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

1996-01-18

1998-03-17

Verdier, Christopher

Fluid reaction surfaces (i.e., impellers)

Having positive means for impeller adjustment

Power or manual actuator on non-rotatable part

416114, 416500, 74581, 74586, 74606R, B64C 1144, B64C 2768

Patent

active

057279268

ABSTRACT:
A pitch link having an adjustable length is constructed as a diamond-shaped frame by coupling and fixing four flexible beams at end portions thereof. Spherical bearings are provided on opposite ends of the structure. A turnbuckle shaft is screwed into vertices of the structure and turned to the length of the pitch link. The turnbuckle shaft can be rotated by a detachable motor.

REFERENCES:
patent: 2104764 (1938-01-01), Sanders et al.
patent: 3736010 (1973-05-01), Larkin
patent: 3782220 (1974-01-01), Ditlinger
patent: 3786695 (1974-01-01), Barrett, Jr.
patent: 3938762 (1976-02-01), Murphy
patent: 4053123 (1977-10-01), Chadwick
patent: 4498842 (1985-02-01), Fischer et al.
patent: 4583421 (1986-04-01), Rose
patent: 4611971 (1986-09-01), Aubry et al.
patent: 4841801 (1989-06-01), Tice
patent: 5242130 (1993-09-01), Mouille et al.

Affiliated with

Also associated with

Rating

Pitch link for rotary wing aircraft and automatic adjuster there does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Pitch link for rotary wing aircraft and automatic adjuster there, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Pitch link for rotary wing aircraft and automatic adjuster there will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-952080