Aerodynamics - Vibration Alleviation
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Joined: Nov 2000
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From: Vancouver, BC, Canada
Aerodynamics - Vibration Alleviation
High Frequency Individual Blade Control for Alleviation of Rotor Induced Vibration.
US Patent # 6,000,000.1/2 +/-
Abstract:
The leading edge of a rotor blade to consist of an un-depleted nuclear fuel-rod, purchased from Russia, before the US drives the price too high. The fuel-rod ionizes the air in front of the blade. An electromagnet is located directly behind this fuel-rod, and it directs the air flow to the upper or lower surface of said blade.
More Abstract:
The probability of high frequency is determined by the magnet's polarization rate.
Even more Abstract:
The probability of parenting is determined by the thickness of the pilot's lead shorts.
US Patent # 6,000,000.1/2 +/-
Abstract:
The leading edge of a rotor blade to consist of an un-depleted nuclear fuel-rod, purchased from Russia, before the US drives the price too high. The fuel-rod ionizes the air in front of the blade. An electromagnet is located directly behind this fuel-rod, and it directs the air flow to the upper or lower surface of said blade.
More Abstract:
The probability of high frequency is determined by the magnet's polarization rate.
Even more Abstract:
The probability of parenting is determined by the thickness of the pilot's lead shorts.
Avoid imitations
Joined: Nov 2000
Aviation Qualifications: ATPL
Posts: 15,110
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From: Wandering the FIR and cyberspace often at highly unsociable times
Would really like to get involved in this one; unfortunately I have something much more important to do.
HERE FIDO - TIME FOR YOUR BATH!......
HERE FIDO - TIME FOR YOUR BATH!......
