Hovering flapping-wing aircraft and its control method
A flapping aircraft and hovering technology, applied in the field of aircraft, can solve the problem of few reports of flapping aircraft. In the 1990s, the bat jointly developed by the California Institute of Technology and the University of Los Angeles in California successfully flew for the first time. In 2002, Stanford The pilot jointly developed by the research center and the University of Toronto has been successfully tested, and many domestic universities have also carried out problems such as easy operation and control, and the control method is convenient and reliable.
- Summary
- Abstract
- Description
- Claims
- Application Information
AI Technical Summary
Problems solved by technology
Method used
Image
Examples
Embodiment Construction
[0019] The present invention will be further described below in conjunction with drawings and embodiments. see Figure 1 to Figure 6 , the flapping-wing aircraft capable of hovering includes a fuselage 1, a flapping wing 2, an empennage 3, a power mechanism 5 and a control mechanism 6, and the fuselage 1 includes a front fuselage 101, a cabin 102 and a rear fuselage 103, and the front The fuselage 101, the cabin 102 and the rear fuselage 103 are connected in sequence; both sides of the cabin 102 are connected with an inverted triangular plate 4 through a rotating shaft, and a straight edge at the upper end of the inverted triangular plate 4 is hinged with the inner end of the flapping wing 2, and the bottom of the inverted triangular plate 4 is hinged. Connect the first rocker arm 601 through the first pull rod 602 of the control mechanism 6;
[0020] The connection between the nacelle 102 and the rear fuselage 103 is provided with a partition 105, and one side of the partiti...
PUM
Login to View More Abstract
Description
Claims
Application Information
Login to View More 


