Accession Number : ADD002547
Title : Stowable Airfoil Structure.
Descriptive Note : Patent Application,
Corporate Author : DEPARTMENT OF THE AIR FORCE WASHINGTON D C
Personal Author(s) : Look,Lance G
Report Date : 24 Mar 1976
Pagination or Media Count : 19
Abstract : The stowable airfoil structure described in the patent application is a tapered, high aspect ratio, retractable and foldable wing for aircraft which provides minimum aerodynamic drag during launch and minimum space for ground storage. The airfoil utilizes a forward leading edge box section to which is attached a plurality of spanwise channels hinged together for movement in a chordwise direction. Retraction of these elements takes place by the utilization of suitable actuators so as to move the hinged elements forwardly in a nested position thereby substantially reducing the width of the wing or airfoil which is then folded to lie along side the fuselage of an aircraft.
Descriptors : *Aerodynamic control surfaces, Taper, Wings, Retractable, Folding, Aerodynamic drag, Width, Airfoils
Subject Categories : Aircraft
Distribution Statement : APPROVED FOR PUBLIC RELEASE