|
AeroVantage |
|||
|
|
|
||
|
Coaxial |
Tandem |
||
|
for Speed |
for Lift |
Overview: Effective Aerodynamic Disk Area |
|
![]()
Overview:
|
|
|
||||||||||
|
Cruise ~ Single Counterrotating Prop Rotor |
|
Hover ~ Dual PropRotors |
|||||||||
![]()
|
|
|
|
|
Cruise ~ Twin Counterrotating Prop Rotors |
Hover ~ Quad PropRotors |
|
![]()
Earlier Transition Mechanism:

The above is a mobile of an early method. It is not the preferred one.
This is the Currently Preferred Method
Additional Transition Mechanisms under Consideration
![]()
The Objective:
![]()
DESIGN, MAKE & BUY
: ~|
Control (Flight & Power) |
||
![]()
OTHER:
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; May 19, 2011
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.