Looking for breakthrough ideas for innovation challenges? Try Patsnap Eureka!

Airplane component attitude adjusting and butting system based on four numeric control positioners, attitude adjusting platform and mobile bracket and corresponding method

A technology of numerical control positioner and mobile bracket, which is applied in the direction of aircraft parts, aircraft assembly, transportation and packaging, etc. It can solve the problems of not meeting the requirements of accurate docking and assembly of large parts, low quality, small volume, etc., and improve the accuracy of assembly Accuracy and assembly efficiency, application adaptability effect

Inactive Publication Date: 2011-04-06
ZHEJIANG UNIV
View PDF5 Cites 154 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

At present, my country's aircraft attitude adjustment and docking system with independent intellectual property rights has just entered the application stage. Most of the popular assembly systems based on robot technology in the market are suitable for production lines with small size and low quality, and cannot meet the requirements of aircraft fuselage sections. Accurate docking assembly requirements for large parts

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
  • Airplane component attitude adjusting and butting system based on four numeric control positioners, attitude adjusting platform and mobile bracket and corresponding method
  • Airplane component attitude adjusting and butting system based on four numeric control positioners, attitude adjusting platform and mobile bracket and corresponding method
  • Airplane component attitude adjusting and butting system based on four numeric control positioners, attitude adjusting platform and mobile bracket and corresponding method

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0048] Such as Figure 1-5As shown, the aircraft component attitude adjustment and docking system based on four CNC positioners, attitude adjustment platforms and mobile brackets, including mobile brackets 3, attitude adjustment platforms 4, multiple CNC positioners 5, and CNC positioner group guide rails 6 , host computer 8, ball hinge connection and laser tracker 7; mobile bracket 3 includes U-shaped frame 15, jack bolt 16 and cone screw 17, cone screw 17 is hollow, and jack bolt 16 is set inside, and adjustment The bolt holes on the posture platform 4 are connected and fixed, and the U-shaped bracket 15 is provided with a wide strap and a belt take-up device for fixing the fuselage section; Sliding table 12, slider guide rail 13, CNC positioner base 14, absolute grating ruler and servo motor, two attitude-adjusting CNC positioners share one CNC positioner base 14 and electrical cabinet, and the electrical cabinet is placed in two CNC positioners. Between machine bases, the...

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 an airplane component attitude adjusting and butting system based on four numeric control positioners, attitude adjusting platform and mobile bracket and a corresponding method. The system comprises a mobile bracket, an attitude adjusting platform, numeric control positioners, a numeric control positioner group guide rail, an upper computer, a ball hinge connection mechanism and a laser tracker. The attitude adjusting and butting method includes the following steps: 1) the mobile bracket is fixed onto the attitude adjusting platform and is supported by the numeric control positioner; 2) fuselage is arranged in place; 3) a site assembly coordinate system and a local coordinate system solidified on the fuselage are established; 4) the current attitude of fuselage A is measured and calculated; 5) motion path of the numeric control positioner is planned; 6) the attitude of the fuselage A is adjusted; 7) coordinates of a butt hole are measured and target attitude offuselage B is calculated; 8) the current attitude of fuselage B is calculated; 9) the attitude of the fuselage B is adjusted; 10) fuselage is butted; 11) the system is reset; 12) the mobile bracket is removed. The invention has the advantages that digitalized attitude adjusting and butting of airplane components are realized and adaptability is strong.

Description

technical field [0001] The invention relates to an aircraft component attitude adjustment and docking system and method based on four numerically controlled locators, attitude adjustment docking and moving brackets. Background technique [0002] In aircraft manufacturing, to complete the final assembly of the aircraft, the pose adjustment of the fuselage section must be realized first, and then the docking work can be carried out. The fuselage section is a special operation object, which has the characteristics of large volume and high quality. At the same time, it requires high accuracy in attitude adjustment and positioning, and the stress and deformation of the fuselage section should be small after assembly. At present, my country's aircraft attitude adjustment and docking system with independent intellectual property rights has just entered the application stage. Most of the popular assembly systems based on robot technology in the market are suitable for production lin...

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): B64F5/00B64F5/10
Inventor 柯映林何丹青陈亮王青李江雄毕运波俞慈君黄鹏金涨军
Owner ZHEJIANG UNIV
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Patsnap Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Patsnap Eureka Blog
Learn More
PatSnap group products

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

© 2024 PatSnap. All rights reserved.Legal|Privacy policy|Modern Slavery Act Transparency Statement|Sitemap|About US| Contact US: help@patsnap.com