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Device for detecting signals of rocket power filling system

A filling system and signal technology, used in transportation and packaging, ground equipment for space navigation, space navigation equipment, etc., can solve the problems of difficult centralized management of the meter head, high cost, and inability to grasp the data of the front-end power filling system in real time. , to achieve the effect of reducing the design process and time cycle, and saving time and cost

Active Publication Date: 2021-09-07
SHANGHAI SPACEFLIGHT ELECTRONICS & COMM EQUIP RES INST
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] The existing launch vehicle power filling system can only display the gas source pressure of the gas distribution platform in the filling warehouse, the pressure of the propellant tank, and the pressure of the gas cylinder through the meter head, and the back-end interpretation hall cannot grasp the front-end in real time. The data of the power filling system is difficult to link the front and rear ends
In addition, because most of the existing signal acquisition equipment is special-purpose equipment, which is only designed for a specific test unit and a specific type of rocket, the general performance is poor, and the multiple meters in the front-end warehouse are difficult to centrally manage, and the cost is high

Method used

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  • Device for detecting signals of rocket power filling system
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Embodiment Construction

[0020] In order to make the above objects, features and advantages of the present invention more comprehensible, the present invention will be further described in detail below in conjunction with the accompanying drawings and specific embodiments.

[0021] Such as figure 1 with 2 As shown, the present invention provides a kind of device for detecting rocket power filling system signal, comprising:

[0022] A pressure measurement transmission conversion unit 104, one side of the pressure measurement transmission conversion unit receives the gas source pressure signals given by the first, second and third gas distribution platforms of the filling warehouse;

[0023] PI optocoupler isolation conversion unit 105;

[0024] Tank filling signal conversion unit 106;

[0025] The digital display controller 107 and the main control computer 108 connected with the digital display controller 107, the digital display controller 107 and the main control computer 108 are respectively con...

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Abstract

The invention provides a device for detecting the signal of the rocket power filling system. In order to solve the problem that there are many heads in the filling warehouse of the shooting range, the data of the front and rear ends of the filling system cannot be linked in real time, and the versatility of each model is not strong. Provide a general-purpose rocket power filling system signal acquisition device based on RS485. By using the present invention, the front-end warehouse meters can be concentrated in one combination, and the purpose of broadcasting and sharing the front-end and back-end data in real time can be assembled on different types of rockets. power filling system. Using the present invention can satisfy the power filling system signal acquisition function of different test sites between different models, carry out front-end detection on the entire filling process of the rocket power system, and transmit the data to the back end for real-time interpretation through RS485 bus technology. When there is a fault in the filling process, it is discovered in time to ensure that the system commander can grasp the filling dynamics in real time, and grasp the display information of the power system range test and propellant filling.

Description

technical field [0001] The invention relates to a device for detecting signals of a rocket power filling system. Background technique [0002] The existing launch vehicle power filling system can only display the gas source pressure of the gas distribution platform in the filling warehouse, the pressure of the propellant tank, and the pressure of the gas cylinder through the meter head, and the back-end interpretation hall cannot grasp the front-end in real time. The data of the power filling system is difficult to link the front and rear ends. In addition, because most of the existing signal acquisition equipment is special-purpose equipment, which is only designed for a specific test unit and a specific type of rocket, the general performance is poor, and the multiple meters in the front-end warehouse are difficult to centrally manage and the cost is high. Contents of the invention [0003] The object of the present invention is to provide a device for detecting signals...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64G5/00
CPCB64G5/00
Inventor 潘搏魏永国曹聪郭嘉俊陈名胜丁宇张明亮戴李刚
Owner SHANGHAI SPACEFLIGHT ELECTRONICS & COMM EQUIP RES INST
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