CN108825384A - A kind of air-fuel mixture starter - Google Patents
A kind of air-fuel mixture starter Download PDFInfo
- Publication number
- CN108825384A CN108825384A CN201810981035.6A CN201810981035A CN108825384A CN 108825384 A CN108825384 A CN 108825384A CN 201810981035 A CN201810981035 A CN 201810981035A CN 108825384 A CN108825384 A CN 108825384A
- Authority
- CN
- China
- Prior art keywords
- working connection
- pipe
- oil
- distribution disk
- fuel distribution
- 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
-
- 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
- F02C7/26—Starting; Ignition
-
- 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
- F02C7/22—Fuel supply systems
-
- 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
- F02C7/22—Fuel supply systems
- F02C7/222—Fuel flow conduits, e.g. manifolds
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Ignition Installations For Internal Combustion Engines (AREA)
Abstract
The present invention relates to engine primer technical fields, and in particular to a kind of air-fuel mixture starter for Micro Turbine Jet Engine.Its main feature is that including working connection conduit and the gas conduct pipe being arranged on engine charge lid and diffuser, working connection conduit and gas conduct pipe are connected with fuel distribution disk, multiple working connection oil pipes and tracheae are provided on fuel distribution disk, working connection oil pipe and tracheae protrude into the indoor evaporation tube of burning, igniter head is mounted on combustion chamber end by fuel distribution disk correspondence, igniter head is connected by igniting oil pipe with igniting oil circuit conduit, the combustion chamber is mounted on air deflector, and air deflector is mounted on the collet on bearing holder (housing, cover).It uses both-initiated strategy mode, and engine prewarming is fast, and Acceleration of starting is fast；Stable and reliable in work using fuel oil igniter head, the service life is long；Simple and reliable for structure, extreme environment is adaptable.
Description
Technical field
The present invention relates to engine primer technical fields, and in particular to a kind of oil gas for Micro Turbine Jet Engine is mixed
Close starter.
Background technique
Because Micro Turbine Jet Engine voluntarily cannot be transferred to working condition by static, it is necessary to use external force turning crankshaft, Zhi Daoqu
Axis reaches engine and starts the necessary revolving speed that burns, and guarantees that the formation, compression and igniting of gaseous mixture can be gone on smoothly.Start
Machine claims the starting of engine by the static overall process for being transferred to working condition.A series of dresses needed for completing engine starting process
Set title engine starting gear.
Current almost all of automobile engine all uses electric starter motor to start.When on motor reel driving gear with
When ring tooth engagement on engine flywheel periphery, the electromagnetic torque that motor generates when rotating passes to engine by flywheel
Crankshaft makes engine start.Electric starter motor abbreviation starter., using battery as power supply, structure is simple and convenient to operate, rises for it
It is dynamic reliable rapidly.
China Patent No. " CN106882393A " discloses unmanned vehicle engine starter.The invention proposes unmanned planes
The head of unmanned plane, including engine spindle is arranged in engine starting gear, engine, and axle sleeve fixed plate is fixed at hair
The outer of motivation main shaft is put on, and starting motor is fixed in axle sleeve fixed plate, including motor and gear；Duplicate gear fixation is set
It sets in axle sleeve fixed plate, including bull wheel and steamboat, the bull wheel in duplicate gear is engaged with the gear in starting motor；Engine
Nested spiral positioning column, ratchet are nested on spiral positioning column, engage with the steamboat in duplicate gear on main shaft；Engine
Propeller hub is arranged in the end of main shaft, and propeller is arranged on propeller hub, and the entire ignition process duration is shorter and easy to use, energy consumption
It is less, it is a kind of fairly simple practical sparking mode, but equally only supports a kind of sparking mode.
Micro turbine engine Starting mode in the prior art is that combustion gas starting or fuel oil start, combustion gas Starting mode fire
Head workload is high, is easily damaged, and igniting has some setbacks when ambient wind velocity is very fast；Fuel oil Starting mode, preheating time is long, and starting is slow
Slowly, fuel slippage reduces under low temperature environment, and ignition failure rate is high.
Summary of the invention
It is a kind of for the non-contact of Micro Turbine Jet Engine it is an object of the invention to avoid the deficiencies in the prior art from providing
Formula electromagnetic clutch, to solve problems of the prior art.
To achieve the above object, the technical scheme adopted by the invention is as follows：A kind of air-fuel mixture starter, it is special
Point be include the working connection conduit and gas conduct pipe being arranged on engine charge lid and diffuser, working connection conduit and combustion gas are led
Pipe is connected with fuel distribution disk, multiple working connection oil pipes and tracheae is provided on fuel distribution disk, working connection oil pipe and tracheae are stretched
Enter and burn in indoor evaporation tube, igniter head is mounted on combustion chamber end by fuel distribution disk correspondence, and igniter head passes through igniting
Oil pipe is connected with igniting oil circuit conduit, and the combustion chamber is mounted on air deflector, and air deflector is mounted on heat-insulated on bearing holder (housing, cover)
It puts on.
The working connection conduit is connected by fuel distribution disk with multiple working connection oil pipes, and gas conduct pipe passes through fuel oil point
It is connected with disk with multiple tracheaes, is additionally provided with shell outside the combustion chamber.
The beneficial effects of the invention are as follows：A kind of air-fuel mixture starter, uses both-initiated strategy mode, starts
Machine preheating is fast, and Acceleration of starting is fast；Stable and reliable in work using fuel oil igniter head, the service life is long；It is simple and reliable for structure, extreme environment
Under it is adaptable.
Detailed description of the invention
Fig. 1 is structural schematic diagram of the invention；
Fig. 2 is igniting oil circuit conduit setting structure schematic diagram of the invention.
As shown in the figure：1. working connection conduit；2. intake cover；3. diffuser；4. fuel distribution disk；5. shell；6. tracheae；7.
Working connection oil pipe；8. combustion chamber；9. air deflector；10. collet；11. bearing holder (housing, cover)；12. igniter head；13. igniting oil pipe；14. combustion
Airway；15. oil circuit conduit of lighting a fire.
Specific embodiment
The principle and features of the present invention will be described below with reference to the accompanying drawings, and the given examples are served only to explain the present invention, and
It is non-to be used to limit the scope of the invention.
As illustrated in fig. 1 and 2, a kind of air-fuel mixture starter, its main feature is that including being arranged in engine charge
Working connection conduit 1 and gas conduct pipe 14 on lid 2 and diffuser 3, working connection conduit 1 and gas conduct pipe 14 and fuel distribution disk 4
It is connected, multiple working connection oil pipes 7 and tracheae 6 is provided on fuel distribution disk 4, working connection oil pipe 7 and tracheae 6 protrude into combustion chamber 8
In interior evaporation tube, igniter head 12 is mounted on 8 end of combustion chamber by the way that fuel distribution disk 4 is corresponding, and igniter head 12 passes through point kerosene
Pipe 13 is connected with igniting oil circuit conduit 15, and the combustion chamber 8 is mounted on air deflector 9, and air deflector 9 is mounted on bearing holder (housing, cover) 11
Collet 10 on.
The working connection conduit 1 is connected by fuel distribution disk 4 with multiple working connection oil pipes 7, and gas conduct pipe 14 passes through
Fuel distribution disk 4 is connected with multiple tracheaes 6, is additionally provided with shell 5 outside the combustion chamber 8.
A kind of air-fuel mixture starter can light combustion gas and fuel oil by igniter head 12 simultaneously, cause
Square combustion chambers burn.
The foregoing is merely presently preferred embodiments of the present invention, is not intended to limit the invention, it is all in spirit of the invention and
Within principle, any modification, equivalent replacement, improvement and so on be should all be included in the protection scope of the present invention.
Claims (2)
1. a kind of air-fuel mixture starter, it is characterized in that including that the working connection being arranged on engine charge lid and diffuser is led
Pipe and gas conduct pipe, working connection conduit and gas conduct pipe are connected with fuel distribution disk, and multiple main oil are provided on fuel distribution disk
Road binders pipe and tracheae, working connection oil pipe and tracheae protrude into the indoor evaporation tube of burning, and igniter head is corresponding by fuel distribution disk
It is mounted on combustion chamber end, igniter head is connected by igniting oil pipe with igniting oil circuit conduit, and the combustion chamber is mounted on water conservancy diversion
On device, air deflector is mounted on the collet on bearing holder (housing, cover).
2. a kind of air-fuel mixture starter as described in claim 1, which is characterized in that the working connection conduit passes through combustion
Oil distributing plate is connected with multiple working connection oil pipes, and gas conduct pipe is connected by fuel distribution disk with multiple tracheaes, the burning
Outdoor is additionally provided with shell.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810981035.6A CN108825384B (en) | 2018-08-27 | 2018-08-27 | Oil-gas mixing starting device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810981035.6A CN108825384B (en) | 2018-08-27 | 2018-08-27 | Oil-gas mixing starting device |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN108825384A true CN108825384A (en) | 2018-11-16 |
| CN108825384B CN108825384B (en) | 2023-10-20 |
Family
ID=64150798
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810981035.6A Active CN108825384B (en) | 2018-08-27 | 2018-08-27 | Oil-gas mixing starting device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108825384B (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110985215A (en) * | 2019-12-27 | 2020-04-10 | 西北工业大学 | Starting and launching integrated system for micro turbojet engine |
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| US5237812A (en) * | 1992-10-07 | 1993-08-24 | Westinghouse Electric Corp. | Auto-ignition system for premixed gas turbine combustors |
| US5511375A (en) * | 1994-09-12 | 1996-04-30 | General Electric Company | Dual fuel mixer for gas turbine combustor |
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| US2914918A (en) * | 1955-12-28 | 1959-12-01 | Poly Ind Inc | Gas turbine jet engine starter with serially-connected concentrically-arranged combustion chambers |
| US4288980A (en) * | 1979-06-20 | 1981-09-15 | Brown Boveri Turbomachinery, Inc. | Combustor for use with gas turbines |
| US5237812A (en) * | 1992-10-07 | 1993-08-24 | Westinghouse Electric Corp. | Auto-ignition system for premixed gas turbine combustors |
| US5511375A (en) * | 1994-09-12 | 1996-04-30 | General Electric Company | Dual fuel mixer for gas turbine combustor |
| CA2335019A1 (en) * | 1998-06-18 | 2000-01-06 | Abb Ab | A method for starting a combustion device |
| US20030019215A1 (en) * | 2001-03-16 | 2003-01-30 | Marcel Stalder | Method for igniting a thermal turbomachine |
| JP2004085123A (en) * | 2002-08-28 | 2004-03-18 | Toyota Central Res & Dev Lab Inc | Combustor for gas turbine |
| CA2504114A1 (en) * | 2004-04-20 | 2005-10-20 | Gustavo Francisco Labala | Turbine, particularly useful for small aircraft |
| US20100043444A1 (en) * | 2006-11-30 | 2010-02-25 | Rafael Advanced Defense Systems Ltd. | Starting turbine engines |
| CN101881238A (en) * | 2010-06-10 | 2010-11-10 | 西北工业大学 | Air-breathing pulse detonation engine and detonation method thereof |
| CN103161576A (en) * | 2011-12-12 | 2013-06-19 | 诺沃皮尼奥内有限公司 | Turning gear for gas turbine arrangements |
| CN104345273A (en) * | 2013-07-24 | 2015-02-11 | 中国国际航空股份有限公司 | Starter performance detection method and apparatus of airplane auxiliary power unit (APU) |
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| CN106762157A (en) * | 2016-12-27 | 2017-05-31 | 中国南方航空工业(集团)有限公司 | Big aircraft floor starting device |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110985215A (en) * | 2019-12-27 | 2020-04-10 | 西北工业大学 | Starting and launching integrated system for micro turbojet engine |
| CN110985215B (en) * | 2019-12-27 | 2024-05-24 | 西安觉天动力科技有限责任公司 | Integrated system for starting of micro turbojet engine |
Also Published As
| Publication number | Publication date |
|---|---|
| CN108825384B (en) | 2023-10-20 |
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| TA01 | Transfer of patent application right |
Effective date of registration: 20220527 Address after: 710075 1-9-291, floor 9, angel building, Chuangye coffee block, No. 9, Gaoxin Second Road, high tech Zone, Xi'an City, Shaanxi Province Applicant after: Xi'an juetian Power Technology Co.,Ltd. Address before: 710072 No. 127 Youyi West Road, Shaanxi, Xi'an Applicant before: Northwestern Polytechnical University |
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| GR01 | Patent grant |