Hovering type folding wing lifting body aircraft based on variable centroid technology
A wing lift and variable center of mass technology, which is applied in the field of aviation aircraft, can solve problems such as difficult maneuvering and control, decreased aircraft stability, and large wing size, so as to facilitate transportation and delivery, improve flight performance and stability, and reduce weight. The effect of small storage space
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[0018] See attached figure 1 , 3 , a hoverable folding wing lifting body aircraft based on variable center of mass technology, which includes: a lifting body fuselage 1, two front wings 41 connected to the lifting body fuselage 1, and two rear wings 42 adopt wing bodies Fused tandem wing layout, the aircraft also includes: variable center mechanism 2, vector thrust mechanism 3 and wing rotation and folding mechanism 4;
[0019] The lifting body fuselage 1 is a fuselage that can provide lift for the aircraft as a whole during flight, so that the wing area can be effectively reduced, and the aircraft still has superior air cruise capability;
[0020] Two front wings 41 and two rear wings 42 adopt the wing-body fusion type tandem wing layout, which is: the front wing 41 and the wing 42 are arranged in pairs before and after and share the aerodynamic layout of the lift; this layout can Reduce the wingspan of the wing, making the aircraft more compact and flexible;
[0021] The ...
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