High stiffness hub assembly for proprotor systems
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United States of America Patent
Stats
-
Mar 19, 2019
Grant Date -
Sep 27, 2018
app pub date -
Mar 22, 2017
filing date -
Mar 22, 2017
priority date (Note) -
In Force
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Abstract
A high stiffness hub assembly for a proprotor system operable to rotate with a mast of a tiltrotor aircraft having helicopter and airplane flight modes. The hub assembly includes a yoke and a constant velocity joint assembly. The yoke has four blade arms each adapted to hold a proprotor blade. The constant velocity joint assembly provides a torque path from the mast to the yoke that includes a trunnion assembly, four drive links and four pillow blocks. The trunnion assembly is coupled to the mast and has four outwardly extending trunnions. Each drive link has a leading bearing coupled to one of the trunnions and a trailing bearing coupled to one of the pillow blocks. Each pillow block is independently mounted between an upper surface of the yoke and a hub plate with two connection members that extend through the yoke and the pillow block.

First Claim
Family

- 15 United States
- 10 France
- 8 Japan
- 7 China
- 5 Korea
- 2 Other
Patent Owner(s)
Patent Owner | Address | |
---|---|---|
BELL HELICOPTER TEXTRON INC | P O BOX 482 FORT WORTH TX 76101 |
International Classification(s)

- [Classification Symbol]
- [Patents Count]
Inventor(s)
Inventor Name | Address | # of filed Patents | Total Citations |
---|---|---|---|
Baldwin, Tyler Wayne | Fort Worth, US | 30 | 94 |
Choi, Jouyoung Jason | Fort Worth, US | 35 | 129 |
Rauber, Richard Erler | Fort Worth, US | 8 | 39 |
Stamps, Frank Bradley | Fort Worth, US | 87 | 534 |
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