CN110285325A - A kind of mixed cool-down method of high temperature gas source water suitable for underwater high-speed navigation device - Google Patents
A kind of mixed cool-down method of high temperature gas source water suitable for underwater high-speed navigation device Download PDFInfo
- Publication number
- CN110285325A CN110285325A CN201910561592.7A CN201910561592A CN110285325A CN 110285325 A CN110285325 A CN 110285325A CN 201910561592 A CN201910561592 A CN 201910561592A CN 110285325 A CN110285325 A CN 110285325A
- Authority
- CN
- China
- Prior art keywords
- water
- water tank
- combustion gas
- outlet pipe
- cool
- 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.)
- Granted
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63H—MARINE PROPULSION OR STEERING
- B63H21/00—Use of propulsion power plant or units on vessels
- B63H21/38—Apparatus or methods specially adapted for use on marine vessels, for handling power plant or unit liquids, e.g. lubricants, coolants, fuels or the like
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17D—PIPE-LINE SYSTEMS; PIPE-LINES
- F17D1/00—Pipe-line systems
- F17D1/02—Pipe-line systems for gases or vapours
- F17D1/04—Pipe-line systems for gases or vapours for distribution of gas
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17D—PIPE-LINE SYSTEMS; PIPE-LINES
- F17D3/00—Arrangements for supervising or controlling working operations
- F17D3/01—Arrangements for supervising or controlling working operations for controlling, signalling, or supervising the conveyance of a product
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Ocean & Marine Engineering (AREA)
- Filling Or Discharging Of Gas Storage Vessels (AREA)
Abstract
The present invention relates to a kind of high temperature gas source water suitable for underwater high-speed navigation device to mix cool-down method, belongs to submarine navigation device combustion gas cooling technology field, solves the problems, such as that existing method can not reasonably cool down to combustion gas.Water of the invention mixes the method that cool-down method is mixed using external water is introduced with high-temperature fuel gas, realizes the purpose for reducing fuel gas temperature.The present invention can carry out continued down to high-temperature fuel gas, reduce structure and equipment heat release, Design on thermal insulation difficulty, while being cooled down by introducing outside water to high-temperature fuel gas, the vapor of generation is as a part of gas source, solid gunpowder dosage can be reduced, increase aircraft overall performance.
Description
Technical field
The present invention relates to submarine navigation device combustion gas cooling technology fields, more particularly to a kind of underwater high-speed that is suitable for navigate by water device
High temperature gas source water mix cool-down method.
Background technique
Underwater high-speed navigates by water device, and there are gas supply requirement, gas source and gas control equipments to be built in aircraft
Portion, if gas source uses high pressure gas cylinder mode, gas energy density is low, and occupancy aircraft inner space is big, will substantially reduce underwater
Aircraft performance.The mode of high-temperature fuel gas is generated currently, burning frequently with solid gunpowder, solid gunpowder energy density is high, can subtract
Occupied space inside small aircraft, but fuel gas temperature is high (1000-2000 degrees Celsius), and this is to aircraft construction, cable arrangements, gas
The Design on thermal insulation of body control valve element design and equipment brings extreme difficulty.
Summary of the invention
In view of above-mentioned analysis, the present invention is intended to provide a kind of mixed drop of high temperature gas source water suitable for underwater high-speed navigation device
Warm method, to solve the problems, such as that existing method can not reasonably cool down to combustion gas.
The purpose of the present invention is mainly achieved through the following technical solutions:
In technical solution of the present invention, a kind of mixed cool-down method of high temperature gas source water suitable for underwater high-speed navigation device, high temperature
Gas source water mix cool-down method the step of include:
S1, fuel chamber's igniting, are passed through outlet pipe distributor chamber for high-temperature fuel gas；
S2, the first water tank is filled the water, until the first water tank fills water；
S3, combustion gas is successively passed through to the first water tank and outlet pipe distributor chamber cools down；
S4, when the water in the first water tank is all discharged with combustion gas, combustion gas is successively passed through the second water tank and
Outlet pipe distributor chamber cools down；
S5, when the water in the second water tank is all discharged with combustion gas, carry out step S3；
S6, circulating repetition step S4, S5 are until fuel chamber stops burning.
In technical solution of the present invention, high temperature gas source water mixes the mixed cooling system of high temperature gas source water that cool-down method uses and includes:
Fuel chamber, the first water tank, the second water tank and outlet pipe distributor chamber；
Fuel chamber is connect by combustion gas supervisor with outlet pipe distributor chamber；Fuel chamber passes through the first combustion gas looped pipeline and the first storage
Water tank connection；Fuel chamber is connect by the second combustion gas looped pipeline with the second water tank；First water tank is by the first mixing tube and goes out
The connection of air pipe distributor chamber；Second water tank is connect by the second mixing tube with outlet pipe distributor chamber；First water tank and
Two water tanks are equipped with water injection pipe, and water injection pipe is equipped with water injection valve.
In technical solution of the present invention, step S1 specifically: after fuel chamber's igniting, the flow control valve of combustion gas supervisor is opened,
And the gas flow of outlet pipe distributor chamber is adjusted into being not less than target flow by flow control valve.
In technical solution of the present invention, step S2 specifically: the water injection valve for opening the first water tank carries out the first water tank
Water filling, until the first water tank is filled with water.
In technical solution of the present invention, in step S3, combustion gas is passed through the first water tank and is cooled down, the combustion gas after cooling with
Water is passed through outlet pipe distributor chamber together, starts simultaneously at and fills the water to the second water tank.
In technical solution of the present invention, step S3 specifically: open the first solenoid valve of the first combustion gas looped pipeline, close the first storage
Combustion gas is passed through the first water tank, the water of the first water tank is made to cool down combustion gas by the water injection valve of water tank, and combustion gas and water are together
Enter outlet pipe distributor chamber by the first mixing tube, simultaneously evaporative cooling is sufficiently mixed in outlet pipe distributor chamber；It beats simultaneously
The water injection valve for opening the second water tank fills the water the second water tank.
In technical solution of the present invention, in step S4, when the water in the first water tank is all discharged with combustion gas, combustion gas is led to
Enter the second water tank to cool down, the combustion gas after cooling is passed through outlet pipe distributor chamber with water together, starts simultaneously at and stores up to first
Water tank is filled the water.
In technical solution of the present invention, step S4 specifically: when all evaporations of the water in the first water tank, and be discharged with combustion gas
When, the second solenoid valve of the second combustion gas looped pipeline is opened, the water injection valve of the second water tank is closed, combustion gas is passed through the second water tank,
The water of the second water tank is set to cool down combustion gas, combustion gas and water pass through the second mixing tube together and enter outlet pipe distributor chamber,
Simultaneously evaporative cooling is sufficiently mixed in outlet pipe distributor chamber；The water injection valve for opening simultaneously the first water tank, to the first water tank
It is filled the water.
In technical solution of the present invention, step S5 specifically: when all evaporations of the water in the second water tank, and be discharged with combustion gas
Shi Chongfu step S3；
The first solenoid valve of the first combustion gas looped pipeline is opened, the water injection valve of the first water tank is closed, combustion gas is passed through the first storage
Water tank makes the water of the first water tank cool down combustion gas, and combustion gas and water pass through the first mixing tube together and enters outlet pipe point
With room, simultaneously evaporative cooling is sufficiently mixed in outlet pipe distributor chamber；The water injection valve for opening simultaneously the second water tank is stored up to second
Water tank is filled the water.
In technical solution of the present invention, in step S6, circulating repetition step S4, S5 is until fuel chamber stops burning, by first
Water in water tank and the second water tank is all discharged.S4, S5 technical solution of the present invention at least can be realized one of following effect:
1, the present invention can effectively cool down to combustion gas by way of water cooling, and the combustion gas for preventing temperature excessively high is to whole
A aircraft damages.
2, the present invention is cooled down in the form of evaporating water cooling, and more heat can be absorbed by way of evaporation
Amount, keeps this method more preferable to the cooling effect of combustion gas.
3, the present invention further increases cooling effect using the alternate mode of two-way water cooling, prevents single water route for a long time
The cooling effect that works weakens.
4, the vapor of generation is evaporated in the present invention as a part of gas source, is reduced solid gunpowder dosage, is increased navigation
The overall performance of device.
It in the present invention, can also be combined with each other between above-mentioned each technical solution, to realize more preferred assembled schemes.This
Other feature and advantage of invention will illustrate in the following description, also, certain advantages can become from specification it is aobvious and
It is clear to, or understand through the implementation of the invention.The objectives and other advantages of the invention can by specification, claims with
And it is achieved and obtained in specifically noted content in attached drawing.
Detailed description of the invention
Attached drawing is only used for showing the purpose of specific embodiment, and is not to be construed as limiting the invention, in entire attached drawing
In, identical reference symbol indicates identical component.
Fig. 1 is a kind of schematic device that the mixed cool-down method of the high temperature gas source water for navigating by water device suitable for underwater high-speed uses.
Appended drawing reference:
1- fuel chamber；The first water tank of 201-；The second water tank of 202-；3- outlet pipe distributor chamber；4- flow control valve；
The first check valve of 501-；502- second one-way valve；The first solenoid valve of 601-；602- second solenoid valve.
Specific embodiment
Specifically describing the preferred embodiment of the present invention with reference to the accompanying drawing, wherein attached drawing constitutes the application a part, and
Together with embodiments of the present invention for illustrating the principle of the present invention, it is not intended to limit the scope of the present invention.
For submarine navigation device in such a way that solid gunpowder burns and generates high-temperature fuel gas, solid gunpowder energy density is high at present,
Occupied space inside aircraft can be reduced, but fuel gas temperature is high (1000-2000 DEG C), this is to aircraft construction, cable arrangements, gas
The Design on thermal insulation of body control valve element design and equipment brings extreme difficulty.The present invention disadvantage high for high-temperature fuel gas temperature,
The method for proposing to mix using external water is introduced with high-temperature fuel gas realizes the purpose for reducing fuel gas temperature.
Specifically, the embodiment of the invention provides a kind of high temperature gas source water suitable for underwater high-speed navigation device to mix cooling side
Method, as shown in Figure 1, it includes: that fuel chamber 1, first stores up that wet source water, which mixes the high temperature gas source water that cool-down method uses to mix cooling system,
Water tank 201, the second water tank 202 and outlet pipe distributor chamber 3；Fuel chamber 1 is connected by combustion gas supervisor and outlet pipe distributor chamber 3
It connects；Fuel chamber 1 is fixed on inside submarine navigation device, and gunpowder is poured inside fuel chamber 1, and 1 structure of fuel chamber makees heat release and heat-insulated place
Reason；Fuel chamber 1 is connect by the first combustion gas looped pipeline with the first water tank 201；Fuel chamber 1 passes through the second combustion gas looped pipeline and the second storage
Water tank 202 connects；First water tank 201 is connect by the first mixing tube with outlet pipe distributor chamber 3；Second water tank 202 is logical
The second mixing tube is crossed to connect with outlet pipe distributor chamber 3；First water tank 201 and the second water tank 202 are equipped with water injection pipe, and
Water injection pipe is equipped with water injection valve, and water main, which is open, is arranged in the shoulder of aircraft, is in communication with the outside.
In actual use, the first water route include the first water tank 201, the first combustion gas looped pipeline and the first mixing tube, second
Water route includes the second water tank 202, the second combustion gas looped pipeline and the second mixing tube, and two water routes are used alternatingly, a water route into
When row cooling, another water route is filled the water, and also the last time can also can be dropped to this water route by water filling when furthermore filling the water
Residual heat when warm in water tank is absorbed, and two water routes have preferably cooling effect always when can be effectively.
In order to switch over to two water routes, combustion gas supervisor is equipped with flow control valve 4；First mixing tube is equipped with the
One check valve 501；Second mixing tube is equipped with second one-way valve 502；First combustion gas looped pipeline is equipped with the first solenoid valve 601；Second combustion
Gas looped pipeline is equipped with second solenoid valve 602.Unidirectional valve action is setting flow direction, when in water tank pressure greater than outlet pipe point
When with room 3, fluid media (medium) flows to outlet pipe distributor chamber 3 by water tank, when pressure is lower than outlet pipe distributor chamber 3 in water tank
When interior pressure, no fluid media (medium) flowing.Solenoid valve is only used as switch.Flow control valve 4 is in addition to can be realized combustion gas supervisor
Switch outside, moreover it is possible to adjust the gas flow in outlet pipe distributor chamber 3.
In addition, outlet pipe distributor chamber 3 is equipped with flow monitoring device, need to make the flow and mesh of outlet pipe distributor chamber 3
It is approximately equal to mark flow.The flow in two water routes is fixed, therefore when being cooled down, and can also directly pass through flow control
Valve 4 adjusts the gas flow in outlet pipe distributor chamber 3.Target flow can be slightly larger than the stream in single water route under normal conditions
Amount, both can control flow by flow control valve 4, the excessive combustion gas that do not cool down will not be made to enter outlet pipe distributor chamber
3.During practical adjustment, measured discharge should be not less than target flow, prevent gas in whole system excessive, and pressure is excessive,
It damages.
The high temperature gas source water of the embodiment of the present invention mixes the step of cool-down method and includes:
S1, fuel chamber 1 light a fire, and high-temperature fuel gas is passed through outlet pipe distributor chamber 3；
After fuel chamber 1 lights a fire, turn-on flow rate control valve 4, and outlet pipe distributor chamber is adjusted by flow control valve 4
3 gas flow is to being not less than target flow.
S2, the first water tank 201 is filled the water, until the first water tank 201 fills water；
The water injection valve for opening the first water tank 201 fills the water the first water tank 201, until 201 quilt of the first water tank
Water is filled, pressure is greater than pressure in the first water tank 201 in outlet pipe distributor chamber 3 at this time, and the first check valve 501, which is in, closes
State flows between the first water tank 201 and outlet pipe distributor chamber 3 without fluid media (medium).
S3, combustion gas is passed through to the first water tank 201 cools down, the combustion gas after cooling is passed through outlet pipe point with water together
With room 3, starts simultaneously at and the second water tank 202 is filled the water；
The first solenoid valve 601 is opened, the water injection valve of the first water tank 201 is closed, combustion gas is passed through the first water tank 201,
The water of the first water tank 201 is set to cool down combustion gas, combustion gas and water pass through the first mixing tube together and enters outlet pipe distribution
Room 3 is sufficiently mixed simultaneously evaporative cooling in outlet pipe distributor chamber 3, is at this time high temperature and high pressure environment in fuel chamber 1, and pressure
Greater than in outlet pipe distributor chamber 3 in the first water tank of pressure 201 water 1 high pressure of fuel chamber effect under through the first check valve 501
Into outlet pipe distributor chamber 3, the water into outlet pipe distributor chamber 3 mixes vaporization, high-temperature fuel gas temperature drop with high-temperature fuel gas
It is low；The water injection valve for opening simultaneously the second water tank 202 fills the water the second water tank 202, at this time outlet pipe distributor chamber 3
Interior pressure is greater than pressure in the second water tank 202, and second one-way valve 502 is in close state, the second water tank 202 and escape pipe
It is flowed between road distributor chamber 3 without fluid media (medium).
S4, when the water in the first water tank 201 is all discharged with combustion gas, combustion gas is passed through the second water tank 202 and is carried out
Cooling, the combustion gas after cooling are passed through outlet pipe distributor chamber 3 together with water, start simultaneously at and fill the water to the first water tank 201；
When the water in the first water tank 201 all evaporates, and when being discharged with combustion gas, second solenoid valve 602 is opened, closes the
Combustion gas is passed through the second water tank 202, drops the water of the second water tank 202 to combustion gas by the water injection valve of two water tanks 202
Temperature, combustion gas and water pass through the second mixing tube together and enter outlet pipe distributor chamber 3, are sufficiently mixed in outlet pipe distributor chamber 3
And evaporative cooling；The water injection valve for opening simultaneously the first water tank 201 fills the water the first water tank 201.
S5, when the water in the second water tank 202 is all discharged with combustion gas, repeat step S3；
When the water in the second water tank 202 all evaporates, and when being discharged with combustion gas, the first solenoid valve 601 is opened, closes the
Combustion gas is passed through the first water tank 201, drops the water of the first water tank 201 to combustion gas by the water injection valve of one water tank 201
Temperature, combustion gas and water pass through the first mixing tube together and enter outlet pipe distributor chamber 3, are sufficiently mixed in outlet pipe distributor chamber 3
And evaporative cooling；The water injection valve for opening simultaneously the second water tank 202 fills the water the second water tank 202.
S6, circulating repetition step S4, S5 make water in water tank continue into outlet pipe under the effect of 1 high pressure of fuel chamber
Distributor chamber 3, cools down to combustion gas；Until fuel chamber 1 stops burning, it will be in the first water tank 201 and the second water tank 202
Water is all discharged.
In step S4, S5 and S6, the gas flow of outlet pipe distributor chamber 3 is adjusted into extremely by flow control valve 4
Not less than target flow.The flow in two water routes is fixed, therefore when being cooled down, and can also directly pass through flow control
Valve 4 adjusts the gas flow in outlet pipe distributor chamber 3.Target flow can be slightly larger than the stream in single water route under normal conditions
Amount, both can control flow by flow control valve 4, the excessive combustion gas that do not cool down will not be made to enter outlet pipe distributor chamber
3.During practical adjustment, measured discharge should be not less than target flow, prevent gas in whole system excessive, and pressure is excessive,
It damages.
The embodiment of the invention provides a kind of high temperature gas source water suitable for underwater high-speed navigation device to mix cool-down method, this hair
Bright effectively to be cooled down to combustion gas by way of water cooling, the combustion gas for preventing temperature excessively high causes to damage to entire aircraft
It is bad；The present invention is cooled down in the form of evaporating water cooling, and more heats can be absorbed by way of evaporation, make we
Method is more preferable to the cooling effect of combustion gas；The present invention further increases cooling effect using the alternate mode of two-way water cooling, prevents
Single water route work long hours cooling effect decrease；The vapor of generation is evaporated in the present invention as a part of gas source, can be reduced
Solid gunpowder dosage increases aircraft overall performance.
The foregoing is only a preferred embodiment of the present invention, but scope of protection of the present invention is not limited thereto,
In the technical scope disclosed by the present invention, any changes or substitutions that can be easily thought of by anyone skilled in the art,
It should be covered by the protection scope of the present invention.
Claims (10)
1. a kind of high temperature gas source water suitable for underwater high-speed navigation device mixes cool-down method, which is characterized in that the high temperature gas source
Water mix cool-down method the step of include:
S1, fuel chamber (1) igniting, are passed through outlet pipe distributor chamber (3) for high-temperature fuel gas；
S2, the first water tank (201) is filled the water, until the first water tank (201) fill water；
S3, combustion gas is successively passed through to the first water tank (201) and outlet pipe distributor chamber (3) cools down；
S4, when the water in the first water tank (201) is all discharged with combustion gas, combustion gas is successively passed through to the second water tank
(202) cool down with outlet pipe distributor chamber (3)；
S5, when the water in the second water tank (202) is all discharged with combustion gas, carry out step S3；
S6, circulating repetition step S4, S5 are until fuel chamber (1) stops burning.
2. high temperature gas source water according to claim 1 mixes cool-down method, which is characterized in that the mixed cooling of the high temperature gas source water
It includes: fuel chamber (1), the first water tank (201), the second water tank (202) that the high temperature gas source water that method uses, which mixes cooling system,
With outlet pipe distributor chamber (3)；
The fuel chamber (1) is connect by combustion gas supervisor with outlet pipe distributor chamber (3)；The fuel chamber (1) passes through the first combustion
Gas looped pipeline is connect with the first water tank (201)；The fuel chamber (1) is connected by the second combustion gas looped pipeline and the second water tank (202)
It connects；First water tank (201) is connect by the first mixing tube with outlet pipe distributor chamber (3)；Second water tank
(202) it is connect by the second mixing tube with outlet pipe distributor chamber (3)；First water tank (201) and the second water tank
(202) it is equipped with water injection pipe, and water injection pipe is equipped with water injection valve.
3. high temperature gas source water according to claim 2 mixes cool-down method, which is characterized in that the step S1 specifically: combustion
After gas chamber (1) igniting, the flow control valve (4) of combustion gas supervisor is opened, and be adjusted into outlet pipe by flow control valve (4)
The gas flow of distributor chamber (3) is to being not less than target flow.
4. high temperature gas source water according to claim 2 mixes cool-down method, which is characterized in that the step S2 specifically: beat
The water injection valve for opening the first water tank (201) fills the water the first water tank (201), until the first water tank (201) are filled with
Water.
5. high temperature gas source water according to claim 2 mixes cool-down method, which is characterized in that in the step S3, by combustion gas
It is passed through the first water tank (201) to cool down, the combustion gas after cooling is passed through outlet pipe distributor chamber (3) with water together, opens simultaneously
Beginning fills the water the second water tank (202).
6. high temperature gas source water according to claim 5 mixes cool-down method, which is characterized in that the step S3 specifically: beat
The first solenoid valve (601) of the first combustion gas looped pipeline is opened, the water injection valve of the first water tank (201) is closed, combustion gas is passed through the first storage
Water tank (201) makes the water of the first water tank (201) cool down combustion gas, and combustion gas and water pass through the entrance of the first mixing tube together
Outlet pipe distributor chamber (3) is sufficiently mixed simultaneously evaporative cooling in outlet pipe distributor chamber (3)；Open simultaneously the second water tank
(202) water injection valve fills the water the second water tank (202).
7. high temperature gas source water according to claim 2 mixes cool-down method, which is characterized in that in the step S4, when first
When water in water tank (201) is all discharged with combustion gas, combustion gas is passed through the second water tank (202) and is cooled down, after cooling
Combustion gas is passed through outlet pipe distributor chamber (3) with water together, starts simultaneously at and fills the water to the first water tank (201).
8. high temperature gas source water according to claim 7 mixes cool-down method, which is characterized in that the step S4 specifically: when
Water in first water tank (201) all evaporates, and when being discharged with combustion gas, opens the second solenoid valve of the second combustion gas looped pipeline
(602), the water injection valve for closing the second water tank (202), is passed through the second water tank (202) for combustion gas, makes the second water tank (202)
Water cool down to combustion gas, combustion gas and water pass through the second mixing tube together and enter outlet pipe distributor chamber (3), in outlet pipe
Simultaneously evaporative cooling is sufficiently mixed in distributor chamber (3)；The water injection valve for opening simultaneously the first water tank (201), to the first water tank
(201) it is filled the water.
9. high temperature gas source water according to claim 2 mixes cool-down method, which is characterized in that the step S5 specifically: when
Water in second water tank (202) all evaporates, and while being discharged with combustion gas repeats step S3；
The first solenoid valve (601) of the first combustion gas looped pipeline is opened, the water injection valve of the first water tank (201) is closed, combustion gas is passed through
First water tank (201) makes the water of the first water tank (201) cool down combustion gas, and combustion gas and water pass through the first mixing together
Pipe enters outlet pipe distributor chamber (3), and simultaneously evaporative cooling is sufficiently mixed in outlet pipe distributor chamber (3)；Open simultaneously second
The water injection valve of water tank (202) fills the water the second water tank (202).
10. high temperature gas source water described in -9 mixes cool-down method according to claim 1, which is characterized in that in the step S6, circulation
Step S4, S5 is repeated until fuel chamber (1) stopping burning, complete by the water in the first water tank (201) and the second water tank (202)
Portion's discharge.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910561592.7A CN110285325B (en) | 2019-06-26 | 2019-06-26 | High-temperature air source water-mixing cooling method suitable for underwater high-speed aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910561592.7A CN110285325B (en) | 2019-06-26 | 2019-06-26 | High-temperature air source water-mixing cooling method suitable for underwater high-speed aircraft |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN110285325A true CN110285325A (en) | 2019-09-27 |
| CN110285325B CN110285325B (en) | 2020-08-14 |
Family
ID=68006292
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910561592.7A Active CN110285325B (en) | 2019-06-26 | 2019-06-26 | High-temperature air source water-mixing cooling method suitable for underwater high-speed aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN110285325B (en) |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2421531Y (en) * | 2000-05-15 | 2001-02-28 | 董立新 | Multi-jet nozzle bundling type shock wave soot blower |
| CN102243025A (en) * | 2011-06-20 | 2011-11-16 | 北京中冶设备研究设计总院有限公司 | Process and device for recycling flue gas afterheat of electric furnace |
| CN105805749A (en) * | 2016-05-04 | 2016-07-27 | 福建铁拓机械有限公司 | Pitch aggregate drying and heating combustor and combustor air supplying and cooling method |
| GB2536905A (en) * | 2015-03-30 | 2016-10-05 | Edwards Ltd | Radiant burner |
| US20170009984A1 (en) * | 2015-07-08 | 2017-01-12 | Hanwha Techwin Co., Ltd. | Impinging-type temperature uniformity device |
| CN109563991A (en) * | 2016-07-28 | 2019-04-02 | 弗罗拉德瑞有限公司 | Fractional combustion |
| CN109838684A (en) * | 2019-01-25 | 2019-06-04 | 集美大学 | The use of underwater boat device exhaust gas and storage device and its method |
-
2019
- 2019-06-26 CN CN201910561592.7A patent/CN110285325B/en active Active
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2421531Y (en) * | 2000-05-15 | 2001-02-28 | 董立新 | Multi-jet nozzle bundling type shock wave soot blower |
| CN102243025A (en) * | 2011-06-20 | 2011-11-16 | 北京中冶设备研究设计总院有限公司 | Process and device for recycling flue gas afterheat of electric furnace |
| GB2536905A (en) * | 2015-03-30 | 2016-10-05 | Edwards Ltd | Radiant burner |
| US20170009984A1 (en) * | 2015-07-08 | 2017-01-12 | Hanwha Techwin Co., Ltd. | Impinging-type temperature uniformity device |
| CN105805749A (en) * | 2016-05-04 | 2016-07-27 | 福建铁拓机械有限公司 | Pitch aggregate drying and heating combustor and combustor air supplying and cooling method |
| CN109563991A (en) * | 2016-07-28 | 2019-04-02 | 弗罗拉德瑞有限公司 | Fractional combustion |
| CN109838684A (en) * | 2019-01-25 | 2019-06-04 | 集美大学 | The use of underwater boat device exhaust gas and storage device and its method |
Also Published As
| Publication number | Publication date |
|---|---|
| CN110285325B (en) | 2020-08-14 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US7661414B2 (en) | Internal combustion engine system | |
| JP2012007796A (en) | Heat storage system | |
| CN107202383A (en) | The refrigerating plant of combined supply system | |
| CN106164599B (en) | The fluid treating device and method of fluid stream is heated or cooled | |
| JP5141101B2 (en) | Steam generation system | |
| US20180219237A1 (en) | Fuel Cell Freeze Protection Device and System | |
| US20170008367A1 (en) | Hybrid type heating system capable of supplying heat and hot water | |
| JP5208567B2 (en) | Hydrogen gas release / storage system | |
| CN110155280A (en) | A kind of mixed cooling system of high temperature gas source water suitable for underwater high-speed navigation device | |
| CN110285325A (en) | A kind of mixed cool-down method of high temperature gas source water suitable for underwater high-speed navigation device | |
| CN105444309B (en) | A kind of LNG ship air-conditioning and jelly library system | |
| US20110088665A1 (en) | Fuel Economizer Fuel Vapor System For Internal Combustion Engine | |
| JP2018035764A (en) | Exhaust heat recovery device for engine | |
| US10654583B2 (en) | Fuel tank inerting system and method | |
| US9033317B2 (en) | Fuel carburetor | |
| KR102578398B1 (en) | Temperature Control System for Exhaust Gas Treatment Device | |
| CN106414123A (en) | Vehicle cooling device capable of instant cooling, vehicle comprising same, and instant cooling method for vehicle | |
| KR101165304B1 (en) | Heat-Exchange Apparatus with Micro-channels | |
| KR102469059B1 (en) | Pipeline network system supplying thermal effluent and CO2 emitted from power plant to greenhouse | |
| CN109404720A (en) | The cooling of the vaporized component of liquefied gas for dynamic power machine, equipment or the vehicles | |
| KR101631388B1 (en) | Vaporization Apparatus for Liquefied Natural Gas | |
| CN211400368U (en) | Adsorption type refrigeration cycle system | |
| JP2002039692A (en) | Heat exchanger and heat exchange system for liquefied natural gas | |
| US20200188625A1 (en) | Cooling device and process for cooling for a closed-circuit respirator | |
| RU2177894C2 (en) | Airship |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant |