WO2007128195A1

WO2007128195A1 - An engine with a fluid spraying turbine

Info

Publication number: WO2007128195A1
Application number: PCT/CN2007/001173
Authority: WO
Inventors: Wanyi Cai
Original assignee: Wanyi Cai
Priority date: 2006-04-28
Filing date: 2007-04-11
Publication date: 2007-11-15
Also published as: CN1952351A; CN100393983C

Abstract

An engine with a fluid spraying turbine includes a power part, the power part has a main shaft (1) which is attached on a housing via a bearing (6). A turbine (3) is attached at the front of the main shaft (1), and the turbine (3) connects with a generator (4) integrally. An axis flywheel (19) connecting with a starter (56) is located at the trailing of the main shaft (1). A fluid pump (14) and a lubricant pump (60) connect with a pump casing (15) via a bracket (17), the pump casing (15) connects with a cylinder block (12), and a cylinder lid (8) is located on the cylinder block (12). The engine can use pressurized liquid and pressurized air to drive the turbine rapidly.

Description

Hydraulic air jet flywheel air vortex rotor idle speed engine

The invention belongs to the technical field of engines, and particularly relates to a high-speed engine of a hydraulic airflow jet flywheel vortex rotor with liquid and gas as energy sources.

Background technique

Commonly used various types of reciprocating engines, such as steam turbines, gas engines, and jet engines, which use fuel as a source of warm air flow, which is injected linearly from the front end of the fuselage to the rear end of the fuselage to make the vane rotor Rotate. When rotating, it has large torque, large vibration, unstable operation, high noise and serious pollution. Due to the large number of internal components and the high temperature gas flow for a long time, it is easily damaged and deformed, resulting in the engine not working. This type of engine must be manufactured with special, expensive, heat-resistant alloy steels that are complex in process, difficult to manufacture, and costly.

Summary of the invention

The object of the present invention is to provide an inertial action capable of overcoming mechanical motion in view of the disadvantages and problems of the above-mentioned engine, using liquid and gas as energy sources, high output power, high rotation speed, stable operation, and low noise. It has low pollution and good use effect. It can be widely used in various vehicles such as airplanes, trains, ships, automobiles, motorcycles, etc., and hydraulic air jet flywheel vortex rotor high-speed engines used as prime movers for power generation and agricultural machinery.

The engine of the present invention is composed of two parts: power and liquid gas. The power part consists of a main shaft, a fastener, a turbo fan, a generator, a turbofan casing, a bearing sleeve, a lubricating oil passage pipe, a cylinder head, a bolt, a sealing ring, an axial flywheel vortex rotor, a cylinder block, a cylinder lubrication pipe, Liquid gas pump, pump casing, heat pipe, fixing frame, axial flywheel casing, axial flywheel, bearing, power casing, exhaust pipe, high pressure liquid gas nozzle, external heat dissipation air passage, internal heat dissipation air passage, sealing sheet, Starter and lubricant pump components.

The liquid gas part consists of a lubricating oil distribution pipe, a longitudinal storage circulation pipe, a tertiary high pressure circulation pipe, a liquid gas casing, an ultra-pressing control circulation pipe, a sealing cover, a liquid gas filter, a sewage bolt, a secondary high pressure circulation pipe, and a lateral storage cycle. Tube, start valve, primary high pressure circulation pipe, lubricating oil discharge pipe, high pressure liquid gas discharge pipe, single liquid gas pump discharge pipe, internal lubricating oil circulation oil inlet pipe, high pressure lubricating oil discharge pipe, external lubricating oil filler pipe, high pressure liquid gas passage Pipe, external liquid gas inlet pipe, liquid gas inlet pipe in the tail end, double liquid gas pump discharge pipe, liquid gas communication pipe, separator, liquid gas outer casing bolt, liquid gas inlet pipe at the head end, lubricating oil filter parts composition.

The main shaft of the engine power portion of the present invention is fastened to the power housing via a bearing sleeve. The end of the power housing is provided with an axial flywheel housing with an exhaust pipe, and the bottom end is provided with a liquid gas portion. The turbo fan is connected to the generator It is fastened to the front end of the spindle. The liquid gas pump provided with the heat pipe is connected with the lubricating oil pump provided with the heat pipe to form a combination pump, and the other two liquid gas pumps respectively provided with the heat pipe are connected to form another combination pump. At least two combined pumps are adjacent to at least three axial flywheel air vortex rotors and are respectively fastened to the main shaft, and the end of the main shaft is provided with an axial flow flywheel connected to the starter. The liquid gas pump and the lubricating oil pump are respectively connected to the pump casing via a fixing frame, the pump casing is connected with the cylinder block, and the cylinder head is provided on the cylinder block.

Another combination pump consisting of a combination pump of a single liquid air pump and a lubricating oil pump of the engine of the present invention and two other liquid air pumps is a set of four pumps, which have the same structure and different uses. The liquid-gas pump is composed of an external drain air passage, an inner drain air passage, a sliding vane and a liquid-gas pump rotor provided with a pressure rail. The upper and lower ends of the liquid gas pump and the upper and lower ends of the lubricating oil pump are respectively connected to the heat pipe through the heat pipe connecting piece. The liquid gas filter and the lubricating oil filter respectively provided with the sealing cover are respectively connected to the liquid gas pump and the lubricating oil pump through the pipeline. The bottom of the liquid gas filter and the lubricating oil filter are respectively provided with drain bolts.

The engine of the invention has three axial flow flywheel vortex rotors of the same structure disposed on the main shaft thereof, and the first, middle and rear end high-pressure liquid gas of the same structure are respectively arranged on the axial flow flywheel vortex rotors of the first, middle and rear ends. nozzle. One side of the first-end high-pressure liquid-gas nozzle and one high-pressure liquid-gas circulation pipe provided with an ultra-compressed circulation pipe and the left and right lateral storage circulation pipes, the start valve, the two-liquid gas discharge pipe and the heat pipe provided with the separators in turn connection. The other side of the head end high pressure liquid gas nozzle is sequentially connected with the first end high pressure liquid gas discharge pipe and the second high pressure circulation pipe. The other side of the middle-end high-pressure liquid-gas nozzle is connected in series with the middle-end high-pressure liquid gas discharge pipe and the three high-pressure circulation pipes. The other side of the tail end high pressure liquid gas nozzle and the tail end high pressure liquid gas discharge pipe, the longitudinal storage circulation pipe, the liquid gas communication pipe, the external liquid gas inlet pipe, the internal liquid gas inlet pipe, the double liquid gas pump discharge pipe, the high pressure liquid gas The channel tube and the liquid gas inlet pipe in the first end are connected in sequence. A seal ring is arranged on both sides of the axial flow flywheel vortex rotor. The inner side of the axial flow flywheel vortex rotor is provided with an internal heat dissipation air passage, an external heat dissipation air passage, a cylinder lubrication duct and a sealing piece.

The turbofan casing provided at the head end of the engine power casing of the present invention is connected to the upper and lower cylinder heads of the head end, and the cylinder heads of the first, middle and rear ends are bolted to the cylinders of the first, middle and rear ends. A lubricating oil distribution pipe and a lubricating oil discharge pipe are respectively disposed on the upper and lower cylinder caps of the first, middle, and rear ends. The lubricating oil distribution pipe is connected with the external lubricating oil filler pipe, and the lubricating oil discharge pipe is connected with the internal lubricating oil circulating oil inlet pipe. A lubricating oil passage pipe is disposed on the lubricating oil distribution pipe and the lubricating oil discharge pipe, respectively. The liquid-gas outer casing is fastened to the bottom end of the power casing via a liquid-gas outer casing bolt.

The engine of the present invention utilizes liquid gas as an energy source, is compressed into a high-pressure liquid gas through a series of mechanical operations, and transmits a large static pressure generated by a hydraulic airflow through a closed pipe to push the axial, axial, and flywheel vortex rotors at the first, middle, and rear ends simultaneously. The enormous energy generated by the cyclic idling rotation is used as a driving force. The working principle is to start the starter, rotate the axial flywheel to drive the turbine fan of the generator on the main shaft, and pump the liquid gas into the machine through the two-liquid pump. Shrink into high pressure liquid gas. The high-pressure liquid gas is cooled by the heat-dissipating tube, and then cooled into a single-liquid air pump for compression. After being cooled and cooled by the heat-dissipating tube, it is discharged by the single-liquid pump discharge tube, and then ejected through the start valve and the high-pressure circulation pipe to the first-end high-pressure liquid gas nozzle. Then, the first-end axial-flow flywheel gas vortex rotor is rotated for one rotation, and then discharged from the first-end high-pressure liquid gas discharge pipe to the secondary high-pressure circulation pipe, and is sprayed through the middle-end high-pressure liquid gas nozzle, thereby pushing the middle-end axial flow flywheel gas vortex rotor Rotate for one week, and then discharge through the middle-end squeezing liquid gas discharge pipe. After three high-pressure circulation pipes are sprayed to the high-pressure liquid gas nozzle at the end, the end-shaft axial-wheel flywheel vortex rotor is pushed for one rotation, and then the tail end is pressed. The gas discharge pipe is discharged to the longitudinal storage circulation pipe, the liquid gas communication pipe, the liquid gas inlet pipe in the tail end to the liquid gas filter, the double liquid air pump discharge pipe, the high pressure liquid gas passage pipe, the first end inner liquid gas inlet pipe The single-liquid pump is discharged from the single-liquid pump discharge pipe, and then sprayed out through the start valve and the high-pressure circulation pipe to the first-end pressure liquid gas nozzle, so that the operation is repeated.

The lubricating oil enters the lubricating oil filter from the outer lubricating oil filler pipe, and is compressed into high-pressure lubricating oil by the lubricating oil pump. The high-pressure lubricating oil is cooled and cooled by the heat-dissipating pipe, and sequentially enters the lubricating oil distribution pipe, the lubricating oil discharge pipe, and the cylinder lubricating pipe. Then, through the lubricating oil circulating oil inlet pipe, the lubricating oil pump is compressed into a high-pressure lubricating oil through the pipeline of the lubricating oil filter, so that the engine is repeatedly operated, thereby achieving the friction reducing resistance of the engine of the invention and reducing the wear between the components, reducing the power. Loss, ensuring its normal operation and extending its service life.

DRAWINGS

Figure 1 is a front elevational view of the engine of the present invention;

Figure 2 is a left side cross-sectional view of Figure 1;

Figure 3 is a plan view of the bottom of Figure 1;

Figure 4 is a flow chart of Figure 3;

Figure 5 is a main (cross-sectional) view of the liquid-gas pump;

Figure 6 is a plan view of the liquid gas pump;

Figure 7 is a cross-sectional view showing the connection of the single liquid air pump to the liquid gas portion;

Figure 8 is a cross-sectional view showing the connection of the lubricating oil pump to the liquid gas section

Figure 9 is a cross-sectional view showing the connection of the two-liquid pump to the liquid-gas portion;

Figure 10 is a cross-sectional view showing the connection of the first end axial flow flywheel vortex rotor to the liquid gas portion;

Figure 11 is a cross-sectional view showing the connection of the middle end axial flow flywheel vortex rotor to the liquid gas portion;

Figure 12 is a cross-sectional view showing the connection of the tail axial axial flywheel gas vortex rotor and the liquid gas portion;

Figure 13 is a cross-sectional view showing the connection of the axial flywheel housing to the end cylinder head.

detailed description

The engine embodiment of the present invention will be further described in detail below in conjunction with the above-described examples of the drawings. Examples of the engine of the present invention include two parts of power and liquid gas. The power part consists of the main shaft 1, the fastener 2, the turbo fan 3, the generator 4, the turbo fan casing 5, the bearing sleeve 6, the lubricating oil passage tube 7, the cylinder head 8, the bolt 9, the sealing ring 10, the axial flywheel vortex Rotor 11, cylinder 12, cylinder lubrication pipe 13, liquid air pump 14, pump casing 15, heat pipe 16, fixed frame 17, axial flywheel casing 18, axial flywheel 19, bearing 20, power casing 21, exhaust pipe 22. The high pressure liquid gas nozzle 24, the external heat dissipation air passage 36, the internal heat dissipation air passage 37, the sealing piece 39, the starter 56, and the lubricating oil pump 60 are formed.

The liquid gas portion is composed of a lubricating oil distribution pipe 23, a longitudinal storage circulation pipe 25, a tertiary high pressure circulation pipe 26, a liquid gas casing 27, an overpressure control circulation pipe 28, a sealing cover 29, a liquid gas filter 30, a sewage bolt 31, and two a secondary high pressure circulation pipe 32, a lateral storage circulation pipe 33, a starting valve 34, a primary high pressure circulation pipe 35, a lubricating oil discharge pipe 38, a high pressure liquid gas discharge pipe 40, a single liquid air pump discharge pipe 41, an internal lubricating oil circulation oil inlet pipe 42, a high-pressure lubricating oil discharge pipe 43, an external lubricating oil filler pipe 44, a high-pressure liquid gas passage pipe 45, an external liquid gas inlet pipe 46, a liquid gas inlet pipe 47 in the tail end, a double liquid gas pump discharge pipe 48, a liquid gas communication pipe 49, The partition 57, the liquid-gas outer casing bolt 58, the first-end internal liquid gas inlet pipe 59, and the lubricating oil filter 61 are composed.

In the engine of the present invention, the main shaft 1 of the power portion thereof is fastened to the power casing 21 via a bearing sleeve 6 provided with a bearing 20. The rear end of the power casing 21 is provided with an axial flywheel casing 18 with an exhaust pipe 22, and a liquid gas portion is provided at the bottom end. The turbo fan 3 is integrally coupled to the magnetic tile of the generator 4 and fastened to the keyway 62 at the front end of the main shaft 1 via a fastener 2. The liquid-gas pump 14 provided with the heat-dissipating tube 16 is connected to the lubricating oil pump 60 provided with the heat-dissipating tube 16 to form a combination pump, and the other two liquid-gas pumps 14 respectively provided with the heat-dissipating tubes 16 are connected to form another combination pump. At least two combination pumps are adjacent to at least three axial flywheel vortex rotors 11 and are fastened to the keyway 62 of the main shaft 1 via fasteners 2, and the end of the main shaft 1 is provided with an axial flywheel connected to the starter 56. 19. The liquid gas pump 14 and the lubricating oil pump 60 are respectively connected to the pump casing 15 via a fixing frame 17, and the pump casing 15 is connected to the cylinder block 12. The cylinder block 12 is provided with a cylinder head 8.

Another combination pump composed of a combination of a single-liquid pump 14 and a lubricating oil pump 60 disposed on the engine of the present invention is connected to the other two liquid-gas pumps 14 as two sets of four pumps, which have the same structure and different uses, and they are The invention produces high pressure liquid gas as an important component of power energy. The liquid-gas pump 14 is composed of an outer drain air passage 54, an inner drain air passage 53, a slide 51, and a liquid-gas pump rotor 50 provided with a pressure rail 52. The upper and lower ends of the liquid-gas pump 14 and the upper and lower ends of the lubricating oil pump 60 are respectively connected to the heat-dissipating pipe 16 via the heat-dissipating pipe connecting member 55. The liquid-gas filter 30 and the lubricating oil filter 61, which are respectively provided with the sealing cover 29, are connected to the liquid-gas pump 14 and the lubricating oil pump 60 via their pipes. The liquid gas filter 30 and the lubricating oil filter 61 are respectively provided with a drain bolt 31 at the bottom.

The engine of the present invention has three axial flow flywheel vortex rotors 11 of the same structure disposed on the main shaft 1 thereof. They are important components of the driving force of the present invention. The first, middle, and rear end high-pressure liquid-air nozzles 24 of the same structure are respectively disposed on the first, middle, and rear axial-wheel flywheel vortex rotors 11. One side of the first end high pressure liquid gas nozzle 24 and one primary high pressure circulation pipe 35 provided with the overpressure automatic circulation pipe 28 and the left and right lateral storage circulation pipes 33 provided with the partition 57, the start valve 34, and the two liquid air pump discharge pipe 48 and the heat pipe 16 are connected in sequence. The other side of the first end high pressure liquid gas nozzle 24 is sequentially connected to the first end high pressure liquid gas discharge pipe 40 and the secondary high pressure circulation pipe 32. The other side of the middle-end high-pressure liquid-gas nozzle 24 is sequentially connected to the middle-end high-pressure liquid gas discharge pipe 40 and the tertiary high-pressure circulation pipe 26. The other side of the tail end high pressure liquid gas nozzle 24 and the tail end high pressure liquid gas discharge pipe 40, the longitudinal storage circulation pipe 25, the liquid gas communication pipe 49, the external liquid gas inlet pipe 46, the tail end liquid gas inlet pipe 47, and the double The liquid-gas pump discharge pipe 48, the high-pressure liquid gas passage pipe 45, and the first-end internal liquid gas inlet pipe 59 are sequentially connected. A seal ring 10 is disposed on both sides of the axial flow flywheel vortex rotor 11 , and an inner heat dissipation air passage 37 , an outer heat dissipation air passage 36 , and a cylinder lubrication are disposed from the inside to the outside of the groove of the axial flow flywheel air vortex rotor 11 . Pipe 13, sealing sheet 39.

The turbofan casing 5 provided at the head end of the power casing 21 of the engine of the present invention is connected to the upper and lower cylinder heads 8 of the head end, and the cylinder head 8 of the first, middle and rear ends and the cylinder block 12 of the first, middle and rear ends are bolted 9 Fasten. The upper and lower cylinder heads 8 of the first, middle, and rear ends are respectively provided with a lubricating oil distribution pipe 23 and a lubricating oil discharge pipe 38. The lubricating oil distribution pipe 23 is connected to the external lubricating oil filler pipe 44, and the lubricating oil discharge pipe 38 is connected to the internal lubricating oil circulating oil inlet pipe 42. A lubricating oil passage pipe 7 is disposed on each of the lubricating oil distribution pipe 23 and the lubricating oil discharge pipe 38. The liquid-gas outer casing 27 is fastened to the bottom end of the power casing 21 via a liquid-gas outer casing bolt 58.

Effect of the invention

The engine of the present invention uses high-pressure liquid and high-pressure air as power to push the axial, axial, and flywheel vortex rotors of the first, middle, and rear ends to rotate at a high speed, and the rotational speed reaches 12,000 rpm. It runs smoothly, with low noise and high power. The utility model has the advantages of compact structure, small volume, strong sealing property, good heat dissipation and cooling effect, no special requirements on manufacturing materials, and low cost. It is suitable for use as a prime mover for various vehicles such as airplanes, trains, ships, automobiles, and power generation and agricultural machinery.

Claims

1. A hydraulic air jet jet flywheel vortex rotor high speed engine, characterized in that a main shaft (1) of a power part is fastened to a power casing (21) via a bearing sleeve (6), and a tail end of the power casing (21) is provided An axial flywheel housing (18) with an exhaust pipe (22) and a liquid gas portion at the bottom end, and a turbo fan (3) and a generator (4) are integrally fastened to the front end of the main shaft (1), and are provided with The air pump (14) of the heat pipe (16) is provided with heat dissipation

The lubricating oil pump (60) of the tube (16) is connected to form a combined pump, and the other two liquid pumps (14) respectively provided with the heat pipe (16) are connected to form another combined pump, at least two combined pumps and at least three axial flows. Flywheel vortex rotor (11)

Adjacent, and respectively fastened to the main shaft (1), the end of the main shaft (1) is provided with an axial flow flywheel (19) connected to the starter (56), and the liquid gas pump (14) and the lubricating oil pump (60) are respectively The fixing frame (17) is connected to the pump casing (15), the pump casing (15) is connected to the cylinder block (12), and the cylinder block (12) is provided with a cylinder head (8).

2. An engine according to claim 1 wherein the liquid-gas pump (14) is provided by an external draining air passage (54),

begging

The inner drain air passage (53), the vane (51) and the liquid-gas pump rotor (50) provided with the pressure rail (52) are connected in sequence.

3. The engine according to claim 1, characterized in that the upper and lower ends of the liquid gas pump (14) and the upper and lower ends of the lubricating oil pump (60) are respectively connected to the heat pipe (16) via the heat pipe connection member (55). The liquid gas filter (30) and the lubricating oil filter (61) respectively provided with the sealing cover (29) are respectively connected to the liquid gas pump (14) and the lubricating oil pump (60) through the pipeline.

4. The engine according to claim 1, characterized in that the three axial flow flywheel vortex rotors (11) are respectively provided with high pressure liquid gas nozzles (24), first end high pressure liquid gas nozzles (first), middle and rear ends ( 24) one side and one high pressure circulation pipe (35) provided with an overpressure automatic circulation pipe (28), and left and right lateral storage circulation pipes (33) provided with a partition plate (57), a start valve (34), The two-liquid pump discharge pipe (48) and the heat-dissipating pipe (16) are connected in sequence, and the other side of the first-end pressure liquid-gas nozzle (24) and the first-end pressure liquid gas discharge pipe (40) and the secondary high-pressure circulation pipe ( 32) Connected in turn, the other side of the middle-end high-pressure liquid-gas nozzle (24) is connected in series with the middle-end high-pressure liquid gas discharge pipe (40) and the tertiary high-pressure circulation pipe (26), and the high-pressure liquid gas nozzle (24) at the tail end The other side and the tail end high pressure liquid gas discharge pipe (40), the longitudinal storage circulation pipe (25), the liquid gas communication pipe (49), the external liquid gas inlet pipe (46), and the liquid gas inlet pipe (47) in the tail end , double liquid air pump discharge pipe (48), hydraulic liquid passage pipe (45), first end liquid Inlet pipe (59) are sequentially connected.

The engine according to claim 1 or 4, characterized in that the axial flow flywheel vortex rotor (11) is provided with sealing rings (10) on both sides thereof, and the axial flow flywheel vortex rotor (11) is grooved in the circumference Set from inside to outside The internal heat dissipation air passage (37), the external heat dissipation air passage (36), the cylinder lubrication pipe (13), and the sealing piece (39).

6. The engine according to claim 1, characterized in that the turbofan casing (5) is connected to the upper end upper and lower cylinder heads (8), the first, middle and rear cylinder heads (8) with the first, middle and tail ends End cylinder (12) via bolt

(9) Fasten.

The engine according to claim 1 or 6, wherein the upper, middle and rear end upper and lower cylinder heads (8) are respectively provided with a lubricating oil distribution pipe (23) and a lubricating oil discharge pipe (38). The lubricating oil distribution pipe (23) is connected to the outer lubricating oil filler pipe (44), the lubricating oil discharge pipe (38) is connected to the inner lubricating oil circulating oil inlet pipe (42), the lubricating oil distributing pipe (23), and the lubricating oil discharge pipe ( 38) A lubricating oil passage tube (7) is respectively disposed on the upper side.

8. The engine according to claim 3, characterized in that the bottom of the liquid gas filter (30) and the lubricating oil filter (61) are respectively provided with a drain bolt (31).

9. An engine according to claim 1 wherein the liquid-gas enclosure (27) is secured to the bottom end of the power enclosure (21) via a liquid-gas enclosure bolt (58).