuator, and a universal joint assembly. The pitch frame is pivotably coupled to a device frame via a pitch hinge. The yaw frame is pivotably coupled to the pitch frame via a yaw hinge. The pitch actuator pivots the pitch frame about a pitch axis. The yaw actuator pivots the yaw frame about a yaw axis oriented orthogonal to the pitch axis. The universal joint assembly couples the yaw actuator to the yaw frame, and includes a universal joint slidably coupled to a linear guide mechanism. The guide mechanism axis is oriented at an angle that allows the universal joint to move in a manner accommodating misalignment of the yaw actuator with the yaw frame during pivoting of at least one of the pitch frame and the yaw frame.

First claim

Opening claim text (preview).

What is claimed is: 1. A pitch-yaw actuation system for actuating a device head, comprising: a pitch frame pivotably coupled to a head frame via a pitch hinge having a pitch axis; a yaw frame pivotably coupled to the pitch frame via a yaw hinge having a yaw axis orthogonal to the pitch axis; a pitch actuator configured to pivot the pitch frame about the pitch axis; a yaw actuator configured to pivot the yaw frame about the yaw axis; a universal joint assembly coupling the yaw actuator to the yaw frame, and including: a linear guide mechanism having a guide mechanism axis; a universal joint slidably coupled to the linear guide mechanism; and the guide mechanism axis is oriented at an angle that allows the universal joint to move in a manner accommodating misalignment of the yaw actuator with the yaw frame during pivoting of at least one of the pitch frame and the yaw frame. 2. The pitch-yaw actuation system of claim 1 , wherein: at least one of the pitch actuator and the yaw actuator is a linear actuator. 3. The pitch-yaw actuation system of claim 1 , wherein: the pitch axis is located between the yaw axis and the universal joint. 4. The pitch-yaw actuation system of claim 1 , wherein: the linear guide mechanism is configured to allow the universal joint to translate along the linear guide mechanism while simultaneously rotating about the guide mechanism axis. 5. The pitch-yaw actuation system of claim 1 , wherein: the universal joint is a ball-and-socket joint having a ball, and a joint body having a socket configured to receive the ball. 6. The pitch-yaw actuation system of claim 1 , wherein: the linear guide mechanism comprises a guide pin, and a guide pin bore slidably receiving the guide pin. 7. The pitch-yaw actuation system of claim 1 , wherein: the yaw frame receiving a device head configured to discharge a treatment. 8. The pitch-yaw actuation system of claim 1 , wherein: the yaw frame has a yaw frame opening receiving the device head, the pitch-yaw actuation system includes a pair of yaw hinges respectively on opposite sides of the pitch frame. 9. A device head assembly, comprising: a head frame; a pitch-yaw actuation system, including: a pitch frame coupled to the head frame via a pitch hinge having a pitch axis; a yaw frame coupled to the pitch frame via a yaw hinge having a yaw axis orthogonal to the pitch axis, the yaw frame configured to receive a device head; a pitch actuator coupled to the head frame and configured to pivot the pitch frame about the pitch axis; a yaw actuator coupled to the head frame and configured to pivot the yaw frame about the yaw axis; a universal joint assembly coupling the yaw actuator to the yaw frame, and including: a linear guide mechanism having a guide mechanism axis; a universal joint slidably coupled to the linear guide mechanism; and the guide mechanism axis is oriented at an angle allowing the universal joint to move relative to the linear guide mechanism in a manner accommodating misalignment of the yaw actuator with the yaw frame during pivoting of the pitch frame and the yaw frame. 10. The device head assembly of claim 9 , wherein: the head frame has a head frame cross-sectional perimeter; and at least one of the pitch frame, the yaw frame, the pitch actuator, the yaw actuator, and the universal joint assembly are non-protruding from the head frame cross-sectional perimeter when the head frame is viewed along a direction parallel to an actuator axis of the pitch actuator and the yaw actuator. 11. The device head assembly of claim 9 , wherein: at least one of the pitch actuator and the yaw actuator is a linear actuator. 12. The device head assembly of claim 9 , wherein: the linear guide mechanism allowing the universal joint to translate along the linear guide mechanism while simultaneously rotating about the guide mechanism axis. 13. The device head assembly of claim 9 , wherein: the universal joint is a ball-and-socket joint having a ball, and a joint body having a socket configured to receive the ball. 14. The device head assembly of claim 9 , wherein: the linear guide mechanism comprises a guide pin, and a guide pin bore slidably receiving the guide pin. 15. A method of actuating a device head, comprising: pivoting, using a pitch actuator, a pitch frame about a pitch axis of a pitch hinge coupling the pitch frame to a head frame; pivoting, using a yaw actuator, a yaw frame about a yaw axis of a yaw hinge coupling the yaw frame to the pitch frame, the yaw axis oriented orthogonal to the pitch axis, the yaw actuator coupled to the yaw frame via a linear guide mechanism and a universal joint slidably coupled to the linear guide mechanism; moving the universal joint along the linear guide mechanism; which has the guide mechanism axis is oriented at an angle that allows the universal joint to move in a manner accommodating misalignment of the yaw actuator with the yaw frame during pivoting of at least one of the pitch frame and the yaw frame. 16. The method of claim 15 , wherein at least one of pivoting the pitch frame and pivoting the yaw frame are respectively performed by the pitch actuator and the yaw actuator, each configured as a linear actuator. 17. The method of claim 15 , wherein pivoting the pitch frame about the pitch axis comprises: pivoting the pitch frame about the pitch axis located between the yaw axis and the universal joint. 18. The method of claim 15 , wherein moving the universal joint relative to the linear guide mechanism comprises: rotating a ball within a socket formed in a joint body of a ball-and-socket joint. 19. The method of claim 15 , wherein moving the universal joint relative to the linear guide mechanism comprises: sliding a guide pin within a guide pin bore. 20. The method of claim 15 , further comprising: discharging a treatment from the device head supported by the pitch frame and the yaw frame.

Assignees

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Classifications

  • performed by spraying · CPC title

  • the angular position of the spray heads relative to the straight line being modified during the reciprocating movement · CPC title

  • the liquid or other fluent material being applied to the whole periphery of the cross section of the elongated body · CPC title

  • Arrangement or mounting of spray heads (B05B13/0207 takes precedence) · CPC title

  • with tilting motion mechanisms relative to paper surface · CPC title

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What does patent US12017801B2 cover?
A pitch-yaw actuation system includes a pitch frame, a yaw frame, a pitch actuator, a yaw actuator, and a universal joint assembly. The pitch frame is pivotably coupled to a device frame via a pitch hinge. The yaw frame is pivotably coupled to the pitch frame via a yaw hinge. The pitch actuator pivots the pitch frame about a pitch axis. The yaw actuator pivots the yaw frame about a yaw axis ori…
Who is the assignee on this patent?
Boeing Co
What technology area does this patent fall under?
Primary CPC classification B64F5/10. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Tue Jun 25 2024 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 12 related publications on this page (citations in our corpus or others sharing the same primary CPC).