Vectored thrust airship

Aeronautics and astronautics – Aircraft – lighter-than-air – Airship and helicopter sustained

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Details

244 1713, 244 2, B64B 134

Patent

active

045911126

ABSTRACT:
An airship with provisions for vectored thrust provided by a plurality of controllable pitch rotor thrust producing units attached to the elongated aerostat hull spaced from and on opposite sides of the center of overall mass of the airship. The pitch control systems for the rotors of all thrust units include collective and cyclic pitch controls of the main, horizontally rotating lifting rotors and the control systems are interconnected to be operable by a master control which establishes both similar and differential pitch settings of the rotors of selected thrust units in a manner to establish vectored thrust in directions which establish the required amounts of vertical lift, propulsion thrust, trim and control forces to control all flight aspects of the airship.

REFERENCES:
patent: 1615002 (1927-01-01), Avery
patent: 1821158 (1931-09-01), Howland
patent: 1879345 (1932-09-01), Lawrence
patent: 3008665 (1961-11-01), Piasecki
patent: 3096047 (1963-07-01), Dunn, Jr.
patent: 3222012 (1965-12-01), Piasecki
patent: 3656723 (1972-04-01), Piasecki et al.
patent: 3746279 (1973-07-01), Maciolek et al.
patent: 3801044 (1974-04-01), Moore
patent: 3889902 (1975-06-01), Madet

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