Method for rapidly drilling riveting holes in body structure of airplane

A technology of aircraft fuselage and drilling method, which is applied to aircraft parts, drilling molds for workpieces, transportation and packaging, etc. It can solve the problems of large riveting hole spacing error, high labor intensity, poor riveting quality, etc., and achieve reduction Space error, reduce labor intensity, and ensure the effect of riveting quality

Active Publication Date: 2015-08-12
HARBIN
View PDF8 Cites 2 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Its disadvantages are: high labor intensity, low work efficiency, large spacing error of riveting holes, and poor riveting quality

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
  • Method for rapidly drilling riveting holes in body structure of airplane
  • Method for rapidly drilling riveting holes in body structure of airplane
  • Method for rapidly drilling riveting holes in body structure of airplane

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0024] Embodiment 1, drilling riveting holes on the outer surface of frame 4 of the aircraft fuselage.

[0025] 1. Manufacture the elastic ruler: use spring steel to make the elastic ruler. The length of the elastic ruler is 450mm, the width is 20mm, and the thickness of the elastic ruler is 1mm;

[0026] 2. Drilling process holes: Drill 2 process holes on the aircraft fuselage structure 2, the aperture of the positioning hole is 3mm, use the marking method to determine the position of the process holes, and drill the process holes with a hand-held drilling machine;

[0027] 3. Drill equidistant holes on the elastic ruler 1:

[0028] 3.1. Drilling the elastic ruler process hole: the diameter of the elastic ruler process hole is 3mm;

[0029] 3.2. Drilling equidistant guide holes of the elastic ruler: According to the structural drawings of the aircraft fuselage, the number of riveting holes between the two process holes is determined to be 20, and the distance between the two...

Embodiment 2

[0032] Embodiment 2, drilling riveting holes on the outer surface of frame 4 of the aircraft fuselage.

[0033] 1. Manufacture the elastic ruler: use spring steel to make the elastic ruler. The length of the elastic ruler is 650mm, the width is 20mm, and the thickness of the elastic ruler is 1mm;

[0034] 2. Drilling process holes: Drill 2 process holes on the aircraft fuselage structure 2, the aperture of the positioning hole is 3mm, use the marking method to determine the position of the process holes, and drill the process holes with a hand-held drilling machine;

[0035] 3. Drill equidistant holes on the elastic ruler 1:

[0036] 3.1. Drilling the elastic ruler process hole: the diameter of the elastic ruler process hole is 3mm;

[0037] 3.2. Drilling equidistant guide holes for the elastic ruler: According to the structural drawings of the aircraft fuselage, the number of riveting holes between the two process holes is determined to be 30, and the distance between the tw...

Embodiment 3

[0040] Embodiment 3, drilling riveting holes on the outer surface of the Y45O beam of the aircraft fuselage.

[0041] 1. Manufacture the elastic ruler: use spring steel to make the elastic ruler. The length of the elastic ruler is 650mm, the width is 20mm, and the thickness of the elastic ruler is 1mm;

[0042]2. Drilling process holes: Drill 2 process holes on the aircraft fuselage structure 2, the aperture of the positioning hole is 3mm, use the marking method to determine the position of the process holes, and drill the process holes with a hand-held drilling machine;

[0043] 3. Drill equidistant holes on the elastic ruler 1:

[0044] 3.1. Drilling the elastic ruler process hole: the diameter of the elastic ruler process hole is 3mm;

[0045] 3.2. Drilling equidistant guide holes for the elastic ruler: According to the structural drawings of the aircraft fuselage, the number of riveting holes between the two process holes is determined to be 30, and the distance between t...

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

PropertyMeasurementUnit
widthaaaaaaaaaa
thicknessaaaaaaaaaa
lengthaaaaaaaaaa
Login to view more

Abstract

The invention belongs to an airplane assembling technology, relating to an improved method for drilling riveting holes in a body structure of an air plane. The method is characterized by comprising the following drilling steps: manufacturing an elastic ruler; drilling process holes; drilling equidistant holes in the elastic ruler (1); drilling the riveting holes in the body structure of the airplane. According to the method for rapidly drilling the riveting holes of the body structure of the airplane, the labor intensity is greatly lightened, the working efficiency is improved, the interval error of the riveting holes is reduced, and the riveting quality is ensured.

Description

technical field [0001] The invention belongs to the aircraft assembly technology and relates to the improvement of the drilling method for the riveting holes of the aircraft fuselage structure. Background technique [0002] When drilling the riveting holes of the aircraft fuselage structure, since the aircraft fuselage structure has a profile, the riveting holes on the profile are arranged in a straight line when the profile is unfolded into a plane, and the spacing of the riveting holes is equal. The current practice is: determine the positions of all riveting holes on the profile surface by marking 1, and then drill. Its disadvantages are: high labor intensity, low work efficiency, large spacing error of riveting holes, and poor riveting quality. Contents of the invention [0003] The purpose of the invention is: to propose a fast drilling method for riveting holes in aircraft fuselage structures, so as to reduce labor intensity, improve work efficiency, reduce the spac...

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): B23B35/00B23B47/28
CPCB23B35/00B23B47/28B23B2215/04B23B2247/04
Inventor 苏振龙沈伟张元江李绍飞
Owner HARBIN
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

Browse by: Latest US Patents, China's latest patents, Technical Efficacy Thesaurus, Application Domain, Technology Topic.

© 2024 PatSnap. All rights reserved.Legal|Privacy policy|Modern Slavery Act Transparency Statement|Sitemap