Engine vacuum redundant automatic measurement and control system and method

A measurement and control method and vacuum pumping technology, applied in general control systems, machines/engines, control/regulation systems, etc., can solve problems such as being susceptible to human interference, low degree of automation, and high misoperation rate, so as to reduce electromagnetic interference and enhance Safe operation and high reliability

Active Publication Date: 2018-09-04
XIAN AEROSPACE PROPULSION TESTING TECHN INST
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The vacuuming effect and stability of single equipment are poor. When redundant process equipment is used, manual measurement and control are prone to human interference
Existing vacuum measurement and control methods rely on laying cables and manual buttons for vacuum test, which has low degree of automation, high misoperation rate, poor flexibility and low reliability.

Method used

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  • Engine vacuum redundant automatic measurement and control system and method
  • Engine vacuum redundant automatic measurement and control system and method
  • Engine vacuum redundant automatic measurement and control system and method

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Embodiment Construction

[0036] The present invention proposes a redundant automatic measurement and control system for engine vacuum:

[0037] 1.1] Hardware System

[0038] The measurement and control hardware system is mainly composed of a measurement and control host computer, an optical transceiver, a measurement and control device (lower computer), a signal adapter, a sensor, and a communication optical cable.

[0039] a) The measurement and control device adopts two small wide temperature series PLC (MicroLogix1400) controllers 1766-L32BWAA and its expansion modules, which are mainly responsible for the functions of measurement and control data acquisition, channel control, ultra-high-speed timing counting and data calculation.

[0040] b) The host computer and touch screen centralized control station adopts industrial control computers, notebooks and 10-inch touch screens, and realizes the functions of controlling solenoid valves, monitoring the operation status of network switch ports, real-time data a...

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Abstract

The invention provides an automated redundant measuring and controlling system for engine vacuumizing. The system comprises mutually interchanged optical transceivers arranged in a front-end equipment room and a back-end power square cabin respectively; the optical transceiver in the front-end equipment room is communicated with a touch screen, a first measuring and controlling device and a second measuring and controlling device, and the first measuring and controlling device and the second measuring and controlling device are connected with a signal adapter; the optical transceiver in the back-end power square cabin is communicated with a first measuring and controlling upper computer and a second measuring and controlling upper computer. According to the automated redundant measuring and controlling system for engine vacuumizing, the measuring and controlling integrated scheme with double lower computers and the multiple upper computers is adopted, far-end controlling is achieved, and the reliability is high; meanwhile, by comparing the measuring and controlling integrated scheme with a traditional method separating measuring from controlling, the efficiency is improved.

Description

Technical field [0001] The invention relates to the field of liquid oxygen kerosene engines for rockets, in particular to a redundant automatic measurement and control method for engine vacuum. Background technique [0002] my country's new rockets use liquid oxygen kerosene engines, and the fuel cavity needs to be evacuated and filled before the rocket is launched. According to the rocket launch requirements, the engine vacuum time is after the personnel evacuated before the rocket launch, which is controlled by the operator in the rear power shelter. In order to ensure the smooth launch of the rocket, the vacuum system must work correctly according to the nodes, pumping the engine fuel cavity pressure below the rated value within the specified time while maintaining the pressure not less than 1000s. [0003] At present, my country's existing engine vacuum measurement and control methods are: manual button control vacuum pump, manual valve control ejector two methods for vacuum t...

Claims

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Application Information

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Patent Type & AuthorityPatents(China)
IPC IPC(8): G05B19/05F04B49/06
CPCF04B49/065G05B19/058G05B2219/13015G05B2219/14006G05B2219/31088
Inventor蔡琳李正兵祝敏李波秦永涛王薇
OwnerXIAN AEROSPACE PROPULSION TESTING TECHN INST