Aircraft, having a pair of counter rotating rotors

Aeronautics and astronautics – Aircraft – heavier-than-air – Fluid sustained

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

244 122, 244 123, 244 23B, B64C 2900

Patent

active

050641433

ABSTRACT:
The aircraft has a pair of rotors driven to counter-rotate within a housing. The housing has adjustable air guiding discuss for the rotor stream and a airfoil-like outer shape to generate lift at horizontal flight. The air guiding devices include a circular arrangement of a plurality of individual sectors having tangentially extending blades arranged in a zone below the rotors. In each sector the blades are adjustable in their position relative to the rotor stream. In at least some of the sectors, the blades are arranged in pairs for an adjusting movement in opposite relative sense. The air guiding devices allow precise and easy control of the aircraft maneuvers.

REFERENCES:
patent: 2461435 (1949-02-01), Neumann et al.
patent: 2777649 (1957-01-01), Williams
patent: 2863621 (1958-12-01), Davis
patent: 2880945 (1959-04-01), Crane
patent: 3395876 (1968-08-01), Green
patent: 3397852 (1968-08-01), Katzen
patent: 3437290 (1969-04-01), Norman
patent: 3599901 (1971-08-01), Relkil

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

Aircraft, having a pair of counter rotating rotors does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Aircraft, having a pair of counter rotating rotors, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Aircraft, having a pair of counter rotating rotors will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-1008541

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