Gas turbine engine bleed valve damping guide link
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United States of America Patent
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May 31, 2022
Grant Date -
Dec 10, 2020
app pub date -
Jun 7, 2019
filing date -
Jun 7, 2019
priority date (Note) -
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Abstract
A damping link assembly for a bleed valve of a gas turbine engine. The damping link assembly having: a bleed valve ring having a link aperture; a mechanical fastener disposed in the link aperture; and a damping guide link operatively coupled to the mechanical fastener at one end for rotation about a first axis of the mechanical fastener and the damping guide link being operatively coupled to an idler bracket at an opposite end for rotation about a second axis, the damping guide link being capable of twisting about a third axis different from the first axis and the second axis when the bleed valve ring is rotated from a first position to a second position.
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