Rotor hub assembly with universal joint

US11396371B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-11396371-B2
Application numberUS-202017014897-A
CountryUS
Kind codeB2
Filing dateSep 8, 2020
Priority dateJul 24, 2017
Publication dateJul 26, 2022
Grant dateJul 26, 2022

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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 rotor hub assembly that includes a yoke configured to attach blades thereto, a universal joint configured to attach to, and transmit forces between, a mast and the yoke, and an elastomeric member configured to attenuate vibrations transmitted from the universal joint to the mast.

First claim

Opening claim text (preview).

What is claimed is: 1. A rotor hub assembly, comprising: a yoke having at least two arms extending therefrom; a yoke bracket attached to the yoke; a cross member defining a first aperture with a first central longitudinal axis and a second aperture with a second central longitudinal axis, the first central longitudinal axis being orthogonal to the second central longitudinal axis, the cross member being pivotally attached to the yoke bracket about the first central longitudinal axis; and a drive member, comprising: an inner member configured to engage a mast; an outer member pivotally attached to the cross member about the second central longitudinal axis; and an elastomeric member disposed between the inner member and the outer member; wherein the inner member has a substantially cylindrical outer surface, the outer member has a substantially cylindrical inner surface, and the elastomeric member includes a hollow cylindrical portion configured to fit between the substantially cylindrical outer surface of the inner member and the substantially cylindrical outer surface of the outer member. 2. The rotor hub assembly of claim 1 , wherein the cross member further includes a third aperture coaxial with the first aperture and a fourth aperture coaxial with the second aperture. 3. The rotor hub assembly of claim 1 , wherein the first and second central longitudinal axes are coplanar. 4. The rotor hub assembly of claim 1 , the elastomeric member being configured to attenuate 2/rev vibrations transmitted to the inner member from the outer member. 5. The rotor hub assembly of claim 1 , wherein each of the inner member and outer member comprises a flange extending therefrom, the flanges being coupled to each other. 6. The rotor hub assembly of claim 5 , wherein the elastomeric member comprises a flange extending therefrom, the flange of the elastomeric member being coupled between the flanges of the inner and outer members. 7. The rotor hub assembly of claim 5 , wherein the flanges are coupled to each other with fasteners extending through the flanges. 8. A rotor hub assembly, comprising: a yoke having at least two arms extending therefrom; a yoke bracket attached to the yoke; a cross member defining a first aperture with a first central longitudinal axis and a second aperture with a second central longitudinal axis, the first central longitudinal axis being orthogonal to the second central longitudinal axis, the cross member being pivotally attached to the yoke bracket about the first central longitudinal axis; and a drive member, comprising: an inner member configured to engage a mast; an outer member pivotally attached to the cross member about the second central longitudinal axis; and an elastomeric member disposed between the inner member and the outer member; wherein each of the inner member and outer member comprises a flange extending therefrom, the flanges being coupled to each other. 9. The rotor hub assembly of claim 8 , wherein the cross member further includes a third aperture coaxial with the first aperture and a fourth aperture coaxial with the second aperture. 10. The rotor hub assembly of claim 8 , wherein the first and second central longitudinal axes are coplanar. 11. The rotor hub assembly of claim 8 , the elastomeric member being configured to attenuate 2/rev vibrations transmitted to the inner member from the outer member. 12. The rotor hub assembly of claim 8 , wherein the inner member has a substantially cylindrical outer surface, the outer member has a substantially cylindrical inner surface, and the elastomeric member includes a hollow cylindrical portion configured to fit between the substantially cylindrical outer surface of the inner member and the substantially cylindrical outer surface of the outer member. 13. The rotor hub assembly of claim 8 , wherein the elastomeric member comprises a flange extending therefrom, the flange of the elastomeric member being coupled between the flanges of the inner and outer members. 14. The rotor hub assembly of claim 8 , wherein the flanges are coupled to each other with fasteners extending through the flanges. 15. A rotor hub assembly, comprising: a yoke having at least two arms extending therefrom; a yoke bracket attached to the yoke; a cross member defining a first aperture with a first central longitudinal axis and a second aperture with a second central longitudinal axis, the first central longitudinal axis being orthogonal to the second central longitudinal axis, the cross member being pivotally attached to the yoke bracket about the first central longitudinal axis; and a drive member, comprising: an inner member configured to engage a mast; an outer member pivotally attached to the cross member about the second central longitudinal axis; and an elastomeric member disposed between the inner member and the outer member; wherein each of the inner member, outer member, and elastomeric member comprises a flange extending therefrom, the flanges of the inner and outer members being coupled to each other, and the flange of the elastomeric member being coupled between the flanges of the inner and outer members. 16. The rotor hub assembly of claim 15 , wherein the cross member further includes a third aperture coaxial with the first aperture and a fourth aperture coaxial with the second aperture. 17. The rotor hub assembly of claim 15 , wherein the first and second central longitudinal axes are coplanar. 18. The rotor hub assembly of claim 15 , the elastomeric member being configured to attenuate 2/rev vibrations transmitted to the inner member from the outer member. 19. The rotor hub assembly of claim 15 , wherein the inner member has a substantially cylindrical outer surface, the outer member has a substantially cylindrical inner surface, and the elastomeric member includes a hollow cylindrical portion configured to fit between the substantially cylindrical outer surface of the inner member and the substantially cylindrical outer surface of the outer member.

Assignees

Inventors

Classifications

  • B64C27/35Primary

    having elastomeric joints · CPC title

  • Direct drive between power plant and rotor hub · CPC title

  • B64C27/41Primary

    with flapping hinge or universal joint, common to the blades · CPC title

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Frequently asked questions

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What does patent US11396371B2 cover?
A rotor hub assembly that includes a yoke configured to attach blades thereto, a universal joint configured to attach to, and transmit forces between, a mast and the yoke, and an elastomeric member configured to attenuate vibrations transmitted from the universal joint to the mast.
Who is the assignee on this patent?
Textron Innovations Inc
What technology area does this patent fall under?
Primary CPC classification B64C27/35. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Tue Jul 26 2022 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 4 related publications on this page (citations in our corpus or others sharing the same primary CPC).