The invention relates to an assembled-type unmanned aerial vehicle empennage. The assembled-type unmanned aerial vehicle empennage comprises an empennage framework, a flat empennage stabilizer, a lifting empennage, an empennage rudder, a fuselage, a fuselage tail part, a fixing shaft pin hole and a positioning shaft pin hole. The flat empennage stabilizer is butted with a socket at the fuselage tail part, so that the a fixing pin and a pin hole, a slot and a stabilizing square wall, as well as a lug boss and the socket are coincidently matched respectively; then the fixing shaft pin hole correspondingly coincides with the positioning shaft pin hole; finally, the fixing shaft pin hole and the positioning shaft pin hole are locked by using a fixing shaft pin, and therefore, the flat empennage stabilizer and the fuselage tail part can be connected and fixed into an integral structure. The functions and the effects of the assembled-type unmanned aerial vehicle empennage are the same as those of a traditional unmanned aerial vehicle empennage designed and manufactured integrally. The assembled-type unmanned aerial vehicle empennage has the positive effects that the flat empennage stabilizer and the fuselage are manufactured respectively, so that manufacturing dies are remarkably reduced, the manufacturing cost is greatly saved and the manufacturing difficulty is greatly reduced; the assembled-type unmanned aerial vehicle empennage is convenient for package and transportation of goods and is convenient to assemble, disassemble, repair and maintain.
Assembled-type unmanned aerial vehicle empennage
2015-12-30
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
Empennage type unmanned aerial vehicle launching and recovering device
European Patent Office | 2021
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