Aircraft with safety tail unit

Details Aircraft with safety tail unit Aircraft with safety tail unit

1975-12-15

1977-02-22

Blix, Trygve M.

Aeronautics and astronautics

Aircraft control

Rudders and empennage

244 43, B64C 502

Patent

active

040088677

ABSTRACT:
Aircraft having supersonic and subsonic flight capabilities which utilize variable geometry tail units and fixed front planes to generally improve airworthiness and safety of aircraft during takeoff and landing, and which additionally have a reduced air resistance during high-speed flight and thus save propulsion energy.

REFERENCES:
patent: 1916813 (1933-07-01), Sessa
patent: 2376636 (1945-05-01), Thompson
patent: 2941752 (1960-06-01), Gluhareff
patent: 3181820 (1965-05-01), Burnelli
patent: 3478989 (1969-11-01), Bielefeldt
patent: 3493197 (1970-02-01), Spearman
patent: 3902686 (1975-09-01), Wykes et al.

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