Multi-shaft aircraft arm installing structure
A multi-axis aircraft and installation structure technology, applied in the field of aircraft, can solve the problems of inconvenient use and complex installation structure of the aircraft arm, and achieve the effects of reducing weight, improving production efficiency and product quality, and simplifying the frame structure
Inactive Publication Date: 2014-07-23
TIANJIN TIANHENG ZHIYUAN TECH CO LTD
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AI Technical Summary
Problems solved by technology
[0004] The present invention provides a multi-axis aircraft machine with a simple structure, which can reduce the weight of the aircraft itself and reduce the volume of the aircraft to facilitate the storage and use of the aircraft in order to solve the technical problems of the aircraft arm installation structure complex and inconvenient use in the known technology. Arm Mounting Structure
Method used
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Embodiment Construction
[0012] In order to further understand the invention content, characteristics and effects of the present invention, the following examples are given, and detailed descriptions are as follows in conjunction with the accompanying drawings:
[0013] see figure 1 , a multi-axis aircraft arm installation structure is characterized in that: there is a fuselage upper plate 1 and a fuselage lower plate 2, the fuselage upper plate 1 and the fuselage lower plate 2 are carbon plates with light weight and good toughness, and the fuselage The body panel 1 and the fuselage lower panel 2 are rib-shaped frame structures. The fuselage upper plate 1 and the fuselage lower plate 2 are arranged parallel to each other. Between the fuselage upper plate 1 and the fuselage lower plate 2, a fuselage arm connector 3 is arranged, and the fuselage arm connector 3 is arranged close to the periphery of the fuselage upper plate 1 and the fuselage lower plate 2 . The machine arm connector 3 is connected to ...
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The invention relates to a multi-shaft aircraft arm installing structure. The multi-shaft aircraft arm installing structure is characterized by being provided with an aircraft body upper plate, an aircraft body lower plate, an arm connecting part arranged between the aircraft body upper plate and the aircraft body lower plate and close the peripheries of the aircraft body upper plate and the aircraft body lower plate, and an elastic clamp piece located on the periphery of the aircraft body upper plate, integrally manufactured with the aircraft body upper plate and capable of being in clamped connection with an aircraft arm so as to avoid pin shaft rotation around the aircraft arm, wherein the aircraft body upper plate and the aircraft body lower plate are arranged in parallel. A main aircraft frame structure is simplified, the weight of the main aircraft frame structure is decreased, and the production efficiency and the product quality of an aircraft can be improved. In addition, the aircraft arm in the multi-shaft aircraft arm installing structure can be bent, and storage and usage of the aircraft are facilitated.
Description
technical field [0001] The invention belongs to the technical field of aircraft, and in particular relates to an arm installation structure of a multi-axis aircraft. Background technique [0002] The multi-axis aircraft has the characteristics of low cost, easy operation, high flexibility and ultra-low altitude flight. It can use the camera equipment on board to take pictures, obtain image data, and send the acquired image data back to the ground. Multi-axis aircraft has been widely used in aerial photography, power line inspection, aerial reconnaissance, simulated flight, subsidized unmanned aerial vehicles and other fields, for monitoring evidence collection and observation of special locations, etc., and can realize the transmission of on-site video images for command It is an important tool for obtaining information for the reader to make decisions and judge. In addition, multicopters with simple structures are also widely loved in the field of toys. [0003] The arm i...
Claims
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Login to View More IPC IPC(8): B64D27/26B64D27/24A63H27/14
CPCY02T50/40
Inventor 吴智勇
Owner TIANJIN TIANHENG ZHIYUAN TECH CO LTD