Modular detachable powered nacelle for drones
A modular and unmanned aerial vehicle technology, applied in the direction of aircraft power plant, aircraft power plant components, aircraft parts, etc., can solve the problems that successful modification is not easy to do, and replacement cannot be completed quickly, so as to facilitate debugging, Ease of maintenance and replacement
Active Publication Date: 2018-05-25
北京奇正数元科技股份有限公司
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Problems solved by technology
[0003] Since the power system of the existing UAV is fixedly connected with the body, it will bring a lot of inconvenience to the actual use of the UAV, for example:
[0004] (1) When the drone performs different tasks, it may need to replace different power systems. For example, when flying on a plateau, it needs to replace a power system with a greater thrust. Since the power system of the drone is fixedly connected to the body, Therefore, it is necessary to operate on the entire body, and the replacement cannot be completed quickly
[0005] (2) When you want to design a modification on the existing UAV, such as: modify it into a tilting power vertical take-off and landing UAV, because the power system of the UAV is fixedly connected with the body, the modification is successful not easy to do
Method used
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[0025] The following describes the present invention in detail with reference to the drawings and specific embodiments.
[0026] Reference figure 1 The modular detachable power nacelle of the unmanned aerial vehicle of the present invention adopts a modular design and includes four major parts: a power part 10, a support part 20, a wing connection part 30 and an electronic adjustment part 40. Among them, the power part 10 and the wing connecting part 30 are installed at the front end and the rear end of the support part 20 respectively, and the ESC part 40 is installed inside the support part 20.
[0027] The structures of the power part 10, the support part 20, the wing connecting part 30 and the ESC part 40 are respectively introduced below.
[0028] 1. Power part
[0029] Reference figure 2 , The power part 10 includes: a motor 101 and a motor base 102.
[0030] The motor 101 is fixedly installed in the motor base 102 by screws, and a circlip 103 and a rotating shaft 104 are provid...
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The invention discloses a modularized and detachable type power nacelle of an unmanned aerial vehicle. The modularized and detachable type power nacelle adopts modularized design and is wholly connected with an outer-section wing and an inner-section wing through bolts; the power nacelle is composed of a power part, a supporting part, a wing connecting part and an electric debugging part; the power part and the wing connecting part are mounted at the front end and rear end of the supporting part respectively; the electric debugging part is mounted in the supporting part. The modularized and detachable type power nacelle of the unmanned aerial vehicle has the beneficial effects that the power nacelle is designed into a modularized and detachable type structure, so that the modularized and detachable type power nacelle can be very convenient to maintain and replace and the modularized design is easier to debug.
Description
Technical field [0001] The invention relates to a power nacelle, in particular to a modular and detachable power nacelle of an unmanned aerial vehicle, belonging to the technical field of unmanned aerial vehicles. Background technique [0002] The power system of the drone is used to provide thrust for the flight of the drone, which is a very important part of the design and manufacture of the drone. [0003] Since the power system of the existing UAV is fixedly connected with the body, it will bring a lot of inconvenience to the actual use of the UAV, such as: [0004] (1) When the UAV performs different tasks, it may need to replace different power systems. For example, when flying on a plateau, you need to replace the power system with a larger thrust. Because the power system of the UAV is firmly connected with the body, Therefore, it is necessary to operate on the entire body, and the replacement cannot be completed quickly. [0005] (2) When you want to design a modification on...
Claims
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IPC IPC(8): B64D29/02
CPCB64D29/02
Inventor 杨砚恒
Owner 北京奇正数元科技股份有限公司