AeroVantage

 

To Primary Index

Combining the advantages of speed and distance with that of vertical takeoff, landing and hover.

 

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Coaxial

Higher induced velocity for cruise

 

Tandem

Twice the disk area for hover

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Overview of Effective Aerodynamic Disk Area

 

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Overview:

            ~ 1x2 ~           

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Cruise ~ Single Contra-rotating PropRotor

 

Hover ~ Dual PropRotors

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      ~ 2x4 ~

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Cruise ~ Twin Contra-rotating PropRotors

Hover ~ Quad PropRotors

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~ NeoCaley ~

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Transition Mechanism:

Transition Mechanisms under Consideration

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The Objective:

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Primary Grouping:

Overview of 1x2

 Overview of 2x4

Overview of NeoCaley

Concerns & Tasks

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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Introduction Page | SynchroLite Home Page | Electrotor Home Page | UniCopter Home Page | Nemesis Home Page | AeroVantage Home Page

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; November 6, 2014

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.