B463
OTHER: ~
Helicopter - Inside - Single Rotor - Rotor X Wing![]()
Overview:
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Detail Pages:
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OTHER: Helicopter - Inside - Single Rotor - Rotor X Wing - Flight-Control |
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OTHER: Helicopter - Inside - Single Rotor - Rotor X Wing - Improving Lift During Transformation |
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OTHER: Helicopter - Inside - Single Rotor - Rotor X Wing - Random Notes |
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OTHER: Helicopter - Inside - Single Rotor - Rotor X Wing - Concerns |
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Related Pages:
For proposed means having a stopped rotor see:
OTHER: ~ Rotor Concepts - Traversing Ideal TwistOTHER: Miscellaneous - Thoughtless Ideas - Stopped Rotor
OTHER: Helicopter - Inside - Coaxial / Stopped Rotors - Electric UAV
For related concept see:
OTHER: ~ Rotor Concepts - Reverse Velocity Utilization![]()
Related Patent:
5,405,104 Stopped rotor aircraft utilizing a flipped airfoil X-wing
4,953,098 Higher harmonic control system for X-Wing aircraft
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Initially displayed: September 16, 2002 ~ Latest revision; December 12, 2007
The above application of active traversing blade twist in a helicopter is openly and publicly disclosed on the Internet to negate an entity from patenting it, to the exclusion of all others whom may wish to use it. ~ Reference patent law 35 U.S.C. 102 A person shall be entitled to a patent unless - (a) the invention was known ... by others in this country, ..., before the invention thereof by the applicant for patent.