CN201354680Y - Dual-fuel energy-saving turbojet engine - Google Patents
Dual-fuel energy-saving turbojet engine Download PDFInfo
- Publication number
- CN201354680Y CN201354680Y CNU2009200991564U CN200920099156U CN201354680Y CN 201354680 Y CN201354680 Y CN 201354680Y CN U2009200991564 U CNU2009200991564 U CN U2009200991564U CN 200920099156 U CN200920099156 U CN 200920099156U CN 201354680 Y CN201354680 Y CN 201354680Y
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- combustion
- nozzle
- turbojet engine
- fuel
- saving
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Abstract
The utility model provides a dual-fuel energy-saving turbojet engine which consists of an air inlet channel, an external duct, an internal duct, a combustion chamber, a jet exhaust, a fan, a gas compressor, a turbine and combustion nozzles. The combustion nozzles are arranged in the combustion chamber, fixed on the annular wall of the internal duct and divided into oil nozzles and combustion-supporting nozzles which are arranged alternately and annularly. The dual-fuel energy-saving turbojet engine in the utility model can be used as an engine of the existing power plant and has the advantages of safety, reliability and long service life, effectively saves energy source and is environment-friendly.
Description
Technical field
The utility model belongs to motor, particularly relates to a kind of energy-saving double-fuel turbojet engine.
Background technique
At present in the world oil shortage, cause oil price to escalate, be the device of power with vapour, diesel oil, not only will consume a large amount of energy, and the environmental pollution damage that the discharging of tail gas causes is very big.Seek new alternative energy source and corresponding power plant, imperative.
Summary of the invention
The utility model is intended to overcome the deficiencies in the prior art, and a kind of energy-saving double-fuel turbojet engine of energy-saving and environmental protection is provided.
Energy-saving double-fuel turbojet engine of the present utility model, be to be made of intake duct, by-pass air duct, main duct, firing chamber, puff prot, fan, gas compressor, turbo machine and burning nozzle, the burning nozzle places the firing chamber in, be fixed on the ring wall of main duct and be divided into oil nozzle and combustion-supporting nozzle replaces annular array at interval.
As further improvement of the utility model, each oil nozzle all be surrounded on the main duct outer wall on fuel line be connected, the combustion-supporting pipeline that each combustion-supporting nozzle all is surrounded on the main duct outer wall is connected.
As further improvement of the utility model, fuel line and combustion-supporting pipeline all are surrounded on the outer wall of main duct side by side.
Fuel line of the present utility model is carried existing gasoline, diesel oil etc., and liquid such as combustion-supporting pipeline transporting water, synthetic liquid when ato unit, are opened oil nozzle to make motor carry out work; When engine start to the regular hour, close the fuel flow of half, open combustion-supporting nozzle; Make oil nozzle and combustion-supporting nozzle be ejected to the fuel chambers burning simultaneously, combustion-supporting nozzle ejection liquid produces great energy, because turbojet engine is raised to more than 3000 degree through the turbine compression temperature, this environment is fit to the hydrate fuel combustion condition, because water is more than 2500 ℃ the time, hydrogen-oxygen separates, so the meeting produce power can have been saved fuel oil effectively.
Energy-saving double-fuel turbojet engine of the present utility model can be used as the motor of existing power plant, has safe and reliable, long service life, advantage such as energy saving, environmental protection effectively.
Description of drawings
Fig. 1 is the structural representation of energy-saving double-fuel turbojet engine of the present utility model.
Fig. 2 is that the A-A of Fig. 1 is to sectional drawing.
Fig. 3 is oil nozzle and combustion-supporting nozzle and pipeline distribution planimetric map thereof.
Embodiment
Embodiment 1
Energy-saving double-fuel turbojet engine of the present utility model is to be made of intake duct 1, by-pass air duct 2, main duct 3, firing chamber 4, puff prot 5, fan 6, gas compressor 7, turbo machine 8 and burning nozzle 9.Burning nozzle 9 places in the firing chamber 4, be fixed on the ring wall of main duct 3 and be divided into oil nozzle 10 and combustion-supporting nozzle 11 annular array alternately at interval.
Energy-saving double-fuel turbojet engine of the present utility model is to be made of intake duct 1, by-pass air duct 2, main duct 3, firing chamber 4, puff prot 5, fan 6, gas compressor 7, turbo machine 8 and burning nozzle 9.Burning nozzle 9 places in the firing chamber 4, be fixed on the ring wall of main duct 3 and be divided into oil nozzle 10 and combustion-supporting nozzle 11 annular array alternately at interval, each oil nozzle 10 all be surrounded on main duct 3 outer walls on fuel line 12 be connected, the combustion-supporting pipeline 13 that each combustion-supporting nozzle 11 all is surrounded on main duct 3 outer walls is connected.
Energy-saving double-fuel turbojet engine of the present utility model is to be made of intake duct 1, by-pass air duct 2, main duct 3, firing chamber 4, puff prot 5, fan 6, gas compressor 7, turbo machine 8 and burning nozzle 9.Burning nozzle 9 places in the firing chamber 4, be fixed on the ring wall of main duct 3 and be divided into oil nozzle 10 and combustion-supporting nozzle 11 annular array alternately at interval, each oil nozzle 10 all be surrounded on main duct 3 outer walls on fuel line 12 be connected, the combustion-supporting pipeline 13 that each combustion-supporting nozzle 11 all is surrounded on main duct 3 outer walls is connected.Wherein, fuel line 12 and combustion-supporting pipeline 13 all are surrounded on the outer wall of main duct 3 side by side.
Claims (3)
1, energy-saving double-fuel turbojet engine, be to be made of intake duct (1), by-pass air duct (2), main duct (3), firing chamber (4), puff prot (5), fan (6), gas compressor (7), turbo machine (8) and burning nozzle (9), the nozzle (9) that it is characterized in that burning places in the firing chamber (4), be fixed on the ring wall of main duct (3) and be divided into oil nozzle (10) and combustion-supporting nozzle (11) replaces annular array at interval.
2, energy-saving double-fuel turbojet engine as claimed in claim 1, it is characterized in that each oil nozzle (10) all be surrounded on main duct (3) outer wall on fuel line (12) be connected, the combustion-supporting pipeline (13) that each combustion-supporting nozzle (11) all is surrounded on main duct (3) outer wall is connected.
3, energy-saving double-fuel turbojet engine as claimed in claim 2 is characterized in that fuel line (12) and combustion-supporting pipeline (13) all are surrounded on the outer wall of main duct (3) side by side.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU2009200991564U CN201354680Y (en) | 2009-02-24 | 2009-02-24 | Dual-fuel energy-saving turbojet engine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU2009200991564U CN201354680Y (en) | 2009-02-24 | 2009-02-24 | Dual-fuel energy-saving turbojet engine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201354680Y true CN201354680Y (en) | 2009-12-02 |
Family
ID=41411021
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNU2009200991564U Expired - Fee Related CN201354680Y (en) | 2009-02-24 | 2009-02-24 | Dual-fuel energy-saving turbojet engine |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN201354680Y (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2013117145A1 (en) * | 2012-02-10 | 2013-08-15 | Zhu Xiaoyi | Supercharging device and turbine engine |
-
2009
- 2009-02-24 CN CNU2009200991564U patent/CN201354680Y/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2013117145A1 (en) * | 2012-02-10 | 2013-08-15 | Zhu Xiaoyi | Supercharging device and turbine engine |
| US9835085B2 (en) | 2012-02-10 | 2017-12-05 | Xiaoyi Zhu | Fluid supercharging device and turbine engine |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20091202 Termination date: 20120224 |