Hydroelastic damper, and an aircraft
US-2019367163-A1 · Dec 5, 2019 · US
US8932015B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-8932015-B2 |
| Application number | US-201113105996-A |
| Country | US |
| Kind code | B2 |
| Filing date | May 12, 2011 |
| Priority date | May 6, 2011 |
| Publication date | Jan 13, 2015 |
| Grant date | Jan 13, 2015 |
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A hydraulic blade speed control apparatus and method. The apparatus includes a rotor assembly comprising a shaft; a first blade assembly pivotably attached to the shaft at a first initial position; a second blade assembly pivotably attached to the shaft assembly at a second initial position opposite to the first initial position; and a hydraulic movement mechanism. An initial angle of 180 degrees exists between the first blade assembly with said respect to the second blade assembly. The rotor assembly is configured to rotate the first blade assembly and the second blade assembly in a first direction and a second direction opposite to the first direction. The hydraulic movement mechanism is configured to pivotably move the first blade assembly in different angular positions with respect to the rotor assembly and the second blade assembly.
Opening claim text (preview).
The invention claimed is: 1. An apparatus comprising: a rotor assembly comprising a center shaft; a first blade assembly pivotably and directly attached to said shaft assembly at a first initial position, wherein said first blade assembly is in direct mechanical contact with said center shaft; a second blade assembly pivotably and directly attached to said center shaft at a second initial position opposite to said first initial position, wherein said second blade assembly is i…
Operations & Transport · mapped topic
Operations & Transport · mapped topic
Operations & Transport · mapped topic
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