Shifting horizontal tail with helical motions

Details Shifting horizontal tail with helical motions Shifting horizontal tail with helical motions

1976-03-17

1977-05-24

Blix, Trygve M.

Aeronautics and astronautics

Aircraft, heavier-than-air

Airplane sustained

244 43, 244 87, B64C 510

Patent

active

040250075

ABSTRACT:
An aircraft having a bulky propulsion system positioned near its symmetrical axis and utilizing two shifting horizontal tail halves that are moved rearwards and forwards along the outer side walls of two rear wing cantilevers for varying flight operations. The two horizontal tail halves change their lateral inclination angles during the shifting operations, and the propulsive jet streams of the engines are discharged between the two rear wing cantilevers.

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

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