Assembly tool and assembly technological process for horizontal tail of unmanned aerial vehicle
By designing the assembly tooling of the flat tail of the drone, including support, cross beam and longitudinal beam, the problems of high subjectivity and difficult to guarantee quality in traditional assembly methods are solved, and precise assembly and efficient production of the flat tail are achieved.
CN119527568AActive Publication Date: 2025-02-28SHANGHAI JIAOTONG UNIV +1
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Patent Information
- Application Number
- CN202311109980.4
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- Filing Date
- 2023-08-30
- Publication Date
- 2025-02-28
- Estimated Expiration
- 2043-08-30
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Figure CN119527568A_ABST
Abstract
The assembly tool comprises a support, two cross beams and two longitudinal beams, the cross beams and the longitudinal beams are horizontally arranged and fixedly installed on the support, any cross beam is provided with a supporting groove, a main beam of the horizontal tail of the unmanned aerial vehicle is placed on the supporting groove, and the main beam of the horizontal tail of the unmanned aerial vehicle is fixedly installed on the support. A plurality of wing rib clamping grooves are formed in any longitudinal beam, a plurality of wing ribs of the horizontal tail of the unmanned aerial vehicle are placed on the wing rib clamping grooves respectively, and a height adjusting device is arranged at the bottom of the support. The supporting groove is formed in the cross beam, the main beam of the horizontal tail of the unmanned aerial vehicle is placed on the supporting groove, the wing rib clamping grooves are formed in the longitudinal beam, the wing ribs of the horizontal tail of the unmanned aerial vehicle are placed on the wing rib clamping grooves correspondingly, and the height adjusting device is arranged at the bottom of the support. The requirements for high wing shape precision and high assembly requirements of the horizontal tail of the unmanned aerial vehicle can be met, the assembly efficiency can be improved, and the cost can be reduced.
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