Blade Flyer

VTOL Conventional flight
Non-Published Patent Allowed - Abstract

Features

Business Plan Contents

Solicitation

The original version convinced Darold Cummings to convince Empirical Systems Aerospace to develop a presentation (2.9 MB PPT) for DARPA, which we later learned had a transition during 1 G turn without loss of altitude requirement. With no analysis program available to model the complex aerodynamics during transition, a physical model was necessary to perform wind tunnel and captive tests.
 
Original version with perch.
Segmented hub version animation and 3-D images.
Segmented hub version components 3-D images
Extended segmented hub version animation and 3-D images.
Extended segmented hub in VTOL mode

Contact: Bill Holmes via email or 661-305-9465


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