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Aircraft part machining and clamping mechanism

A technology of clamping mechanism and parts, which is applied in the field of aircraft parts processing clamping mechanism, can solve the problems of only one specification of clamping hinge, the above-mentioned device is overturned, and the staff is inconvenient to work, so as to achieve a wide range of use and not easy to lose , Ease of use

Inactive Publication Date: 2020-04-03
义乌市鼎寒机械设备有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0004] However, the above-mentioned device still has the following obvious defects during use: the above-mentioned device cannot be well fixed on the ground during use, which makes it inconvenient for the staff to use force. When the staff tightens the above-mentioned device When the fastening parts are hinged, it is easy to cause the above-mentioned device to roll over, causing the staff to work inconveniently, and the clamping joint of the above-mentioned device has only one specification, which cannot be well adapted to other cylindrical aircraft parts with different diameters, resulting in the use of the above-mentioned device. not wide range

Method used

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Embodiment Construction

[0024] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.

[0025] see Figures 1 to 4 , the present invention provides a technical solution:

[0026] A clamping mechanism for processing aircraft parts, including a working plate 5, the top of the working plate 5 is fixedly connected with a fixed seat 6, the top of the fixed seat 6 is movably connected with a rotating shaft 7, and the top of the rotating shaft 7 is fixedly connected with a clamping plate 35 , the inside of the clamping plate 35 is provided with a guide...

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Abstract

The invention discloses an aircraft part machining and clamping mechanism. The aircraft part machining and clamping mechanism comprises a working plate. The top of the working plate is fixedly connected with fixed seats. The top of each fixed seat is movably connected with a first rotating shaft. The top of each first rotating shaft is fixedly connected with a clamping plate. A first guide rail isarranged in each clamping plate. The bottom of the working plate is fixedly connected with a height adjusting screw. The bottom of the height adjusting screw is fixedly connected with a height adjusting seat. The bottom of the height adjusting seat is fixedly connected with a stabilizing plate. According to the aircraft part machining and clamping mechanism, the screw, telescopic seats and telescopic columns are adjusted through the height of the bottom of the working plate, the distance between a workbench of the device and the ground can be effectively adjusted, and a first connecting plateand a second connecting plate can be freely adjusted through the clamping plate, so that the height between a hexagonal clamping groove and a circular limiting plate and the workbench can be freely adjusted according to actual requirements, so that the device is more convenient to use in the use process, high in practicability and very worthy of popularization.

Description

technical field [0001] The invention relates to the technical field of clamping processing equipment, in particular to a clamping mechanism for processing aircraft parts. Background technique [0002] During the processing of aircraft parts, parts need to be positioned, especially tubular parts. According to different processing procedures, tubular parts need to be in different states during positioning. At this time, different positioning mechanisms need to be designed. The manufacturing cost is increased, and the positioning mechanism is constantly replaced, which increases the error. [0003] In the prior art, a clamping mechanism for aircraft parts processing with the notification number CN207495011U belongs to the field of aircraft processing equipment, including a base, a first clamping part, a second clamping part, a first mounting seat, and a first positioning part , the second mounting seat and the second positioning part, the first clamping part is hinged on the b...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B25B11/00B64F5/10
CPCB25B11/00B64F5/10
Inventor 李浩阳
Owner 义乌市鼎寒机械设备有限公司