CN105626303A - Jet engine with rotary cylinder body - Google Patents

Abstract

A jet engine with a rotary cylinder body is characterized in that the engine is composed of the rotary cylinder body, a piston, an upper cover of the rotary cylinder body, a lower cover of the rotary cylinder body, shafts, shaft pipes, a frame for fixing the cylinder body, bearings, electronic igniters, electronic control valves, electromagnets, pipeline channels, nozzles and the like, wherein the shafts and the shaft pipes are integrated with the upper cover and the lower cover correspondingly. After the engine is started, the rotary cylinder body rotates clockwise or anticlockwise and directly acts outwards. The novel technical scheme provided by the invention provides a new possibility for further improving work efficiency of the engine, saving energy and reducing air pollution.

Description

rotary block jet engine

The invention relates to a rotary block jet engine. The engine consists of a rotating cylinder, a piston, an upper cover and a lower cover of the rotating cylinder, a shaft and a shaft tube integrated with the upper and lower covers, a frame for fixing the cylinder, bearings, an electronic igniter, an electronic control valve, an electromagnet, and a pipeline channel , Nozzles, etc. When the rotating cylinder is burning fuel, it can perform clockwise or counterclockwise axial rotation and directly act externally.

The invention relates to a rotary cylinder jet engine, which does not have the useless linear motion of a four-stroke engine; it also does not have the air leakage problem that the combustion chamber of the engine cannot be completely closed, and the radial sealing sheet wears quickly; The structure is complex and the parts are worn out.

The purpose of the present invention is to provide a new technical solution, further improve the working efficiency of the engine, and provide a new possibility for saving energy and reducing air pollution.

The purpose of the present invention is achieved through the following measures. The rotary cylinder jet engine provided by the present invention has two kinds of internal combustion type and external combustion type. The nozzle on the side wall of the cylinder is sprayed out, pushing the rotating cylinder to rotate clockwise or counterclockwise, and directly acting externally. The external combustion fuel is not ignited in the cylinder cavity of the rotating cylinder, but is ignited on the nozzle after the fuel fills the cylinder cavity and reaches the nozzle, and a large amount of gas is generated and injected from the nozzle, pushing the rotating cylinder clockwise or counterclockwise. The rotating movement of the hour hand directly does work externally.

The present invention will be further described below in conjunction with accompanying drawing and embodiment:

(FIG. 1) is a schematic view of the appearance of the first embodiment.

(FIG. 2) is an overall side sectional view of the first embodiment.

(Fig. 3) is a side sectional view of the inner layer circular tube type rotary cylinder of the second embodiment

(Fig. 4) is a side sectional view of the outer layer circular tube type rotary cylinder of the second embodiment

(Fig. 5) is an overall side sectional view of the second embodiment

(Fig. 6) is an overall side sectional view of the third embodiment

(Fig. 7) is the overall side sectional view of the 4th embodiment

(Fig. 8) is a simple schematic diagram of other shapes of rotating cylinders.

In the figure, 1 round tube type rotating cylinder, 2 outer layer round tube type rotating cylinder, 3 inner layer round tube type rotating cylinder, 4 cylinder cavity, 5 frame, 6 frame upper end bearing, 7 frame lower end bearing, 8 Piston, 9 electromagnets, 10 upper electronic igniters,

11 lower electronic igniter, 12 electronic igniter in nozzle, 13 upper pipe shaft, 14 lower pipe shaft, 15 upper cover, 16 lower cover, 17 nozzle, 18 communication pipe between cylinder cavity and nozzle, 19 upper pipe electronic Control valve, 20 lower pipe electronic control valve, 21 upper exhaust electronic control valve, 22 lower exhaust electronic control valve, 23 electronic control valve in channel, 24 shaft integrated with lower cover, 25 inner circular tube type rotary cylinder The through hole on the body, 26 the passage of the outer circular tube type rotary cylinder connected to the nozzle, 27 the inlet of the combustion aid, 28 the passage of the fuel reaching the nozzle, 29 the passage of the combustion aid reaching the nozzle, 30 the outer circular tube type rotary cylinder The closed space between the inner circular tubular rotating cylinder.

Please see first embodiment: internal-combustion circular tube type rotary cylinder jet engine, see (Fig. 1), (Fig. 2).

At the upper and lower ends of the circular tube type rotating cylinder block 1 are upper cover 15 and lower cover 16, in the center of upper cover 15 there is an upper pipeline shaft 13 connected with cylinder cavity 4, in the center of lower cover 16 there is a lower pipeline shaft 14 and The cylinder cavity 4 is penetrated, and the upper pipeline shaft 13 passes through the middle of the frame upper end bearing 6 and is fixed on the frame 5 . The lower pipeline shaft 14 passes through the middle of the frame lower end bearing 7 and is fixed on the frame 5 . At this time, the circular tube type rotary cylinder can only rotate clockwise or counterclockwise. On the top of the loam cake 15, there is also an upper electronic igniter 10 and an upper exhaust electronic control valve 21, an upper electronic igniter 11 and a lower exhaust electronic control valve 22 are arranged on the lower cover 16; Pipeline electric control valve 19, there is lower pipeline electronic control valve 20 in lower pipeline shaft 14, piston 8 is arranged in cylinder cavity 4, and nozzle 17 is a plurality of rows of communication pipelines 18 passing through cylinder cavity and nozzle, The arrangement is on the side wall of the circular tube type rotary cylinder 1, and there is an electronically controlled valve 23 in a passage in the communication pipe 18 between each cylinder cavity and the nozzle.

Working principle: First, the upper pipeline electronic control valve 19 is opened, and the fuel enters the cylinder cavity 4 through the upper pipeline shaft 13. At this time, the upper exhaust electronic control valve 21 is closed, and the electronic control valve 23 in the channel is closed, and the lower exhaust The electronically controlled valve 22 is opened, and the electronically controlled valve 20 of the lower pipeline is closed. Along with the fuel continuously entering, the piston 8 in the cylinder chamber 4 is also pushed downwards, and the air in front of the piston 8 is excluded from the cylinder chamber 4 through the lower exhaust electronic control valve 22 . When the piston 8 reaches the lower end of the cylinder cavity 4, the upper pipeline electronic control valve 19 closes and the fuel does not continue to enter the cylinder cavity 4, the upper electronic igniter 10 ignites, and at the same time as the ignition, the electronic control valve 23 in the channel is opened, A large amount of gas generated by fuel combustion rapidly expands and is sprayed out from the nozzle 17, pushing the circular tubular rotating cylinder 1 to rotate clockwise or counterclockwise to directly perform work on the outside.

After the fuel in the cylinder chamber 4 is burned, the lower pipe electronic control valve 20 is opened, and at this time, the fuel begins to enter the cylinder chamber 4 through the lower pipe shaft 14. At this time, the lower exhaust electronic control valve 22 is closed, and the electronic control valve 20 in the passage The control valve 23 is closed, and the upper exhaust electronic control valve 21 is opened. With the continuous entry of fuel, the piston 8 is continuously pushed up, and the burned exhaust gas in front of the piston 8 is continuously passed through the upper exhaust electronic control valve 21 Excluded from the cylinder chamber 4. When the piston reaches the top of the cylinder chamber 4, the lower pipeline electronic control valve 20 is closed, and the fuel does not continue to enter the cylinder chamber 4. At this time, the lower electronic igniter 11 is ignited, and the electronic control valve 23 in the passage is opened at the same time as the ignition. A large amount of gas generated by fuel combustion in the cylinder cavity 4 rapidly expands and is sprayed out from the nozzle 17, pushing the circular tube-shaped rotating cylinder 1 to rotate clockwise or counterclockwise to directly perform work on the outside. Then enter the process of the next cycle.

Please see the 2nd embodiment, this is an internal-combustion double-deck circular tube type rotary cylinder engine. The present embodiment will be described in detail below in conjunction with ( FIG. 3 ), ( FIG. 4 ), ( FIG. 5 ).

In this embodiment, the purpose of using a double-layer circular tube type rotating cylinder is to make the relative rotation between the two layers of cylinders close or to connect the communication pipeline between the cylinder cavity 4 and the nozzle 17 according to actual needs.

(Fig. 3) what draw is the side sectional view of inner layer circular tube type rotary cylinder body 3: in figure front view, the through hole 25 on the inner layer circular tube type rotary cylinder body, on the front view, is in cylinder Indicated by the circular hole on the side wall of the body and the notch penetrating the side wall of the cylinder. The top view is cut at the arrow on the front view, so as to clearly show the azimuth relationship between the through hole 25 on the inner circular tubular rotating cylinder and the cylinder.

(Fig. 4) what draw is the side sectional view of outer layer circular tube type rotary cylinder body 2: in front view, the passage 26 of outer layer circular tube type rotary cylinder body Unicom nozzle is formed by the through hole on the cylinder body and It consists of pipes welded to the outside of the through hole. The top view is cut at the arrow place in the front view, so that the passage 26 of the outer layer circular tube type rotary cylinder body 2 and the outer layer circular tube type rotary cylinder body communicating with the nozzle, and the nozzle 17, the connection between the three Relationships and orientations are clearly revealed.

(Fig. 5) is that the outer layer circular tube type rotary cylinder body 2 and the inner layer circular tube type rotary cylinder body 3 are set together, and the inner and outer layers of the two layers of cylinder bodies that are set together can be separately arranged in the axial direction. There are only two results for rotating, respectively rotating: the one is to connect the through hole 25 on the inner layer circular tube type rotary cylinder with the passage 26 of the outer layer circular tube type rotary cylinder Unicom nozzle, and the other is to make this connection channel dislocation blocking.

In (Fig. 5), there is a piston 8 in the cylinder cavity 4, and the upper end of the inner circular tube type rotating cylinder body 3 is an upper cover 15, and an upper exhaust electronic control valve 21 and an upper electronic igniter 10 are arranged on the upper end of the 15. In the center of the upper cover 15, there is an upper pipe shaft 13 that runs through the cylinder chamber 4, and in the center of the lower cover 16, there is a lower pipe shaft 14 that runs through the cylinder chamber 4. The upper pipe shaft 13 passes through the middle of the frame bearing 6 and is fixed on the frame. 5 on. The lower pipeline shaft 14 passes through the middle of the frame lower end bearing 7 and is fixed on the frame 5 . At this time, the circular tubular rotating cylinder can only rotate clockwise or counterclockwise. On the side wall of the outer circular tube type rotary cylinder body 2 there are nozzles 17 and the passage 26 of the outer layer circular tube type rotary cylinder body Unicom nozzle, and an electromagnet 9.

Since the inner and outer two-layer cylinder blocks can independently rotate axially, the space in the cylinder chamber 4 is sometimes in a state of being connected to the nozzle, and sometimes in a closed state of being inaccessible to the nozzle. 25 and 26 are connected when being in the through state, and are dislocation disconnected between 25 and 26 when being in the closed state. What is drawn on (FIG. 5) is the ON state.

Working principle: First, the upper pipeline electronic control valve 19 is opened, and the fuel enters the cylinder chamber 4 through the upper pipeline shaft 13. At this time, the upper exhaust electronic control valve 21 is closed, the lower exhaust electronic control valve 22 is opened, and the lower pipeline electronically controls Valve 20 is closed. The electromagnet 9 is connected in the forward direction, so that there is a relative rotation between the two layers of cylinders, and there is a misalignment between 25 and 26, which blocks the passage between the cylinder chamber 4 and the nozzle 17, so that the cylinder chamber 4 is relatively closed. status.

As the fuel continuously enters the piston 8 and continues to move downward, the gas in front of the piston 8 is discharged from the lower exhaust electronic control valve 22. When the piston 8 moves to the bottom of the cylinder cavity, the upper pipeline electronic control valve 19 is closed , the fuel is no longer entering the cylinder chamber 4. At this time, the upper electronic igniter 10 is ignited. At the same time of ignition, the electromagnet 9 is turned on in reverse so that the dislocation between 25 and 26 is restored and connected, allowing the cylinder chamber A large amount of gas generated in 4 passes through and is sprayed out from the nozzle, pushing the double-layer circular tube rotating cylinder to generate axial rotation and directly acting externally.

After the fuel in the cylinder cavity 4 is burned, the lower pipeline electronic control valve 20 is opened, and the fuel begins to enter the cylinder cavity 4 through the lower pipeline shaft 14 again. At this time, the lower exhaust electronic control valve 22 is closed, and the upper exhaust electronic control valve The control valve 21 is opened, and at this time, the electromagnet 9 is turned on again, and the relative rotation occurs between the two layers of cylinders, and a misalignment occurs between 25 and 26, blocking the passage between the cylinder chamber 4 and the nozzle 17 , making the cylinder chamber 4 in a relatively closed state again. With the continuous entry of fuel, the piston 8 continues to move upwards, and the exhaust gas in front of the piston 8 is discharged from the upper exhaust electronic control valve 21. When the piston 8 moves to the top of the cylinder cavity, the lower pipeline electronic control valve 20 is closed, Fuel does not continue to enter the cylinder cavity 4, and at this moment, the lower electronic igniter 11 ignites, and at the same time of ignition, the electromagnet 9 is turned on in reverse again, so that the dislocation that occurs between 25 and 26 is restored and turned on again, allowing the cylinder A large amount of gas generated in the cavity 4 passes through and is sprayed out from the nozzle, pushing the double-layer circular tube-type rotating cylinder to generate axial rotation and directly acting externally. Then enter the process of the next cycle.

Please see the 3rd embodiment: this is an external-combustion circular tube type rotary cylinder jet engine, see (Fig. 6). At the upper and lower ends of the circular tube type rotating cylinder block 1 are upper cover 15 and lower cover 16, in the center of upper cover 15 there is an upper pipe shaft 13 which communicates with cylinder chamber 4, and in the center of lower cover 16 there is a shaft integrated with the lower cover. Axis 24. The upper pipeline shaft 13 passes through the middle of the upper end bearing 6 of the frame and is fixed on the frame 5, and the shaft 24 integrated with the lower cover passes through the middle of the lower end bearing 7 of the frame and is fixed on the frame 5. At this time, the circular tube type rotary cylinder The body can only rotate clockwise or counterclockwise. The nozzles 17 are multiple rows of communication pipes 18 passing through the cylinder cavity and the nozzles, arranged on the side wall of the circular tube type rotating cylinder 1, and there is a nozzle installed in the nozzles in each nozzle. Electronic igniter 12.

Working principle: First, the upper pipe electronic control valve 19 is opened, the fuel enters the cylinder chamber 4 through the upper pipe shaft 13, and then reaches the nozzle 17 through the communication pipe 18 between the cylinder chamber and the nozzle. At this time, the nozzle in the nozzle 17 The electronic igniter 12 inside is ignited, the fuel is ignited in the nozzle, a large amount of gas is generated and ejected, and the circular tube-shaped rotating cylinder is driven to rotate clockwise or counterclockwise, and directly perform work externally. As long as the upper pipeline electronic control valve 19 is not closed, the fuel will continuously enter the cylinder 4, so that the combustion and the rotary motion of the cylinder continue.

Please see the 4th embodiment: this is an external-combustion double-layer circular tube type rotary cylinder jet engine, see (Fig. 7).

The upper end of the inner circular tubular rotating cylinder 3 communicates with the upper pipeline shaft 13, the upper pipeline shaft 13 passes through the middle of the bearing 6 at the upper end of the frame and is fixed on the frame 5, and communicates with the lower end of the outer circular tubular rotating cylinder 2 Down the pipeline shaft 14, the lower pipeline shaft 14 passes through the middle of the frame lower end bearing 7 and is fixed on the frame 5. At this time, the double-layer circular tube type rotating cylinder can only rotate clockwise or counterclockwise. Multiple rows of multiple nozzles 17 are installed on the side wall of the outer circular tube type rotary cylinder 2, and for the sake of clarity, only one of them is drawn as a representative in the figure. There is an upper pipeline electronic control valve 19 in the upper pipeline shaft 13, and a lower pipeline electronic control valve 20 in the lower pipeline shaft 14.

Working principle: First, the upper pipeline electronic control valve 19 is opened, the fuel enters the cylinder cavity 4 through the upper pipeline shaft 13, and then reaches the nozzle 17 through the passage 28 where the fuel reaches the nozzle, and at the same time, the lower pipeline electronic control valve in the lower pipeline shaft 14 20 is also opened, and the combustion aid enters the closed space 30 between the outer circular tube type rotary cylinder and the inner circular tube type rotary cylinder through the lower pipe shaft, and reaches the nozzle 17 through the channel 29 where the combustion aid reaches the nozzle. .At this time, the electronic igniter 12 in the nozzle 17 is ignited, the fuel and the combustion aid are ignited in the nozzle, a large amount of gas is generated and ejected, and the double-layer circular tube rotating cylinder is driven to rotate clockwise or counterclockwise. Work directly externally. As long as the upper pipeline electronic control valve 19 and the lower pipeline electronic control valve 20 are not closed, the fuel and the combustion aid will be continuously supplied, so that the engine will continue to work.

The rotating cylinder can be made into various shapes according to different actual needs; for example, the triangular column type is shown in Figure 8c, the square column type is shown in Figure 8d, the polygonal column type is shown in Figure 8e, the spherical shape is shown in Figure 8b, and the conical shape is shown in Figure 8f. If cooling is required, the rotating cylinder block and other parts of the engine can be made hollow so that gas or liquid can flow through it to achieve the purpose of cooling. In addition, the rotating cylinder engine can be placed vertically or horizontally according to actual needs, as shown in Figure 8a.

Claims (8)

1. A rotary cylinder jet engine is characterized in that: the engine is composed of a rotary cylinder, a piston, a loam cake and a lower cover of the rotary cylinder, an integral shaft and shaft tube with the upper and lower covers, and the frame of the fixed cylinder , bearings, electronic igniters, electronic control valves, electromagnets, pipeline channels, nozzles, and other components. 2. A kind of rotary cylinder jet engine according to claim 1, characterized in that: the upper and lower ends of the circular tube type rotary cylinder 1 are upper cover 15 and lower cover 16, and there is an upper cover 15 at the center of the upper cover 15. The pipeline shaft 13 is connected with the cylinder chamber 4, and a lower pipeline shaft 14 is connected with the cylinder chamber 4 at the center of the lower cover 16, and the upper pipeline shaft 13 passes through the middle of the frame upper end bearing 6 and is fixed on the frame 5. The lower pipeline shaft 14 passes through the middle of the frame lower end bearing 7 and is fixed on the frame 5 . At this time, the circular tubular rotating cylinder can only rotate clockwise or counterclockwise. On the top of the loam cake 15, there is also an upper electronic igniter 10 and an upper exhaust electronic control valve 21, an upper electronic igniter 11 and a lower exhaust electronic control valve 22 are arranged on the lower cover 16; Pipeline electronic control valve 19, there is lower pipeline electronic control valve 20 in lower pipeline shaft 14, piston 8 is arranged in cylinder chamber 4, and nozzle 17 is a plurality of rows of communication pipelines 18 through the cylinder chamber and the nozzle. For example, on the sidewall of the circular tube type rotary cylinder body 1, and in the communication pipeline 18 between each cylinder cavity and the nozzle, there is an electronically controlled valve 23 in the passage. 3. A kind of rotary cylinder jet engine according to claim 1, characterized in that: this is an internal combustion double-layer circular tube type rotary cylinder engine, the side wall of the inner layer circular tube type rotary cylinder 3 On, the through hole 25 on the inner layer circular tube type rotating cylinder body, piston 8 is arranged in the cylinder cavity 4, the upper end of the inner layer circular tube type rotating cylinder body 3 is loam cake 15, has upper cover 15 above The exhaust electronic control valve 21 and the upper electronic igniter 10 have an upper pipe shaft 13 in the center of the upper cover 15 that runs through the cylinder cavity 4, and the upper pipe shaft 13 passes through the middle of the upper end bearing 6 of the frame and is fixed on the frame 5. The lower end of the inner circular tube type rotary cylinder 3 is a lower cover 16, and in the center of the lower cover 16, there is a lower pipe shaft 14 which runs through the cylinder cavity 4, and the lower pipe shaft 14 passes through the middle of the lower end bearing 7 of the frame and is fixed on the frame 5. At this time, the circular tubular rotary cylinder can only rotate clockwise or counterclockwise, and there are nozzles 17 on the side wall of the outer circular tubular rotary cylinder 2 and the connecting nozzles of the outer circular tubular rotary cylinder. Channel 26, and electromagnet 9. 4. A kind of rotary cylinder jet engine according to claim 1, characterized in that: the upper and lower ends of the circular tube type rotary cylinder 1 are an upper cover 15 and a lower cover 16, and there is an upper cover 15 at the center of the upper cover 15. The pipeline shaft 13 communicates with the cylinder cavity 4, and a shaft 24 integrated with the lower cover is arranged at the center of the lower cover 16. The upper pipe shaft 13 passes through the middle of the frame upper end bearing 6 and is fixed on the frame 5 . The shaft 24 integrated with the lower cover passes through the middle of the frame lower end bearing 7 and is fixed on the frame 5. At this time, the circular tube type rotating cylinder can only rotate clockwise or counterclockwise. The nozzles 17 are multiple rows of communication pipes 18 passing through the cylinder cavity and the nozzles, arranged on the side wall of the circular tube type rotating cylinder 1, and there is a nozzle installed in the nozzles in each nozzle. Electronic igniter 12. 5. A kind of rotary cylinder jet engine according to claim 1, characterized in that: this is an external combustion type double-layer circular tube type rotary cylinder jet engine, and the inner circular tube type rotary cylinder 3 The upper end communicates with the upper pipeline shaft 13, and the upper pipeline shaft 13 passes through the middle of the upper end bearing 6 of the frame and is fixed on the frame 5. The lower end of the outer circular tube type rotating cylinder 2 communicates with the lower pipeline shaft 14, and the lower pipeline shaft 14 passes through the middle of the frame upper end bearing 6. The frame lower end bearing 7 passes through and is fixed on the frame 5 in the middle, and at this moment, the double-layer circular tube type rotating cylinder body can only rotate clockwise or counterclockwise. Multiple rows of multiple nozzles 17 are installed on the side wall of the outer circular tube type rotary cylinder 2, and for the sake of clarity, only one of them is drawn as a representative in the figure. There is an upper pipeline electronic control valve 19 in the upper pipeline shaft 13, and a lower pipeline electronic control valve 20 in the lower pipeline shaft 14. The fuel enters the cylinder cavity 4 through the upper pipeline shaft 13, and reaches the nozzle through the passage 28 where the fuel reaches the nozzle. 17. The combustion aid enters the closed space 30 between the outer circular tube type rotating cylinder body and the inner layer circular tube type rotating cylinder body through the lower pipe shaft 14, and reaches the nozzle 17 through the passage 29 where the combustion aid reaches the nozzle. 6. A rotary cylinder jet engine according to claim 1, 2, 3, 4, 5, characterized in that: the rotary cylinder can be made into various shapes according to different actual needs: such as triangular column type, see Figure 8c Figure 8d for the square column type, Figure 8e for the polygonal column type, Figure 8b for the spherical type, and Figure 8f for the conical type. 7. A rotary cylinder jet engine according to claims 1, 2, 3, 4, 5, 6, characterized in that: the rotary cylinder and other parts of the engine can be made hollow. 8. A rotary cylinder jet engine according to claims 1, 2, 3, 4, 5, 6, 7, characterized in that: the rotary cylinder engine can be placed vertically or horizontally, see Figure 8a .