CN110374749A - A kind of consumption reduction speed-raising reduction infrared radiation device for jet engine - Google Patents
A kind of consumption reduction speed-raising reduction infrared radiation device for jet engine Download PDFInfo
- Publication number
- CN110374749A CN110374749A CN201910737668.7A CN201910737668A CN110374749A CN 110374749 A CN110374749 A CN 110374749A CN 201910737668 A CN201910737668 A CN 201910737668A CN 110374749 A CN110374749 A CN 110374749A
- Authority
- CN
- China
- Prior art keywords
- jet engine
- raising
- reduction
- speed
- infrared radiation
- 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.)
- Pending
Links
- 230000005855 radiation Effects 0.000 title claims abstract description 8
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims abstract description 20
- 238000002485 combustion reaction Methods 0.000 claims description 4
- 230000002708 enhancing effect Effects 0.000 abstract description 2
- 239000007921 spray Substances 0.000 description 4
- 238000004519 manufacturing process Methods 0.000 description 3
- 239000000567 combustion gas Substances 0.000 description 2
- 239000007789 gas Substances 0.000 description 2
- 239000003921 oil Substances 0.000 description 2
- 238000009834 vaporization Methods 0.000 description 2
- 230000008016 vaporization Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 239000003595 mist Substances 0.000 description 1
- 239000010705 motor oil Substances 0.000 description 1
- 238000005507 spraying Methods 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/08—Cooling; Heating; Heat-insulation
- F01D25/12—Cooling
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/12—Cooling of plants
- F02C7/16—Cooling of plants characterised by cooling medium
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Control Of Turbines (AREA)
Abstract
The present invention provides a kind of consumption reduction speed-raising reduction infrared radiation device for jet engine, and device includes water tank strainer, low-pressure pump, high-pressure hydraulic pump, injector nozzle temperature sensor.The present invention provide consumption reduction speed enhancing apparatus make aircraft faster, oil consumption is lower, thrust is bigger, reduces infra-red radiation, the temperature on turbo blade is lower.
Description
Technical field
The invention belongs to the speed-raising of jet engine consumption reduction, reduction Turbine Blade Temperature Field, the technical fields for reducing infra-red radiation.
More particularly to a kind of consumption reduction speed enhancing apparatus for jet engine.
Background technique
Because present jet engine thrust is small, speed is slow, oil consumption is high and turbo blade manufacture difficulty is big, and turbine leaf
Piece, which does not require nothing more than, wants high temperature resistant, also wants intensity height.
Summary of the invention
For the problem that jet engine thrust in the prior art is small, speed is slow, the high turbo blade manufacture difficulty of oil consumption is big,
The present invention is for the speed-raising of jet engine, increase thrust, consumption reduction, the device for reducing Turbine Blade Temperature Field.
In order to achieve the above object, technical solution of the present invention is as follows:
A kind of device radiated for the consumption reduction of jet engine, speed-raising, increase thrust, reduction Turbine Blade Temperature Field, drop.Packet
It includes: water tank, strainer, low-pressure pump, high-pressure hydraulic pump, nozzle, temperature sensor.
Further, after engine start, water spout is both to spraying water before turbo blade behind combustion chamber.Water vapour at high temperature
Change, with thousands of times of volume expansions, pushes turbine rotation, and spray backward with high-voltage high-speed, combustion gas is also reduced after water vapor
Temperature reduces the temperature on turbo blade, and the water that the spout after turbine sprays vaporizes at high temperature, makes to spray gas velocity more
Height, infra-red radiation are lower.
Further described, when temperature height to certain temperature, high temperature signal is passed to computer, computer instruction by temperature sensor
High-pressure hydraulic pump increases water.
The utility model has the advantages that the present invention provides consumption reduction, speed-raising, the device for reducing Turbine Blade Temperature Field, make jet engine oil consumption
It is lower, speed faster, thrust it is bigger, Turbine Blade Temperature Field is lower, reduces manufacture difficulty, keeps infra-red radiation lower.
Detailed description of the invention
Fig. 1 is the structural diagram of the present invention.
In figure, 1- water tank, 2- strainer, 3- low-pressure pump, 4- high-pressure hydraulic pump, 5a, 5b- water spout, 6- temperature sensor, 7-
Compressor, the combustion chamber 8-, 9- turbine.
Specific embodiment
The present invention is described below with reference to specific embodiments.It will be appreciated by those skilled in the art that these embodiments are only
For illustrating the present invention, do not limit the scope of the invention in any way.
A kind of device reducing Turbine Blade Temperature Field for the consumption reduction speed-raising of jet engine.As shown, including water tank
1 strainer, 2 low-pressure pump, 3 high-pressure hydraulic pump, 4 water spout 5a is behind combustion chamber 8 before turbine 9, after the engine is started up
Water mist is sprayed into, at high temperature rapid vaporization, so that rapid spatial expansion is pushed turbine rotation, and spray backward with high-voltage high-speed, water
The temperature of combustion gas is also reduced after vaporization, reduces the temperature on turbo blade.When temperature height to certain temperature, temperature sensor
High temperature signal is passed to computer by 6, increases water by computer instruction water pump, after turbo blade, the water of ejection exists water spout 5b
It is vaporized under high temperature, keeps the temperature of nozzle lower, pressure is higher, makes the infrared special speed for demonstrate,proving lower gas ejection faster.
Claims (1)
1. a kind of for the consumption reduction speed-raising of jet engine, reduction Turbine Blade Temperature Field and reduction infrared radiation device；Its feature
It include: water tank, strainer low-pressure pump, high-pressure hydraulic pump, nozzle, temperature sensor；Water spout behind combustion chamber, before turbo blade and
Position after blade.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910737668.7A CN110374749A (en) | 2019-08-12 | 2019-08-12 | A kind of consumption reduction speed-raising reduction infrared radiation device for jet engine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910737668.7A CN110374749A (en) | 2019-08-12 | 2019-08-12 | A kind of consumption reduction speed-raising reduction infrared radiation device for jet engine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN110374749A true CN110374749A (en) | 2019-10-25 |
Family
ID=68258814
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910737668.7A Pending CN110374749A (en) | 2019-08-12 | 2019-08-12 | A kind of consumption reduction speed-raising reduction infrared radiation device for jet engine |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN110374749A (en) |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1623031A (en) * | 2002-01-25 | 2005-06-01 | 阿尔斯通技术有限公司 | Method for operating a turbine group |
| CN101078367A (en) * | 2007-07-04 | 2007-11-28 | 中国船舶重工集团公司第七○三研究所 | Method for increasing PG 6531 combustion turbine power |
| CN101144431A (en) * | 2006-09-11 | 2008-03-19 | 燃气涡轮机效率公司 | Systems and methods for increasing turbine power output |
| CN102900528A (en) * | 2012-11-06 | 2013-01-30 | 通化师范学院 | Self power consumption reduction method of double-working-medium combined cycle turbine |
| CN104712431A (en) * | 2014-11-30 | 2015-06-17 | 李启山 | High-pressure flame water-cooling gasification supercharging turbine engine |
| CN107725192A (en) * | 2017-10-18 | 2018-02-23 | 福建亿谷新能源有限公司 | New energy turbogenerator |
| CN108397291A (en) * | 2017-02-06 | 2018-08-14 | 三菱日立电力系统株式会社 | Utilize moisture gas turbine |
-
2019
- 2019-08-12 CN CN201910737668.7A patent/CN110374749A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1623031A (en) * | 2002-01-25 | 2005-06-01 | 阿尔斯通技术有限公司 | Method for operating a turbine group |
| CN101144431A (en) * | 2006-09-11 | 2008-03-19 | 燃气涡轮机效率公司 | Systems and methods for increasing turbine power output |
| CN101078367A (en) * | 2007-07-04 | 2007-11-28 | 中国船舶重工集团公司第七○三研究所 | Method for increasing PG 6531 combustion turbine power |
| CN102900528A (en) * | 2012-11-06 | 2013-01-30 | 通化师范学院 | Self power consumption reduction method of double-working-medium combined cycle turbine |
| CN104712431A (en) * | 2014-11-30 | 2015-06-17 | 李启山 | High-pressure flame water-cooling gasification supercharging turbine engine |
| CN108397291A (en) * | 2017-02-06 | 2018-08-14 | 三菱日立电力系统株式会社 | Utilize moisture gas turbine |
| CN107725192A (en) * | 2017-10-18 | 2018-02-23 | 福建亿谷新能源有限公司 | New energy turbogenerator |
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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 | ||
| WD01 | Invention patent application deemed withdrawn after publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20191025 |