发明名称 AIRSHIP BALLAST SYSTEM
摘要 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.
申请公布号 US2007001054(A1) 申请公布日期 2007.01.04
申请号 US20050064313 申请日期 2005.02.23
申请人 BOSCHMA JAMES H JR;SULLIVAN CALLUM R;MCNABB MICHAEL 发明人 BOSCHMA JAMES H.JR.;SULLIVAN CALLUM R.;MCNABB MICHAEL
分类号 B64B1/58 主分类号 B64B1/58
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