CN106979070A - Water-cooled vertical single cylinder diesel engine with disjunctor airframe structure - Google Patents
Water-cooled vertical single cylinder diesel engine with disjunctor airframe structure Download PDFInfo
- Publication number
- CN106979070A CN106979070A CN201710136998.1A CN201710136998A CN106979070A CN 106979070 A CN106979070 A CN 106979070A CN 201710136998 A CN201710136998 A CN 201710136998A CN 106979070 A CN106979070 A CN 106979070A
- Authority
- CN
- China
- Prior art keywords
- disjunctor
- cylinder
- crankcase
- piston
- cooling
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B75/00—Other engines
- F02B75/16—Engines characterised by number of cylinders, e.g. single-cylinder engines
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01L—CYCLICALLY OPERATING VALVES FOR MACHINES OR ENGINES
- F01L1/00—Valve-gear or valve arrangements, e.g. lift-valve gear
- F01L1/02—Valve drive
- F01L1/04—Valve drive by means of cams, camshafts, cam discs, eccentrics or the like
- F01L1/047—Camshafts
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01P—COOLING OF MACHINES OR ENGINES IN GENERAL; COOLING OF INTERNAL-COMBUSTION ENGINES
- F01P5/00—Pumping cooling-air or liquid coolants
- F01P5/10—Pumping liquid coolant; Arrangements of coolant pumps
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01P—COOLING OF MACHINES OR ENGINES IN GENERAL; COOLING OF INTERNAL-COMBUSTION ENGINES
- F01P5/00—Pumping cooling-air or liquid coolants
- F01P5/10—Pumping liquid coolant; Arrangements of coolant pumps
- F01P5/12—Pump-driving arrangements
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02F—CYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
- F02F1/00—Cylinders; Cylinder heads
- F02F1/02—Cylinders; Cylinder heads having cooling means
- F02F1/10—Cylinders; Cylinder heads having cooling means for liquid cooling
- F02F1/16—Cylinder liners of wet type
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02F—CYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
- F02F7/00—Casings, e.g. crankcases or frames
- F02F7/006—Camshaft or pushrod housings
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M59/00—Pumps specially adapted for fuel-injection and not provided for in groups F02M39/00 -F02M57/00, e.g. rotary cylinder-block type of pumps
- F02M59/02—Pumps specially adapted for fuel-injection and not provided for in groups F02M39/00 -F02M57/00, e.g. rotary cylinder-block type of pumps of reciprocating-piston or reciprocating-cylinder type
- F02M59/10—Pumps specially adapted for fuel-injection and not provided for in groups F02M39/00 -F02M57/00, e.g. rotary cylinder-block type of pumps of reciprocating-piston or reciprocating-cylinder type characterised by the piston-drive
- F02M59/102—Mechanical drive, e.g. tappets or cams
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Cylinder Crankcases Of Internal Combustion Engines (AREA)
Abstract
The invention discloses a kind of water-cooled vertical single cylinder diesel engine with disjunctor airframe structure, including block assembly, crankcase, fuel injector, valve actuating mechanism, fuel pump and cooling water pump, block assembly includes the cylinder cap for being cast integrally structure formation disjunctor fuselage, cylinder body and cylinder sleeve, piston is installed in the combustion chamber that inner chamber between cylinder body and cylinder sleeve is formed, piston is connected by connecting rod with the transmission of crankshaft in crankcase, crankshaft two end is separately installed with flywheel and gear train, cooling jacket provided with the covering whole impulse stroke of piston in disjunctor fuselage two side, cooling jacket pipeline connects cooling water pump.The present invention uses disjunctor fuselage, without parts such as cylinder bolt, cylinder pads, eliminates the Joint failure risk and leak Leakage of cylinder bolt, with can explosion pressure in lift cylinder, improve fuel economy and discharge performance；Because cooling jacket completely surrounds the whole movement travel of piston, the cooling effect of piston and cylinder cap is improved.
Description
Technical field
The present invention relates to diesel engine technologies field, especially a kind of water-cooled vertical single cylinder with disjunctor airframe structure
Diesel engine.
Background technology
Electric-controlling injection system being used existing single cylinder diesel, to improve HP, hp/litre, reduction discharge and fuel oil more
Consumption.And use the single cylinder diesel engine of electric-controlling injection system at present to improve HP, hp/litre and properties, it is necessary to
Increase electric-control system and more new atomizer, and corresponding control unit, sensor etc., bring single cylinder diesel to make
Cost is significantly increased, and single cylinder diesel is widely used in farm machinery, being significantly increased of cost can allow consumer hope and
Step.And traditional single cylinder diesel engine, due to foundry engieering limitation, its cylinder cap, cylinder body and cylinder sleeve are generally cast using split
After making, it is connected with integral, the seal using cylinder pad etc is also needed to prevent leakage, in connection procedure, it is more main
Want, because cylinder cap, cylinder body are split production, therefore the cooling jacket of Cooling Water flowing is located at cylinder cover wall and cylinder body respectively
Is connected by pipeline in wall, in cylinder cap and cylinder body junction due in the absence of cooling jacket, therefore the flowing of cooling water can not be covered
The whole movement travel of lid piston, causes the radiating effect of engine undesirable, so as to influence the raising of HP, hp/litre.
The content of the invention
The technical problem to be solved in the present invention is：Overcome deficiency in the prior art that there is disjunctor fuselage knot there is provided one kind
The water-cooled vertical single cylinder diesel engine of structure, allows cooling jacket completely to surround the whole movement travel of piston, to improve hair
The power per liter of cooling effect and engine when motivation works, reaches the purpose of economical and energy saving.
The technical solution adopted for the present invention to solve the technical problems is：A kind of water-cooled vertical with disjunctor airframe structure
Single cylinder diesel engine, including block assembly, crankcase, fuel injector, valve actuating mechanism, fuel pump and cooling water pump, it is described
Block assembly includes cylinder cap, cylinder body and the cylinder sleeve for being cast integrally structure formation disjunctor fuselage, the inner chamber between cylinder body and cylinder sleeve
Piston is installed, piston is connected by connecting rod with the transmission of crankshaft in crankcase, the song in the combustion chamber formed
Axle two ends are separately installed with flywheel and gear train, the two side of the disjunctor fuselage provided with the covering whole impulse stroke of piston
Cooling jacket, described cooling jacket pipeline connection cooling water pump.
Described crankcase includes upper crankcase body and low crankcase, and low crankcase bottom has as oil sump
Inner chamber, the bell housing of Flywheel is provided with positioned at the left side of upper and lower crankcase, and described bell housing has two parts up and down
And the upper and lower crankcase integrally casting of correspondence.
Described fuel pump is arranged on the upper crankcase body of crankcase, and fuel injector pipeline connects fuel pump by fuel oil high pressure
Spray into combustion chamber.
Described cooling water pump is fixed on the cylinder body of disjunctor fuselage, and cooling water pump is connected with detection and judged in cooling water channel
The belt pulley of driving cooling water pump operating is installed on the thermostat of flowed through cooling water temperature, bent axle.
The camshaft that described valve actuating mechanism is put in including, camshaft provided with driving fuel pump fuel pump cam, with
Cam shaft gear, admission cam and the exhaust cam of gear train engaged transmission.
The beneficial effects of the invention are as follows：The present invention by gray iron monoblock cast into integrated machine after one's death, it is no longer necessary to cylinder cap
The parts such as bolt, cylinder pad, it is thus eliminated that between the Joint failure risk of cylinder bolt, and cylinder cap, cylinder body and cylinder pad
Leak Leakage, at the same the disjunctor airframe structure can explosion pressure in lift cylinder, improve fuel economy and discharge performance etc.；
Using the single cylinder diesel of disjunctor fuselage, because cooling jacket can completely surround the whole movement travel of piston, work is improved
The cooling effect of plug and cylinder cap, therefore more fuel oils can be sprayed to improve the power per liter of engine.
Brief description of the drawings
The present invention is further described with reference to the accompanying drawings and examples.
Fig. 1 is the structural representation of the present invention.
Fig. 2 is Fig. 1 left view.
Fig. 3 is the cross section structure diagram of the present invention.
Fig. 4 is cross section structure diagram and the signal of pistons work stroke of disjunctor fuselage.
Fig. 5 is the structural representation of valve actuating mechanism.
It is bent on the cooling jacket 7. of 1. disjunctor fuselage, 2. cylinder head cover, 3. speed adjusting gear, 4. combustion chamber, 5. piston 6. in figure
The flywheel 13. of 11. connecting rod of axle box 8. low crankcase, 9. bent axle, 10. balance shaft 12. starts the oil filtration of motor 14.
The tensioner of 20. belt pulley of device 15. fuel injector, 16. fuel pump, 17. fuel injector sleeve, 18. cooling water pump, 19. cooling fan 21.
The valve rocker 28. of 26. valve of device 22. valve retainer, 23. inlet manifold, 24. exhaust manifold, 25. valve actuating mechanism 27.
The camshaft of 29. cam shaft gear of valve lifter 30.
Embodiment
Presently in connection with accompanying drawing and preferred embodiment, the present invention is further illustrated.These accompanying drawings are simplified signal
Figure, only illustrates the basic structure of the present invention in a schematic way, therefore it only shows the composition relevant with the present invention.
A kind of water-cooled vertical single cylinder diesel engine with disjunctor airframe structure as shown in Figure 1 to 4, including body
Assembly, crankcase, valve actuating mechanism 25, fuel system and cooling system.
Described block assembly includes being cast integrally cylinder cap, cylinder body and cylinder sleeve that structure forms the disjunctor fuselage 1,
Cylinder cap is provided with cylinder head cover 2, and side of cylinder block is provided with speed adjusting gear 3, the combustion chamber 4 that the inner chamber between cylinder body and cylinder sleeve is formed
Piston 5 is inside installed, the cylinder cap of disjunctor fuselage 1 is constituted, the cooling jacket 6 provided with monoblock type, the cooling in the two side of cylinder body
Water jacket covers the whole impulse stroke of piston 5 about 6.
Crankcase is located at the lower section of combustion chamber 4, and described crankcase is surrounded and constituted by upper crankcase body 7 and low crankcase 8,
Bent axle 9 and balance shaft 10 are installed by bearings in crankcase, piston 5 is connected by connecting rod 11 with bent axle 9, bent axle
9 two ends are separately installed with flywheel 12 and gear train, and gear train is located in the gear chamber of engine cylinder-body, the startup motor of engine
13 drive bent axle 9 to rotate by gear train, while gear train is by driving balance shaft 10, to reduce the reciprocal inertia of engine
Power, lifts engine NVH performances；There is the inner chamber as oil sump in the bottom of low crankcase 8 simultaneously, positioned at upper and lower bent axle
The left side of casing 7,8 is provided with the bell housing of Flywheel 12, described bell housing be divided into above and below two parts and the upper and lower song of correspondence
Axle box 7,8 integrally castings, the Joint failure risk of bell housing and crankcase can be reduced with this.
Described fuel system includes fuel tank, oil filter 14, fuel injector 15 and fuel pump 16 with Unit injector,
Fuel pump 16 is installed on the upper crankcase body 7 of crankcase, and fuel injector 15 is arranged on the fuel injector with the integrally casting of disjunctor fuselage 1
In set 17, the fuel oil exported from fuel tank enters fuel pump 16 after being filtered through oil filter 14, and fuel pump 16 passes through fuel pipe
To the conveying high-pressure fuel oil of fuel injector 15, fuel injector 15 sprays into fuel oil in combustion chamber 4 by Unit injector timing, quantitatively.
The cooling system that this engine is set has cooling water pump 18 and cooling fan 19, using Forced water cooling and air-cooled side
Formula is to engine cooling, and the belt pulley 20 on bent axle 9 drives cooling water pump 18 and cooling fan 19 by multi-rib-belt,
Cooling water pump 18 is using being bolted on the cylinder body of disjunctor fuselage 1, and cooling fan 19 is fixed by bolts to the upper song of crankcase
On axle box 7, described cooling jacket 6 is connected with the water cavity pipeline of cooling water pump 18, and the cooling system also has thermostat, makes
Used time judges cooling water temperature height by thermostat, determines whether cooling water needs cold by the radiating of engine radiator
But, while setting swelling device 21 to adjust the elastic of multi-rib-belt in crankcase relevant position.
When the vertical type single-cylinder diesel engine works, the cooling water pump 18 in cooling system is by the belt on bent axle 9
Wheel 20 is driven by multi-rib-belt and operated, and water inlet of the cooling water on cooling water pump 18 is forced to input into cooling jacket 6
In water cavity, cooling water is flowed from lower to upper, and cooling water is led to the water inlet pipe of thermostat by cooling water pipe, if water temperature mistake
Height, then return again to cooling water pump 18 after the engine radiator cooling outside cooling current direction and circulated, if coolant water temperature
Degree is not high, then directly flowing to cooling water pump 18 by thermostat inner flow passage is circulated, and the cooling water circulated will start
The waste heat that machine burning is produced is taken away, because cooling jacket 6 covers the whole impulse stroke of piston 5, that is, covers whole
The surrounding of combustion chamber 4, radiating effect is greatly improved, therefore is conducive to vertical type single-cylinder diesel engine to be substantially improved after power
Thermic load requirement.
As shown in figure 5, described valve actuating mechanism 25 is arranged on by valve retainer 22 on the cylinder cap of disjunctor fuselage 1, including
On the inlet manifold 23 and exhaust manifold 24 that are connected on cylinder cap two side, the camshaft 30 driven by gear train, camshaft 30
The fuel pump cam of driving fuel pump 16, cam shaft gear 29, admission cam and exhaust with gear train engaged transmission are installed
Cam.Camshaft 30 in valve actuating mechanism 25 drives valve rocker 27 by valve lifter 28, and then drives air inlet and exhaust
Valve 26 is moved, and valve 26 is opened or closed in the correct time；Camshaft 30 also drives fuel pump 16 simultaneously, makes fuel pump
Fuel injector 15 is conveyed to after 16 increase fuel pressures.
When vertical type single-cylinder diesel engine is started working, start motor 13 first and switch on power, pass through the He of gear set drive bent axle 9
Flywheel 12 is operated, and valve actuating mechanism 25 drives camshaft 30 to rotate also by gear train engaged transmission cam shaft gear 29, realizes handle
Fresh air timing in inlet manifold 23, in quantitative feeding combustion chamber 4, while fuel pump 16 by the timing of fuel injector 15,
Fuel oil is quantitatively sprayed into combustion chamber 4, the rotation of bent axle 9 moved up and down by connecting rod 11 with piston 5, complete air inlet, compression,
Do manual work, four strokes of exhaust, the gas of engine discharge drains into air outside the exhaust manifold 24, this process realize heat energy to
The conversion of kinetic energy, the kinetic energy of generation is outwards exported by bent axle 9 and flywheel 12.
The present invention is by gray iron monoblock cast into after disjunctor fuselage 1, it is no longer necessary to the parts such as cylinder bolt, cylinder pad,
It is thus eliminated that the leak Leakage between the Joint failure risk of cylinder bolt, and cylinder cap, cylinder body and cylinder pad, should simultaneously
The structure of disjunctor fuselage 1 can explosion pressure in lift cylinder, improve fuel economy and discharge performance etc.；Using the list of disjunctor fuselage 1
Cylinder diesel, because cooling jacket 6 can completely surround the whole movement travel of piston 5, improves the cooling of piston 5 and cylinder cap
Effect, therefore more fuel oils can be sprayed to improve the power per liter of engine, contrasted with existing single cylinder diesel, fuel consumption
Rate is reduced to about 260k/kWh, reduction about 20% by about 320k/kWh；Specific mass is reduced to 8kg/kW by 15kg/kW, is emitted on
A generation can be lifted on the basis of existing state II, is required close to or up the U.S. EPA phase III.
The above embodiments merely illustrate the technical concept and features of the present invention, and its object is to allow person skilled in the art
Scholar can understand present disclosure and be carried out, and it is not intended to limit the scope of the present invention, all according to the present invention
The equivalent change or modification that Spirit Essence is made, should all cover within the scope of the present invention.
Claims (5)
1. a kind of water-cooled vertical single cylinder diesel engine with disjunctor airframe structure, including block assembly, crankcase, oil spout
Device, valve actuating mechanism, fuel pump and cooling water pump, it is characterized in that：Described block assembly is formed including being cast integrally structure
Piston, piston are installed in cylinder cap, cylinder body and the cylinder sleeve of disjunctor fuselage, the combustion chamber that the inner chamber between cylinder body and cylinder sleeve is formed
It is connected by connecting rod with the transmission of crankshaft in crankcase, the crankshaft two end is separately installed with flywheel and gear train, institute
State the cooling jacket provided with the covering whole impulse stroke of piston in the two side of disjunctor fuselage, described cooling jacket pipeline connection
Cooling water pump.
2. the water-cooled vertical single cylinder diesel engine according to claim 1 with disjunctor airframe structure, it is characterized in that：Institute
The crankcase stated includes upper crankcase body and low crankcase, and low crankcase bottom has the inner chamber as oil sump, is located at
The left side of upper and lower crankcase is provided with the bell housing of Flywheel, described bell housing have two parts up and down and correspondence it is upper,
Low crankcase integrally casting.
3. the water-cooled vertical single cylinder diesel engine according to claim 2 with disjunctor airframe structure, it is characterized in that：Institute
The fuel pump stated is arranged on the upper crankcase body of crankcase, and fuel injector pipeline, which connects fuel pump and sprays into fuel oil high pressure, to burn
Room.
4. the water-cooled vertical single cylinder diesel engine according to claim 1 with disjunctor airframe structure, it is characterized in that：Institute
The cooling water pump stated is fixed on the cylinder body of disjunctor fuselage, and cooling water pump is connected with detection and judges to flow through cooling in cooling water channel
The belt pulley of driving cooling water pump operating is installed on the thermostat of coolant-temperature gage, bent axle.
5. the water-cooled vertical single cylinder diesel engine according to claim 1 with disjunctor airframe structure, it is characterized in that：Institute
The camshaft that the valve actuating mechanism stated is put in including, camshaft is provided with the fuel pump cam of driving fuel pump, engaged with gear train
Cam shaft gear, admission cam and the exhaust cam of transmission.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710136998.1A CN106979070A (en) | 2017-03-09 | 2017-03-09 | Water-cooled vertical single cylinder diesel engine with disjunctor airframe structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710136998.1A CN106979070A (en) | 2017-03-09 | 2017-03-09 | Water-cooled vertical single cylinder diesel engine with disjunctor airframe structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106979070A true CN106979070A (en) | 2017-07-25 |
Family
ID=59338280
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710136998.1A Pending CN106979070A (en) | 2017-03-09 | 2017-03-09 | Water-cooled vertical single cylinder diesel engine with disjunctor airframe structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106979070A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109322741A (en) * | 2018-09-26 | 2019-02-12 | 绵阳新晨动力机械有限公司 | A kind of engine assembly |
| CN110454270A (en) * | 2019-08-30 | 2019-11-15 | 百变动力科技(深圳)有限公司 | Water-cooled engine |
| CN113847158A (en) * | 2021-09-10 | 2021-12-28 | 马义礼 | Cylinder of four-stroke internal combustion engine |
| CN114135412A (en) * | 2021-12-17 | 2022-03-04 | 广西玉柴机器股份有限公司 | Cylinder head and crankcase disjunctor structure |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2042632A (en) * | 1979-02-23 | 1980-09-24 | Steyr Daimler Puch Ag | Sound-proofing I.C. Engines |
| JPH10325359A (en) * | 1997-05-23 | 1998-12-08 | Yanmar Diesel Engine Co Ltd | Single cylinder water-cooled engine |
| CN1493782A (en) * | 2002-09-27 | 2004-05-05 | 本田技研工业株式会社 | Four-stroke direct jet engine |
| CN102562353A (en) * | 2012-03-08 | 2012-07-11 | 重庆三华工业有限公司 | Integrated aluminum alloy tank |
| CN103946530A (en) * | 2011-06-22 | 2014-07-23 | Avl里斯脱有限公司 | Internal combustion engine having at least one cylinder |
| US20150053154A1 (en) * | 2012-03-30 | 2015-02-26 | Mahindra And Mahindra Limited | Monoblock Engine |
| CN206957817U (en) * | 2017-03-09 | 2018-02-02 | 斯太尔动力（常州）发动机有限公司 | Water-cooled vertical single cylinder diesel engine with disjunctor airframe structure |
-
2017
- 2017-03-09 CN CN201710136998.1A patent/CN106979070A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2042632A (en) * | 1979-02-23 | 1980-09-24 | Steyr Daimler Puch Ag | Sound-proofing I.C. Engines |
| JPH10325359A (en) * | 1997-05-23 | 1998-12-08 | Yanmar Diesel Engine Co Ltd | Single cylinder water-cooled engine |
| CN1493782A (en) * | 2002-09-27 | 2004-05-05 | 本田技研工业株式会社 | Four-stroke direct jet engine |
| CN103946530A (en) * | 2011-06-22 | 2014-07-23 | Avl里斯脱有限公司 | Internal combustion engine having at least one cylinder |
| CN102562353A (en) * | 2012-03-08 | 2012-07-11 | 重庆三华工业有限公司 | Integrated aluminum alloy tank |
| US20150053154A1 (en) * | 2012-03-30 | 2015-02-26 | Mahindra And Mahindra Limited | Monoblock Engine |
| CN206957817U (en) * | 2017-03-09 | 2018-02-02 | 斯太尔动力（常州）发动机有限公司 | Water-cooled vertical single cylinder diesel engine with disjunctor airframe structure |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109322741A (en) * | 2018-09-26 | 2019-02-12 | 绵阳新晨动力机械有限公司 | A kind of engine assembly |
| CN109322741B (en) * | 2018-09-26 | 2023-12-19 | 绵阳新晨动力机械有限公司 | Engine assembly |
| CN110454270A (en) * | 2019-08-30 | 2019-11-15 | 百变动力科技(深圳)有限公司 | Water-cooled engine |
| CN113847158A (en) * | 2021-09-10 | 2021-12-28 | 马义礼 | Cylinder of four-stroke internal combustion engine |
| CN114135412A (en) * | 2021-12-17 | 2022-03-04 | 广西玉柴机器股份有限公司 | Cylinder head and crankcase disjunctor structure |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN106979070A (en) | Water-cooled vertical single cylinder diesel engine with disjunctor airframe structure | |
| CN102733947B (en) | Contraposition two-stroke engine | |
| CN106224094A (en) | 12 cylinder water-cooled Diesel engines | |
| CN206957817U (en) | Water-cooled vertical single cylinder diesel engine with disjunctor airframe structure | |
| CN102748132A (en) | Mechanical-hydraulic double-power output engine | |
| CN1854493B (en) | Supercharged internal-combustion engine | |
| JP2008248838A (en) | Cam driven exhaust valve operation system for large size two cycle diesel engine | |
| CN101008337A (en) | Turbocharging engine | |
| CN102877932A (en) | Turbo supercharged engine | |
| CN202900406U (en) | Turbocharged engine | |
| CN103993958A (en) | Energy-saving and environment-friendly type high-power locomotive diesel engine | |
| CN103016138A (en) | Turbocharged engine | |
| AU713009B2 (en) | Internal combustion engines | |
| CN205135819U (en) | Variable displacement engine and camshaft holder | |
| CN202900405U (en) | Turbocharged engine | |
| CN1814992A (en) | Piston-type IC engine of continuous variable valve timing and gas-distributing mechanism | |
| CN105697141B (en) | Air-cooled Λ type two-stroke double stopper type diesel supercharging engine | |
| CN103147857B (en) | Engine with horizontally-opposed air cylinder | |
| CN203962154U (en) | A kind of energy saving and environment friendly high-power locomotive diesel engine | |
| CN204082333U (en) | Air-cooled pancake engine in a kind of engine driven supercharging formula | |
| CN201211926Y (en) | Outboard engine by employing internal circulation water-cool engine as power | |
| JP5189069B2 (en) | Cam-driven exhaust valve actuation system for large two-cycle diesel engines | |
| CN201953494U (en) | Engine cylinder head | |
| JP5015975B2 (en) | Cam-driven exhaust valve actuation system for large two-cycle diesel engines | |
| CN2835598Y (en) | Diesel engine |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WD01 | Invention patent application deemed withdrawn after publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20170725 |