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Multi-shaft posture adjusting platform for airplane engine mounting

A multi-axis attitude-adjusting platform and aircraft engine technology, applied in aircraft assembly, aircraft parts, ground installations, etc., can solve the problems of mutual friction and extrusion, low installation efficiency, poor bearing capacity, etc., and achieve a high degree of automation and lighten the Labor intensity, the effect of improving installation efficiency

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

AI Technical Summary

Problems solved by technology

This type of equipment mainly has the following deficiencies: 1) The attitude adjustment accuracy is low, and mutual friction and extrusion often occur during assembly; 2) There are few adjustable attitudes, and multi-axis attitude adjustment cannot be realized; 3) The bearing capacity is poor and cannot meet Requirements for heavy load and partial load of large parts; 4) Poor degree of automation, low installation efficiency, and high skill requirements for workers

Method used

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  • Multi-shaft posture adjusting platform for airplane engine mounting
  • Multi-shaft posture adjusting platform for airplane engine mounting
  • Multi-shaft posture adjusting platform for airplane engine mounting

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Embodiment Construction

[0017] The specific embodiments of the present invention will be described in detail below in conjunction with the technical solutions and accompanying drawings.

[0018] Such as figure 1 , figure 2 As shown, an aircraft engine multi-axis attitude adjustment platform includes a working platform 1, a translation mechanism 2, a turntable mechanism 3, a lifting and pitching mechanism 4, a platform base 5 and a servo system, wherein the translation mechanism 2 is connected to the working platform 1 through linear guide rails on both sides. The lower surface is fixed, the screw nut seat of the translation mechanism 2 is fixed to the working platform 1, the inner ring of the large-scale bearing with inner teeth of the turntable mechanism 3 is fixed to the lower bottom surface of the translation mechanism 2, and the left upper sliding seat 6 of the lifting and pitching mechanism is fixed. Connect with the left side of the turntable mechanism 3 through the linear guide rail, the upp...

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Abstract

The invention discloses a multi-shaft posture adjusting platform for airplane engine mounting and belongs to the technical field of assembly automation. The multi-shaft posture adjusting platform is characterized by comprising a worktable (1), a translating mechanism (2), a turntable mechanism (3), a lifting and elevating mechanism (4), a platform base (5) and the like. The lifting and elevating mechanism (4) comprises a left upper slide seat (6), a right upper fixing sea (9), a left lifting mechanism (7) and a right lifting mechanism (8), wherein the left lifting mechanism (7) and the right lifting mechanism (8) are of structures conforming to identical operating principles and has a single-side lifting posture adjusting function. All motion mechanisms are of purely mechanical structures driven by a servo motor. The multi-shaft posture adjusting platform has the advantages that carrying capacity is high, mounting accuracy is high, and adjustment range is large; labor intensity of operators is alleviated, and operation efficiency and mounting quality are improved. The multi-shaft posture adjusting platform is widely applicable to accurate assembly of multi-shaft posture adjustment of heavy parts.

Description

technical field [0001] The invention belongs to the technical field of assembly automation and relates to the design of a multi-axis attitude adjustment platform for aircraft engine installation. Background technique [0002] As the core power component of the aircraft, the aircraft engine needs to be loaded and unloaded frequently and inspected and maintained. However, aircraft engines have the characteristics of complex structure, large volume, high quality, and small assembly gaps, which are difficult to load and unload, which makes it often impossible to achieve accurate attitude adjustment when loading and unloading aircraft engines, and its loading and unloading quality will have an important impact on the dynamic performance of the aircraft. . [0003] At present, when assembling aircraft engines, manual mechanical devices or hydraulic mechanisms are often used to adjust the various attitudes of the engines. This type of equipment mainly has the following deficienci...

Claims

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Application Information

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IPC IPC(8): B64F5/00B64F5/10
Inventor 高航雷海峰赵哲刘学术盛贤君
Owner DALIAN UNIV OF TECH
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