STOL/VTOL free wing aircraft with modular wing and tail

Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

244131, 244120, 244124, B64C 338

Patent

active

059414782

ABSTRACT:
A mechanism for quickly removing and installing the free wings and/or the tail booms of a freewing aircraft to the fuselage. The fuselage includes a free wing cross tube extending transversely through the fuselage at the spanwise axis, and each of the left and right free wings includes a support tube disposed therein, also along the spanwise axis, with a portion of the wing structural tube being received within the fuselage cross tube. A quick-release pin is insertable in holes disposed in both the structural tube and the cross tube when the holes are placed in alignment. A second cross tube extends transversely through the rear end of the fuselage at the tail boom pivot axis. At least a portion of each tail boom member is disposed in surrounding relationship to the cross tube. In a preferred embodiment, a quick-release pin is insertable in holes disposed in both the tail boom member portion and the cross tube when the holes are placed in alignment.

REFERENCES:
patent: 1016929 (1912-02-01), Black
patent: 2438309 (1948-03-01), Zimmerman
patent: 2481379 (1949-09-01), Zimmerman
patent: 2580312 (1951-12-01), Moore
patent: 2708081 (1955-05-01), Dobson
patent: 5395073 (1995-03-01), Rutan 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

STOL/VTOL free wing aircraft with modular wing and tail does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with STOL/VTOL free wing aircraft with modular wing and tail, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and STOL/VTOL free wing aircraft with modular wing and tail will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-459324

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