Tiltrotor articulated wing extension
作者： Brent Chadwick Ross , Steven Ray Ivans
DOI:
关键词:
摘要: An aircraft has a wing, pylon carried by the at least one of rotor system component and drive disposed within pylon, wing extension component, wherein is foldable relative to selectively reduce an overall space occupied aircraft.
lens.org 参考文章(19)
Timin Mitchell E, Strand Torstein, Levinsky Ely S, Vtol aircraft having free-floating wings and independently tilting propellers ,(1967)
Thomas F. Fitzgibbon, Wing fold actuator system for aircraft ,(1991)
Bob Collins, John J. Corrigan, Frank B. Stamps, Mark E. Dreier, Wing extension control surface ,(2009)
Abe Karem, Tilt outboard wing for tilt rotor aircraft ,(2006)
Wayne S. Steffier, William E. Rumberger, Wing pivot structure ,(1992)
Russel G. Perkins, John C. Vaughan, Tilt-rotor wing fold mechanism and method ,(1985)
James E Lipp, Frank N Fleming, Newton H Anderson, Osear A Swanson, Folding wing aircraft ,(1940)
Abe Karem, Compact aircraft wing folding systems and methods ,(2011)
Jennifer D. Langston, Walter C. Joiner, Daniel B. Robertson, Dudley E. Smith, David J. Ludolph, Rotorcraft with Variable Incident Wing ,(2009)
Abe Karem, Combination spar and trunnion structure for a tilt rotor aircraft ,(2009)