VARIABLE PARAMETER ROTARY WING

摘要

The present application takes into account an approach adapted to aviation which, through rigid wings, forces and imposes the flight envelope thereof into onerous and non-modifiable configurations. A specific modification to the principle of known airplane technology which represents the abandonment of stationary wings for a rotary double wing constitutes the present application, referred to as Pica-Gyr. Conventional airplanes comprise a mechanical rigidity which by default leads to crashes in the event of not adhering to regulations. Flight configuration is rendered difficult, maneuverability which is unsuitable for the circumstances is learnt by our brain but is not natural, the rigid wing tool is not adapted for useful speeds which are different on the same airplane, and the rigid wing imposes minimal speeds and behaviors to which one must conform and respect in any given circumstances. More flexible behaviors in terms of lift variables enable the easier adaptation of flight configurations and practical demands, and ensure translations at high speeds and safe vertical departure. The solution of the equation of the demand for flexibility of use is integrating a modifiable lift parameter by modifying the driving of the speed of the rotary wing, driven by at least one separate engine for this purpose or coupled to the translation engine. The principle of the double rotary wing is in fact the main lift technique that is adaptable in the known field of aeronautics, but replaces the stationary wings of airplanes, and reduces drag, fuel consumption, vibration, and noise.