Torque transfer system for a rotorcraft

US9382001B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9382001-B2
Application numberUS-201414338531-A
CountryUS
Kind codeB2
Filing dateJul 23, 2014
Priority dateJul 23, 2014
Publication dateJul 5, 2016
Grant dateJul 5, 2016

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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.

One example of a torque transfer system for a rotorcraft includes a first rotational joint connected to a rotorcraft rotary shaft. The first rotational joint receives a portion of a torque generated by rotation of the rotorcraft rotary shaft and transfers the portion of the torque to a rotorcraft rotating component. The torque transfer system also includes a second rotational joint of a different type connected to the rotorcraft rotary shaft. The second rotational joint receives a remainder of the torque generated by the rotation of the rotorcraft rotary shaft and transfers the remainder of the torque to the rotorcraft rotating component.

First claim

Opening claim text (preview).

What is claimed is: 1. A torque transfer system for a rotorcraft, the system comprising: a first rotational joint connected to a rotorcraft rotary shaft, the first rotational joint to receive a portion of a torque generated by rotation of the rotorcraft rotary shaft and to transfer the portion of the torque to a rotorcraft rotating component; and a second rotational joint separate from and transferring torque using a different mechanism than the first rotational joint, wherein t…

Assignees

Inventors

Classifications

  • Mechanical Engineering · mapped topic

  • Operations & Transport · mapped topic

  • B64C27/12Primary

    Operations & Transport · mapped topic

  • Mechanical Engineering · mapped topic

  • Operations & Transport · mapped topic

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Frequently asked questions

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What does patent US9382001B2 cover?
One example of a torque transfer system for a rotorcraft includes a first rotational joint connected to a rotorcraft rotary shaft. The first rotational joint receives a portion of a torque generated by rotation of the rotorcraft rotary shaft and transfers the portion of the torque to a rotorcraft rotating component. The torque transfer system also includes a second rotational joint of a differe…
Who is the assignee on this patent?
Bell Helicopter Textron Inc
What technology area does this patent fall under?
Primary CPC classification B64C27/12. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Tue Jul 05 2016 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).