Single-drive automatic aligning and clamping mechanism for air vehicle
A clamping mechanism, single-drive technology, applied in aircraft parts, equipment for loading and unloading goods, transportation and packaging, etc., can solve the problem that the clamping and fixing process cannot be automated, ignore the relationship between the load and the center of the aircraft, and increase the difficulty of aircraft control. and other problems, to achieve the effect of good clamping effect, simple structure and fast centering
Pending Publication Date: 2017-06-23
BEIJING HONGWAN WEIPENG INFORMATION TECH
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AI Technical Summary
Problems solved by technology
In the whole process of transportation, if the clamping and fixing cannot be realized quickly and reliably, the whole transportation process will be affected and the transportation efficiency will be directly affected. Therefore, it is necessary to ensure the fast and effective realization of the clamping and fixing
[0003] In the prior art, the clamping and fixing process generally cannot be automated and requires manual participation; or the central relationship between the load and the aircraft is ignored, which increases the difficulty of controlling the aircraft
Method used
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Embodiment
[0014] Embodiment: a kind of aircraft single-drive automatic centering clamping mechanism, such as Figure 1-Figure 4 As shown, the single-drive automatic centering clamping mechanism includes a guide frame 1, a guide disc 2, a guide piece 3, a short connecting rod 4, a long connecting rod 5, a driving unit 6, a baffle 7, a bearing 8, and a bearing 2 9 , bearing three 10; described guide frame 1, guide disc 2 are disc-shaped; described guide frame 1 and described baffle plate 7 coaxial, are fixedly connected by screw; Described guide disc 2 and described guide The frame 1 and the baffle plate 7 are coaxial, are located between the guide frame 1 and the baffle plate 7, and are assembled in the inner hole of the guide frame 1, and the guide disc 2 can be placed on the guide frame 1 for rotation; the long connecting rod 5 connects the guide disc 2 and the short connecting rod 4; the driving unit 6 is fixed on the baffle 7, and the driving unit 6 has an output shaft The short con...
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The invention provides a single-drive automatic aligning and clamping mechanism for an air vehicle. The mechanism comprises a guide frame, a guide disc, multiple guide sheets, a short connecting rod, a long connecting rod, a drive unit, a baffle and bearings; the guide frame and the guide disc is in a disc shape; the guide frame and the baffle are coaxial and are fixedly connected through a threaded part; the guide disc is coaxial with the guide frame and the baffle, is located between the guide frame and the baffle and assembled in an inner hole of the guide frame and can rotate in the inner hole of the guide frame; the long connecting rod is connected with the guide disc and the short connecting rod; the drive unit is fixed to the baffle and provided with an output shaft; the short connecting rod is connected with the long connecting rod and the output shaft of the drive unit; the guide sheets have the same shape, are symmetrically distributed along the center and are all connected with the bearings through rotating shafts; the bearings are installed in sliding grooves, which are symmetrically formed along the center, of the guide frame and sliding groves, which are symmetrically formed along the center, of the guide disc. The mechanism is rapid to align, good in clamping effect and stability and high in transportation efficiency.
Description
technical field [0001] The invention relates to a centering clamping mechanism, in particular to a single-drive automatic centering clamping mechanism capable of rapidly aligning an aircraft with a load center, having a stable fixing effect and improving transportation efficiency. Background technique [0002] Aircraft such as fixed-wing aircraft, helicopters, multi-rotor UAVs, etc., need to clamp and fix transport items during flight transportation. Its mode is either direct connection or connection through transition parts. In the whole process of transportation, if the clamping and fixing cannot be realized quickly and reliably, the whole transportation process will be affected and the transportation efficiency will be directly affected. Therefore, it is necessary to ensure the fast and effective realization of the clamping and fixing. [0003] In the prior art, the clamping and fixing process generally cannot be automated and requires manual participation; or the centra...
Claims
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IPC IPC(8): B64D9/00
CPCB64D9/00
Inventor 张延伟鞠健项天远蔡立峰
Owner BEIJING HONGWAN WEIPENG INFORMATION TECH