Airship ballast system

Aeronautics and astronautics – Aircraft control – Stabilizing weights

Reexamination Certificate

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Details

C244S097000, C165S041000

Reexamination Certificate

active

11064313

ABSTRACT:
An airship ballast system includes an engine driven propeller and a cooling tube that is positioned coplanar with the propeller and outside its tip path. One end of the cooling tube is connected to receive exhaust gases from the engine while the other end is connected to a ballast tank. In operation, exhaust gases from the engine are cooled as they transit the cooling tube, and water condensed from the cooled exhaust gases is pumped to the ballast tank to maintain a ballast for the airship.

REFERENCES:
patent: 1653603 (1927-12-01), Schroder
patent: 1853376 (1932-04-01), Powelson et al.
patent: 2018535 (1935-10-01), Rober
patent: 2310767 (1943-02-01), Durr
patent: 2330632 (1943-09-01), Seligman
patent: 3204401 (1965-09-01), Serriades
patent: 3927526 (1975-12-01), Tedrow
patent: 3930625 (1976-01-01), Krivka
patent: 4813632 (1989-03-01), Woodhouse
patent: 5537974 (1996-07-01), Palmer
patent: 5722249 (1998-03-01), Miller, Jr.
patent: 5816181 (1998-10-01), Sherman, Jr.
patent: 6650541 (2003-11-01), Simon et al.

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