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CN2373579Y - Reaction engine - Google Patents

Reaction engine Download PDF

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Publication number
CN2373579Y
CN2373579Y CN99216867.8U CN99216867U CN2373579Y CN 2373579 Y CN2373579 Y CN 2373579Y CN 99216867 U CN99216867 U CN 99216867U CN 2373579 Y CN2373579 Y CN 2373579Y
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end cap
right end
wheel
utility
model
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Expired - Fee Related
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CN99216867.8U
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Chinese (zh)
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张胜利
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Individual
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Individual
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    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/12Improving ICE efficiencies

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Abstract

本实用新型涉及一种反动式发动机,该发动机有一个固定轮座,其上设有左端盖及右端盖,传动轴通过轴承安装在左、右端盖上,传动轴的中部安装一个工作轮,该工作轮由内环、外环及导叶构成,内、外环之间装有多个燃烧室,右端盖上安装有一个固定式导风轮,该导风轮上设有多个辐流式导向叶片,该导风轮内缘上设有集气流道和气流出口,所述的固定轮座的内壁上设有多条反射槽,该反射槽通过右端盖的孔道与外界连通。

Figure 99216867

The utility model relates to a reaction engine. The engine has a fixed wheel seat, on which a left end cover and a right end cover are arranged, and a drive shaft is installed on the left and right end covers through bearings. A working wheel is installed in the middle of the drive shaft. The working wheel is composed of an inner ring, an outer ring and guide vanes. Multiple combustion chambers are installed between the inner and outer rings. A fixed wind guide wheel is installed on the right end cover. As for the guide blade, the inner edge of the wind deflector wheel is provided with an air-collecting channel and an air outlet, and the inner wall of the fixed wheel base is provided with a plurality of reflection grooves, and the reflection grooves communicate with the outside through the channel of the right end cover.

Figure 99216867

Description

Retroacting engine
The utility model relates to a kind of Retroacting engine, and this motor is to utilize cooling back-heating, punching press compression, the new work engine of isochoric combustion and jet reaction work done.
Motor is a kind of ordinary skill of extensive use, and after producing the steamer in modern age, all kinds have appearred in the needs along with science and technology development and productive life, the motor of various uses.Wherein the technology of vapour, diesel engine is gradually perfect, though gas turbine and rotary piston engine have just begun to promote, has also run on material, the thermal efficiency and service cycle and is difficult to the shortcoming that overcomes in a short time.Particularly the thermal efficiency of these several motors of widespread usage also can not surpass 50 percent now, and weight/power ratio also is difficult to drop to the level of air breathing engine.Though domestic and international vast researcher is attached great importance to this work, drop into great amount of manpower and material resources and captured this difficulty, also there is not Updated product to occur so far.
The purpose of this utility model is to propose a kind of thermal efficiency that makes to improve greatly, and weight/power ratio is near the Retroacting engine of air breathing engine.
The purpose of this utility model is realized by following technical proposals: a kind of Retroacting engine, a fixedly wheel seat is arranged, fixedly wheel seat is provided with left end cap and right end cap, left end cap is communicated with the relief opening of described compressor, described transmission shaft by Bearing Installation on a left side, on the right end cap, an active wheel is installed at the middle part of transmission shaft, this active wheel is by interior ring, outer shroud and stator constitute, in, a plurality of described firing chambers are housed between the outer shroud, on encircling in the suction port of this firing chamber is located at, exhaust nozzle is located on the outer shroud, a fixed inducer is installed on the described right end cap, this inducer is provided with a plurality of radial-flow guide vanes, this inducer inner edge is provided with gas collection runner and flow outlet, and in the zone of this flow outlet between 230 ° of-360 ° of angles, this air flow outlet is provided with oil nozzle and spark plug, the inwall in zone is provided with many reflection grooves between 180 ° of-360 ° of angles of described fixedly wheel seat, and this reflection groove is in communication with the outside by the duct of right end cap.
Figure 15 is a working principle schematic representation of the present utility model, working principle of the present utility model is: by compressor with the gas compression to 4 that sucks to 6 air pressure, gas enters the space outerpace of active wheel and firing chamber from left end cap, gas is accelerated when being moved into inducer backward under the effect of stator, the temperature of gas will be enhanced, also cooled off simultaneously active wheel and on the firing chamber, so this motor can be provided with special-purpose cooling system, the gas that enters inducer flows along fixing circulating direction, do entad to flow from the circumferential center of circle earlier, it is moving to remake diverted flow then, become clockwise direction at last and enter firing chamber on the active wheel from the inducer air flow outlet, rotation of working time counterclockwise rotation this moment, thereby compressed-air actuated flow direction is opposite with air inlet of combustion chamber moving direction, the exhaust nozzle of firing chamber is in closed position, therefore, pressurized air produces the punching type compression once more in the firing chamber, when active wheel moves forward in the process at 130 ° of angles, be full of pressurized gas in the firing chamber, the air inlet compression process finishes, when active wheel continues to move forward, the oil spout of oil nozzle elder generation, the spark plug post-ignition, gas rapid burning expansion in igniting back forms high-temperature high-pressure fuel gas, simultaneously the exhaust nozzle of the firing chamber on the active wheel is in the reflection groove position on the fixing wheel seat, and be in opening state, the energy of combustion gas in exhaust nozzle, change into kinetic energy with high velocity shock to reflection groove, active wheel produces running torque and externally exports mechanical work, waste gas after the expansion acting is discharged to atmosphere by the duct of right end cap, active wheel moves 20 ° of angles more forward and discharges all waste gases, and a thermodynamic cycle is finished.
Compared with the prior art the utility model has following advantage:
1, be rotary component owing to the utility model has only an active wheel in whole conversion process of energy, its cooling is the pressurized air that does work by not, so the energy of mechanical friction and cooling loss reduces half than vapour, diesel engine.
2, again because firing chamber of the present utility model is that isochoric combustion does not need very high suction pressure, so the energy loss ratio gas turbine in compressor and exhaust also can reduce half.
3, simple structure of the present utility model can have 2 to 4 firing chambers to work at the same time on the active wheel, so its weight/power ratio can surpass gas turbine and approaching jet level of starting.
The utility model is described in further detail below in conjunction with drawings and Examples.
Fig. 1 is structural representation of the present utility model (sectional view)
Fig. 2 is structural representation of the present utility model (Figure 1A-A, B-B, C-C, a D-D sectional view)
Fig. 3 is a decomposing schematic representation of the present utility model
Fig. 4 is an active wheel schematic representation of the present utility model (sectional view)
Fig. 5 is an active wheel schematic representation of the present utility model (sectional view)
Fig. 6 is active wheel front view of the present utility model (Fig. 4 E is to view)
Fig. 7 is combustion chamber burner schematic representation of the present utility model (Fig. 4 F is to view)
Fig. 8 is air inlet of combustion chamber schematic representation of the present utility model (Fig. 4 G is to view)
Fig. 9 is a fixedly wheel seat schematic representation of the present utility model (half sectional view)
Figure 10 is fixedly wheel seat schematic representation of the present utility model (Fig. 9 N-N sectional view)
Figure 11 is a rear end cover schematic representation of the present utility model (sectional view)
Figure 12 is rear end cover schematic representation of the present utility model (Figure 11 M is to view)
Figure 13 is an inducer schematic representation of the present utility model (sectional view)
Figure 14 is inducer schematic representation of the present utility model (Figure 13 H is to view)
Figure 15 is a working principle schematic representation of the present utility model
Referring to Fig. 1-Figure 14, in Fig. 2, first quartile is the B-B sectional view, expression active wheel left side situation, second quadrant is the C-C sectional view, expression firing chamber working condition, third quadrant is the D-D sectional view, expression inducer working condition, four-quadrant is limited to the A-A sectional view, expression left end cap situation, Fig. 1, arrow among Fig. 2 is represented gas flow direction, Retroacting engine of the present utility model, a fixedly wheel seat 4 is arranged, fixedly wheel seat is provided with left end cap 1 and right end cap 6, left end cap is communicated with the relief opening of described compressor 7, described transmission shaft 3 is installed in a left side by bearing 8, on the right end cap, an active wheel 2 is installed at the middle part of transmission shaft, this active wheel is by interior ring 201, outer shroud 202 and stator 203 constitute, in, a plurality of described firing chambers 204 are housed between the outer shroud, present embodiment is provided with 3 firing chambers, on encircling in the suction port 205 of this firing chamber is located at, exhaust nozzle 206 is located on the outer shroud, a fixed inducer 5 is installed on the described right end cap, and this inducer is provided with a plurality of radial-flow guide vanes 501, and this inducer inner edge 502 is provided with gas collection runner and flow outlet 503, in the zone of this flow outlet between 230 ° of-360 ° of angles, this air flow outlet is provided with oil nozzle and spark plug, and fuel feeding and ignition mechanism are prior arts, are not described, the inwall in zone is provided with many reflection grooves 401 between 180 ° of-360 ° of angles of described fixedly wheel seat, and this reflection groove is in communication with the outside by the duct 601 of right end cap.The rotor shaft of described compressor is to join through speed change gear and engine driveshaft, and the power start arbor joins by engaging and disengaging gear and transmission shaft.
Efficiency is to weigh the leading indicator of thermo-mechanical property, because this hot machine needn't resemble the restriction that is subjected to the high temperature resistant and intensity of blade the gas turbine, the operating temperature of combustion gas can be unrestricted, needn't suck excessive air in order to reduce the temperature of combustion gas, also reduce the dump energy in the combustion gas simultaneously.Cooling loss in vapour, diesel engine on the other hand, the energy of mechanical friction loss is almost identical with the energy that changes mechanical work into, but, the cooling of active wheel firing chamber is finished by displacement in the utility model, the energy of cooling work wheel is brought back in the motor by air-flow again, has reduced and reduced the energy that cooling is scattered and disappeared.The consumption of general gas turbine almost needs about 2/3rds of total output at the power on the gas compressor, but the utility model is isochoric combustion, needn't suck the excessive air and the gas of high pressure very, reduced the energy that gas compressor consumes, therefore efficient of the present utility model will improve significantly.
The utility model has been used punching type air compression method and new energy merit conversion regime, reduced cooling system, thermal efficiency height, weight/power ratio is low, simple in structure, fuel saving and raw material have been eliminated the parts that blade, piston, bent axle etc. easily break down simultaneously, and the running principle is simple, operation is reliable, easy to maintenance, so its use can give national economy, national defense construction brings huge benefit.

Claims (1)

1, a kind of Retroacting engine, compressor is arranged, firing chamber and transmission shaft, it is characterized in that: a fixedly wheel seat (4) is arranged, fixedly wheel seat is provided with left end cap (1) and right end cap (6), left end cap is communicated with the relief opening of described compressor (7), described transmission shaft (3) is installed in a left side by bearing (8), on the right end cap, an active wheel (2) is installed at the middle part of transmission shaft, this active wheel is by interior ring (201), outer shroud (202) and stator (203) constitute, in, a plurality of described firing chambers (204) are housed between the outer shroud, on encircling in the suction port of this firing chamber (205) is located at, exhaust nozzle (206) is located on the outer shroud, a fixed inducer (5) is installed on the described right end cap, this inducer is provided with a plurality of radial-flow guide vanes (501), this inducer inner edge (502) is provided with gas collection runner and flow outlet (503), in the zone of this flow outlet between 230 ° of-360 ° of angles, this air flow outlet is provided with oil nozzle and spark plug, the inwall in zone is provided with many reflection grooves (401) between 180 ° of-360 ° of angles of described fixedly wheel seat, and this reflection groove is in communication with the outside by the duct (601) of right end cap.
CN99216867.8U 1999-07-14 1999-07-14 Reaction engine Expired - Fee Related CN2373579Y (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN99216867.8U CN2373579Y (en) 1999-07-14 1999-07-14 Reaction engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN99216867.8U CN2373579Y (en) 1999-07-14 1999-07-14 Reaction engine

Publications (1)

Publication Number Publication Date
CN2373579Y true CN2373579Y (en) 2000-04-12

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN99216867.8U Expired - Fee Related CN2373579Y (en) 1999-07-14 1999-07-14 Reaction engine

Country Status (1)

Country Link
CN (1) CN2373579Y (en)

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C19 Lapse of patent right due to non-payment of the annual fee
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