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Punching operation method for aircraft with camera

A technology of aircraft and camera, which is applied in the field of aircraft drilling operations, can solve the problems of adjusting the position of high-altitude operations and not providing them, and achieve the effect of improving synchronization and improving efficiency

Inactive Publication Date: 2021-06-29
黎图(晋江)科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] To sum up, in the prior art, there is no one that can adjust the position of high-altitude work according to the actual situation of the top wall, and at the same time drill holes and implant nails. The drill bit and fixing nails between the top of the wall perform combined actions to improve drilling efficiency, reduce motor consumption, and can adjust the drilling position with a camera. The aircraft drilling method with a camera can adjust the drilling position.

Method used

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  • Punching operation method for aircraft with camera
  • Punching operation method for aircraft with camera
  • Punching operation method for aircraft with camera

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Embodiment Construction

[0047] The present invention will be further described below in conjunction with the examples, but the present invention is not limited in any way, and any transformation or substitution made based on the teaching of the present invention belongs to the protection scope of the present invention.

[0048] Such as Figure 1-6 As shown, the aircraft with an adjustable punching position with a camera of the present invention includes a housing 1, a drive motor 2, a rotating shaft 3, a drilling shaft 4, a drill bit 6, a fixing nail 7, a linkage mechanism 8, and a fixing nail sleeve 9. Push mechanism 10, camera 18, lifting blade 21, horizontal propulsion mechanism 22, ring chuck 27, upper ring 28, lower ring 29, rotating motor A33 and rotating motor B36, drive motor 2 is fixedly installed in the shell The inside of body 1, and the driving motor is a double-axis motor, the rotating shaft 3 is connected to the lower end of the driving motor 2, the rotating shaft 3 passes through the o...

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Abstract

The invention discloses a punching operation method for an aircraft with a camera, which can adjust the high-altitude operation position through the camera according to the actual condition of a top wall, can perform drilling and fixing nail implanting operation simultaneously, can adjust the positions of fixing nails, and can adapt to the condition that different fixing nail angles are needed, meanwhile, a pushing mechanism is arranged at the bottoms of the fixing nails, the pushing mechanism can be pressurized by starting an oil pump, linkage punching can be conducted between a drill bit and the fixing nails, and the drill bit and the fixing nails alternately advance, and therefore the drilling efficiency can be improved through the combined action of the drill bit and the fixing nails implanted between wall tops, the motor consumption is reduced, and the fixing nails can enter the wall further.

Description

technical field [0001] The invention relates to the technical field of high-altitude operations, in particular to an aircraft drilling method with a camera. Background technique [0002] In the prior art, the technology of using an aircraft to punch holes is still immature, and the cost is relatively high. For example, Patent Document 1 discloses a wireless device installation device, which uses a UAV aircraft to punch holes on the top wall to place wireless The equipment is installed on the top of the wall, but the installation device leaves the aircraft itself on the top of the wall while installing the wireless equipment, which causes a great waste of energy. On the plate 324, the mounting plate 324 moves down along with the trigger block 111. Therefore, when starting to drill the top wall, the mounting rod does not have enough upward driving force to drill the drill rod into the top of the wall, and its drilling effect Poor, and the installation rod is not a standard dr...

Claims

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Application Information

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IPC IPC(8): B28D1/14B28D7/00B28D7/02
CPCB28D1/14B28D7/005B28D7/02B64U2101/00
Inventor 王明丹王金伟陈小蓉
Owner 黎图(晋江)科技有限公司
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