Airframe design

Details Airframe design Airframe design

1983-06-20

1985-10-08

Blix, Trygve M.

Aeronautics and astronautics

Aircraft control

Rudders and empennage

244 91, 244199, B64C 508

Patent

active

045455520

ABSTRACT:
This invention relates to aircraft designs with substantial trim drag reduction while maintaining commercially feasible low parasitic and induced drag. The stable or control configured aircraft utilizes controllable winglets to generate pitching, yawing, and rolling moments in flying wing or tailless airframe configurations which are preferably of a swept forward style.

REFERENCES:
patent: D117419 (1939-10-01), Munk et al.
patent: D143847 (1946-02-01), Northrop
patent: D147875 (1947-11-01), Shannon
patent: 2397526 (1946-04-01), Bonbright
patent: 2406588 (1946-08-01), Cornelius
patent: 2418301 (1947-04-01), Heal
patent: 2565990 (1951-08-01), Richard
patent: 2576981 (1951-12-01), Vogt
patent: 2846165 (1958-08-01), Axelson
patent: 3438597 (1969-04-01), Kasper
patent: 4247062 (1981-01-01), Brueckner
patent: 4247063 (1981-01-01), Jenkins
patent: 4457479 (1984-07-01), Daude
Gulfstreamer, vol. 5, No. 6, Winter 1976, p. 9.

Affiliated with

Also associated with

Rating

Airframe design does not yet have a rating. At this time, there are no reviews or comments for this patent.

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

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-2215715