Vertical take-off and landing aircraft capable of...

Details Vertical take-off and landing aircraft capable of... Vertical take-off and landing aircraft capable of...

B - Operations, Transporting

64

C

244/6

B64C 29/00 (2006.01)

Patent

CA 2010417

ABSTRACT OF THE DISCLOSURE A vertical take-off and landing aircraft which can be of basically very simple construction and compact size includes an air flow chamber and an impulsion device such as an engine-driven propeller for driving a high-velocity air flow through the air flow chamber. The high-velocity air flow can be directed to flow across the upper surfaces of the aircraft wings, to thereby generate dynamic lift during take-off or landing operation, and can be directed to flow out from the rear of the aircraft fuselage to produce propulsive force during normal forward flying operation. - 1 -

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