Multicopter with Detachable Wing
First Claim
1. An unmanned aerial vehicle assembly, comprising:
- a plurality of propeller drives comprising a propeller attached to an electric motor,a rigid frame wherein the said plurality of propeller drives are mounted,said electric motors wherein each of the rotor axes are in a vertical orientation,said rigid frame wherein a detachable wing can be mounted,whereby the said unmanned aerial vehicle can ascend, descend, hover, and move forward with or without the said detachable wing.
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Accused Products
Abstract
An unmanned aerial vehicle (UAV) that can operate both as a conventional multicopter with no wing attached, or, it can operate as a winged multicopter. The detachable wing design used in the invention provides versatility without compromising performance; the wing attachment receptacles add no weight to the wingless multicopter configuration because they also function as the leg receptacles. In one embodiment, the base multicopter configuration is a quad-copter with four propeller drives. Four tubular receptacles, two forward and two aft, provide attachment points for the vertical struts of a detachable rectangular shaped wing, these vertical struts also function as the legs of the multicopter. The wing is fabricated using lightweight struts and rip stop nylon fabric which can be easily folded into a compact shape using quick release pins. In another embodiment, the wing is fabricated using a foam core. In both embodiments, the angle of the detachable wing can be adjusted to optimize lift and drag in the forward thrust, tilted position of the multicopter.
32 Citations
13 Claims
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1. An unmanned aerial vehicle assembly, comprising:
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a plurality of propeller drives comprising a propeller attached to an electric motor, a rigid frame wherein the said plurality of propeller drives are mounted, said electric motors wherein each of the rotor axes are in a vertical orientation, said rigid frame wherein a detachable wing can be mounted, whereby the said unmanned aerial vehicle can ascend, descend, hover, and move forward with or without the said detachable wing. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10)
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11. An unmanned aerial vehicle assembly, comprising:
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a plurality of propeller drives comprising a propeller attached to an electric motor, a rigid frame comprising a centrally located housing and a plurality of tubular spars extending outward from the said housing, a plurality of motor mounts each attached to the distal end of each said tubular spar, wherein each of the said propeller drives are mounted to each of the said motor mounts, a plurality of lateral struts wherein each said lateral strut is attached to two said motor mounts providing a means of stiffening the fixation of the said motor mounts, whereby the said unmanned aerial vehicle can extend the propeller drives outward for added flight stability while adding minimal weight. - View Dependent Claims (12, 13)
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Specification