All electrical self-contained fuel control system for a burner i

Aeronautics and astronautics – Aircraft control – Airship control

Patent

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244 30, B64B 162

Patent

active

040822397

ABSTRACT:
A thermal airship having a hull formed of an elongate soft envelope of flexible material being aerodynamic shaped for horizontal flight with tail members at the aft end for controlling the direction of horizontal flight and a gondola carried below the hull with a power propelling member for driving the airship horizontally and a pressurizing inflation opening in the base of the envelope with a hot air pressure generating system for superpressurizing the envelope and a controlled fuel operated burner for heating the air coming into the envelope and a thermocouple suspended within the envelope near the top but spaced from the outer wall with a variable control for the thermocouple controlling the fuel valve for the burner so as to maintain the hot air within the envelope at a predetermined controlled temperature.

REFERENCES:
patent: 3170658 (1965-02-01), Yost
patent: 3174534 (1965-03-01), Weber
patent: 3881863 (1975-05-01), Creuz

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