CN105523186B - It is a kind of for/the synthesis thermojet driver of frost/ice and the application of dehumidifying - Google Patents
It is a kind of for/the synthesis thermojet driver of frost/ice and the application of dehumidifying Download PDFInfo
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- CN105523186B CN105523186B CN201510920386.2A CN201510920386A CN105523186B CN 105523186 B CN105523186 B CN 105523186B CN 201510920386 A CN201510920386 A CN 201510920386A CN 105523186 B CN105523186 B CN 105523186B
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- thermojet
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- ice
- frost
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- 230000015572 biosynthetic process Effects 0.000 title claims abstract description 42
- 238000003786 synthesis reaction Methods 0.000 title claims abstract description 42
- 230000002194 synthesizing effect Effects 0.000 claims abstract description 27
- 239000012528 membrane Substances 0.000 claims abstract description 8
- 239000000203 mixture Substances 0.000 claims abstract description 3
- 238000005485 electric heating Methods 0.000 claims description 13
- 239000011521 glass Substances 0.000 claims description 5
- 230000005611 electricity Effects 0.000 claims description 3
- 238000010257 thawing Methods 0.000 abstract description 9
- 238000005265 energy consumption Methods 0.000 abstract description 3
- 230000004044 response Effects 0.000 abstract description 3
- 238000010438 heat treatment Methods 0.000 abstract description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 10
- 238000010586 diagram Methods 0.000 description 9
- 239000007789 gas Substances 0.000 description 8
- 238000000034 method Methods 0.000 description 5
- 239000003595 mist Substances 0.000 description 5
- 238000009434 installation Methods 0.000 description 4
- 230000008569 process Effects 0.000 description 4
- 238000001035 drying Methods 0.000 description 3
- 230000005284 excitation Effects 0.000 description 3
- 238000004781 supercooling Methods 0.000 description 3
- 230000007423 decrease Effects 0.000 description 2
- 238000009792 diffusion process Methods 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 239000003292 glue Substances 0.000 description 2
- 238000002347 injection Methods 0.000 description 2
- 239000007924 injection Substances 0.000 description 2
- 239000000243 solution Substances 0.000 description 2
- 239000002918 waste heat Substances 0.000 description 2
- 206010009866 Cold sweat Diseases 0.000 description 1
- 235000014676 Phragmites communis Nutrition 0.000 description 1
- 206010037660 Pyrexia Diseases 0.000 description 1
- 238000007664 blowing Methods 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 238000004140 cleaning Methods 0.000 description 1
- 238000007791 dehumidification Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000001704 evaporation Methods 0.000 description 1
- 230000008020 evaporation Effects 0.000 description 1
- 239000000295 fuel oil Substances 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 239000003921 oil Substances 0.000 description 1
- 230000001737 promoting effect Effects 0.000 description 1
- 230000000644 propagated effect Effects 0.000 description 1
- 230000005855 radiation Effects 0.000 description 1
- 238000005057 refrigeration Methods 0.000 description 1
- 230000002195 synergetic effect Effects 0.000 description 1
- 230000009466 transformation Effects 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D15/00—De-icing or preventing icing on exterior surfaces of aircraft
- B64D15/02—De-icing or preventing icing on exterior surfaces of aircraft by ducted hot gas or liquid
- B64D15/04—Hot gas application
-
- A—HUMAN NECESSITIES
- A47—FURNITURE; DOMESTIC ARTICLES OR APPLIANCES; COFFEE MILLS; SPICE MILLS; SUCTION CLEANERS IN GENERAL
- A47G—HOUSEHOLD OR TABLE EQUIPMENT
- A47G25/00—Household implements used in connection with wearing apparel; Dress, hat or umbrella holders
- A47G25/14—Clothing hangers, e.g. suit hangers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60S—SERVICING, CLEANING, REPAIRING, SUPPORTING, LIFTING, OR MANOEUVRING OF VEHICLES, NOT OTHERWISE PROVIDED FOR
- B60S1/00—Cleaning of vehicles
- B60S1/02—Cleaning windscreens, windows or optical devices
- B60S1/54—Cleaning windscreens, windows or optical devices using gas, e.g. hot air
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60S—SERVICING, CLEANING, REPAIRING, SUPPORTING, LIFTING, OR MANOEUVRING OF VEHICLES, NOT OTHERWISE PROVIDED FOR
- B60S1/00—Cleaning of vehicles
- B60S1/02—Cleaning windscreens, windows or optical devices
- B60S1/56—Cleaning windscreens, windows or optical devices specially adapted for cleaning other parts or devices than front windows or windscreens
- B60S1/60—Cleaning windscreens, windows or optical devices specially adapted for cleaning other parts or devices than front windows or windscreens for signalling devices, e.g. reflectors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D15/00—De-icing or preventing icing on exterior surfaces of aircraft
- B64D15/12—De-icing or preventing icing on exterior surfaces of aircraft by electric heating
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Air-Conditioning For Vehicles (AREA)
Abstract
The invention belongs to fluidics field, it is related to a kind of for/the synthesis thermojet driver of frost/ice and the application of dehumidifying.The synthesis thermojet driver is made of synthesizing jet-flow excitor and heat source；The synthesizing jet-flow excitor is made of cavity, vibrating membrane and outlet, and the cavity offers one or more outlets；Portion in the cavity is arranged in the heat source.The present invention can be used alone, and can also be mounted on and need to be used by the inside composition array of heating equipment, be to increase heat generating device in existing driver inside cavity, the thermojet of fair speed be synthesized in exit, for dehumidifying, defrosting and deicing.The present invention have many advantages, such as without air source, it is simple and light, be swift in response, high efficiency, low energy consumption, can be used for the deicing such as middle-size and small-size aircraft, automobile, refrigerator defrosting, also can be used with the dehumidifying such as hand dryer, clothesdrier, shoe drier.
Description
Technical field
The invention belongs to fluidics field more particularly to it is a kind of for dehumidify/the synthesis thermojet driver of frost/ice and
Using.
Background technology
Icing is a kind of phenomenon being widely present in aircraft flight, and cause flight safety accident main hidden danger it
One.When aircraft flight under the conditions of subfreezing icing meteorology, the super-cooling waterdrop in air strikes aircraft surfaces, freezes
Phenomenon is just easy to occur in parts surfaces such as wing, empennage, rotor, air intake duct, windshield, antenna house, gauge sensors.
Aircraft, which freezes, not only increases the weight of aircraft, and destroys the aerodynamic configuration of aircraft surfaces, changes Flow Field, destroys
Aeroperformance causes aircraft maximum lift to decline, flight resistance rises, operating characteristics declines, stability reduces, primary rank
The accumulated ice of section can substantially reduce lift and increase resistance.Currently, the anti-deicing system on passenger plane, which includes mainly gas heat, prevents/deicing
Prevent/deicing two ways with electric heating.Both anti-/ deicing modes consume energy, and big, increase quality is big, is suitable for large aircraft.And it is right
It being difficult to adapt to if some middle-size and small-size aircraft such as unmanned plane, one side unmanned plane is easier to freeze and harm is more serious, nobody
Machine cabinet size is small, it is easier to which freeze (under the same terms, aircraft is smaller, easier icing), the opposite thickness that freezes of unit interval
Degree is big (the smaller anti-ice ability of aircraft is poorer), and the harm that the ice of same thickness generates aircraft is more serious；On the other hand, unmanned plane
Payload is small, and fuel oil carrying amount is limited, and the energy is most valuable on machine, and big energy cannot be consumed as large aircraft and is prevented and kill off
Ice.
Automobile front and rear windshield, rearview mirror generally existing fogging frosting problem, since vehicle internal-external temperature difference makes interior moisture
Mist or frost are formed to the cold and in inside glass, seriously affects traffic safety.At present automobile demisting mainly by air conditioner dehumidification come
Carry out demisting.Defrosting just needs to open warm wind, and radiating fin of hot air machine is flowed through by the water that engine comes, and starts fan, diffusion
The heat that engine comes.Defrosting process needs first hot vehicle, and engine water temperature is waited for rise, and opens warm-air drier defrosting later, compares
Take time and effort oil consumption.Sleety weather rearview mirror is easy attached water and drips mist, seriously affects traffic safety, generally passes through electric heating at present
Piece heats glass back and carries out demisting and evaporation water droplet, very time-consuming power-consuming.
In daily life, travelling and outdoor sports, generally existing dehumidifying, removes ice problem at defrosting, as frosting freezes in refrigerator
Refrigeration for refrigerator effect is caused to decline；The rainy water of winter-spring season, especially southern area, weather cool, damp, the clothing cleaned
Be not easy to dry, footgear it is moist；In travelling and outdoor sports, we usually also have such puzzlement：Clothes footgear cannot dry in the air in time
It is dry, tent and sleeping bag are clammy etc..
Invention content
It is a kind of for the/synthesis thermojet driver of frost/ice that dehumidifies to solve the problems, such as to provide in the prior art, there is nothing
Need air source, it is simple and light, be swift in response, high efficiency, low energy consumption and be easy to electrical parameter control jet stream is cold and hot and wind speed size
The advantages that.Specific technical solution is as follows：
It is a kind of for the/synthesis thermojet driver of frost/ice that dehumidifies, be made of synthesizing jet-flow excitor and heat source；It is described
Synthesizing jet-flow excitor is made of cavity, vibrating membrane and outlet, and the cavity offers one or more outlets；The heat source is set
Set portion in the cavity.
Further, the heat source is electric heating piece, is arranged on the cavity inner surface of synthesizing jet-flow excitor, is used for and chamber
Internal air contacts and propagates heat；
Further, fin is set on the electric heating piece, for increasing and air contact area in cavity and accelerated heat
It propagates.
Further, the heat source is resistance net or resistance wire, is set to inside cavity.
Further, the heat source replaces with external heat source, and heat is introduced to synthesizing jet-flow excitor by heat conduction pipeline
Inside cavity.
Further, the synthesizing jet-flow excitor is monofilm single-chamber synthesizing jet-flow excitor or monofilm two-chamber synthesizing jet-flow
Driver.
The present invention also provides a kind of for the/synthesis thermojet exciter array of frost/ice that dehumidifies, by several above-mentioned use
It is formed by array combination in the synthesis thermojet driver of dehumidifying/frost/ice.
The present invention also provides three kinds of application processes, respectively：By described for the/synthesis thermojet of frost/ice that dehumidifies
Driver is mounted at windshield or in rearview mirror, for removing mist or frost above windshield, or for blowing down
Water mist on rearview mirror and water droplet.By it is described for dehumidify/the synthesis thermojet exciter array of frost/ice is mounted on aircraft machine
On the wing, anti-/ deicing of aerofoil surface is realized.By it is described for dehumidify/the synthesis thermojet driver of frost/ice is mounted on the clothing that dries in the air
On frame, the drying for accelerating clothing footgear.Because of light and small of the present invention, portable, can be also used for being mounted on refrigerator inside, for removing
White deicing etc..
The present invention have without air source, it is simple and light, be swift in response, high efficiency, low energy consumption and be easy to electrical parameter control
The advantages that jet stream processed is cold and hot and wind speed is adjustable, specially：1. improving synthesizing jet-flow excitor, fever dress is increased inside it
It sets, makes it possible to injection thermojet；2. synthesizing jet-flow excitor in the prior art converts electrical energy into energy of the impinging jet, and synthesizes
Thermojet driver converts electric energy to jet stream thermal energy and kinetic energy, kinetic energy and thermal energy synergistic effect simultaneously, can substantially speed up heat
Diffusion is transported, the efficiency of dehumidifying, defrosting, deicing is greatly improved；3. it is that full electricity inputs to synthesize thermojet driver, it is easy to electricity
The temperature and intensity of state modulator jet stream, and it is not necessarily to air source and pipeline supply system, it is simple in structure light and handy, it can be designed as being convenient for
Modular array formula that is portable portable and being easily integrated installation；4. the present invention can be applicable to daily dehumidifying, defrost, remove
Ice and the dehumidifying of windshield and rearview mirror, defrosting, array synthesis thermojet driver can be applicable to middle-size and small-size flight
The anti-deicing of device.
Description of the drawings
Fig. 1 is the synthesis thermojet exciter structure schematic diagram that heat source of the present invention is electric heating piece；
Fig. 2 is the synthesis thermojet exciter structure schematic diagram that heat source of the present invention is resistance net；
Fig. 3 is the synthesis thermojet exciter structure schematic diagram that heat source of the present invention is external heat source；
Fig. 4 is stereochemical structure diagrammatic cross-section of the present invention；
Fig. 5 is the synthesis thermojet exciter array structural schematic diagram of the present invention；
Fig. 6 is the integral installation structural schematic diagram of the invention applied in the anti-deicing of wing；
Each label indicates in figure：
1, thermojet driver is synthesized；11, synthesizing jet-flow excitor；111, the first cavity；112, the second cavity；113, it shakes
Dynamic film；114, the first cavity outlet；115, the second cavity outlet；116, thermojet is synthesized；12, heat source；121, electric heating piece；122、
Fin；123, resistance net；124, heat conduction and heat radiation pipeline；125, external heat source；2, wing；3, incoming；4, the virtual aerodynamic configuration of hot gas.
Specific implementation mode
In the following, the invention will be further described with reference to the drawings and specific embodiments.
As shown in Figure 1, for the synthesis thermojet exciter structure schematic diagram that heat source of the present invention is electric heating piece；By synthesizing jet-flow
Driver 11 is formed with heat source 12；The synthesizing jet-flow excitor is made of cavity, vibrating membrane and outlet, and the cavity offers
One or more outlet；Portion in the cavity is arranged in the heat source.In Fig. 1, the synthesizing jet-flow excitor synthesizes for monofilm two-chamber
Jet-flow excitor, concrete structure include the first cavity 111, the second cavity 112, vibrating membrane 113, the first cavity 111 and the second chamber
It is separated by vibrating membrane between body 112, it is right that the correspondence of the first cavity 111 opens up the first cavity outlet 114, the second cavity 112
It should start the second cavity outlet 115.Electric heating piece 121 is by adiabatic glue in synthesizing jet-flow excitor inner surface to gas in cavity
Body is heated.Further, on the electric heating piece 121 can by heat conduction glue fin 122, for increase with it is empty in cavity
Gas contact area accelerated heat is propagated.First cavity outlet, 114 and second cavity outlet 115 can be it is single or multiple,
Outlet shapes are hole or seam；The arrow of 113 left and right sides of vibrating membrane indicates vibration processes back and forth in figure.
When power supply outside synthesis thermojet driver connection is worked, electric heating piece is powered, and synthesizes thermojet
Driver injection synthesis thermojet carries out the/frost/ice that dehumidifies.Thermojet driver will be synthesized shown in Fig. 1 to keep off in automobile
Antifogging defrosts before wind glass, and the fair speed thermojet that casket is blown out in automobile rearview mirror can directly be blown down rapidly
Water droplet water mist on rearview mirror is placed on fixed position in refrigerator and carries out quick deicing defrosting cleaning, installation to icing frosting position
It is used for Quick clothes drying on clothes hanger, or is placed in shoes and is used for fast quick-drying shoes.
Fig. 2 is the synthesis thermojet exciter structure schematic diagram that heat source of the present invention is resistance net；It is heated by resistance net 123
Portion in the cavity is arranged in driver intracavity gas, resistance net, can be by carrying out contact fixation with cavity wall and cavity bottom.
Fig. 3 is the synthesis thermojet exciter structure schematic diagram that heat source of the present invention is external heat source；External heat source can in embodiment
Using the waste heat of automobile engine or aircraft engine, waste heat to be introduced to the chamber of synthesizing jet-flow excitor by heat conduction pipeline
Fin is arranged on conduit within the cavity in internal portion, for increasing and air contact area in cavity and accelerated heat biography
It broadcasts.
Fig. 4 is stereochemical structure diagrammatic cross-section of the present invention；Wherein, Fig. 4 (a) figures indicate that heat source is that the synthesis heat of electric heating piece is penetrated
Flow driver；Fig. 4 (b) indicates that heat source is the synthesis thermojet driver of resistance net.
As shown in figure 5, the present invention also provides a kind of for the/synthesis thermojet exciter array of frost/ice that dehumidifies, if by
Dry it is above-mentioned for dehumidify/the synthesis thermojet driver of frost/ice formed by array combination.The array synthesis heat of the present invention
Jet-flow excitor array can it is transversely arranged can also longitudinal arrangement or two ways Common arrangements combination.
As shown in fig. 6, the present invention applies the integral installation structural schematic diagram in the anti-deicing of wing.For/frost/the ice that dehumidifies
Synthesis thermojet exciter array is embedded in inside wing 2, and thermojet driver is each synthesized in array combination by monofilm two-chamber
Synthesizing jet-flow excitor and heat source composition；The outlet of the synthesis thermojet driver and 2 flush with outer surface of wing.Specifically anti-/
De-icing work principle is：Synthesis thermojet driver in array is embedded in wing, and driver outlet is concordant with aerofoil surface
Not changing aerofoil surface shape, electric heating piece operational heat heats driver chamber air, meanwhile, vibrating reed is in periodical telecommunications
Number excitation under vibrate, driver export (i.e. aerofoil surface) integrated array thermojet, to realize prevent/removing for aerofoil surface
Ice.
It, can the one or more groups of synthesis thermojets excitations of arrangement in wing 2 according to actual conditions in specific implementation process
Device array；When synthesizing the work of thermojet exciter array, array thermojet 116 is ejected；Generated array thermojet exists
Aerofoil surface forms the virtual aerodynamic configuration 4 of hot gas, can dispel or evaporate the super-cooling waterdrop in incoming 3, prevent and reduce supercooling
Water droplet freezes on 2 surface of wing；If 2 surface of wing has frozen, thermojet is ejected in synthesis thermojet exciter array work
116, to wing 2 into the hot deicing of promoting the circulation of qi.Thermojet exciter array is synthesized while carrying out 2 anti-deicing of wing, to boundary-layer
It injects high momentum gas and sucks low-momentum gas, the aerodynamic characteristics of wing 2 can be improved.
The present invention synthesizes the jet stream of thermojet driver synthesis, can control excitation of the present invention by controlling heat source switch
Device works, and realizes that jet stream is cold and hot and the adjusting of temperature by controlling heating power, can also pass through and control vibrating membrane electrical parameter tune
Save the wind speed and frequency of thermojet.
The above is only the present embodiment, not does any restrictions to the present invention, every substantially right according to the technology of the present invention
Synthesizing jet-flow excitor (is such as replaced with other to penetrate by any modification, change and equivalent structure transformation made by above example
Stream actuator) either applied in any dehumidifying/frost/ice field using other array patterns or by synthesis thermojet driver
Still fall within the protection domain of the method for the present invention technical solution.
Claims (7)
1. a kind of for the/synthesis thermojet driver of frost/ice that dehumidifies, it is characterised in that：By synthesizing jet-flow excitor and heat source
Composition；The synthesizing jet-flow excitor is made of cavity, vibrating membrane and outlet, and the cavity offers one or more outlets；
Portion in the cavity is arranged in the heat source；The synthesizing jet-flow excitor is mounted on unmanned plane wing or is mounted on automotive windshield glass
Before glass or in automotive rear-view dressing case or on clothes hanger.
2. as described in claim 1 a kind of for the/synthesis thermojet driver of frost/ice that dehumidifies, it is characterised in that：The heat
Source is electric heating piece, is arranged on synthesizing jet-flow excitor cavity inner surface.
3. as claimed in claim 2 a kind of for the/synthesis thermojet driver of frost/ice that dehumidifies, it is characterised in that：The electricity
Fin is provided on backing.
4. as described in claim 1 a kind of for the/synthesis thermojet driver of frost/ice that dehumidifies, it is characterised in that：The heat
Source is resistance net or resistance wire, is set to inside cavity.
5. as described in claim 1 a kind of for the/synthesis thermojet driver of frost/ice that dehumidifies, it is characterised in that：The heat
Source replaces with external heat source, and heat is introduced to the inside cavity of synthesizing jet-flow excitor by heat conduction pipeline.
6. as described in claim 1 a kind of for the/synthesis thermojet driver of frost/ice that dehumidifies, it is characterised in that：The conjunction
It is monofilm single-chamber synthesizing jet-flow excitor or monofilm two-chamber synthesizing jet-flow excitor at jet-flow excitor.
7. a kind of for the/synthesis thermojet exciter array of frost/ice that dehumidifies, which is characterized in that by several such as claim 1
It is described for dehumidify/the synthesis thermojet driver of frost/ice formed by array combination.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510920386.2A CN105523186B (en) | 2015-12-11 | 2015-12-11 | It is a kind of for/the synthesis thermojet driver of frost/ice and the application of dehumidifying |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510920386.2A CN105523186B (en) | 2015-12-11 | 2015-12-11 | It is a kind of for/the synthesis thermojet driver of frost/ice and the application of dehumidifying |
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| Publication Number | Publication Date |
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| CN105523186A CN105523186A (en) | 2016-04-27 |
| CN105523186B true CN105523186B (en) | 2018-08-14 |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| CN106072994B (en) * | 2016-07-28 | 2018-01-05 | 中国计量大学 | A kind of heat-radiated shoes |
| CN110043369A (en) * | 2019-04-10 | 2019-07-23 | 南京航空航天大学 | A kind of aero-engine anti-icing equipment using synthesizing jet-flow auxiliary continuity jet stream |
| CN110834734A (en) * | 2019-11-14 | 2020-02-25 | 中国人民解放军63831部队 | Deicing system is prevented to wing |
| CN115038637A (en) * | 2019-12-29 | 2022-09-09 | 阿克塔塞斯有限公司 | Controlling temperature using an active flow control actuator |
| CN111688892B (en) * | 2020-06-23 | 2021-05-18 | 西北工业大学 | Active flow control system for wing body fusion underwater glider |
Family Cites Families (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0680878B1 (en) * | 1994-04-13 | 1999-12-22 | The B.F. Goodrich Company | Electrothermal deicing system |
| KR100707211B1 (en) * | 2006-02-03 | 2007-04-13 | 삼성전자주식회사 | Synthetic jet actuator |
| GB2453769B (en) * | 2007-10-18 | 2012-09-05 | Gkn Aerospace Services Ltd | An aircraft leading edge thermoplastic heating mat |
| JP2011183922A (en) * | 2010-03-08 | 2011-09-22 | Mitsubishi Heavy Ind Ltd | Anti-icing and deicing device at wing leading edge part in aircraft and main wing of aircraft |
| EP3060778B1 (en) * | 2013-10-25 | 2019-03-20 | Short Brothers Plc | Anti-icing system for an aircraft |
| CN104168743A (en) * | 2014-07-10 | 2014-11-26 | 中国人民解放军国防科学技术大学 | Vector synthesis dual-jet exciter-based electronic element and heat radiation method thereof |
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