AeroVantage

To Primary Index

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VTOL aircraft with 2x4 PropRotor (2-state disk area)

 

Cruise ~ Twin Counterrotating PropRotors

2 x 4

Hover ~ Quad PropRotors

 

For larger view of the craft click on either of the above drawings.

 

The Objective:

Animations:

Proposed method; Item1642

Lengthening the upper arms on 1642, to make its gap and stager closer to 1655 below.

Proposed method; Item1655

Primary Grouping:

Overview

Workup of Flying Wing UAV w/ 2x4 PropRotor - Overview

Concerns & Tasks

DESIGN, MAKE & BUY: ~ ~ ~ ~ ~ ~ The light gray texts below do not yet have linked pages.

PropRotor

Motor

Weight & Balance

Fuselage

Transition Mechanism

Dimension, Area & Drag

Landing Gear

Control

Trim, Stability & Control

Instrument

Power Storage

Vibration Analysis

Electrical

 

Special Tool

OTHER:

Aerodynamics

Intermeshing Information

Miscellaneous

Flight Dynamics

Helicopters - Outside

Regulations

Mechanics

Helicopters - Inside

Composites

Electrics

Rotor Concepts:

CNC Workstation

To Search This Site

Go to Google ~ Enter; 'the desired words or phrases etc' ~ Then append the entry with; 'UniCopter'.

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 20, 2008

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.