Rotorcraft with Variable Incident Wing
作者： Jennifer D. Langston , Walter C. Joiner , Daniel B. Robertson , Dudley E. Smith , David J. Ludolph
DOI:
关键词: Forward flight 、 Wing 、 Structural engineering 、 Wing configuration 、 Aerospace engineering 、 Engineering 、 Wing twist 、 Landing gear 、 Mast (sailing) 、 Fuselage 、 Thrust
摘要: A twin-rotor side-by-side compound rotorcraft has a fuselage and variable incident wing assembly that pivots relative to fuselage. The aircraft also landing gear tail fin assembly. is pivotally attached the fuselage, includes members, engines fixedly mounted members or another area of rotorcraft, mast at fixed angle members. Then may be located near rotorcraft. capable pivoting about pivot axis, thereby allowing orientation in least hover position forward flight position. rotors provide additional thrust wings lift, when
lens.org 参考文章(20)
Frederick M Taylor, V/stol aircraft with variable tilt wing ,(1970)
Barth W. Shenk, Compound tilting wing for high lift stability and control of aircraft ,(2001)
Evan A. Fradenburgh, Mechanism for synchronously varying diameter of a plurality of rotors and for limiting the diameters thereof ,(1977)
Iii Joseph Stuart, Control system for interconnected propellers ,(1962)
David W Main, Pitch control device for rotor blades ,(1943)
Claudius Dornier, Florian Windischbauer, Aircraft with engine pods tiltable about a transverse axis ,(1990)
Kenneth Sye Ballew, Avia tilting-rotor convertiplane ,(2004)
Russel G. Perkins, John C. Vaughan, Tilt-rotor wing fold mechanism and method ,(1985)
Paul E. Bender, Gadi Karmi, Roberto Padovani, Matthew S. Grob, Method and apparatus for signal combining in a high data rate communication system ,(2002)