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Numerical-control electric frame truck for airplane engine mounting

An aircraft engine and electric technology, applied in aircraft assembly, aircraft parts, ground equipment and other directions, can solve the problems of low installation efficiency, low design accuracy, large load deformation, etc., to improve installation efficiency, reduce labor intensity of workers, and achieve high precision. Effects of quick adjustments

Inactive Publication Date: 2013-07-17
DALIAN UNIV OF TECH +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

This type of installation equipment often has the following disadvantages: (1) poor rigidity of the mechanism, large load deformation; (2) low design accuracy, it is difficult to achieve precise adjustment of small strokes; (3) less adjustable posture, unable to achieve multi-axis NC adjustment of attitude; (4) low degree of automation, requiring manual operation one by one to adjust the attitude of each degree of freedom; (5) poor maneuverability, most of which require additional transportation tools to transport related installation equipment to the installation site; (6) installation Low efficiency, high labor intensity, requiring multiple assemblers to cooperate and cooperate repeatedly

Method used

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  • Numerical-control electric frame truck for airplane engine mounting
  • Numerical-control electric frame truck for airplane engine mounting
  • Numerical-control electric frame truck for airplane engine mounting

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Embodiment Construction

[0019] The specific embodiments of the present invention will be described in detail below in conjunction with the technical solutions and accompanying drawings.

[0020] Such as figure 1 As shown in the figure, the CNC electric frame vehicle for aircraft engine installation includes a multi-axis attitude adjustment platform 1, an attitude adjustment platform frame 2, a long axis feed mechanism 3, a body frame 4, a left and right rotation mechanism 5, an auxiliary support mechanism 6, a hydraulic Outrigger 7, driving wheel train 8, car body underframe 9, steering wheel train 10, driver's cab 11, hydraulic control system and servo control system, wherein two sets of left and right turning mechanisms 5 and two sets of auxiliary support mechanisms 6 form the car body to rotate Mechanism, six identical hydraulic support legs 7 and a hydraulic control system form a hydraulic support system, and these four parts of a driving wheel train 8, a vehicle body chassis 9, a steering wheel ...

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Abstract

The invention relates to a numerical-control electric frame truck for airplane engine mounting and belongs to the technical field of assembly automation. The numerical-control electric frame truck is characterized by comprising a multi-shaft posture adjusting platform (1), a posture adjusting platform frame (2), a long-shaft feed mechanism (3), a truck body frame (4), left and right rotation mechanisms (5), an auxiliary support mechanism (6), hydraulic support legs (7), a driving wheel system (8), a truck body underframe (9), steering wheel systems (10), a driving cab (11), a hydraulic control system and a servo control system. Posture of five shafts is driven and adjusted by a servo motor, and posture of the rest one shaft is manually adjusted. Travelling of the frame truck is driven by the mode of electric vehicle. The numerical-control electric frame truck has the advantages that positioning accuracy is high, maneuverability is good, stability is high, engine mounting efficiency is improved, and labor intensity of operators is reduced. Besides, the numerical-control electric frame truck is applicable to automatic mounting operation of heavy complicated shaft parts requiring multi-shaft posture adjustment.

Description

technical field [0001] The invention belongs to the technical field of assembly automation and relates to the design of a numerically controlled electric carriage used for aircraft engine installation. Background technique [0002] The aircraft engine is the core power component of the aircraft, and it needs to be installed, inspected and maintained frequently. However, the engine has the characteristics of high quality, large volume, complex structure, etc. At the same time, there are also difficult assembly problems such as small assembly clearance, complex inner cabin structure, and easy deformation of installation equipment, which makes it often impossible to achieve accurate attitude adjustment and positioning when the engine is installed. . Therefore, during the installation process, it is necessary to repeatedly adjust the attitude of the engine and perform repeated trial installations. This repetitive installation process occupies most of the labor in engine assembl...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64F5/00B64F5/10
Inventor 高航郭东明雷海峰刘国赵哲郭显华杜宝瑞杨颖
Owner DALIAN UNIV OF TECH
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