Variable-structure rope-traction parallel robot for wind tunnel test

A wind tunnel test and rope traction technology, applied in the field of robotics, can solve the problems of small movement space of the model, damage to the air flow field, and single experimental items, and achieve the effects of small air flow field interference, fast response speed, and expanded work space

Active Publication Date: 2015-01-07
XIAMEN UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The purpose of the present invention is to provide a low interference to the air flow field, a variety of test items, a large working space, and a fast response speed, which can overcome the traditional hard wind tunnel support method in destroying the air flow field, single experimental items, small model movement space, and fast response. The disadvantage of slow speed; and a simple structure, easy to manufacture, assemble and maintain a variable structure rope traction parallel robot for wind tunnel tests

Method used

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  • Variable-structure rope-traction parallel robot for wind tunnel test
  • Variable-structure rope-traction parallel robot for wind tunnel test
  • Variable-structure rope-traction parallel robot for wind tunnel test

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Embodiment Construction

[0021] The specific structure of the present invention can be designed according to the requirements of wind tunnel tests and the shape of the model, and the number of towing ropes must be more than the freedom of movement of the aircraft model.

[0022] Now, the specific implementation scheme of the present invention is explained by taking a robot that can realize the six-degree-of-freedom movement of the aircraft model and 8 traction ropes as an example.

[0023] See Figure 1~3 The embodiment of the present invention is provided with a frame 1, an aircraft model 2, a towing rope 3, a movable universal hinge point 4, a movable hinge point driving assembly 5, a towing rope driving assembly 6, and a fixed universal hinge point 7; The aircraft model 2 is towed by the towing rope 3 to achieve six degrees of freedom movement, figure 1 The drive number of the mechanism is greater than the number of degrees of freedom, which is a redundant drive parallel robot.

[0024] figure 1 Each gro...

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Abstract

The invention discloses a variable-structure rope-traction parallel robot for a wind tunnel test, relating to a robot. The variable-structure rope-traction parallel robot comprises a stand, an aircraft model, a traction rope, a movable universal hinge point, a movable hinge point driving assembly, a traction rope driving assembly, and a fixed universal hinge point, wherein the aircraft model is drawn by the traction rope to realize motion of six degrees of freedom; the movable hinge point driving assembly is provided with a movable hinge point support, a ball screw, a guide rail, a support, a motor and a coupler; the traction rope driving assembly is provided with a rope-traction support, a ball screw, a guide rail, a screw bearing support, a motor and a coupler; and the fixed universal hinge point and the movable universal hinge point are respectively provided with a deep-groove slit pulley, a radial bearing, a shaft, a locking nut, a vertical support and a horizontal support. The variable-structure rope-traction parallel robot has small interferences to an air flow field, is diverse in test items, large in working space and high in response speed, has the advantage of overcoming the defects of destruction to the air flow field, single test item, small model motion space and low response speed of the traditional hard type wind tunnel support manner, and is simple in structure and easy to manufacture and maintain.

Description

Technical field [0001] The invention relates to a robot, in particular to a variable structure rope traction parallel robot used for wind tunnel tests. Background technique [0002] Existing wind tunnel test support mechanisms mostly use rigid support structures. The inherent properties of rigid support determine that it has the disadvantage of large interference to the air flow field, making it difficult to ensure the reliability and accuracy of wind tunnel test results. Since the traction rope is much smaller in diameter than the rigidly supported bracket, the wind tunnel test using rope traction parallel robot support has little interference to the air flow field. In terms of test capability, ordinary hard supports are difficult to complete the wind tunnel free flight test. Using rope-towed parallel robot technology, a set of supports can be used to complete the wind tunnel's static and dynamic derivatives while realizing the wind tunnel free flight test project. At the same...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B25J11/00G01M9/04
Inventor 林麒王钊岳遂录白志君陈艺新
Owner XIAMEN UNIV
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