CN1287216A - Retroacting engine - Google Patents
Retroacting engine Download PDFInfo
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- CN1287216A CN1287216A CN 99119565 CN99119565A CN1287216A CN 1287216 A CN1287216 A CN 1287216A CN 99119565 CN99119565 CN 99119565 CN 99119565 A CN99119565 A CN 99119565A CN 1287216 A CN1287216 A CN 1287216A
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- end cap
- right end
- inducer
- engine
- wheel seat
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Abstract
The retroacting engine has one fixed wheel seat, right and left end caps on the seat, one transmission shaft installed via bearings on the caps and one working wheel installed in the middle of the shaft. The working shaft consists of inner and outer rings and guide blades, there are several combustion chambers between the inner and outer rings, and one fixed wind guiding wheel on the right end cap has several guide blades, gas collecting flow channel and gas flow outlet in its inner edge. The fixed wheel seat has several reflecting grooves on its inner wall and communicated outwards via duct in the right end cap.
Description
The present invention relates to a kind of Retroacting engine, 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 objective of the invention is to propose a kind of thermal efficiency that makes and improve greatly, weight/power ratio is near the Retroacting engine of air breathing engine.
The objective of the invention is to realize: a kind of Retroacting engine by following technical proposals, 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 invention, working principle of the present invention 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 present invention has following advantage:
1, be rotary component owing to the present invention 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 invention 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 invention 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 invention will be further described below in conjunction with drawings and Examples.
Fig. 1 is structural representation of the present invention (sectional view)
Fig. 2 is structural representation of the present invention (Figure 1A-A, B-B, C-C, a D-D sectional view)
Fig. 3 is a decomposing schematic representation of the present invention
Fig. 4 is an active wheel schematic representation of the present invention (sectional view)
Fig. 5 is an active wheel schematic representation of the present invention (sectional view)
Fig. 6 is active wheel front view of the present invention (Fig. 4 E is to view)
Fig. 7 is combustion chamber burner schematic representation of the present invention (Fig. 4 F is to view)
Fig. 8 is air inlet of combustion chamber schematic representation of the present invention (Fig. 4 G is to view)
Fig. 9 is a fixedly wheel seat schematic representation of the present invention (half sectional view)
Figure 10 is fixedly wheel seat schematic representation of the present invention (Fig. 9 N-N sectional view)
Figure 11 is a rear end cover schematic representation of the present invention (sectional view)
Figure 12 is rear end cover schematic representation of the present invention (Figure 11 M is to view)
Figure 13 is an inducer schematic representation of the present invention (sectional view)
Figure 14 is inducer schematic representation of the present invention (Figure 13 H is to view)
Figure 15 is a working principle schematic representation of the present invention
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 invention, 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, 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, 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, fuel feeding and ignition mechanism are prior arts, be 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 in the present invention finished by displacement, 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 present invention is isochoric combustion, needn't suck the excessive air and the gas of high pressure very, reduce the energy that gas compressor consumes, therefore efficient of the present invention will improve significantly.
The present invention has 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.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN99119565A CN1124404C (en) | 1999-09-03 | 1999-09-03 | Retroacting engine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN99119565A CN1124404C (en) | 1999-09-03 | 1999-09-03 | Retroacting engine |
Publications (2)
Publication Number | Publication Date |
---|---|
CN1287216A true CN1287216A (en) | 2001-03-14 |
CN1124404C CN1124404C (en) | 2003-10-15 |
Family
ID=5280962
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN99119565A Expired - Fee Related CN1124404C (en) | 1999-09-03 | 1999-09-03 | Retroacting engine |
Country Status (1)
Country | Link |
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CN (1) | CN1124404C (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN101825017A (en) * | 2005-05-23 | 2010-09-08 | 马同金 | Engine |
CN109236468A (en) * | 2018-11-21 | 2019-01-18 | 北京驰宇空天技术发展有限公司 | A kind of disc type combustion gas wheel turboshaft engine |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN1013046B (en) * | 1988-08-10 | 1991-07-03 | 戎华庆 | Combined rotary-reciprocating engine |
CN1058074A (en) * | 1990-12-08 | 1992-01-22 | 马强 | Firing engine |
CN1064130A (en) * | 1991-02-08 | 1992-09-02 | 邵立民 | Turbine-type heat engino |
HU213242B (en) * | 1995-07-17 | 1997-05-28 | Soos | Adiabatic, tangetial driving hydrogen engine |
-
1999
- 1999-09-03 CN CN99119565A patent/CN1124404C/en not_active Expired - Fee Related
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN101825017A (en) * | 2005-05-23 | 2010-09-08 | 马同金 | Engine |
CN101825017B (en) * | 2005-05-23 | 2015-03-18 | 马同金 | Engine |
CN109236468A (en) * | 2018-11-21 | 2019-01-18 | 北京驰宇空天技术发展有限公司 | A kind of disc type combustion gas wheel turboshaft engine |
Also Published As
Publication number | Publication date |
---|---|
CN1124404C (en) | 2003-10-15 |
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