Posture adjusting device and posture adjusting method capable of realizing multi-degree-of-freedom motion

A degree of freedom and motion technology, applied in the direction of large fixed members, metal processing machinery parts, metal processing equipment, etc., can solve the problems of lack of flexible assembly, high difficulty and high procurement cost, achieve flexible manual and rapid adjustment, improve assembly accuracy, The effect of saving assembly time

Active Publication Date: 2020-06-19
XIAN AIRCRAFT IND GROUP
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The above technology uses motion superposition to realize six-degree-of-freedom motion. The X / Y / C axis can be adjusted manually, but its degree of freedom cannot be quantitatively adjusted; although the Z / A / B axis can be quantitatively controlled through servo control, it lacks the requirements for flexible assembly , it is impossible to quickly complete the handling and posture adjustment of the whole mechanism
At the same time, this structure is difficult to control and highly dependent on system control. If one of the four electric cylinders has a problem, it cannot be used normally and must be replaced, and the purchase cost is relatively high.

Method used

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  • Posture adjusting device and posture adjusting method capable of realizing multi-degree-of-freedom motion
  • Posture adjusting device and posture adjusting method capable of realizing multi-degree-of-freedom motion
  • Posture adjusting device and posture adjusting method capable of realizing multi-degree-of-freedom motion

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Embodiment Construction

[0018] Referring to the accompanying drawings, the present invention is a device for realizing multi-degree-of-freedom movement and attitude adjustment of aircraft components and a fast and accurate installation and use method.

[0019] From figure 1 Seen from the middle, the bottom plate 1 is used as a bearing for an attitude adjustment device, and two groups of screw lifters 2 are fixed on both sides of the bottom plate. Four connecting seats 4 are respectively fixed on the four corners of the screw jack 2. There is a circular through hole in the center of the connecting seat 4. The screw rod of the screw jack 2 passes through the round through hole of the connecting seat. The central opening of the connecting seat 4 avoids the screw jack 2. screw drive. The bearing tray 3 is carried by the nut on the screw mandrel of the screw jack 2, and the bearing tray 3 moves along the screw mandrel of the screw jack 2 in the vertical direction (Z direction).

[0020] The lead screws ...

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Abstract

The invention provides a posture adjusting device and posture adjusting method capable of realizing multi-degree-of-freedom motion. Six-degree-of-freedom motion of a component is realized by utilizinga spiral elevator, a cross sliding table, a tension spring and a ball and ball socket structure. X/Y directional translational motion and A/B/C tri-directional micro-adjustment of an aircraft part can be manually and rapidly adjusted, a Z directional lifting motion and the A directional rotation motion of the aircraft part depend on quantitative adjustment of the spiral elevator, real-time quantitative control is realized, and six-degree-of-freedom motion is realized. The posture adjusting device has high degree of freedom, is precise in butt joint during assembly, can realize quantitative control, and flexible manual quick adjustment during assembly, so that the assembly precision of the aircraft part is greatly improved, and the assembly time is saved. The device may be directly popularized to applications in the butt joint assembly field of other industries.

Description

technical field [0001] The invention relates to the field of docking installation of large aircraft parts in the aviation manufacturing industry, in particular to a device and method for fast and accurate docking installation of large aircraft parts. Background technique [0002] At this stage, the attitude adjustment device or assembly test device used in the field of docking and assembly of large aircraft parts is not flexible enough in structure freedom, and the operation is manually operated and the docking is difficult, which not only consumes time and affects the assembly accuracy of large aircraft parts, but also affects the aircraft and personnel safety. The posture adjustment device with multi-degree-of-freedom movement is flexible in operation, capable of three-dimensional movement and three-dimensional rotation, and realizes six-degree-of-freedom movement in space. [0003] Patent CN 103434655 A discloses an aircraft nose landing gear assembly test vehicle, which...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B23Q1/26
CPCB23Q1/26
Inventor 赵远鹏李国涛吴远东白培荣刘钰铉
Owner XIAN AIRCRAFT IND GROUP
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