CN207286684U - Spray heat-proof device in a kind of model of an airplane foam whirlpool - Google Patents
Spray heat-proof device in a kind of model of an airplane foam whirlpool Download PDFInfo
- Publication number
- CN207286684U CN207286684U CN201721177478.7U CN201721177478U CN207286684U CN 207286684 U CN207286684 U CN 207286684U CN 201721177478 U CN201721177478 U CN 201721177478U CN 207286684 U CN207286684 U CN 207286684U
- Authority
- CN
- China
- Prior art keywords
- wall
- model
- heat
- cooler bin
- foam
- Prior art date
- 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.)
- Expired - Fee Related
Links
Abstract
The utility model discloses a kind of model of an airplane foam whirlpool to spray heat-proof device, including the heat-sink shell being socketed on foam turbojet engine, the heat-sink shell outer wall welding has cooling water pipe, and the specification of cooling water pipe is adapted with the specification of heat-sink shell, the cooling water pipe outer wall is bonded with thermal insulation layer, and thermal insulation layer top exterior walls and bottom outer wall are both provided with support plate, the corner of two support plate opposite side outer walls is fixed with support leg by screw, and support leg is fixed by screws on thermal insulation layer away from support plate one end, two opposite side outer walls of support plate are fixed with the first cooler bin and the second cooler bin by screw respectively.The utility model good water-cooling effect, effectively heat-insulated and heat dissipation, reduce the damage of model of an airplane other parts, temperature in use sensor monitors the turbojet engine temperature of model aircraft in real time, regulation and control in time, equipment damage rate is reduced, semiconductor chilling plate in time cools down the water source for absorbing heat, improves cooling effect.
Description
Technical field
It the utility model is related to model of an airplane technical field, more particularly to a kind of model of an airplane foam whirlpool spray heat-proof device.
Background technology
Turbojet is a kind of turbogenerator, and feature is to be completely dependent on combustion gas stream to produce thrust.It is typically used as
The power of high-speed aircraft, but oil consumption is higher than turbofan, and turbojet engine is divided into centrifugal and two kinds of axial-flow type, centrifugation
Formula is invented by British Frank Hui Teer jazz in nineteen thirty, but until aircraft ability of the nineteen forty-one equipped with this engine
Go up to the sky for the first time, also do not participate in World War II；Axial-flow type is born in Germany, and the jet practical as the first
The power of formula fighter plane Me-262 puts into battlefield in summer nineteen forty-four, and compared to centrifugal turbojet engine is played, axial-flow type has transversal
The advantages of face is small, and compression ratio is high, current turbojet engine are mostly axial-flow type, the foam whirlpool used in the existing model of an airplane
Spray is often excessive because generating heat, and often results in other parts internal combustion in aircraft, causes equipment damage serious.
The content of the invention
The purpose of this utility model is and a kind of model of an airplane bubble proposed in order to solve shortcoming existing in the prior art
Spray heat-proof device in foam whirlpool.
To achieve these goals, the utility model employs following technical solution：
Heat-proof device, including the heat-sink shell being socketed on foam turbojet engine are sprayed in a kind of model of an airplane foam whirlpool, described
Heat-sink shell outer wall welding has cooling water pipe, and the specification of cooling water pipe is adapted with the specification of heat-sink shell, outside the cooling water pipe
Wall is bonded with thermal insulation layer, and thermal insulation layer top exterior walls and bottom outer wall are both provided with support plate, and two support plates are with respect to one
The corner of side outer wall is fixed with support leg by screw, and support leg is fixed by screws in thermal insulation layer away from support plate one end
On, two opposite side outer walls of support plate are fixed with the first cooler bin and the second cooler bin, and first by screw respectively
Cooler bin side outer wall is fixed with the second water pump by screw, and the second cooler bin side outer wall is fixed with first by screw
Water pump, and the second water pump water outlet end and the water outlet of the first water pump are plugged with L-shaped conduit, two L-shaped conduit outer walls point
The first solenoid valve and second solenoid valve are not connected with by clip, and two L-shaped conduits be plugged on away from support plate one end it is cold
But in water pipe, first cooler bin and the second cooler bin are fixed with semiconductor system close to support plate side inner wall by screw
Cold, and the first cooler bin and the second cooler bin are fixed with waterproof cover, semiconductor close to support plate side inner wall by screw
Cooling piece is located in waterproof cover.
Preferably, the thermal insulation layer is fixed with alarm close to the first cooler bin side outer wall by screw, and alarm,
First water pump, the second water pump, the first solenoid valve and second solenoid valve are respectively connected with switch, and switch is connected with model DATA-
7311 controller, the first water pump and the second water pump are two-way suction pump.
Preferably, the heat-sink shell top inner wall is provided with card slot, and card slot inner wall is connected with the temperature biography of model BM100
Sensor, temperature sensor output terminal are connected by signal wire with controller.
Preferably, the waterproof cover is semicircular structure, and the specification of waterproof cover and the specification of semiconductor chilling plate are mutually fitted
Match somebody with somebody.
Preferably, first cooler bin and the second cooler bin are provided with water inlet away from support plate side outer wall, and into
Mouth of a river inner wall has been connected through a screw thread end cap.
Preferably, the specification of the thermal insulation layer is adapted with the specification of cooling water pipe, and thermal insulation layer top exterior walls and bottom
Outer wall is provided with through hole, and L-shaped conduit is plugged in through hole.
The beneficial effects of the utility model are：In the utility model, coordinated by water tank and water cooling tube, good water-cooling effect,
Effectively heat-insulated and heat dissipation, reduces the damage of model of an airplane other parts, and aircraft mould is monitored in real time by using temperature sensor
The turbojet engine temperature of type, in time regulation and control, reduces equipment damage rate, will absorb the water of heat in time using semiconductor chilling plate
Source cooling, improves cooling effect.
Brief description of the drawings
Fig. 1 be the utility model proposes a kind of model of an airplane foam whirlpool spray heat-proof device structure diagram；
Fig. 2 be the utility model proposes a kind of model of an airplane foam whirlpool spray heat-proof device structure top view.
In figure：1 first cooler bin, 2 cooling water pipes, 3 thermal insulation layers, 4 first solenoid valves, 5 first water pumps, 6 support plates, 7 are prevented
Water cover, 8 second cooler bins, 9 temperature sensors, 10 second water pumps, 11 semiconductor chilling plates, 12 second solenoid valves, 13 alarms,
14 heat-sink shells.
Embodiment
The following is a combination of the drawings in the embodiments of the present utility model, and the technical scheme in the embodiment of the utility model is carried out
Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole
Embodiment.
Referring to Figures 1 and 2, a kind of model of an airplane foam whirlpool spray heat-proof device, including be socketed on foam turbojet engine
Heat-sink shell 14,14 outer wall welding of heat-sink shell has cooling water pipe 2, and the specification of cooling water pipe 2 and the specification of heat-sink shell 14 are mutually fitted
Match somebody with somebody, 2 outer wall of cooling water pipe is bonded with thermal insulation layer 3, and 3 top exterior walls of thermal insulation layer and bottom outer wall are both provided with support plate 6, two
The corner of 6 opposite side outer wall of support plate is fixed with support leg by screw, and support leg passes through spiral shell away from 6 one end of support plate
Nail is fixed on thermal insulation layer 3, and the opposite side outer wall of two support plates 6 is fixed with the first cooler bin 1 and second by screw respectively
Cooler bin 8, and 1 side outer wall of the first cooler bin is fixed with the second water pump 10 by screw, 8 side outer wall of the second cooler bin passes through
Screw is fixed with the first water pump 5, and 10 water outlet of the second water pump and the water outlet of the first water pump 5 are plugged with L-shaped conduit, two
L-shaped conduit outer wall is connected with the first solenoid valve 4 and second solenoid valve 12 by clip respectively, and two L-shaped conduits are away from support
6 one end of plate is plugged in cooling water pipe 2, and the first cooler bin 1 and the second cooler bin 8 pass through close to 6 side inner wall of support plate
Screw is fixed with semiconductor chilling plate 11, and the first cooler bin 1 and the second cooler bin 8 pass through close to 6 side inner wall of support plate
Screw is fixed with waterproof cover 7, and semiconductor chilling plate 11 is located in waterproof cover 7.
In the utility model, thermal insulation layer 3 is fixed with alarm 13 close to 1 side outer wall of the first cooler bin by screw, and
Alarm 13, the first water pump 5, the second water pump 10, the first solenoid valve 4 and second solenoid valve 12 are respectively connected with switch, switch connection
There is a controller of model DATA-7311, the first water pump 5 and the second water pump 10 are two-way suction pump, in the top of heat-sink shell 14
Wall is provided with card slot, and card slot inner wall is connected with the temperature sensor 9 of model BM100, and temperature sensor output terminal passes through signal
Line is connected with controller, and waterproof cover 7 is semicircular structure, and the specification of waterproof cover 7 and the specification phase of semiconductor chilling plate 11
Adaptation, the first cooler bin 1 and the second cooler bin 8 are provided with water inlet away from 6 side outer wall of support plate, and water inlet inner wall passes through
End cap is threaded with, the specification of thermal insulation layer 3 is adapted with the specification of cooling water pipe 2, and outside 3 top exterior walls of thermal insulation layer and bottom
Wall is provided with through hole, and L-shaped conduit is plugged in through hole.
Operation principle：By the heat-sink shell 14 being adapted with the spray of model of an airplane foam whirlpool on the model of an airplane, temperature sensing
Device 9 monitors air temperature in real time, when temperature is excessive, opens the first water pump 5 and the second water pump 10, water source is in cooling water pipe 2
Circulate, complete cooling, thermal insulation layer 3 separates turbojet engine and other parts, and semiconductor chilling plate 11 will absorb heat
Water source cooling afterwards, realization recycle.
The above, is only the preferable embodiment of the utility model, but the scope of protection of the utility model is not
This is confined to, any one skilled in the art is in the technical scope that the utility model discloses, according to this practicality
New technical solution and its utility model design are subject to equivalent substitution or change, should all cover the protection model in the utility model
Within enclosing.
Claims (6)
1. heat-proof device, including the heat-sink shell being socketed on foam turbojet engine are sprayed in a kind of model of an airplane foam whirlpool（14）, its
It is characterized in that, the heat-sink shell（14）Outer wall welding has cooling water pipe（2）, and cooling water pipe（2）Specification and heat-sink shell（14）
Specification be adapted, the cooling water pipe（2）Outer wall is bonded with thermal insulation layer（3）, and thermal insulation layer（3）Top exterior walls and bottom outer wall
It is both provided with support plate（6）, two support plates（6）The corner of opposite side outer wall is fixed with support leg by screw,
And support leg is away from support plate（6）One end is fixed by screws in thermal insulation layer（3）On, two support plates（6）Opposite side
Outer wall is fixed with the first cooler bin by screw respectively（1）With the second cooler bin（8）, and the first cooler bin（1）Side outer wall leads to
Cross screw and be fixed with the second water pump（10）, second cooler bin（8）Side outer wall is fixed with the first water pump by screw（5）,
And second water pump（10）Water outlet and the first water pump（5）Water outlet be plugged with L-shaped conduit, two L-shaped conduit outer walls
The first solenoid valve is connected with by clip respectively（4）And second solenoid valve（12）, and two L-shaped conduits are away from support plate（6）One
End is plugged on cooling water pipe（2）It is interior, first cooler bin（1）With the second cooler bin（8）Close to support plate（6）Side inner wall
Semiconductor chilling plate is fixed with by screw（11）, and the first cooler bin（1）With the second cooler bin（8）Close to support plate（6）
Side inner wall is fixed with waterproof cover by screw（7）, semiconductor chilling plate（11）Positioned at waterproof cover（7）It is interior.
A kind of 2. model of an airplane foam whirlpool spray heat-proof device according to claim 1, it is characterised in that the thermal insulation layer
（3）Close to the first cooler bin（1）Side outer wall is fixed with alarm by screw（13）, and alarm（13）, the first water pump
（5）, the second water pump（10）, the first solenoid valve（4）And second solenoid valve（12）Switch is respectively connected with, switch is connected with model
The controller of DATA-7311, the first water pump（5）With the second water pump（10）It is two-way suction pump.
A kind of 3. model of an airplane foam whirlpool spray heat-proof device according to claim 1, it is characterised in that the heat-sink shell
（14）Top inner wall is provided with card slot, and card slot inner wall is connected with the temperature sensor of model BM100（9）, temperature sensor is defeated
Outlet is connected by signal wire with controller.
A kind of 4. model of an airplane foam whirlpool spray heat-proof device according to claim 1, it is characterised in that the waterproof cover
（7）For semicircular structure, and waterproof cover（7）Specification and semiconductor chilling plate（11）Specification be adapted.
A kind of 5. model of an airplane foam whirlpool spray heat-proof device according to claim 1, it is characterised in that first cooling
Case（1）With the second cooler bin（8）Away from support plate（6）Side outer wall is provided with water inlet, and water inlet inner wall is connected by screw thread
It is connected to end cap.
A kind of 6. model of an airplane foam whirlpool spray heat-proof device according to claim 1, it is characterised in that the thermal insulation layer
（3）Specification and cooling water pipe（2）Specification be adapted, and thermal insulation layer（3）Top exterior walls and bottom outer wall are provided with through hole, L
Shape conduit is plugged in through hole.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721177478.7U CN207286684U (en) | 2017-09-14 | 2017-09-14 | Spray heat-proof device in a kind of model of an airplane foam whirlpool |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721177478.7U CN207286684U (en) | 2017-09-14 | 2017-09-14 | Spray heat-proof device in a kind of model of an airplane foam whirlpool |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207286684U true CN207286684U (en) | 2018-05-01 |
Family
ID=62441357
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721177478.7U Expired - Fee Related CN207286684U (en) | 2017-09-14 | 2017-09-14 | Spray heat-proof device in a kind of model of an airplane foam whirlpool |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207286684U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110834733A (en) * | 2019-11-14 | 2020-02-25 | 中国商用飞机有限责任公司 | Air preparation system |
-
2017
- 2017-09-14 CN CN201721177478.7U patent/CN207286684U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110834733A (en) * | 2019-11-14 | 2020-02-25 | 中国商用飞机有限责任公司 | Air preparation system |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN105468117A (en) | Liquid cooling system of server | |
| CN207286684U (en) | Spray heat-proof device in a kind of model of an airplane foam whirlpool | |
| CN103299142A (en) | Cooling device for a super conductor and super conducting synchronous machine | |
| CN103779048A (en) | Main-transformation heat-dissipating device with SF6 (sulfur hexafluoride) as refrigerant medium and heat-dissipating method | |
| CN203120720U (en) | Long-distance storage and transportation device for temporary farming of fresh and alive aquatic products | |
| CN102548364B (en) | Dual-heat-sink device for cooling electronic equipment | |
| CN209136175U (en) | Condensing unit and steam oven | |
| CN203761201U (en) | Water-cooled permanent magnet brushless direct-current motor | |
| CN207179378U (en) | A kind of LED using radiating structure is towards day lamp | |
| CN106766344A (en) | Semiconductor electronic refrigerating system and the net water dispenser with it | |
| CN207382771U (en) | A kind of Backpack type radiator | |
| CN205823436U (en) | A kind of diesel-driven generator | |
| CN108422916B (en) | A kind of energy complicated utilization type vehicle-carrying foodstuff, drink storage system | |
| CN108194185A (en) | A kind of vertical pivot water jacket of internal combustion engine exhaust pipe device | |
| CN105680629A (en) | Permanent magnet motor outer water cooling device | |
| CN112901384A (en) | High-pressure common rail pipe of methanol fuel engine | |
| CN204511636U (en) | Evaporative type intercooler | |
| CN202628256U (en) | Water-cooling circulating system of motorcycle engine | |
| CN207235310U (en) | A kind of electric cabinet cooling system | |
| CN208352818U (en) | A kind of low-pressure electric cabinet with recyclable heat sinking function | |
| JPS5746016A (en) | Suction gas cooling device of internal combustion engine with supercharger | |
| CN205747575U (en) | The explosion-proof type lithium bromide absorption-type machine unit that absorbing liquid pump frequency conversion controls controls device | |
| CN205279314U (en) | Damp curtain air cooler | |
| CN204419336U (en) | A kind of exhaust manifold thermal shield, engine cooling water route system and automobile | |
| CN213208339U (en) | Environment-friendly cooling water system |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20180501 Termination date: 20210914 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |