CN103899447A - Ozone combustion-supporting device for aircraft engine - Google Patents
Ozone combustion-supporting device for aircraft engine Download PDFInfo
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- CN103899447A CN103899447A CN201210576504.9A CN201210576504A CN103899447A CN 103899447 A CN103899447 A CN 103899447A CN 201210576504 A CN201210576504 A CN 201210576504A CN 103899447 A CN103899447 A CN 103899447A
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- ozone
- voltage power
- engine
- aeroengine
- ozone generation
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/12—Improving ICE efficiencies
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- Oxygen, Ozone, And Oxides In General (AREA)
Abstract
The invention provides an ozone combustion-supporting device for an aircraft engine, and relates to an astronautical technology. A grille type ozone generator is connected with an air inlet of the engine, the grille type ozone generator is in a mesh shape and is formed by a plurality of grille plates which are arrayed in parallel at certain intervals, a plurality of grids are formed, and ozone generating pieces are arranged around the inner sides of each grid. An ozone generating piece electrode is arranged on the surface of each ozone generating piece, leads on all the ozone generating piece electrodes are in parallel connection and then are connected with a high-voltage power line, and the high-voltage power line is connected with a high-frequency and high-voltage power source. The ozone combustion-supporting device for the aircraft engine is simple in structure, safe and reliable in performance, and convenient to mount and maintain. An ozone technology is used in the turbine and turbine shaft aircraft engine, the grille type ozone generator is arranged on the air inlet of the engine, ozone gas generated during working of the ozone generator can improve the combustion efficiency of aircraft fuel, using of the aircraft fuel is saved, emission of waste pollution gas is reduced, and flight cost is lowered.
Description
Technical field
The present invention relates to a kind of space technology, particularly a kind of aeroengine ozone to support combustion device, is applicable to be provided with fighter plane and the helicopter of turbine and turbine shaft aeroengine.
Background technique
In recent years, along with the sharply variation of Energy situation, global energy safety problem is more and more subject to the extensive concern of international community.The energy is to support the important substance basis of socio-economic development, to realizing national economy and social sustainable development is significant.Current international and domestic Energy situation sternness, the fluctuation, the particularly rise of Aviation Fuel price of international, domestic oil price, increased flight cost of transportation.Along with China's fast increasing economy, the development potentiality of aircraft industry is huge.Aircraft industry is advancing under the overall situation of " conservation-minded society ", within the scope of safe operation, energy resource saving, implements flight in most economical mode, seems particularly important.Aeroengine is the motor that flight required drive is provided for aircraft.Fighter plane in Aero-Space and national defence industry and helicopter use at present turbine and turbine shaft aeroengine, be by drawing the oxygenant of air as fuel combustion, thereby make fighter plane and helicopter obtain the aeroengine of flying power.There is a certain distance in China with advanced country in the world in the development of aeroengine always, and domestic engine consumption is high, power is low, and the waste gas of discharge also has serious pollution to atmosphere.Therefore reducing oil consumption, increase power and reduce toxic emission, is to improve in design aeroengine constantly to pursue, and also has great strategic importance to strengthening national defense construction.In recent years, R&D institution and science and technology in enterprise personnel, in constantly research, exploration, utilized modern science and technology, although obtained technically some progress, still existed the technical barrier not yet overcoming in practice.
Summary of the invention
The object of the invention is to overcome above deficiency, a kind of aeroengine ozone to support combustion device is provided, ozone technology is applied in aeroengine, be mainly used in fighter plane and helicopter on turbine and turbine shaft aeroengine, set up a spacing grid type ozonizer at this aeroengine suction port place, when the ozone producing and fuel oil mixed combustion, oil inflame is obtained more abundant, further promote aeroengine oil inflame efficiency, save Aviation Fuel, reduce the discharge of waste gas, increased flying power.
The technical solution adopted for the present invention to solve the technical problems is: contain ozone generation flake, ozone generation flake electrode, lattice plate, spacing grid type ozonizer, engine intake, high-voltage power-line, high-frequency and high-voltage power supply, motor air outlet, motor is provided with engine intake and motor air outlet, spacing grid type ozonizer is connected with engine intake, spacing grid type ozonizer is netted, be arranged in parallel and form at a certain distance by several lattice plates, form several grids, inside each grid, surrounding is provided with ozone generation flake, each ozone generation flake surface is provided with ozone generation flake electrode, after wire parallel connection on each ozone generation flake electrode, be connected with high-voltage power-line, high-voltage power-line is connected with high-frequency and high-voltage power supply, form a kind of aeroengine ozone to support combustion device.
The technology used in the present invention principle is: in the time taking off, turbine and the work of turbine shaft aeroengine, high-frequency and high-voltage power supply carries out work simultaneously, and engine intake can suck large quantity of air, when air passes through spacing grid type ozonizer, under the driving of high-frequency and high-voltage power supply, ozone generation flake carries out coronal discharge, and the airborne oxygen being inhaled into is punctured by electrion, forms single oxygen atom, be combined with oxygen molecule around again, thereby produce a large amount of ozone gas.Ozone gas is inhaled into the firing chamber of motor, and ozone, except having extremely strong oxidability, also will bring out fuel oil and carry out chain reaction, promote the further burning of Aviation Fuel, oil inflame be obtained more abundant.In aviation flight, the utilization of this device can be saved fuel oil 10% left and right, increases flying power 10% left and right, and the discharge of harmful gas reduces more than 20%.In turbine and turbine shaft aeroengine, adopt ozone technology, spacing grid type ozonizer is arranged on to the suction port place of motor, rational in infrastructure, installation, easy to maintenance.
The invention has the beneficial effects as follows: this apparatus structure is simple, and performance safety is reliable installation and easy to maintenance.In turbine and turbine shaft aeroengine, adopt ozone technology, suction port place at motor arranges spacing grid type ozonizer, the ozone gas producing when its work, can promote the combustion efficiency of Aviation Fuel, save the use of Aviation Fuel, reduce the discharge of discarded dusty gas, reduce flight cost.
Brief description of the drawings
In conjunction with the accompanying drawings and embodiments the present invention to be further described below:
Fig. 1 is the local enlarged diagram of a kind of aeroengine ozone to support combustion device;
Fig. 2 is the left TV structure schematic diagram of a kind of aeroengine ozone to support combustion device.
In the drawings: 1. ozone generation flake, 2. ozone generation flake electrode, 3. lattice plate, 4. spacing grid type ozonizer, 5. engine intake, 6. high-voltage power-line, 7. high-frequency and high-voltage power supply, 8. motor air outlet.
Embodiment:
At Fig. 1, in Fig. 2: motor is provided with engine intake 5 and motor air outlet 8, spacing grid type ozonizer 4 is connected with engine intake 5, spacing grid type ozonizer 4 is netted, be arranged in parallel and form at a certain distance by several lattice plates 3, form several grids, inside each grid, surrounding is provided with ozone generation flake 1, each ozone generation flake 1 surface is provided with ozone generation flake electrode 2, after wire parallel connection on each ozone generation flake electrode 2, be connected with high-voltage power-line 6, high-voltage power-line 6 is connected with high-frequency and high-voltage power supply 7, form a kind of aeroengine ozone to support combustion device.
In the time taking off, turbine and the work of turbine shaft aeroengine, high-frequency and high-voltage power supply 7 carries out work simultaneously, and engine intake 5 can suck large quantity of air, when air passes through spacing grid type ozonizer 4, under the driving of high-frequency and high-voltage power supply 7, ozone generation flake 1 carries out coronal discharge, and the airborne oxygen being inhaled into is punctured by electrion, forms single oxygen atom, be combined with oxygen molecule around again, thereby produce a large amount of ozone gas.Ozone gas is inhaled into the firing chamber of motor, and ozone, except having extremely strong oxidability, also will bring out fuel oil and carry out chain reaction, promote the further burning of Aviation Fuel, oil inflame be obtained more abundant.In aviation flight, the utilization of this device can be saved fuel oil 10% left and right, increases flying power 10% left and right, and the discharge of harmful gas reduces more than 20%.In turbine and turbine shaft aeroengine, adopt ozone technology, spacing grid type ozonizer 4 is arranged on to engine intake 5 places, rational in infrastructure, installation, easy to maintenance.
Claims (1)
1. an aeroengine ozone to support combustion device, contain ozone generation flake, ozone generation flake electrode, lattice plate, spacing grid type ozonizer, engine intake, high-voltage power-line, high-frequency and high-voltage power supply, motor air outlet, it is characterized in that: motor is provided with engine intake and motor air outlet, spacing grid type ozonizer is connected with engine intake, spacing grid type ozonizer is netted, be arranged in parallel and form at a certain distance by several lattice plates, form several grids, inside each grid, surrounding is provided with ozone generation flake, each ozone generation flake surface is provided with ozone generation flake electrode, after wire parallel connection on each ozone generation flake electrode, be connected with high-voltage power-line, high-voltage power-line is connected with high-frequency and high-voltage power supply, form a kind of aeroengine ozone to support combustion device.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201210576504.9A CN103899447A (en) | 2012-12-27 | 2012-12-27 | Ozone combustion-supporting device for aircraft engine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201210576504.9A CN103899447A (en) | 2012-12-27 | 2012-12-27 | Ozone combustion-supporting device for aircraft engine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN103899447A true CN103899447A (en) | 2014-07-02 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201210576504.9A Pending CN103899447A (en) | 2012-12-27 | 2012-12-27 | Ozone combustion-supporting device for aircraft engine |
Country Status (1)
| Country | Link |
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| CN (1) | CN103899447A (en) |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5010869A (en) * | 1989-08-11 | 1991-04-30 | Zenion Industries, Inc. | Air ionization system for internal combustion engines |
| CN2709668Y (en) * | 2004-04-02 | 2005-07-13 | 王怡泰 | Engine air inlet aeration device |
| WO2010000909A1 (en) * | 2008-07-04 | 2010-01-07 | Hurtado Sarria Jose Juan | Device for improving the performance of an injection internal combustion engine |
| CN102128108A (en) * | 2011-05-05 | 2011-07-20 | 上海工程技术大学 | Circular multipoint ozone generation device for composite tungsten metal ceramics |
-
2012
- 2012-12-27 CN CN201210576504.9A patent/CN103899447A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5010869A (en) * | 1989-08-11 | 1991-04-30 | Zenion Industries, Inc. | Air ionization system for internal combustion engines |
| CN2709668Y (en) * | 2004-04-02 | 2005-07-13 | 王怡泰 | Engine air inlet aeration device |
| WO2010000909A1 (en) * | 2008-07-04 | 2010-01-07 | Hurtado Sarria Jose Juan | Device for improving the performance of an injection internal combustion engine |
| CN102128108A (en) * | 2011-05-05 | 2011-07-20 | 上海工程技术大学 | Circular multipoint ozone generation device for composite tungsten metal ceramics |
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Application publication date: 20140702 |