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Integrated constant tension sling control device with measuring and buffering functions

A control device and constant tension technology, which is applied to the simulation device, hoisting device, transportation and packaging of space navigation conditions, etc., can solve the problems of unsatisfactory accuracy, reduced tension control accuracy, unsatisfactory spring method head, etc. To achieve the effect of compact output and simple structure

Inactive Publication Date: 2017-02-01
BEIJING INST OF SPACECRAFT ENVIRONMENT ENG
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  • Summary
  • Abstract
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  • Claims
  • Application Information

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Problems solved by technology

[0019] The accuracy of the existing counterweight method does not meet the requirements during the acceleration movement of the mechanical arm; the head of the spring method cannot meet the requirements; the accuracy of the current closed-loop control method does not meet the requirements; the torque sensor is easily affected by the drum inertia, and the accuracy does not meet the requirements; only The tension sensor method can meet the head and precision requirements, but the tension sensor needs to be arranged at the moving end, which will cause additional inertia and reduce the tension control accuracy on the one hand, and on the other hand, it is difficult to implement wiring

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  • Integrated constant tension sling control device with measuring and buffering functions
  • Integrated constant tension sling control device with measuring and buffering functions
  • Integrated constant tension sling control device with measuring and buffering functions

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Embodiment Construction

[0045] The following is a specific implementation manner of the content of the present invention, and the content of the present invention will be further clarified through the specific implementation mode below. Of course, the following specific embodiments are described only to illustrate different aspects of the present invention, and should not be construed as limiting the scope of the present invention.

[0046] see figure 2 , figure 2 It shows a schematic diagram of the base structure of an embodiment of the integrated constant tension sling control device of the present invention; wherein, the base 1 includes a bottom plate 21 and bearing seats 22 arranged on both sides of the bottom plate 21, and the bearing seats are used for passing through and supporting The ball spline shaft 2 and the coupling 9 connected to the output end of the motor, the base plate 21 are provided with a sling outlet hole 23 for the sling to pass through the bottom of the base plate from the ...

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Abstract

The invention discloses an integrated constant-tension sling control device with the measurement and buffering functions. A motor is installed on one side of a base, provides torque output and transmits the torque to a ball spline shaft through a coupling, the ball spline shaft transmits the torque to a ball spline housing and then a coil spring, one end of the coil spring is connected with the ball spline housing, the other end of the coil spring is connected with a coiling block, the coiling block and the ball spline housing form a revolute pair through a bearing, the revolute pair is matched with a sling, rotation is converted into linear movement of the sling, and through cooperation of a ball sliding groove and a channel of the coiling block, the position of a sling outlet point of the sling relative to the base is not changed in the rotating process of the coiling block. Compared with the prior art, the integrated constant-tension sling control device with the measurement and buffering functions is high in tension control precision, fixed in sling outlet point and small in volume mass.

Description

technical field [0001] The invention belongs to the technical field of spacecraft ground tests, and in particular relates to using a constant tension sling control device to meet the requirements of spacecraft ground microgravity environmental tests. Background technique [0002] Domestic constant tension sling control methods are mainly divided into: counterweight method, spring mechanism method, pure motor torque control method, torque sensor closed-loop control method and tension sensor closed-loop control method. Among them, the counterweight method uses weights to control the tension of the sling; the spring mechanism method uses a special mechanism to convert the variable elastic force of the spring into a constant force, which acts on the sling to generate constant tension; the pure motor torque control method uses a DC motor or a permanent The magnetic synchronous motor, according to the principle that the motor current and the torque are approximately linear, realiz...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B66D1/50B64G7/00
CPCB64G7/00B66D1/505
Inventor 孟凡伟易旺民高峰杜瑞兆代海林刘孟周刘浩淼卫月娥刘涛姜旭刘同辉王鹏飞胡立欣
Owner BEIJING INST OF SPACECRAFT ENVIRONMENT ENG