发明名称 Aircraft with a fuselage substantially designed as an aerostatic lifting body
摘要 The airship has a fuselage (1) built as an aerostatic buoyant body, having propellers (11,12,13,14) with respective shafts (121) and drive units (7,8,9,10). The respective propeller shaft (121) rotation plane (113) can be tilted all round relative to a drive shaft (104) of the allocated propeller drive, and the hull also does duty as aerodynamic float in a ship devoid of activatable aerodynamic steering system. The hull can be circular or elliptical to give an elliptical section whose upper shell is more steeply curved than the flatter bottom shell. The hull is fitted with a stiffener ring in its equatorial belt with the ring also of elliptical section in its exterior.
申请公布号 IL130655(D0) 申请公布日期 2000.06.01
申请号 IL19980130655 申请日期 1998.01.02
申请人 KUENKLER HERMANN 发明人
分类号 B64B1/06;B63H5/125;B64B1/30;B64B1/32;B64C11/02;B64C27/28;B64C27/52;B64C29/00;B64D35/00;(IPC1-7):B64B 主分类号 B64B1/06
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