Compound tool applicable to high-speed and accurate holing on aircraft panel

A technology for aircraft siding and composite cutters, which is applied in the direction of manufacturing tools, drilling accessories, drilling/drilling equipment, etc., can solve the problems of increasing the amount of cutting tools, low efficiency, and reducing efficiency, so as to improve the accuracy of the hole surface and improve Economic benefits, the effect of reducing the amount of tools

Inactive Publication Date: 2012-11-28
ZHEJIANG UNIV
View PDF5 Cites 12 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

In order to meet the accuracy requirements of fastener connecting holes, the current process is to drill the initial hole with a drill bit, then use a large-diameter drill bit to ream the hole, and then use a series of reamers with increasing diameters to ream the holes. The amount of reaming per knife It is about 0.5mm, so each connection hole needs to be processed many times to complete, and it needs a lot of tools and processing time, the efficiency is low, and there are many factors affecting the accuracy
In addition, with the existing technology, after the connection hole is processed to meet the diameter requirement, it is necessary to perform spot facing separately, which further increases the amount of tools and reduces the efficiency
And because the connection hole and the taper socket are processed separately, the coaxial accuracy of the hole and the taper socket is affected

Method used

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
View more

Image

Smart Image Click on the blue labels to locate them in the text.
Viewing Examples
Smart Image
  • Compound tool applicable to high-speed and accurate holing on aircraft panel
  • Compound tool applicable to high-speed and accurate holing on aircraft panel
  • Compound tool applicable to high-speed and accurate holing on aircraft panel

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0015] figure 1 Shown is the structure of the fastener hole 13 in the workpiece 12, consisting of a hole wall 15 and a conical socket 14 at the top of the hole. like image 3 As shown, after the compound tool drills a through hole on the workpiece 12, it continues to feed, and the countersink 8 of the compound tool is used to process the conical dimple 14, and the transition fillet between the hole wall 15 and the conical dimple 14 is also processed. When the tool needs to be replaced with a new tool due to damage, the position of the countersink 8 can be determined by using the end face 17 of the tool handle 16 to locate the step positioning surface 11, thereby ensuring the depth 18 of the taper pocket.

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to view more

PUM

No PUM Login to view more

Abstract

The invention discloses a compound tool applicable to high-speed and accurate holing on an aircraft panel. The compound tool is provided with a double-helical side edge, the helical angle of the side edge is 30-40 degrees, a bottom edge is divided into three sections, i.e., a chisel edge, rough machining edges and finish machining edges; the included angle of the two rough machining edges is 120-150 degrees, and the included angle of the two finish machining edges is 60-65 degrees; a dimpling edge is connected with the helical side edge; and after holes are drilled through, the tool is fed continuously, and the dimple machining is finished by utilizing the dimpling edge. The compound tool disclosed by the invention has the advantages that the hole drilling, hole reaming and dimpling can be finished once without need of tool change, and the roughness of the machining surfaces of the holes reaches Ra1.6.

Description

technical field [0001] The invention belongs to the technical field of aircraft assembly, and relates to a compound tool suitable for high-speed and precise hole making of aircraft wall panels. Background technique [0002] An aircraft is made up of a large number of parts connected by fasteners. In order to connect parts with fasteners, holes must be made in aircraft parts. Holes for fasteners on aircraft require low surface roughness and high precision. Moreover, in order to ensure the smooth outer surface of the aircraft and reduce air resistance, the fastener holes on the outer skin surface of the fuselage and wing must be spot-faced after drilling. After the fastener is inserted into the connecting hole, the nail head and the skin surface flush. In order to meet the accuracy requirements of fastener connecting holes, the current process is to drill the initial hole with a drill bit, then use a large-diameter drill bit to ream the hole, and then use a series of reamer...

Claims

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to view more

Application Information

Patent Timeline
no application Login to view more
Patent Type & Authority Applications(China)
IPC IPC(8): B23B51/08
Inventor 董辉跃马超虹柯映林李江雄
Owner ZHEJIANG UNIV
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Try Eureka
PatSnap group products