Pitch link for rotary wing aircraft and automatic adjuster there

Details Pitch link for rotary wing aircraft and automatic adjuster there Pitch link for rotary wing aircraft and automatic adjuster there

1997-09-10

1999-09-07

Luong, Vinh T.

Machine element or mechanism

Elements

Pitmans and connecting rods

74586, 74 8915, G05G 100

Patent

active

059469811

ABSTRACT:
A pitch link for a rotary wing aircraft includes first and second shaft members threadingly engaged with each other. A first rod end is fixedly secured to the first shaft member and a second rod end is rotatably coupled to the second shaft member. First and second spherical bearings are mounted on the first and second rod ends, respectively. A guide member guides the first shaft member for movement in an axial direction of the first shaft with respect to the second shaft while preventing rotation of the first shaft.

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