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Flexible fixture device and method for processing long stringers of aircraft composite materials

A technology of flexible fixtures and composite materials, applied to metal processing machinery parts, positioning devices, manufacturing tools, etc., can solve problems such as single form, poor reliability, and high cost, and achieve the effects of convenient operation, low cost, and high efficiency

Active Publication Date: 2017-05-17
SHANGHAI AIRCRAFT MFG +1
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  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0005] Aiming at the problems of poor reliability, single form and high cost existing in the existing aircraft composite material long stringer milling fixture, the present invention provides a flexible clamping device and method for processing aircraft composite material stringer, which can adapt to the long stringer of aircraft composite material. The transformation of the geometric shape of the truss structure realizes the reliable positioning and clamping of the composite long truss structure of the aircraft

Method used

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  • Flexible fixture device and method for processing long stringers of aircraft composite materials
  • Flexible fixture device and method for processing long stringers of aircraft composite materials
  • Flexible fixture device and method for processing long stringers of aircraft composite materials

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Embodiment Construction

[0030] In the following detailed description of the preferred embodiment, reference is made to the accompanying drawings which form a part hereof. The accompanying drawings show, by way of example, specific embodiments in which the invention can be practiced. The illustrated embodiments are not intended to be exhaustive of all embodiments in accordance with the invention. It is to be understood that other embodiments may be utilized and structural or logical changes may be made without departing from the scope of the present invention.

[0031] Such as Figure 1 to Figure 2 As shown in , the flexible clamp device of the present invention mainly includes a movable chuck assembly 10 , a positioning block assembly 20 and an end positioning assembly 30 . Wherein the movable chuck assembly 10 is installed on the CNC machining machine tool, the movable chuck assembly 10 includes a base 11, a fixed chuck 12 and a movable chuck 13, the fixed chuck 12 is fixedly connected with the ba...

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Abstract

The invention provides a flexible clamp device for machining airplane composite material stringer and a method thereof. The flexible clamp device comprises a movable chuck assembly and a locating block assembly. The movable chuck assembly comprises a base, a fixed chuck and a movable chuck, the fixed chuck is fixedly connected with the base. The movable chuck is arranged on the base in a sliding mode and can move towards or away from the fixed chuck. The locating block assembly is arranged between the fixed chuck and the movable chuck and comprises a fixed locating block and a movable locating block. The fixedly locating block is connected to the fixed chuck, and a clearance is reserved between the fixed locating block and the top surface of the base. The movable locating block is connected to the movable chuck, and a clearance is reserved between the movable locating block and the top surface of the base. When the movable chuck moves towards the fixed chuck, the movable chuck drives the movable locating block to move towards the fixed locating block, so that a stringer is clamped between the movable locating block and the fixed locating block.

Description

technical field [0001] The invention relates to a flexible fixture device and a method for processing aircraft composite material stringers. The flexible fixture device can be installed on the numerical control processing equipment, and is used for the milling and cutting processing of the aircraft composite material long truss structure. Background technique [0002] As a typical structural part on the aircraft, the stringer is an important part of the aircraft wing panel, fuselage panel and empennage panel. The characteristics of this kind of parts are: it is mainly made of carbon fiber composite materials, and its edges need to be trimmed; it has a remarkable slender structure, with a length of up to 20,000mm and a width of only about 100mm; each aircraft contains long trusses. The quantity is very large, about 150 or so. These stringer structures are similar in form but vary in size. [0003] At present, the domestic aircraft composite material long truss is mainly pr...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B23Q3/00
CPCB23C3/002B23Q3/062
Inventor 龚佑宏杨霓虹邵严张冬梅韩舒花磊
Owner SHANGHAI AIRCRAFT MFG
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