CN201241758Y - Small-sized gas turbine with air inlet and exhaust valves and free wheel - Google Patents
Small-sized gas turbine with air inlet and exhaust valves and free wheel Download PDFInfo
- Publication number
- CN201241758Y CN201241758Y CNU2008200997602U CN200820099760U CN201241758Y CN 201241758 Y CN201241758 Y CN 201241758Y CN U2008200997602 U CNU2008200997602 U CN U2008200997602U CN 200820099760 U CN200820099760 U CN 200820099760U CN 201241758 Y CN201241758 Y CN 201241758Y
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- valve
- welded
- spline
- central shaft
- gas turbine
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Abstract
A small gas turbine provided with intake and exhaust valves and a freewheel relates to the gas turbines, wherein a baffle (13) at the front end of a cylinder case (5) is welded with two parallel chutes (15), a valve (16) is mounted in the groove between the two chutes (15), two shoulders of the valve (16) abut against one end of a spring (14) which another end is welded on the plate of the valve (16), the top end of the valve (16) abuts against a cam (12) which is connected with a center shaft (10) via a spline, the cylinder case (5) is provided with an internal combustion chamber and an exhaust valve (17) at the back end, the plate of the exhaust valve (17) is provided with an exhaust port (7) connected with the center shaft (10) via a spline, a twisted single-stage energy-focused vane (8) is connected with the center shaft (10) via a spline, an output shaft (11) is welded with a twisted multistage energy-focused vane group (9), the internal screws of two inclined holes of the cylinder case (5) are respectively meshed with the external screws of a spark plug (18) and a nozzle (19). The small gas turbine has the advantages of simple structure, less friction among all components, low accident ratio and prolonged service life.
Description
One, technical field
The utility model relates to gas engine, especially a kind of small size gas turbine that has inlet and exhaust valve and freewheel.
Two, background technique
At present, the internal-combustion engine formed by bent axle, connecting rod, piston and cylinder of known vehicular engine structure.Fuel-air mixture is sucked cylinder internal, by spark plug it is lighted, explodes again, the impact force of generation promotes piston, thereby through two or four external output mechanical energies of operation cycle that working procedure forms.This process can change mechanical energy into interior, and this principle just begins to use from Steam Engine Age.But there are some inherent defects in it: (1) complex structure, and it is serious, easy to wear to rub between each parts, the rate of fault height, working life is short.(2) utilization ratio to fuel is low.(3) weight and volume is bigger.(4) can not automatic speed-changing and torque-converting, need install gearbox additional.(5) incombustible pluralities of fuel, bad adaptability.
Three, summary of the invention
In order to improve the above shortcoming of existing internal-combustion piston engine, the purpose of this utility model provides a kind of small size gas turbine that has inlet and exhaust valve and freewheel.
The technological scheme that the purpose of this utility model adopted is, include magneto casing and be welded with the supercharging blade, be connected with spline between central shaft and the mixed flow fan, magneto casing and mixed flow fan are welded to connect, after central shaft passes the cylinder case axis, be connected with spline between the single-stage cumulative blade, the central shaft outer shaft sleeve has output shaft, be welded with parallel groove on the dividing plate plate of its cylinder casing front end, in the groove valve is housed between two chutes, there is spring one end on valve two shoulder tops, the spring the other end is welded on the stigmal plate, and the valve top heads on cam, and spline is connected between cam and the central shaft, combuster in the cylinder casing shell, there is exhaust valve the rear end, on the exhaust door-plate relief opening is arranged, be connected with the central shaft spline, the single-stage cumulative blade of distortion is connected with the central shaft spline, be welded with the multistage cumulative vane group of distortion on the output shaft axle, cylinder casing two inclined hole internal threads respectively with the spark plug outside thread, the engagement of oil nozzle outside thread.
The utility model, it is indoor that ignition section of spark plug inserts the firing chamber.
The utility model, it is indoor that the oil nozzle ejiction opening inserts the firing chamber.
Working procedure of the present utility model, the rotation of mixed flow fan and supercharging blade, play water conservancy diversion and pressurized air effect, make air enter the firing chamber from suction port, spray bar sprays into fuel oil detonation under the plug ignition effect, and detonation gas is gone out from relief opening, goes out gas and promotes single-stage cumulative blade and the rotation of multistage cumulative vane group, thereby single-stage cumulative blade drives the mixed flow fan rotation, and multistage cumulative vane group drives the output shaft rotation.
The utility model: (1) has simple in structure, and friction is lacked between each parts, and the advantage that rate of fault is low can increase the service life greatly; (2), can reach 2-3 times of ordinary internal combustion engine to the utilization ratio height of fuel; (3) can realize automatic speed-changing and torque-converting, not need gearbox, thereby greatly reduce weight and volume; (4) incendivity pluralities of fuel is as gasoline, kerosene, diesel oil, alcohol, combustion gas etc.; (5) production technology is simple.
Four, description of drawings
Further specify the utility model below in conjunction with embodiment.
Fig. 1 is the utility model sectional structure schematic representation;
Fig. 2 is that Fig. 1 D-D is to the TV structure schematic representation;
Fig. 3 is that Figure 1A-A is to the TV structure schematic representation;
Fig. 4 is that Fig. 1 C-C is to the TV structure schematic representation;
Fig. 5 is that Figure 1B-B is to the TV structure schematic representation.
Among the figure: the multistage cumulative vane group of 1-mixed flow fan 2-supercharging blade 3-suction port 4-magnetogenerator 5-cylinder casing 6-firing chamber 7-relief opening 8-single-stage cumulative blade 9-10-central shaft 11-output shaft 12-cam 13-dividing plate 14-spring 15-chute 16-valve 17-exhaust valve 18-spark plug 19-oil nozzle
Five, embodiment
As Fig. 1, Fig. 2, Fig. 3, Fig. 4, shown in Figure 5, include magnetogenerator 4 shells and be welded with supercharging blade 2, be connected with spline between central shaft 10 and the mixed flow fan 1, magnetogenerator 4 shells and mixed flow fan 1 are welded to connect, after central shaft 10 passes cylinder casing 5 axle center, be connected with spline between the single-stage cumulative blade 8, central shaft 10 outer shaft sleeves have output shaft 11, be welded with parallel groove 15 on dividing plate 13 plates of its cylinder casing 5 front ends, in the groove valve 16 is housed between two chutes 15, there are spring 14 1 ends on 16 liang of shoulder tops of valve, spring 14 the other ends are welded on valve 16 plates, valve 16 tops head on cam 12, spline is connected between cam 12 and the central shaft 10, combuster 6 in cylinder casing 5 shells, there is exhaust valve 17 rear end, on exhaust valve 17 plates relief opening 7 is arranged, be connected with central shaft 10 splines, the single-stage cumulative blade 8 of distortion is connected with central shaft 10 splines, be welded with the multistage cumulative vane group 9 of distortion on 11 of the output shafts, 5 liang of inclined hole internal threads of cylinder casing respectively with spark plug 18 outside threads, the engagement of oil nozzle 19 outside threads.It is indoor that ignition section of spark plug 18 inserts firing chamber 6.It is indoor that oil nozzle 19 ejiction openings insert firing chamber 6.
Cylinder casing 5 shells have thermal-protective coating outward.
Claims (3)
1, a kind of small size gas turbine that has inlet and exhaust valve and freewheel, include magnetogenerator (4) shell and be welded with supercharging blade (2), be connected with spline between central shaft (10) and the mixed flow fan (1), magnetogenerator (4) shell and mixed flow fan (1) are welded to connect, after central shaft (10) passes cylinder casing (5) axle center, be connected with spline between the single-stage cumulative blade (8), central shaft (10) outer shaft sleeve has output shaft (11), it is characterized in that being welded with parallel groove (15) on dividing plate (13) plate of cylinder casing (5) front end, valve (16) is housed in the groove between two chutes (15), there are spring (14) one ends on valve (16) two shoulder tops, spring (14) the other end is welded on valve (16) plate, valve (16) top heads on cam (12), spline is connected between cam (12) and the central shaft (10), combuster (6) in cylinder casing (5) shell, there is exhaust valve (17) rear end, on exhaust valve (17) plate relief opening (7) is arranged, be connected with central shaft (10) spline, the single-stage cumulative blade (8) of distortion is connected with central shaft (10) spline, be welded with the multistage cumulative vane group (9) of distortion on output shaft (11) axle, cylinder casing (5) two inclined hole internal threads respectively with spark plug (18) outside thread, the engagement of oil nozzle (19) outside thread.
2, a kind of small size gas turbine that has inlet and exhaust valve and freewheel according to claim 1 is characterized in that ignition section insertion firing chamber (6) of spark plug (18) is indoor.
3, a kind of small size gas turbine that has inlet and exhaust valve and freewheel according to claim 1 is characterized in that oil nozzle (19) ejiction opening insertion firing chamber (6) is indoor.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CNU2008200997602U CN201241758Y (en) | 2008-08-21 | 2008-08-21 | Small-sized gas turbine with air inlet and exhaust valves and free wheel |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CNU2008200997602U CN201241758Y (en) | 2008-08-21 | 2008-08-21 | Small-sized gas turbine with air inlet and exhaust valves and free wheel |
Publications (1)
Publication Number | Publication Date |
---|---|
CN201241758Y true CN201241758Y (en) | 2009-05-20 |
Family
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Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CNU2008200997602U Expired - Fee Related CN201241758Y (en) | 2008-08-21 | 2008-08-21 | Small-sized gas turbine with air inlet and exhaust valves and free wheel |
Country Status (1)
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CN (1) | CN201241758Y (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102695918A (en) * | 2009-12-16 | 2012-09-26 | 斯奈克玛 | Guiding of a spark plug into a turbine engine combustion chamber |
CN105736409A (en) * | 2015-11-30 | 2016-07-06 | 王庆昌 | Supercharging assembly of water-driven no-power exhaust fan |
CN111503659A (en) * | 2020-04-28 | 2020-08-07 | 中国航发湖南动力机械研究所 | Flame tube, micro turbojet engine and preparation process of flame tube |
-
2008
- 2008-08-21 CN CNU2008200997602U patent/CN201241758Y/en not_active Expired - Fee Related
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102695918A (en) * | 2009-12-16 | 2012-09-26 | 斯奈克玛 | Guiding of a spark plug into a turbine engine combustion chamber |
CN102695918B (en) * | 2009-12-16 | 2015-04-01 | 斯奈克玛 | Method for guiding of a spark plug into a turbine engine combustion chamber |
CN105736409A (en) * | 2015-11-30 | 2016-07-06 | 王庆昌 | Supercharging assembly of water-driven no-power exhaust fan |
CN111503659A (en) * | 2020-04-28 | 2020-08-07 | 中国航发湖南动力机械研究所 | Flame tube, micro turbojet engine and preparation process of flame tube |
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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: 20090520 Termination date: 20110821 |