Portable measuring and controlling system for rocket engine ground tests

A rocket engine and ground test technology, which is applied in the direction of rocket engine devices, machines/engines, mechanical equipment, etc., can solve the problems that the system is difficult to meet the use requirements, the system has no control function, etc., to improve safety and scalability, and improve safety High performance and versatility

Inactive Publication Date: 2011-05-04
BEIHANG UNIV
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  • Abstract
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  • Application Information

AI Technical Summary

Problems solved by technology

However, the system has no control function and is mainly used for data collection of solid rocket motor tests. For liquid rocket motor

Method used

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  • Portable measuring and controlling system for rocket engine ground tests
  • Portable measuring and controlling system for rocket engine ground tests
  • Portable measuring and controlling system for rocket engine ground tests

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Embodiment Construction

[0027] The present invention will be described in further detail below in conjunction with the accompanying drawings and embodiments.

[0028] The present invention proposes a measurement and control system for a portable rocket engine ground test, such as figure 1 , mainly including computer 1, data acquisition and control card 2 and measurement and control box 3. The measurement and control box 3 mainly includes: AC power interface 4, measurement and control box power switch 5, DC power supply 6, current display meter 7, voltage display meter 8, backup power interface 9, measurement power switch 10, ignition power switch 11, Control power switch 12, signal isolator 13, aviation plug 14, power amplifier chip 16, emergency stop switch 17, relay A18, relay B24, manual switch 19, standard data interface 22 and measurement and control cable 23. Described computer 1 adopts portable computer, is connected with data acquisition and control card 2 by USB data line, and described dat...

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Abstract

The invention provides a portable measuring and controlling system for rocket engine ground tests, relating to the field of measurement and control of rocket engine tests. The system mainly comprises a computer, a data acquisition and control card and a measuring and controlling box, wherein the measuring and controlling box mainly comprises an alternating current power supply interface, a measuring and controlling box power switch, a measuring power switch, a signal isolator, a power amplifier chip, an emergency stop switch, relays and the like. The system mainly solves the problem that the existing measuring and controlling systems for rocket engine tests have low integration level and poor portability and the measuring system and control system are mutually independent. The system has the following advantages and beneficial effects: the system realizes integration of various measuring and controlling components by adopting the portable measuring and controlling box and integrates the measuring system and the controlling system; based on development of the data acquisition and control cards in National Instruments (NI), the system has high data sampling rate and multiple measuring and controlling channels; by adopting a shunt circuit switchable power supply system, the system has good safety and strong expansibility; and the system has universality and can meet the requirements of various rocket engine tests on measurement and control.

Description

technical field [0001] The invention belongs to the technical field of rocket engine test measurement and control, in particular to a portable rocket engine ground test measurement and control system. Background technique [0002] The rocket engine ground test has the characteristics of high cost and high risk, and requires a large amount of information to be obtained. At the same time, the supporting measurement and control system is required to have high reliability and precision to ensure the success and effectiveness of the test. The existing rocket engine ground test measurement and control systems are mostly fixed, with poor portability, and are often only used for specific tests, resulting in a serious waste of funds and resources. In the document Solid Rocket Technology-2001-24(4) "Solid Rocket Ramjet Ground Test Device and Measurement and Control System", Northwestern Polytechnical University established a ground test system for solid rocket ramjet based on PXI bus ...

Claims

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Application Information

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IPC IPC(8): F02K9/96
Inventor 蔡国飙李新田李君海
Owner BEIHANG UNIV
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