FLYING BODY
PCT No. PCT/EP96/04590 Sec. 371 Date Apr. 28, 1998 Sec. 102(e) Date Apr. 28, 1998 PCT Filed Oct. 23, 1996 PCT Pub. No. WO97/16343 PCT Pub. Date May 9, 1997For an aircraft (1) having a balancing torque and including a motor-driven propeller (5) arranged on a central axis (3), and a useful load contai...
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Sprache: | cze ; eng |
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Zusammenfassung: | PCT No. PCT/EP96/04590 Sec. 371 Date Apr. 28, 1998 Sec. 102(e) Date Apr. 28, 1998 PCT Filed Oct. 23, 1996 PCT Pub. No. WO97/16343 PCT Pub. Date May 9, 1997For an aircraft (1) having a balancing torque and including a motor-driven propeller (5) arranged on a central axis (3), and a useful load container (6), a solution should be provided which would insure that the aircraft is capable of carrying useful loads in a stable flying attitude and with simple control means. This is achieved by that the central propeller (5) driven by the drive motor (4), on one hand, and relative thereto, the motor (4) and/or torque-balancing means arranged thereon, on the other hand, are rotatable in opposite directions and together are supported for rotation relative to the useful load container. At that, the drawing figure to be published: FIG. 1. |
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