CN104035324B - The preposition measuring and controlling equipment power relay full cabinet redundancy control system of power - Google Patents
The preposition measuring and controlling equipment power relay full cabinet redundancy control system of power Download PDFInfo
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- CN104035324B CN104035324B CN201410215877.2A CN201410215877A CN104035324B CN 104035324 B CN104035324 B CN 104035324B CN 201410215877 A CN201410215877 A CN 201410215877A CN 104035324 B CN104035324 B CN 104035324B
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Abstract
A kind of preposition measuring and controlling equipment power relay full cabinet redundancy control system of power, including energy supply control module, ground core one-level distribution platform control module, ground core graduation two gas platform control module, rocket engine valve control module, wired measuring parameter acquisition display module；Power module is controlled using master and slave power supply hot backup redundancy；The Redundant Control that the control signal of power relay rack is powered up using double base device synchronization.The present invention constitutes control unit as much as possible using a small amount of functional module, stable performance, simple structure, because module uses standard interface, ensure that the combination of difference in functionality module and the exchange of identical function module, simplify whole machine supporting, by various combination and extension, not only meet the transmitting of polytypic carrier rocket, and the capability of fast response for penetrating preceding failure can also be improved, can apply in power preposition equipment or be generalized in other unit products, meet the demand of rocket " zero window " launch mission.
Description
Technical field
It is to be related to a kind of preposition measuring and controlling equipment of power to move specifically the present invention relates to a kind of measuring and controlling equipment control system
Power relay full cabinet redundancy control system.
Background technology
The preposition measuring and controlling equipment of power is rocket launching site power TT＆amp corollary equipment, is collection control function and wired survey
Amount parameter acquisition function in the preposition measuring and controlling equipment of one, due to rocket unit test in launching site to be participated in, general inspection, penetrate before push away
Enter agent filling stage all control work, therefore it is required that the preposition measuring and controlling equipment of power has reliability higher, flowed before incidence is entered
If the journey stage breaks down has quick-replaceable responding ability, in the past supporting preposition control device is deposited in actual use
In deficiency：One is that low integration degree, each control module associativity and interchangeability are poor, causes rack to configure and is answered with State Transferring
It is miscellaneous, change the spare part time long；Two is that all control signals use unit component control mode, if flow stages go out before incidence is entered
Existing failure, it is difficult to meet the demand of " zero window " launch mission.
The content of the invention
For above-mentioned deficiency of the prior art, the present invention provides a kind of stable performance, the preposition survey of power of simple structure
Control equipment dynamic relay full cabinet redundancy control system.
The technical solution used in the present invention is：
A kind of preposition measuring and controlling equipment power relay full cabinet redundancy control system of power, including power supply mould
Block, ground core one-level distribution platform control module, ground core graduation two gas platform control module, rocket engine valve control module,
Wired measuring parameter acquisition display module；The power module is controlled using master and slave power supply hot backup redundancy；Power relay rack
Control signal using double base device synchronization power-up Redundant Control.
The energy supply control module, by least 6 pieces high power relay control modules and middle power relay control module,
Transient state suppresses and redundancy testing circuit module and signal display module composition.
The ground core one-level distribution platform control module includes control base plate and be arranged on control base plate at least 14
Power relay control module, transient state suppression circuit module, signal display module composition in block.
The ground core graduation two gas platform control module includes control base plate and be arranged on control base plate at least 11
Power relay control module, transient state suppression circuit module, signal display module composition in block.
The rocket engine valve control module include control base plate and be arranged on control base plate at least 5 pieces in
Power relay control module, transient state suppression circuit module and signal display module composition.
The wired measuring parameter acquisition display module includes control base plate and is arranged at least 5 pieces controlled on base plate
Redundant power module and at least 5 pieces wired measuring parameter acquisition display module compositions.
The high power relay control module and middle power relay control module by Redundant Control double base device structure
Into.
The redundancy testing circuit module is powered up by the component timesharing that control is mutually redundant, and is realized to single channel component
Test.
Present invention beneficial effect compared with the prior art：
The preposition measuring and controlling equipment power relay full cabinet redundancy control system of power of the present invention, using a small amount of function
Module constitutes control unit as much as possible, makes its stable performance, simple structure, because module uses standard interface, it is ensured that
The combination of difference in functionality module and the exchange of identical function module, it is supporting to simplify whole machine, by various combination and extension, not only
Meet the transmitting of polytypic carrier rocket, and the capability of fast response for penetrating preceding failure can also be improved；Using double base device or
Integrated circuit the technique on redundant control, the control technology is to improve the maximally effective means of unit product reliability, otherwise for double base
Device control mode, develops and is mutually redundant single channel component testing technology, it is ensured that be mutually redundant component synchronous working.
The present invention can be applied in power preposition equipment or be generalized in other unit products, meet rocket " zero window "
The demand of launch mission.
Brief description of the drawings
Fig. 1 is the power relay of the preposition measuring and controlling equipment power relay full cabinet redundancy control system of power of the present invention
Device rack theory diagram；
Fig. 2 is the power supply of the preposition measuring and controlling equipment power relay full cabinet redundancy control system of power of the present invention
Module principle block diagram；
Fig. 3 is the ground core one of the preposition measuring and controlling equipment power relay full cabinet redundancy control system of power of the present invention
Level distribution platform control module theory diagram；
Fig. 4 is the ground core two of the preposition measuring and controlling equipment power relay full cabinet redundancy control system of power of the present invention
Level distribution platform control module theory diagram；
Fig. 5 is the rocket motor of the preposition measuring and controlling equipment power relay full cabinet redundancy control system of power of the present invention
Machine valve control module theory diagram；
Fig. 6 is the wired measuring of the preposition measuring and controlling equipment power relay full cabinet redundancy control system of power of the present invention
Parameter collection module theory diagram；
Fig. 7 be the preposition measuring and controlling equipment power relay full cabinet redundancy control system of power of the present invention it is high-power after
Electrical control module theory diagram；
Fig. 8 be the preposition measuring and controlling equipment power relay full cabinet redundancy control system of power of the present invention middle power after
Electrical control module theory diagram；
Fig. 9 is that the transient state of the preposition measuring and controlling equipment power relay full cabinet redundancy control system of power of the present invention suppresses
And redundancy testing circuit module theory diagram；
Figure 10 is the redundant electric of the preposition measuring and controlling equipment power relay full cabinet redundancy control system of power of the present invention
Source module theory diagram；
Figure 11 is wired survey of the preposition measuring and controlling equipment power relay full cabinet redundancy control system of power of the present invention
Amount parameter acquisition display module theory diagram；
Figure 12 is that the signal of the preposition measuring and controlling equipment power relay full cabinet redundancy control system of power of the present invention shows
Show module principle block diagram.
Specific embodiment
Referring to the drawings and embodiment the present invention will be described in detail：
Accompanying drawing 1-12 understands that a kind of preposition measuring and controlling equipment power relay full cabinet redundancy control system of power is wrapped
Energy supply control module, ground core one-level distribution platform control module, ground core graduation two gas platform control module, rocket engine is included to live
Door control module, wired measuring parameter acquisition display module；The power module is controlled using master and slave power supply hot backup redundancy；It is dynamic
The Redundant Control that the control signal of power relay rack is powered up using double base device synchronization.
The energy supply control module, by least 6 pieces high power relay control modules and middle power relay control module,
Transient state suppresses and redundancy testing circuit module and signal display module composition.
The ground core one-level distribution platform control module includes control base plate and be arranged on control base plate at least 14
Power relay control module, transient state suppression circuit module, signal display module composition in block.
The ground core graduation two gas platform control module includes control base plate and be arranged on control base plate at least 11
Power relay control module, transient state suppression circuit module, signal display module composition in block.
The rocket engine valve control module include control base plate and be arranged on control base plate at least 5 pieces in
Power relay control module, transient state suppression circuit module and signal display module composition.
The wired measuring parameter acquisition display module includes control base plate and is arranged at least 5 pieces controlled on base plate
Redundant power module and at least 5 pieces wired measuring parameter acquisition display module compositions.
The high power relay control module and middle power relay control module by Redundant Control double base device structure
Into.
The redundancy testing circuit module is powered up by the component timesharing that control is mutually redundant, and is realized to single channel component
Test.
Redundant power module is responsible for system has line pressure, temperature transmitter to power（DC24V）, its reliability directly determines
Monitoring system reliability, so must assure that power-supply system being capable of safe and reliable, long-term, stable operation, power module use
Master and slave power supply hot backup redundancy control mode, in primary source failure, automatically switches from power supply and exports.
Wired measuring parameter acquisition display module is responsible for wired measuring parameter acquisition, display, transmission.Mainly by signal isolation
Circuit, signal acquisition circuit, A/D change-over circuits, parameter display unit composition.
Signal display module is responsible for status signal and is shown and system earth detection.
Modularization Redundancy Design theory uses quite varied in computer realm, electron trade, but in carrier rocket control
Belong to first Application in technology, modularization the technique on redundant control is used in the preposition measuring and controlling equipment of power and can realize following beneficial effect：
A. on the basis of functional requirement is met, control unit as much as possible is constituted with a small amount of functional module, makes it
Stable performance, simple structure, because module uses standard interface, it is ensured that the combination of difference in functionality module and identical function module
Exchange, it is supporting to simplify whole machine, by various combination and extension, not only meets the transmitting of polytypic carrier rocket, and can also
The capability of fast response that raising is broken down before penetrating；
B. double base device or integrated circuit the technique on redundant control are used, the control technology is to improve unit product reliability most
Effective means, otherwise for double base device control mode, develop and are mutually redundant single channel component testing technology, it is ensured that each other
Redundancy component works asynchronously.
In New Launch ground installation, the modularization the technique on redundant control that exploitation is intended to improve unit reliability shows
Obtain particularly important, the present invention can be applied in power preposition equipment or be generalized in other unit products, meet rocket " zero window
The demand of mouth " launch mission.
Claims (6)
1. the preposition measuring and controlling equipment power relay full cabinet redundancy control system of a kind of power, it is characterised in that including electricity
Source control module, ground core one-level distribution platform control module, ground core graduation two gas platform control module, rocket engine valve control
Molding block, wired measuring parameter acquisition display module；The power module is controlled using master and slave power supply hot backup redundancy；Power after
The Redundant Control that the control signal of cabinet of electric appliance is powered up using double base device synchronization；
The energy supply control module, by power relay control module at least 6 pieces high power relay control modules and 1 piece,
Transient state suppresses and redundancy testing circuit module and signal display module composition.
2. the preposition measuring and controlling equipment power relay full cabinet redundancy control system of power according to claim 1, it is special
Levy and be：The ground core one-level distribution platform control module includes control base plate and is arranged at least 14 pieces controlled on base plate
Middle power relay control module, transient state suppression circuit module, signal display module composition.
3. the preposition measuring and controlling equipment power relay full cabinet redundancy control system of power according to claim 1, it is special
Levy and be：The ground core graduation two gas platform control module includes control base plate and is arranged at least 11 pieces controlled on base plate
Middle power relay control module, transient state suppression circuit module, signal display module composition.
4. the preposition measuring and controlling equipment power relay full cabinet redundancy control system of power according to claim 1, it is special
Levy and be：The rocket engine valve control module include control base plate and be arranged on control base plate at least 5 pieces in
Power relay control module, transient state suppression circuit module and signal display module composition.
5. the preposition measuring and controlling equipment power relay full cabinet redundancy control system of power according to claim 1, it is special
Levy and be：The high power relay control module and middle power relay control module by Redundant Control double base device structure
Into.
6. the preposition measuring and controlling equipment power relay full cabinet redundancy control system of power according to claim 1, it is special
Levy and be：The redundancy testing circuit module is powered up by the component timesharing that control is mutually redundant, and is realized to single channel component
Test.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410215877.2A CN104035324B (en) | 2014-05-21 | 2014-05-21 | The preposition measuring and controlling equipment power relay full cabinet redundancy control system of power |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410215877.2A CN104035324B (en) | 2014-05-21 | 2014-05-21 | The preposition measuring and controlling equipment power relay full cabinet redundancy control system of power |
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| CN104035324A CN104035324A (en) | 2014-09-10 |
| CN104035324B true CN104035324B (en) | 2017-07-11 |
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Families Citing this family (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105626312A (en) * | 2014-10-31 | 2016-06-01 | 北京精密机电控制设备研究所 | Three-redundancy digital double-pendulum servo system with low-temperature hydrogen as energy |
| CN104597750B (en) * | 2014-11-28 | 2017-10-24 | 固安华电天仁控制设备有限公司 | A kind of core relay failure detection and redundancy control system and control method |
| FR3037668B1 (en) * | 2015-06-17 | 2017-06-02 | Schneider Electric Ind Sas | POWER SUPPLY SYSTEM FOR PROGRAMMABLE AUTOMATE |
| CN112366986A (en) * | 2020-12-12 | 2021-02-12 | 江西洪都航空工业集团有限责任公司 | Modularized combination type driver group capable of being increased and decreased |
| CN113433886A (en) * | 2021-08-04 | 2021-09-24 | 上海航天电子通讯设备研究所 | Gas distribution table measurement and control integrated device based on PLC |
| CN113985847A (en) * | 2021-10-28 | 2022-01-28 | 北京宇航系统工程研究所 | Ground measurement and control equipment fast switch adaptation system suitable for polytype rocket |
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| CN101071865A (en) * | 2006-05-12 | 2007-11-14 | 上海神力科技有限公司 | CAN bus duplex redundancy control system for fuel cell power generating system |
| CN202267835U (en) * | 2011-10-23 | 2012-06-06 | 江苏捷诚车载电子信息工程有限公司 | Bi-module redundant heat standby measurement and control device |
| CN202372803U (en) * | 2011-10-27 | 2012-08-08 | 北京航天发射技术研究所 | Hot-standby redundancy control system |
| CN202453698U (en) * | 2011-11-15 | 2012-09-26 | 北京宇航系统工程研究所 | Carrier rocket power measurement and control system |
| CN103592912A (en) * | 2013-10-30 | 2014-02-19 | 北京宇航系统工程研究所 | Distributed power measurement and control system applied to heavy carrier rocket |
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Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101071865A (en) * | 2006-05-12 | 2007-11-14 | 上海神力科技有限公司 | CAN bus duplex redundancy control system for fuel cell power generating system |
| CN202267835U (en) * | 2011-10-23 | 2012-06-06 | 江苏捷诚车载电子信息工程有限公司 | Bi-module redundant heat standby measurement and control device |
| CN202372803U (en) * | 2011-10-27 | 2012-08-08 | 北京航天发射技术研究所 | Hot-standby redundancy control system |
| CN202453698U (en) * | 2011-11-15 | 2012-09-26 | 北京宇航系统工程研究所 | Carrier rocket power measurement and control system |
| CN103592912A (en) * | 2013-10-30 | 2014-02-19 | 北京宇航系统工程研究所 | Distributed power measurement and control system applied to heavy carrier rocket |
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| CN104035324A (en) | 2014-09-10 |
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