The tests of the RC model of ornithopter, by which are realized two of my inventions and my ideas about the properties of the flapping wing are the grounds for this DECLARATION.
By exactly correspondence of the elasticity of the wing to the mass of the ornithopter, it is possible to build ornithopters with every desired mass.
By realization of principle of distribution of the mass of the wing and correlation to the elasticity, the wings act effectively at high loading too.
By virtue of "Ornithopter" and "Wing of ornithopter" inventions, the wings act maximum effectively at different frequencies of the flapping motions at take off and flight.
The control through change of angle of incidence of the wings is very effectively at take off and flight with low velocity.
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