Processing device and processing method for assembly hole at root of inner cavity side wall of composite material component

A technology of composite materials and processing devices, which is applied in metal processing equipment, grinding drive devices, and parts of grinding machine tools, etc., to achieve the effects of flexible adjustment, elimination of axial and radial gaps, and reduction of deformation

Active Publication Date: 2019-06-25
沈阳大工先进技术发展有限公司
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  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0011] The above several patented technologies are all aimed at the assembly hole with the processed hole in an open structure, while for figure 1 There is no relevant literature record on the machining method and equipment of the aircraft deep cavity assembly hole in the semi-closed structure shown

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  • Processing device and processing method for assembly hole at root of inner cavity side wall of composite material component
  • Processing device and processing method for assembly hole at root of inner cavity side wall of composite material component
  • Processing device and processing method for assembly hole at root of inner cavity side wall of composite material component

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Embodiment Construction

[0054] The specific embodiments of the present invention will be described in detail below in conjunction with the technical solutions and accompanying drawings.

[0055] Such as Figure 1-7 As shown, the processing device for the assembly hole at the root of the inner cavity side wall of the composite material part, the processing device is a six-degree-of-freedom cantilever processing device, including the X-direction linear motion part 7, the Y-direction linear motion part 6, and the Z-direction linear adjustment part 8. X' axis cantilever hole making unit 9, Y' axis rotation adjustment part 10 and Z axis rotation adjustment part 11;

[0056] The Y-direction linear motion part 6 is fixed on the UAV assembly truss 5, the X-direction linear motion part 7 is connected to the slider of the Y-direction linear motion part 6, and the Z-axis rotation adjustment part 11 is connected to the X-direction linear motion part 11. On the slider of component 7, the Z-direction linear adjus...

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Abstract

The invention discloses a device and method to machine root fitting holes in the sidewall of an inner chamber of a composite part. The device is a six-DOF (degree of freedom) cantilever machining device, comprising an X-directional linear moving part, a Y-directional linear moving part, a Z-directional linear adjusting part, an X'-axis cantilever hole-making unit, a Y'-axis rotary adjusting part and a Z-axis rotary adjusting part. A pneumatic motor is used as a rotary spindle power source, so that the device has small size and high speed and is suitable for machining boreholes in composites innarrow spaces. A grinding hole-making mode herein can provide reduced X'-axis force, thereby reducing deformation of cantilever structure and improving drilling precision. The six-DOF cantilever machining device and a fitting hole machining method provided herein provide integral machining for fitting holes in a deep cavity of semi-enclosed structure by single tool adjusting on a single station,and coaxiality and dimensional precision can be ensured for fitting holes of different diameters in a multi-wall plate.

Description

technical field [0001] The invention belongs to the technical field of unmanned aerial vehicle assembly, and relates to a method for processing an assembly hole at the root of an inner cavity side wall of a connecting section of a wing and a fuselage of a carbon fiber composite unmanned aerial vehicle. Background technique [0002] UAV is an unmanned aircraft operated by radio remote control equipment and its own program control device. Compared with manned aircraft, UAV has the advantages of small size, low cost, and convenient use, and is often more suitable for use in harsh environments. It can be used for military reconnaissance, aerial photography, disaster rescue, surveying and mapping and many other purposes. Since unmanned aerial vehicles are of great significance to future air combat, all major military countries in the world are stepping up the research and development of unmanned aerial vehicles. [0003] The application of composite materials on drones greatly r...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B24B27/06B24B27/00B24B47/20
CPCB24B27/0023B24B27/0641B24B47/20
Inventor 高航卢守相
Owner 沈阳大工先进技术发展有限公司
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