Travelling tail-unit with circular arc motion

Aeronautics and astronautics – Aircraft power plants

Patent

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Details

244 89, B64D 3302, B64C 510

Patent

active

040378080

ABSTRACT:
Aircraft having subsonic and supersonic flight capabilities which utilize travelling tail units with circular arc motions, connected with the rear fuselage by means of two arm-frames that swing upward and rearward and vice versa, to generally increase stability and control of aircraft during low-speed flight and to reduce accidents at zero altitude operations.

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: 3447761 (1969-06-01), Whitener et al.
patent: 3454239 (1969-07-01), Frey
patent: 3469803 (1969-09-01), Schmielau
patent: 3493197 (1970-02-01), Spearman
patent: 3936017 (1976-02-01), Blythe

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