Assembly test vehicle of airplane main landing gear

A landing gear and test vehicle technology, which is used in aircraft component testing, aircraft parts, ground installations, etc., can solve the problems that the degree of freedom cannot be manually adjusted flexibly and quickly, the entire mechanism cannot be transported, and the degree of freedom cannot be quantitatively adjusted. The effect of easy alignment, high degree of freedom, and improved assembly accuracy

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AI Technical Summary

Problems solved by technology

[0004] The above mechanism uses the superposition of motion to realize the movement of six degrees of freedom. The six degrees of freedom docking platform can be adjusted manually, but the degree of freedom cannot be quantitatively adjusted.
Although the six-degree-of-freedom precision positioning table can be quantitatively adjusted through the piezoelectric ceramic driver, some degrees of freedom that are not demanding cannot be manually adjusted flexibly and quickly
However, the handling of the entire mechanism cannot be realized, and the degree of freedom of the handling operation is not high.

Method used

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  • Assembly test vehicle of airplane main landing gear
  • Assembly test vehicle of airplane main landing gear
  • Assembly test vehicle of airplane main landing gear

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Embodiment Construction

[0023] This embodiment is a test vehicle for assembling the main landing gear of an aircraft.

[0024] refer to Figure 1-Figure 11 , the aircraft main landing gear assembly test vehicle of the present invention uses an air-floating platform to realize the movement of the main landing gear along the X-axis and the Y-axis and the rotation around the Z-axis; four vertical servo electric cylinders are used to realize the movement of the main landing gear along the Z-axis. The movement and rotation around the X-axis and Y-axis; a tilting servo electric cylinder is used to realize the rotation of the pillar of the main landing gear along the wheel axis. The horizontal radial direction of the wheel shaft is the X-axis direction, the axial direction of the wheel shaft is the Y-axis direction, the vertical direction is the Z-axis direction, and the rotation around the wheel shaft is pitching. The docking vehicle should be able to easily move and turn in the factory building, transpor...

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Abstract

The invention discloses an assembly test vehicle of an airplane main landing gear, and an air floatation platform and five servo electric cylinders are used for achieving six-freedom-degree movement of the main landing gear and rotation of a strut of the nose landing gear along an axle. The movement amount, along an X axis and a Y axis, of the main landing gear and the rotation amount, along a Z axis, of the main landing gear can be adjusted manually, the movement amount, along the Z axis, of the main landing gear, the rotation amount, along the X axis and the Y axis, of the main landing gear and the rotation amount, along the axle, of the strut of the main landing gear can be adjusted quantitatively through the servo electric cylinders, and the six-freedom-degree movement is achieved through real-time quantitative control. The assembly test vehicle of the airplane main landing gear is high in freedom degree, easy to align in an assembly process and capable of achieving the quantitative control in the assembly process and flexible manual adjustment, and therefore assembly accuracy of the main landing gear is greatly improved.

Description

technical field [0001] The invention belongs to the field of mechanical structure design, and in particular relates to an aircraft main landing gear assembly test vehicle. Background technique [0002] Chinese patent CN2782326 discloses a six-degree-of-freedom precision positioning workbench. The precision positioning workbench is guided by a flexible hinge, and the drive unit adopts a piezoelectric ceramic driver, which improves the displacement output resolution and positioning accuracy, and realizes the positioning of its mechanism. Compensation to achieve nanometer-level positioning accuracy. [0003] Patent CN101081504 describes a six-degree-of-freedom docking platform. This six-degree-of-freedom docking platform realizes six-degree-of-freedom movements by superimposing the functions of the plane adjustment mechanism and the vertical adjustment mechanism. [0004] The above-mentioned mechanism adopts the superposition of motion to realize the movement of six degrees of...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64F5/00B64F5/60
Inventor 杨旭东徐海亭王俊孙晓朋戴广永
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