CN115059542A - Integrated high-efficiency auxiliary power station system - Google Patents

Integrated high-efficiency auxiliary power station system Download PDF

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Publication number
CN115059542A
CN115059542A CN202210692671.3A CN202210692671A CN115059542A CN 115059542 A CN115059542 A CN 115059542A CN 202210692671 A CN202210692671 A CN 202210692671A CN 115059542 A CN115059542 A CN 115059542A
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CN
China
Prior art keywords
crankshaft
oil
piston
power station
auxiliary power
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Pending
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CN202210692671.3A
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Chinese (zh)
Inventor
吴晗
缪升
谢亮
王字满
李向荣
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Beijing Institute of Technology BIT
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Beijing Institute of Technology BIT
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Priority to CN202210692671.3A priority Critical patent/CN115059542A/en
Publication of CN115059542A publication Critical patent/CN115059542A/en
Pending legal-status Critical Current

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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B63/00Adaptations of engines for driving pumps, hand-held tools or electric generators; Portable combinations of engines with engine-driven devices
    • F02B63/04Adaptations of engines for driving pumps, hand-held tools or electric generators; Portable combinations of engines with engine-driven devices for electric generators
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B23/00Other engines characterised by special shape or construction of combustion chambers to improve operation
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B25/00Engines characterised by using fresh charge for scavenging cylinders
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B75/00Other engines
    • F02B75/02Engines characterised by their cycles, e.g. six-stroke
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B75/00Other engines
    • F02B75/16Engines characterised by number of cylinders, e.g. single-cylinder engines
    • F02B75/18Multi-cylinder engines
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B75/00Other engines
    • F02B75/16Engines characterised by number of cylinders, e.g. single-cylinder engines
    • F02B75/18Multi-cylinder engines
    • F02B75/24Multi-cylinder engines with cylinders arranged oppositely relative to main shaft and of "flat" type
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02KDYNAMO-ELECTRIC MACHINES
    • H02K7/00Arrangements for handling mechanical energy structurally associated with dynamo-electric machines, e.g. structural association with mechanical driving motors or auxiliary dynamo-electric machines
    • H02K7/18Structural association of electric generators with mechanical driving motors, e.g. with turbines
    • H02K7/1807Rotary generators
    • H02K7/1815Rotary generators structurally associated with reciprocating piston engines
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B75/00Other engines
    • F02B75/02Engines characterised by their cycles, e.g. six-stroke
    • F02B2075/022Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle
    • F02B2075/025Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle two
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B75/00Other engines
    • F02B75/16Engines characterised by number of cylinders, e.g. single-cylinder engines
    • F02B75/18Multi-cylinder engines
    • F02B2075/1804Number of cylinders
    • F02B2075/1824Number of cylinders six

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • Supercharger (AREA)

Abstract

The invention provides an integrated high-efficiency auxiliary engine power station system with high compactness, high reliability and low oil consumption. The device comprises a machine body 1, a crank connecting rod mechanism 2, a cylinder sleeve 3, a scavenging system 4, an air inlet side crankshaft 5a, an exhaust side crankshaft 5b, a crankshaft synchronous gear 6, a fuel supply system 7 and an outer rotor disc type generator 8; the crank link mechanisms 2 are placed at two ends of the machine body 1 by means of supporting bearings, the crank link mechanisms are divided into a crank link mechanism of an air inlet side crankshaft 5a and a crank link mechanism of an air outlet side crankshaft 5b by air inlet and air outlet, the crank link mechanisms are connected by the crankshaft synchronous gears 6 to rotate relatively, the cylinder sleeve 3 is placed on a stroke path of a piston in the middle of the machine body, the scavenging system 4 is installed on an air inlet and outlet of the cylinder sleeve 3, the fuel supply system 7 is installed on the cylinder sleeve 3 and driven by the crank link mechanisms 2, the outer rotor disc type generator 8 is fixed on the machine body 1, and an outer rotor and the crankshaft synchronous gears 6 are meshed and connected to rotate and transmit power of the crankshafts.

Description

Integrated high-efficiency auxiliary power station system
Technical Field
The invention belongs to the field of internal combustion engines and generators, and particularly relates to an integrated high-efficiency auxiliary engine power station system based on a double-crankshaft opposed-piston two-stroke engine.
Background
Most of power devices of the conventional auxiliary power station system are conventional engines adopting the traditional piston layout, the integral size and the fuel consumption rate of the power station cannot be reduced due to the inherent structure and the operating characteristics of the conventional engine, and the conventional engine runs counter to the design targets of integration, high compactness, high reliability and low fuel consumption required by the auxiliary power station system. Compared with the conventional engine, the opposed piston engine has the advantages of simple structure, less parts and low cost, cancels a complex valve actuating mechanism and a cylinder cover, greatly reduces the weight and the volume of the engine, and can effectively improve the power density of the engine. The elimination of the valve actuating mechanism can also reduce the number of friction pairs, reduce the friction loss and improve the mechanical efficiency of the engine. The elimination of the cylinder cover can reduce the volume of a cooling system, reduce cooling and heat dissipation and improve the heat efficiency of the engine. In addition, two pistons of the engine reciprocate in the same cylinder in opposite directions, so that the engine has good self-balance, small vibration and small running noise. The two-stroke opposed piston engine completes the air exchange process through the air inlet and the air outlet which are arranged at two ends of the cylinder sleeve in a sweeping way by the piston, does not need an air valve, a high-pressure nozzle and a large radiator, and has high reliability and various fuel compatibility. Based on the advantages, the opposed-piston two-stroke engine can be used as an ideal auxiliary power station system power device.
The existing auxiliary power station system adopts two kinetic energy transmission modes, one is that after an engine flywheel is connected with a crankshaft, a transmission mechanism is driven by a gear ring to carry out mechanical transmission, and the kinetic energy is transmitted to a generator, so that the structure is complex, and the cost of the gear ring is high; the other type is that the belt is connected with a damping belt pulley of an engine, a crankshaft of the engine rotates, the damping belt pulley rotates simultaneously, and then the belt pulley of the generator is driven to rotate through the belt, so that the rotor is driven to rotate to realize power generation. This runs contrary to the original purpose of integration and high-compactness of the auxiliary power station. Therefore, an outer rotor disc type generator can be adopted, the stator support is used for fixing the outer rotor on an engine body, the crankshaft synchronous gear is used for driving the outer rotor, and the outer rotor serves as a connecting gear between crankshafts to transmit power, so that the size and energy loss are reduced, and the integration of the engine and the generator is realized.
Disclosure of Invention
Aiming at the defects of the conventional auxiliary power station, the invention provides an integrated high-efficiency auxiliary power station system with high compactness, high reliability and low oil consumption based on a double-crankshaft opposed-piston two-stroke engine.
An integrated high-efficiency auxiliary power station system comprises an engine and a generator; the device comprises a machine body 1, a crank link mechanism 2, a cylinder sleeve 3, a scavenging system 4, an air inlet side crankshaft 5a, an exhaust side crankshaft 5b, a crankshaft synchronous gear 6, a fuel supply system 7 and an outer rotor disc type generator 8; the crank link mechanisms 2 are placed at two ends of the machine body 1 by means of supporting bearings, the crank link mechanisms are divided into a crank link mechanism of an air inlet side crankshaft 5a and a crank link mechanism of an air outlet side crankshaft 5b by air inlet and air outlet, the crank link mechanisms are connected by the crankshaft synchronous gears 6 to rotate relatively, the cylinder sleeve 3 is placed on a stroke path of a piston in the middle of the machine body, the scavenging system 4 is installed on an air inlet and outlet of the cylinder sleeve 3, the fuel supply system 7 is installed on the cylinder sleeve 3 and driven by the crank link mechanisms 2, the outer rotor disc type generator 8 is fixed on the machine body 1, and an outer rotor and the crankshaft synchronous gears 6 are meshed and connected to rotate and transmit power of the crankshafts.
The invention has the beneficial effects that:
1. compared with the conventional engine, the double-crankshaft opposed two-stroke engine has the advantages of simple structure, less parts, low cost, greatly reduced weight and volume, high power density, high mechanical efficiency, high reliability and multiple fuel compatibility.
2. Compared with the conventional generator, the disc generator has the advantages of short axial size, easy manufacture of a multi-pole structure and higher power-mass ratio.
3. The internal stator is fixed on the engine body through the stator support, the crankshaft synchronous gear is used for driving the external rotor, and meanwhile, the external rotor also serves as a connecting gear for transmitting kinetic energy between crankshafts, so that the effect of killing two birds with one stone is achieved, the volume and energy loss are reduced, and the integration of the engine and the generator is realized.
4. According to the invention, the exhaust port is opened firstly to allow waste gas to flow into the exhaust pipe, the air inlet is opened after the crankshaft rotation angle of 15 degrees CA, new air enters the air cylinder to be mixed and replaced with the waste gas to complete scavenging, and the air inlet is closed after the exhaust port is closed and then passes through the crankshaft rotation angle of 6 degrees CA, so that the scavenging is more sufficient, and approximate constant volume combustion within a certain time can be realized;
5. the invention adopts a side double-swirl combustion chamber 15, two sides of the head part are provided with an oil nozzle reserved channel 16, and a cavity formed by two pistons in an opposite way and the top of the piston are used as a combustion area of mixed gas. Because the curvature of the wall surface close to one side of the sharp ridge is larger, the swirl is generated in the inner concave chamber and the outer concave chamber immediately, the combustion speed of the main combustion period is improved, the combustion duration is shortened, and the indicated thermal efficiency of the engine is improved;
6. the engine and the generator can flexibly install one or more outer rotor disc type generators by adjusting the size of the crankshaft synchronous gear, so as to output different voltages; the generator of the invention can also adopt other forms of disk generators, and the stator is still fixed on the machine body.
Drawings
FIG. 1 is a schematic view of the structure of the present invention.
Fig. 2 is a schematic view of the crank mechanism of the present invention.
FIG. 3 is a schematic diagram of an equivalent valve timing of the present invention.
Fig. 4 is a schematic view of the piston structure of the present invention.
FIG. 5 is a schematic view of the fuel injection of the combustion chamber of the present invention.
Fig. 6(a), (b) and (c) are schematic diagrams of the integrated structure of the engine and the generator of the invention.
Detailed Description
In order to make the objects, technical solutions and advantages of the present invention more apparent, the present invention is described in further detail below with reference to the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are merely illustrative of the invention and are not to be construed as limiting the invention.
As shown in FIG. 1, the integrated high-efficiency auxiliary power station system comprises an engine and a generator;
the engine is a double-crankshaft opposed-piston two-stroke engine and is used for power output; the generator is a disc generator for power output.
The device comprises a machine body 1, a crank connecting rod mechanism 2, a cylinder sleeve 3, a scavenging system 4, an air inlet side crankshaft 5a, an exhaust side crankshaft 5b, a crankshaft synchronous gear 6, a fuel supply system 7 and an outer rotor disc type generator 8; the crank link mechanisms 2 are placed at two ends of the machine body 1 by means of supporting bearings, the crank link mechanisms are divided into a crank link mechanism of an air inlet side crankshaft 5a and a crank link mechanism of an air outlet side crankshaft 5b by air inlet and air outlet, the crank link mechanisms are connected by the crankshaft synchronous gears 6 to rotate relatively, the cylinder sleeve 3 is placed on a stroke path of a piston in the middle of the machine body, the scavenging system 4 is installed on an air inlet and outlet of the cylinder sleeve 3, the fuel supply system 7 is installed on the cylinder sleeve 3 and driven by the crank link mechanisms 2, the outer rotor disc type generator 8 is fixed on the machine body 1, and an outer rotor and the crankshaft synchronous gears 6 are meshed and connected to rotate and transmit power of the crankshafts.
In this embodiment, the engine body 1 is a tubular structure with circular openings at both ends, wherein a mounting hole is arranged at a larger opening along the circumference, an inlet and exhaust pipe reserved port and an injector reserved hole are processed at the upper and lower surfaces of the middle part, the cylinder sleeve 3 is accommodated in the middle inner cavity, the injector reserved hole and the cylinder sleeve mounting hole are symmetrically arranged in the center of the cylinder sleeve 3, an air inlet and an air outlet are respectively arranged at both sides of the center, and sealing rings are arranged at both ends.
In the embodiment, the cylinder sleeve 3 adopts a three-cylinder type, and the working sequence of the cylinders is 1-3-2.
As shown in fig. 2, the crank mechanism 2 includes a piston group 9, a connecting rod group 10, and a crank group 11; the crank mechanism 2 is used to convert the linear motion of the piston group 9 into the rotation of the crank group 11.
The connecting rod group 10 is composed of a connecting rod body, a connecting rod bush, a connecting rod big end cover and a connecting rod bolt, and is divided into a small end and a big end according to the size of the cylindrical structures at the two ends of the connecting rod body, the small end is connected with the piston group 9 through a piston pin, and the big end is connected with the crankshaft group 11 through a crank pin.
As shown in fig. 3, the crank set 11 is composed of crankshafts and synchronous gears 6, the crankshafts are installed at two ends of the machine body and are connected through the synchronous gears 6 and the outer rotor disc type motor 8 which are installed at the same side to ensure synchronous rotation, and the rotation is kept in phase difference. The working process is as follows: the exhaust port is opened firstly to allow waste gas to flow into the exhaust pipe, the air inlet is opened after the crankshaft rotation angle of 15 degrees CA, new air enters the air cylinder to be mixed with the waste gas and is replaced to complete scavenging, and the air inlet is closed after the exhaust port is closed and then is rotated by the crankshaft rotation angle of 6 degrees CA, so that the scavenging is more sufficient, and approximate constant volume combustion within a certain time can be achieved.
As shown in fig. 4, the piston assembly 8 includes a piston body 12, a piston pin 13, an oil ring 14 and a gas ring 15, a side-mounted double-swirl combustion chamber 16 is adopted, oil nozzle reserve channels 17 are reserved on two sides of a head, and a cavity formed by two pistons in opposite directions and the top of the piston are used as a combustion area of mixed gas; the piston pin 13 is fixed on a piston pin hole of the piston body 12, the oil ring 14 and the gas ring 15 are fixed on a piston ring groove, and the side double-swirl combustion chamber 16 and the two-side oil nozzle reserved channels 17 are arranged at the top of the piston body 12; the crank connecting rod mechanism 2 is sleeved on a piston pin 13 through a connecting rod small end of a connecting rod group 10 to drive the piston group 8 to do reciprocating linear motion, an oil ring 14 is used for scraping redundant engine oil on a cylinder, an air ring 15 seals combustible mixed gas in a combustion chamber, and an oil injector is circumferentially arranged on an oil nozzle reserved passage 17 to inject oil to the combustion chamber 16.
As shown in fig. 5, the side double swirl combustion chamber comprises an inner concave chamber 18, a pointed ridge 19 and an outer concave chamber 20, and fig. 5 shows the right half of the combustion chamber; the injector 21 sprays the oil mist to the pistons on both sides, and when the oil mist hits the pointed ridges 19, the oil mist is immediately divided into two oil bundles which flow into the concave chamber 18 and the concave chamber 20, respectively; this is because the wall surface near the sharp ridge 19 has a larger curvature, so that the swirl is generated in the inner and outer concave chambers immediately, the combustion speed of the main combustion period is increased, the combustion duration is shortened, and the indicated thermal efficiency of the engine is improved.
In this embodiment, the scavenging system 4 includes an intake manifold, an exhaust turbine, an intercooler and a compressor, the exhaust gas enters the exhaust manifold, the compressor is driven to rotate by the exhaust turbine, and then part of the exhaust gas and the fresh air passing through the compressor enter the intercooler, and then enter the intake manifold and then enter each cylinder according to the working sequence.
In this embodiment, the fuel supply system 6 includes a fuel injector, a common rail pipe, a high-pressure fuel pump, and an electronic control unit, the high-pressure fuel pump is driven by a crankshaft, the high-pressure fuel pump pressurizes fuel and feeds the pressurized fuel into the common rail pipe, the high-pressure fuel is used for accumulating and distributing fuel, pressure fluctuation is reduced, the highest fuel pressure is limited, and the fuel injector is controlled by the electronic control unit to inject fuel into a cylinder.
In the present embodiment, the generator is an external rotor disc generator 8, as shown in fig. 6(a), the internal stator of the external rotor disc generator includes an internal stator core 22 and internal stator windings 23, the internal stator windings are distributed in winding embedding slots on the outer circumference of the internal stator core and connected in a three-phase arrangement, and the center of the internal stator is connected with a stator support 24; as shown in fig. 6(b), the outer surface of the outer rotor of the disc motor is made into a gear shape 25, and is connected with the crankshaft synchronous gear 6 in a meshing way to rotate and transmit the power of the crankshaft, and the inner surface is annularly adhered with a magnetic steel sheet 26; as shown in fig. 6(c), the stator holder 24 is fixed to the machine body by a bolt hole 27 formed in a circumferential direction. The engine and the generator can flexibly install one or more outer rotor disc type generators by adjusting the size of the crankshaft synchronous gear, thereby outputting different voltages; the generator of the invention can also adopt other forms of disk generators, and the stator is still fixed on the machine body.
The present invention is not limited to the above embodiments, and any other changes, modifications, substitutions, combinations, and simplifications which do not depart from the spirit and principle of the present invention should be construed as equivalents and are included in the scope of the present invention.

Claims (13)

1. An integrated high-efficiency auxiliary power station system comprises an engine and a generator; the method is characterized in that: the device comprises a machine body 1, a crank link mechanism 2, a cylinder sleeve 3, a scavenging system 4, an air inlet side crankshaft 5a, an exhaust side crankshaft 5b, a crankshaft synchronous gear 6, a fuel supply system 7 and an outer rotor disc type generator 8; the crank link mechanisms 2 are placed at two ends of the machine body 1 by means of supporting bearings, the crank link mechanisms are divided into a crank link mechanism of an air inlet side crankshaft 5a and a crank link mechanism of an air outlet side crankshaft 5b by air inlet and air outlet, the crank link mechanisms are connected by the crankshaft synchronous gears 6 to rotate relatively, the cylinder sleeve 3 is placed on a stroke path of a piston in the middle of the machine body, the scavenging system 4 is installed on an air inlet and outlet of the cylinder sleeve 3, the fuel supply system 7 is installed on the cylinder sleeve 3 and driven by the crank link mechanisms 2, the outer rotor disc type generator 8 is fixed on the machine body 1, and an outer rotor and the crankshaft synchronous gears 6 are meshed and connected to rotate and transmit power of the crankshafts.
2. The integrated high-efficiency auxiliary power station system as claimed in claim 1, wherein: the engine body 1 is of a cylindrical structure with circular openings at two ends, wherein a mounting hole is formed in the larger opening along the circumference, an air inlet and exhaust pipe reserved connector and an oil injector reserved hole are machined in the upper surface and the lower surface of the middle of the engine body, and the cylinder sleeve 3 is accommodated in a middle inner cavity.
3. An integrated high efficiency auxiliary power station system as claimed in claim 1 or 2, wherein: the center of the cylinder sleeve 3 is symmetrically provided with an oil sprayer preformed hole and a cylinder sleeve mounting hole, the two sides of the center are respectively provided with an air inlet and an air outlet, and the two ends are provided with sealing rings.
4. An integrated high efficiency auxiliary power station system as claimed in claim 1 or 2, wherein: the cylinder sleeve 3 adopts a three-cylinder type, and the working sequence of the cylinder is 1-3-2.
5. An integrated high efficiency auxiliary power station system as claimed in claim 1 or 2 or 3 or 4 wherein: the crank connecting rod mechanism 2 comprises a piston group 9, a connecting rod group 10 and a crankshaft group 11; the crank mechanism 2 is used to convert the linear motion of the piston group 9 into the rotation of the crank group 11.
6. An integrated high efficiency auxiliary power station system as claimed in claim 5 wherein: the connecting rod group 10 is composed of a connecting rod body, a connecting rod bush, a connecting rod big end cover and a connecting rod bolt, and is divided into a small end and a big end according to the size of the cylindrical structures at the two ends of the connecting rod body, the small end is connected with the piston group 9 through a piston pin, and the big end is connected with the crankshaft group 11 through a crank pin.
7. An integrated high efficiency auxiliary power station system as claimed in claim 5 or 6 wherein: the crankshaft group 11 is composed of a crankshaft and a synchronous gear 6, the crankshaft is arranged at two ends of the machine body, and is connected with an outer rotor disc type motor 8 through the synchronous gear 6 and the outer rotor disc type motor 8 which are arranged at the same side to ensure synchronous rotation, and phase difference is reserved in rotation.
8. An integrated high efficiency auxiliary power station system as claimed in claim 5 or 6 or 7 wherein: the piston group 8 comprises a piston body 12, a piston pin 13, an oil ring 14 and a gas ring 15, a side double-swirl combustion chamber 16 is adopted, oil nozzle reserved channels 17 are reserved on two sides of the head, and a cavity formed by two opposite pistons and the top of the piston are used as a combustion area of mixed gas; the piston pin 13 is fixed on a piston pin hole of the piston body 12, the oil ring 14 and the gas ring 15 are fixed on a piston ring groove, and the side double-swirl combustion chamber 16 and the two-side oil nozzle reserved channels 17 are arranged at the top of the piston body 12; the crank connecting rod mechanism 2 is sleeved on a piston pin 13 through a connecting rod small end of a connecting rod group 10 to drive a piston group 8 to do reciprocating linear motion, an oil ring 14 is used for scraping redundant engine oil on a cylinder, an air ring 15 seals combustible mixed gas in a combustion chamber, and an oil injector is circumferentially arranged on an oil injection nozzle reserved passage 17 to inject oil to the combustion chamber 16.
9. The integrated high-efficiency auxiliary power station system of claim 8, wherein: the side double swirl combustion chamber comprises an inner concave chamber 18, a pointed ridge 19 and an outer concave chamber 20, and the right half of the combustion chamber is shown in FIG. 5; the injector 21 injects the oil mist towards the pistons on both sides and, when the mist hits the pointed ridge 19, it is immediately divided into two oil jets which flow towards the concave chamber 18 and the concave chamber 20, respectively.
10. An integrated high efficiency auxiliary power station system as claimed in claim 1 or 2 or 3 or 4 wherein: the scavenging system 4 comprises an air inlet manifold, an exhaust turbine, an intercooler and a compressor, wherein exhaust gas enters the exhaust manifold, the compressor is driven to rotate by the exhaust turbine, and then part of the exhaust gas and fresh air passing through the compressor enter the intercooler and then enter the air inlet manifold and then enter each cylinder according to the working sequence.
11. An integrated high efficiency auxiliary power station system as claimed in claim 1 or 2 or 3 or 4 wherein: the fuel oil supply system 6 comprises an oil injector, a common rail pipe, a high-pressure oil pump and an electric control unit, wherein the high-pressure oil pump is driven by a crankshaft, oil is pressurized and sent into the common rail pipe for accumulating and distributing fuel oil, pressure fluctuation is reduced, the highest fuel oil pressure is limited, and the oil injector is controlled by the electric control unit to inject oil into a cylinder.
12. An integrated high efficiency auxiliary power station system as claimed in claim 1 or 2 or 3 or 4 wherein: the inner stator of the outer rotor disc type motor comprises an inner stator iron core 22 and an inner stator winding 23, wherein the inner stator winding is distributed in a winding embedding slot on the outer circumference of the inner stator iron core and connected according to three-phase arrangement, and the center of the inner stator is connected with a stator bracket 24.
13. An integrated high efficiency auxiliary power station system as claimed in claim 1 or 2 or 3 or 4 wherein: the outer surface of the outer rotor of the disc type motor is made into a gear shape 25, the gear is meshed with the crankshaft synchronous gear 6 to rotate and transmit the power of the crankshaft, and the inner surface is annularly adhered with a magnetic steel sheet 26.
CN202210692671.3A 2022-06-17 2022-06-17 Integrated high-efficiency auxiliary power station system Pending CN115059542A (en)

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Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1280244A (en) * 1999-07-12 2001-01-17 本田技研工业株式会社 Engine drive device
US20040079299A1 (en) * 2002-07-12 2004-04-29 Pearson Motor Company Limited Lightweight four-stroke engine
CN103016150A (en) * 2012-12-26 2013-04-03 北京理工大学 Balance type range extender engine
CN105240120A (en) * 2014-07-02 2016-01-13 北京理工大学 Horizontally-opposed balance type gasoline range extender and operation method thereof
DE102014115043A1 (en) * 2014-10-16 2016-04-21 Obrist Technologies Gmbh generator
CN106837519A (en) * 2017-03-15 2017-06-13 中北大学 A kind of opposed pistons two stroke diesel engine swirl combustion system
DE102017200924A1 (en) * 2017-01-20 2018-07-26 Bayerische Motoren Werke Aktiengesellschaft Opposed piston engine

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1280244A (en) * 1999-07-12 2001-01-17 本田技研工业株式会社 Engine drive device
US20040079299A1 (en) * 2002-07-12 2004-04-29 Pearson Motor Company Limited Lightweight four-stroke engine
CN103016150A (en) * 2012-12-26 2013-04-03 北京理工大学 Balance type range extender engine
CN105240120A (en) * 2014-07-02 2016-01-13 北京理工大学 Horizontally-opposed balance type gasoline range extender and operation method thereof
DE102014115043A1 (en) * 2014-10-16 2016-04-21 Obrist Technologies Gmbh generator
DE102017200924A1 (en) * 2017-01-20 2018-07-26 Bayerische Motoren Werke Aktiengesellschaft Opposed piston engine
CN106837519A (en) * 2017-03-15 2017-06-13 中北大学 A kind of opposed pistons two stroke diesel engine swirl combustion system

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