CN107152890A - A kind of modularization composite high-energy weapon cooling system and its control method - Google Patents
A kind of modularization composite high-energy weapon cooling system and its control method Download PDFInfo
- Publication number
- CN107152890A CN107152890A CN201710252599.1A CN201710252599A CN107152890A CN 107152890 A CN107152890 A CN 107152890A CN 201710252599 A CN201710252599 A CN 201710252599A CN 107152890 A CN107152890 A CN 107152890A
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- China
- Prior art keywords
- energy weapon
- high energy
- compressor
- condenser
- throttling
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- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41H—ARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
- F41H13/00—Means of attack or defence not otherwise provided for
- F41H13/0043—Directed energy weapons, i.e. devices that direct a beam of high energy content toward a target for incapacitating or destroying the target
- F41H13/005—Directed energy weapons, i.e. devices that direct a beam of high energy content toward a target for incapacitating or destroying the target the high-energy beam being a laser beam
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
- F25B—REFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
- F25B1/00—Compression machines, plants or systems with non-reversible cycle
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
- F25B—REFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
- F25B41/00—Fluid-circulation arrangements
- F25B41/20—Disposition of valves, e.g. of on-off valves or flow control valves
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
- F25B—REFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
- F25B41/00—Fluid-circulation arrangements
- F25B41/30—Expansion means; Dispositions thereof
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
- F25B—REFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
- F25B49/00—Arrangement or mounting of control or safety devices
- F25B49/02—Arrangement or mounting of control or safety devices for compression type machines, plants or systems
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41A—FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
- F41A13/00—Cooling or heating systems; Blowing-through of gun barrels; Ventilating systems
Abstract
The present invention discloses a kind of modularization composite high-energy weapon cooling system and its control method, is made up of high energy weapon-bay and heat dissipation equipment cabin；High energy weapon and evaporator are set in high energy weapon-bay, phase-change material is filled with the periphery of high energy weapon and evaporator；Compressor, condenser, throttling branch road, bypass branch, controller, condenser fluid import and condenser fluid outlet are set in heat dissipation equipment cabin；Evaporator is connected with compressor, condenser and throttling branch road successively by refrigerant line, and throttling branch road and bypass branch are arranged in parallel, and are set on throttling branch road and are set by-passing valve on throttling arrangement, bypass branch.Under different cooling fluids and high energy armament equipment load condition, according to high energy weapon peripheral temperature, the system can realize two kinds of mode of operations.Present system carries two kinds of refrigeration modes, and outside platform need to only provide cooling fluid and can work, and drastically increase flexibility, mobility and the portability of high energy weapon.
Description
Technical field：
The present invention relates to a kind of modularization composite high-energy weapon cooling system and its control method, it is adaptable to airborne, star
The platform superlaser equipment cooling such as load, carrier-borne, vehicle-mounted, belongs to equipment heat management and ring control field.
Background technology：
In recent years, high energy laser weapon is rapidly developed as new weapon of future generation.Research shows that high energy weapon will
The efficiency that electric energy is converted into laser is only 10%~15%, causes heat flow density during execution task to be up to 100~800W/cm2, and
Intermittent pulse stamp is worked, and load fluctuation greatly, very big challenge is proposed to cooling system.In addition, high energy weapon may be in machine
Carry, spaceborne, carrier-borne and vehicle-mounted etc. various working platforms, the environmental condition such as radiating condition and gravity condition difference shows under various platforms
Write.Traditional high energy weapon cooling system depends on external refrigeration, and it is individually designed to be directed to a certain platform, seriously constrains
Flexibility, mobility and the portability of high energy weapon.
In view of the shortcomings of the prior art, the present invention intends proposing a kind of modularization composite high-energy weapon cooling system and its control
Method processed, can under various cooling conditions and gravity condition reliable efficient operation, when coolant water temperature is relatively low and high energy weapon load
When smaller, unit works in power heat pipe pattern (all can normal work under microgravity or overload), safeguards system energy-saving run；When
Coolant water temperature is higher and during larger high energy weapon load, system is worked under vapor compression refrigeration pattern, and safeguards system safely may be used
Lean on.Simultaneously as shared heat exchanger, the system footprint space is small, lightweight, control is easy.The system can it is airborne, spaceborne,
The various platform high efficient and reliable work such as carrier-borne and vehicle-mounted, greatly improve flexibility, mobility and the portability of high energy weapon.
The content of the invention：
The present invention is to provide a kind of modularization composite high-energy weapon to solve the problem of above-mentioned prior art is present
Cooling system and its control method.Using pressure-adjustable than the miniature oil-free frequency-changeable compressor with rotating speed as power source, and realize
" dual-use "：When cooling fluid temperature is higher and high energy weapon load is larger, the operating of compressor high speed and high pressure, throttling arrangement
Work, runs on vapor compression refrigeration pattern, ensures that radiating is safe and reliable；When cooling fluid temperature is relatively low and high energy weapon load
When smaller, compressor low speed low-pressure operation, throttling arrangement is bypassed, runs on power heat pipe circulation pattern, and now compressor is only
Working medium circulation is driven, pressure difference is not set up, power consumption is extremely low, safeguards system energy-saving run..
The present invention is adopted the following technical scheme that：A kind of modularization composite high-energy weapon cooling system, by high energy weapon-bay
With heat dissipation equipment cabin composition；High energy weapon and evaporator are set in the high energy weapon-bay, in high energy weapon and evaporator
Periphery be filled with phase-change material；Compressor, condenser, throttling branch road, bypass branch, control are set in the heat dissipation equipment cabin
Device, condenser fluid import and condenser fluid outlet；The evaporator by refrigerant line successively with compressor, condenser
With throttling branch road connection, throttling branch road and bypass branch are arranged in parallel, and are set and are set on throttling arrangement, bypass branch on throttling branch road
Put by-passing valve.
Further, the compressor is pressure ratio and the adjustable miniature oil-free frequency-changeable compressor of rotating speed.
Further, the phase-change material is direct contact type phase-change material.
Further, the cooling fluid of the condenser is water, air or oil.
The present invention is also adopted the following technical scheme that：A kind of control method of modularization composite high-energy weapon cooling system,
Control compressor, throttling arrangement and by-passing valve after controller collection high energy weapon peripheral temperature, in different cooling fluid and height
Under energy weapon load condition, according to high energy weapon peripheral temperature, the system realizes two kinds of mode of operations：
(a) when high energy weapon load is larger or cooling fluid temperature is higher, surface temperature T>During a, wherein a is pre- for system
If temperature value, controller control compressor high speed, high pressure ratio operating, throttling arrangement work, by-passing valve are closed, evaporator, compression
Machine, condenser and throttling branch road constitute Vapor Compression Refrigeration Cycle；
(b) when high energy weapon load is smaller and cooling fluid temperature is relatively low, surface temperature T<During a, wherein a is pre- for system
If temperature value, controller control compressor low pressure low-speed running, by-passing valve open, throttling arrangement close, evaporator, compressor,
Condenser and bypass branch constitute the circulation of power drive heat pipe.
The present invention has the advantages that：
(1), when cooling fluid temperature is higher or high energy weapon load is larger, compressor runs at high speed and throttling arrangement work
Make, meet cooling requirements, ensure radiating peace；When cooling fluid temperature is relatively low and high energy weapon load is smaller, compressor low pressure
Low-speed running, the power consumption driving working medium circulation minimum by paying, construction force heat pipe circulation meets heat transfer on the basis of energy-conservation
It is required that, and the power heat pipe circulation can under microgravity or overload situations reliability service；Compressor " dual-use ", power heat pipe
Pattern (Fig. 3) and steam compressed pattern (Fig. 2) share evaporator and condenser, and circuit design is succinctly smooth so that system weight
Gently, floor space is small, control is easy.
(2), high energy weapon has discontinuous operation, and the characteristics of load fluctuation is big, by adding phase-change material, can greatly cut
The impact of moment thermic load when subtracting the work of high energy weapon, safeguards system is safe and reliable.
(3), the system carries two kinds of refrigeration modes, can efficiently may be used under the various cooler environments of different platform and gravity condition
By work, outside platform need to only provide cooling fluid and can work, drastically increase the flexibility of high energy weapon, mobility and
It is portable.
Brief description of the drawings：
Fig. 1 is the structure principle chart of modularization composite high-energy weapon cooling system of the present invention.
Fig. 2 is the steam compressed flow chart of modularization composite high-energy weapon cooling system of the present invention.
Fig. 3 is the power heat pipe flow chart of modularization composite high-energy weapon cooling system of the present invention.
In figure：
1- high energy weapon-bays；2- heat dissipation equipments cabin；3- high energy weapons；4- phase-change materials；5- evaporators；6- is controlled
Device；7- compressors；8- condensers；9- throttling branch roads；10- bypass branch；11- throttling arrangements；12- by-passing valves；13- is cold
Condenser fluid inlet；14- condenser fluids are exported.
Embodiment：
The present invention is further illustrated below in conjunction with the accompanying drawings.
Modularization composite high-energy weapon cooling system of the present invention is made up of high energy weapon-bay 1 and heat dissipation equipment cabin 2；High energy
High energy weapon 3 and evaporator 5 are set in weapon-bay 1, phase-change material is filled with the periphery of high energy weapon 3 and evaporator 5
4.Compressor 7, condenser 8, throttling branch road 9, bypass branch 10, controller 6, condenser fluid is set to enter in heat dissipation equipment cabin 2
Mouth 13 and condenser fluid outlet 14；Evaporator 5 by refrigerant line successively with compressor 7, condenser 8 and throttling branch road 9
Connection, throttling branch road 9 and bypass branch 10 are arranged in parallel, and are set on throttling arrangement 11, bypass branch 10 and are set on throttling branch road 9
By-passing valve 12.Compressor 7 is pressure ratio and the adjustable miniature oil-free frequency-changeable compressor of rotating speed；The collection high energy weapon of controller 6 periphery
Compressor 7, throttling arrangement 11 and by-passing valve 12 are controlled after temperature, under different cooling fluids and the load condition of high energy weapon 3,
According to the peripheral temperature of high energy weapon 3, the system can realize two kinds of mode of operations：
(a) when the load of high energy weapon 3 is larger or cooling fluid temperature is higher, surface temperature T>During a, wherein a is system
Preset temperature value, the high speed of the control of controller 6 compressor 7, high pressure ratio operating, throttling arrangement 11 is worked, and by-passing valve 12 is closed, evaporation
Device 5, compressor 7, condenser 8 and throttling branch road 9 constitute Vapor Compression Refrigeration Cycle；
(b) when the load of high energy weapon 3 is smaller and cooling fluid temperature is relatively low, surface temperature T<During a, wherein a is system
Preset temperature value, the control low pressure low-speed running of compressor 7 of controller 6, by-passing valve 12 is opened, and throttling arrangement 11 is closed, evaporator
5th, compressor 7, condenser 8 and bypass branch 10 constitute the circulation of power drive heat pipe.
Phase-change material 4 is direct contact type phase-change material in such scheme, and the cooling fluid of condenser 8 is water, air, oil
Deng fluid.
Described above is only the preferred embodiment of the present invention, it is noted that for the ordinary skill people of the art
For member, some improvement can also be made under the premise without departing from the principles of the invention, and these improvement also should be regarded as the present invention's
Protection domain.
Claims (5)
1. a kind of modularization composite high-energy weapon cooling system, it is characterised in that：By high energy weapon-bay (1) and heat dissipation equipment cabin
(2) constitute；High energy weapon (3) and evaporator (5) are set in the high energy weapon-bay (1), in high energy weapon (3) and evaporation
The periphery of device (5) is filled with phase-change material (4)；Compressor (7), condenser (8), throttling are set in the heat dissipation equipment cabin (2)
Branch road (9), bypass branch (10), controller (6), condenser fluid import (13) and condenser fluid outlet (14)；It is described to steam
Hair device (5) by refrigerant line successively with compressor (7), condenser (8) and throttling branch road (9) be connected, throttle branch road (9) and
Bypass branch (10) is arranged in parallel, and throttling arrangement (11) is set on throttling branch road (9), and bypass branch sets by-passing valve on (10)
(12)。
2. modularization composite high-energy weapon cooling system as claimed in claim 1, it is characterised in that：The compressor (7)
For pressure ratio and the adjustable miniature oil-free frequency-changeable compressor of rotating speed.
3. modularization composite high-energy weapon cooling system as claimed in claim 1, it is characterised in that：The phase-change material
(4) it is direct contact type phase-change material.
4. modularization composite high-energy weapon cooling system as claimed in claim 1, it is characterised in that：The condenser (8)
Cooling fluid be water, air or oil.
5. a kind of control method of modularization composite high-energy weapon cooling system, it is characterised in that：Controller (6) gathers high energy
Compressor (7), throttling arrangement (11) and by-passing valve (12) are controlled after weapon peripheral temperature, it is military in different cooling fluids and high energy
Under device (3) load condition, according to high energy weapon (3) peripheral temperature, the system realizes two kinds of mode of operations：
(a) when high energy weapon (3) load is larger or cooling fluid temperature is higher, surface temperature T>During a, wherein a is pre- for system
If temperature value, controller (6) control compressor (7) high speed, high pressure ratio operating, throttling arrangement (11) work, by-passing valve (12) are closed
Close, evaporator (5), compressor (7), condenser (8) and throttling branch road (9) constitute Vapor Compression Refrigeration Cycle；
(b) when high energy weapon (3) load is smaller and cooling fluid temperature is relatively low, surface temperature T<During a, wherein a is pre- for system
If temperature value, controller (6) control compressor (7) low pressure low-speed running, by-passing valve (12) is opened, and throttling arrangement (11) is closed,
Evaporator (5), compressor (7), condenser (8) and bypass branch (10) constitute the circulation of power drive heat pipe.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710252599.1A CN107152890B (en) | 2017-04-18 | 2017-04-18 | A kind of modularization composite high-energy weapon cooling system and its control method |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710252599.1A CN107152890B (en) | 2017-04-18 | 2017-04-18 | A kind of modularization composite high-energy weapon cooling system and its control method |
Publications (2)
| Publication Number | Publication Date |
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| CN107152890A true CN107152890A (en) | 2017-09-12 |
| CN107152890B CN107152890B (en) | 2019-01-11 |
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| CN201710252599.1A Active CN107152890B (en) | 2017-04-18 | 2017-04-18 | A kind of modularization composite high-energy weapon cooling system and its control method |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP3865787A1 (en) * | 2020-02-17 | 2021-08-18 | BAE SYSTEMS plc | Thermal management apparatus |
| WO2021165646A1 (en) * | 2020-02-17 | 2021-08-26 | Bae Systems Plc | Thermal management apparatus |
| US20230400283A1 (en) * | 2022-06-13 | 2023-12-14 | Hamilton Sundstrand Corporation | Thermal storage for high load short duration cooling |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20120174602A1 (en) * | 2009-08-07 | 2012-07-12 | Renault S.A.S. | System for the overall control of heat for electrically propelled motor vehicle |
| CN102721246A (en) * | 2012-06-04 | 2012-10-10 | 中国电子科技集团公司第十一研究所 | Cold-storage circulating fluid cooling device |
| CN102874069A (en) * | 2012-09-18 | 2013-01-16 | 江苏晨宇车业有限公司 | Cold-warm air exchange system based on high-efficiency motor driving for automobile |
| CN104697236A (en) * | 2015-02-11 | 2015-06-10 | 南京航空航天大学 | Cooling system and method of airborne heating elements based on evaporative refrigeration |
| CN106288513A (en) * | 2016-09-30 | 2017-01-04 | 广州高菱能源技术有限公司 | A kind of band phase change cold-storage and the cold, hot two-purpose heat pump of accumulation of heat |
| CN106546025A (en) * | 2016-12-07 | 2017-03-29 | 珠海格力电器股份有限公司 | Heat-exchange system and air-conditioner |
-
2017
- 2017-04-18 CN CN201710252599.1A patent/CN107152890B/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20120174602A1 (en) * | 2009-08-07 | 2012-07-12 | Renault S.A.S. | System for the overall control of heat for electrically propelled motor vehicle |
| CN102721246A (en) * | 2012-06-04 | 2012-10-10 | 中国电子科技集团公司第十一研究所 | Cold-storage circulating fluid cooling device |
| CN102874069A (en) * | 2012-09-18 | 2013-01-16 | 江苏晨宇车业有限公司 | Cold-warm air exchange system based on high-efficiency motor driving for automobile |
| CN104697236A (en) * | 2015-02-11 | 2015-06-10 | 南京航空航天大学 | Cooling system and method of airborne heating elements based on evaporative refrigeration |
| CN106288513A (en) * | 2016-09-30 | 2017-01-04 | 广州高菱能源技术有限公司 | A kind of band phase change cold-storage and the cold, hot two-purpose heat pump of accumulation of heat |
| CN106546025A (en) * | 2016-12-07 | 2017-03-29 | 珠海格力电器股份有限公司 | Heat-exchange system and air-conditioner |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP3865787A1 (en) * | 2020-02-17 | 2021-08-18 | BAE SYSTEMS plc | Thermal management apparatus |
| WO2021165646A1 (en) * | 2020-02-17 | 2021-08-26 | Bae Systems Plc | Thermal management apparatus |
| US20230400283A1 (en) * | 2022-06-13 | 2023-12-14 | Hamilton Sundstrand Corporation | Thermal storage for high load short duration cooling |
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| Publication number | Publication date |
|---|---|
| CN107152890B (en) | 2019-01-11 |
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