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Title:
FLAP DESIGN FOR FIXED WING AIRCRAFT
Document Type and Number:
WIPO Patent Application WO/2015/183347
Kind Code:
A3
Abstract:
A new flap design for fixed wing aircraft increases stability and performance of the aircraft through a wide range of air speeds and flight dynamics when implemented on the flap of a fixed wing aircraft. The flap comprises a step configuration on the underside of the flap. Aircraft may be retrofitted with flaps having the new design.

Inventors:
THOMPSON ROY (US)
Application Number:
PCT/US2015/015152
Publication Date:
January 21, 2016
Filing Date:
February 10, 2015
Export Citation:
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Assignee:
THOMPSON ROY (US)
International Classes:
B64C9/16; B64C3/50
Foreign References:
RU2072944C11997-02-10
EP0210399B11989-05-31
US5551651A1996-09-03
Attorney, Agent or Firm:
FLINT, Nancy (#424Plantation, Florida, US)
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