Transverse folding type four-rotor aircraft
A four-rotor aircraft, horizontal folding technology, applied in the direction of aircraft, rotorcraft, motor vehicles, etc., can solve the problems of inconvenient transportation and use, large volume, etc., and achieve the effect of simple structure, portability and operation
- Summary
- Abstract
- Description
- Claims
- Application Information
AI Technical Summary
Problems solved by technology
Method used
Image
Examples
specific Embodiment approach
[0015] The preferred embodiment of the laterally folding quadrotor aircraft of the present invention is:
[0016] It includes a fuselage, the side of the fuselage is provided with a plurality of transverse folding arms, the lower part of the fuselage or the transverse folding arms is provided with a plurality of detachable landing gears, and the ends of the transverse folding arms are provided with Has detachable rotors.
[0017] The horizontal folding support arm includes an inner arm and an outer arm, one side of the inner arm and the outer arm are hinged to each other, the other side of the inner arm is provided with a pin shaft, and the other side of the outer arm is provided with an elastic When the inner arm and the outer arm are unfolded, the protrusion is stuck on the pin shaft, and when the inner arm and the outer arm are folded, the protrusion is separated from the pin shaft.
[0018] The lower part of the fuselage or the transverse folding arm is provided with a so...
specific Embodiment
[0020] Such as Figure 1 to Figure 5b As shown, it includes detachable landing gear 1, fuselage 2, detachable rotor 3, lateral folding arm 4 and other parts.
[0021] Such as figure 1 As shown, the detachable rotor 3 can be quickly folded and supported by the horizontal folding arm 4, and the specific folding method is as follows Figure 2a , 2b , as shown in 2c, its support and fixing methods are as follows Figure 3a , 3b shown. The dismounting and fixing mode of detachable undercarriage 1 are as follows: Figure 4a , 4b As shown, the partially enlarged schematic diagram of the detachable landing gear 1 is shown as Figure 5a , 5b shown.
[0022] Each component is described as follows:
[0023] (1) The four horizontal folding arms of the aircraft can be folded horizontally, and are in the folded state during storage and transportation, such as Figure 2c As shown, the transportation space can be reduced. When working, the arm can be opened, such as Figure 2a sh...
PUM
Login to View More Abstract
Description
Claims
Application Information
Login to View More 


