Anti-torque system for helicopters

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

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

B64C 2782

Patent

active

052402053

ABSTRACT:
A rotating wing aircraft of helicopter type is provided, according to the invention, with an anti-torque system which comprises, in combination, an auxiliary tail rotor, a vertical tail fin developing lateral lift and optionally provided with a trailing edge control surface, and a blower device.

REFERENCES:
patent: 2322715 (1943-06-01), Kloeren
patent: 2369652 (1945-02-01), Avery
patent: 2609053 (1952-09-01), Lee
patent: 4200252 (1980-04-01), Logan et al.
patent: 4585391 (1986-04-01), Vuillet et al.
patent: 4708305 (1987-11-01), Kelley 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

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

Rate now

     

Profile ID: LFUS-PAI-O-2293305

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