AeroVantage

		AeroVantage
$Description: Description: Description: C:\Helicopter\Web_Page\Arrow_Left.gif$ ▬ $Description: Description: Description: C:\Helicopter\Web_Page\Arrow_Left.gif$	$Description: Description: Description: C:\Helicopter\Web_Page\Arrow_Up.gif$ ▬▬ $Description: Description: Description: C:\Helicopter\Web_Page\Arrow_Up.gif$
Coaxial	Tandem
for Speed	for Lift		To Primary Index
__________	_________		_______________
		Overview of Effective Aerodynamic Disk Area

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Overview:

~ 1x2 ~
$Description: Description: Description: C:\Helicopter\Web_Page\1681_1x2_Micro_Cruise.gif$		$Description: Description: Description: C:\Helicopter\Web_Page\1681_1x2_Micro_Hover.gif$
Cruise ~ Single Counterrotating PropRotor		Hover ~ Dual PropRotors

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~ 2x4 ~
$Description: Description: Description: C:\Helicopter\Web_Page\1718_Micro_Cruise.gif$		$Description: Description: Description: C:\Helicopter\Web_Page\1718_Micro_Hover.gif$
Cruise ~ Twin Counterrotating PropRotors		Hover ~ Quad PropRotors

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~ NeoCaley ~

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Transition Mechanism:

This is the Currently Preferred Method

Additional Transition Mechanisms under Consideration

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The Objective:

A VTOL aircraft that is aerodynamically superior to other existing and proposed craft. This is due to the generation of a low velocity thrust from a large disk area during hover and a high velocity thrust from a small disk area during cruise.

To aerodynamically reduce the EFFECTIVE total disk area of the PropRotors in cruise by 50% from their PHYSICAL total disk area in hover. Thereby creating a PropRotor VTOL craft that has;

A greater figure of merit in hover then current tilt-rotors, and
A faster speed and greater efficiency in cruise then current tilt-rotors.

To negate any downwash on the wings and fuselage until the wings are carrying a significant portion of the lift.
See; Effective Aerodynamic Disk Area

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Primary Grouping:

DESIGN, MAKE & BUY: ~

PropRotor	Motor	Weight & Balance
WingRotor	Power Train	Dimension, Area & Drag
Fuselage & Wing	Transition Mechanism	Trim, Stability & Control
Landing Gear	Control (Flight & Power)	Vibration Analysis
Instrument	Power Storage	Special Tool
	Electrical

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OTHER:

Aerodynamics	Intermeshing Information	Miscellaneous
Flight Dynamics	Helicopters - Outside	Regulations
Mechanics	Helicopters - Inside	Composites
Electrics	Rotor Concepts:	CNC Workstation

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Initially displayed: January 30, 2008 ~ Posted on PPRuNe; January 31, 2008 ~ Posted on Rotary Wing: January 31, 2008 ~ Posted on Eng-Tips: February 1, 2008 ~ Latest revision; June 11, 2013

The above utility invention 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.