Aircraft having buoyant gas balloon

Aeronautics and astronautics – Aircraft – lighter-than-air – Balloons

Patent

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Details

244 2, 244 3, 2441181, 244115, 244153A, B64B 156, B64B 166

Patent

active

043657729

ABSTRACT:
An aircraft is provided utilizing a spherical balloon filled with buoyant gas such as helium at a pressure substantially greater than atmospheric so that its dimensions are substantially unaffected by changes in atmospheric pressure or temperature. The aircraft may take the form of a self-propelled and self-contained airship, or may be merely a passive device for providing lift and intended to be towed by and controlled from a helicopter. The spherical balloon is mounted on a normally horizontal axle having end portions projecting from opposite sides of the balloon, and includes a rigid load supporting yoke including two arms extending upwardly from a central load supporting structure and each with an upper end suspended from the axle.

REFERENCES:
patent: 1087946 (1914-02-01), Hutson
patent: 1426726 (1922-08-01), Gilbert
patent: 1905345 (1933-04-01), Dandini
patent: 3017138 (1962-01-01), Flint
patent: 3369774 (1968-02-01), Struble, Jr.
patent: 3658278 (1972-04-01), Batchelor
patent: 3976265 (1976-08-01), Doolittle
patent: 4195694 (1980-04-01), Gizzarelli
patent: 4207026 (1980-06-01), Kushto

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