发明名称 HYBRID THERMAL AIRSHIP
摘要 An airship comprises a shell, a gas storage system, an air storage system, a cargo storage system, a heating system, and a propulsion system. The shell encompasses a volume. The gas storage system is located within the volume, wherein the gas storage system is capable of storing a lighter than air gas. The air storage system is located within the volume, wherein the air storage system is capable of storing heated air. The heating system is capable of heating air. The propulsion system is capable of propelling the shell during flight.
申请公布号 US2009314879(A1) 申请公布日期 2009.12.24
申请号 US20080131655 申请日期 2008.06.02
申请人 KWOK DAVID W;RAWDON BLAINE KNIGHT;SKORUPA JOHN ANTHONY 发明人 KWOK DAVID W.;RAWDON BLAINE KNIGHT;SKORUPA JOHN ANTHONY
分类号 B64B1/06;B64B1/00;B64B1/20;B64B1/22 主分类号 B64B1/06
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