Rotor system for helicopters

Aeronautics and astronautics – Aircraft – heavier-than-air – Helicopter or auto-rotating wing sustained – i.e. – gyroplanes

Reexamination Certificate

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

C244S017190, C446S037000

Reexamination Certificate

active

06929215

ABSTRACT:
A tail rotor system for a helicopter includes a gear box housing retainer (66) coupled to the tail boom (16) of the helicopter. The tail rotor system also includes a power-limiting device (50) configured to disconnect the tail rotor from a power plant for driving the tail rotor about a rotor axis of rotation.

REFERENCES:
patent: 2542682 (1951-02-01), Kloss
patent: 3589833 (1971-06-01), Lancioni
patent: 5360376 (1994-11-01), Baldino
patent: 5609312 (1997-03-01), Arlton et al.
patent: 5749540 (1998-05-01), Arlton
patent: 5836545 (1998-11-01), Arlton et al.

LandOfFree

Say what you really think

Search LandOfFree.com for the USA inventors and patents. Rate them and share your experience with other people.

Rating

Rotor system for helicopters does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Rotor system for helicopters, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Rotor system for helicopters will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-3490218

  Search
All data on this website is collected from public sources. Our data reflects the most accurate information available at the time of publication.