发明名称 Concentrated load transport balloon - has load attachment point situated under front third of fuselage
摘要 <p>The dirigible balloon has a fuselage with an attachment point (2) for a concentrated load (10), situated under the front third of the fuselage. The fixed loads, e.g. the driving engines (9) can be mounted at the rear, typically on the rigid tail assembly (8) which is in turn supported on inflated tubes (6,7) forming ribs extending from the rear of the hull. The load attachment point can be secured to a rigid structure of between 0.2 and 0.5 times the diameter of the hull, and attached by internal suspension ropes to the envelope assembly.</p>
申请公布号 FR2452422(A1) 申请公布日期 1980.10.24
申请号 FR19790007696 申请日期 1979.03.27
申请人 COSTES DIDIER 发明人
分类号 B64B1/22;(IPC1-7):64B1/22 主分类号 B64B1/22
代理机构 代理人
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