Single side soft absorption type automatic drilling robot

A robot and adsorption technology, applied in the field of automatic hole making technology and robots, can solve the problems of low degree of automation, poor stability of aircraft quality, low precision, etc., and achieve the effect of improving quality and efficiency, reducing processing difficulty and improving work quality.

Active Publication Date: 2012-11-07
SHANGHAI AIRCRAFT MFG +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, there are many problems in my country's large aircraft manufacturing: low degree of automation, slow processing speed of connection holes, poor reliability; low precision; low degree of intelligence, aircraft assembly holes mostly rely on manual tool hole making, and the overall accuracy level is H9 , the international level has reached H8, which seriously restricts fatigue resistance and safe service life
The quality stability of my country's aircraft is poor and the efficiency is low, and there is a big gap with foreign countries. The reason is that my country's assembly and hole making technology and equipment technology level is relatively low

Method used

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  • Single side soft absorption type automatic drilling robot
  • Single side soft absorption type automatic drilling robot
  • Single side soft absorption type automatic drilling robot

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Embodiment Construction

[0052] The present invention will be further described in detail below in conjunction with the accompanying drawings.

[0053] join figure 1 and figure 2 As shown, the present invention consists of seven parts: a flexible rail assembly 1, an XY-moving carrier assembly 2, an X-motion drive assembly 3, an actuator feed module 4, a spindle assembly 5, a positioning assembly 6 and an air source assembly 7.

[0054] see figure 1 As shown, the high-pressure air pump 71 provides a high-pressure air source, and the high-pressure air generated by it is delivered to the vacuum chuck 13 in the flexible track assembly 1 through the air guide tube 72, wherein the two ends of the air guide tube 72 are connected to the high-pressure air pump 71 and the air guide reversing tube 14, The control of the flow rate of the air flow through the air guide reversing tube 14 enables the vacuum chuck to be adsorbed on the surface of the workpiece. The high-pressure gas enters the vacuum suction cup ...

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Abstract

The invention provides a single side soft absorption type automatic drilling robot which is applicable to operation such as hold drilling, reaming, dimpling and the like at wings and fuselage parts, and the machining for materials which are hard to machine such as titanium alloy (Ti) and composite materials (CPRF) is realized. The robot is fixed at an expected machining area by using a gas source provided by a vacuum generator and by using a vacuum chuck; and a soft track can adapt to different machining curves according to different curvature. The positioning of a drilled hole and the adjustment of the verticality of a drill bit are realized according to a drill plate. A pneumatic main shaft is adopted as the main shaft of the robot; and in combination of an ultrasonic vibration machining technology, the quality and efficiency of the machining are improved; the machining difficulty is reduced; the current detection at a feeding direction can be carried out in real time during the hole making process; and the protection and precise control for the machining process are realized.

Description

technical field [0001] The present invention generally relates to automatic hole-making technology and robot technology, and more specifically, the present invention relates to vibration hole-making technology, a hole-making robot with a single-side flexible track, and a drilling mold automatic positioning and attitude adjustment system. Background technique [0002] The requirements for the safe service life of modern aircraft are increasing day by day. The service life of mainline aircraft is required to reach more than 50,000 flight hours respectively. The fatigue life of many advanced aircraft in the world has reached 80,000 flight hours. Now the main connection method used in aircraft structure is mechanical connection. There are approximately 1.5 to 2 million connecting holes on a large aircraft, and the load carried by the aircraft is transmitted through the connecting parts, resulting in stress concentration at the connecting parts. According to statistics, 70% of ai...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B25J11/00B23B47/00B23B47/28
Inventor 袁培江余蕾斌公茂震邢宏文沈立恒马福存黄稳
Owner SHANGHAI AIRCRAFT MFG
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