CN106939830B - Heavy oil aviation rotary engine - Google Patents
Heavy oil aviation rotary engine Download PDFInfo
- Publication number
- CN106939830B CN106939830B CN201710310784.1A CN201710310784A CN106939830B CN 106939830 B CN106939830 B CN 106939830B CN 201710310784 A CN201710310784 A CN 201710310784A CN 106939830 B CN106939830 B CN 106939830B
- Authority
- CN
- China
- Prior art keywords
- scribing
- heavy oil
- rotary engine
- needle
- end cap
- 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.)
- Active
Links
- 239000000295 fuel oil Substances 0.000 title claims description 64
- 239000010687 lubricating oil Substances 0.000 claims abstract description 17
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 27
- 230000006835 compression Effects 0.000 claims description 17
- 238000007906 compression Methods 0.000 claims description 17
- 238000002485 combustion reaction Methods 0.000 claims description 13
- 229910052742 iron Inorganic materials 0.000 claims description 12
- 239000000446 fuel Substances 0.000 claims description 8
- 230000000149 penetrating effect Effects 0.000 claims description 5
- 239000000203 mixture Substances 0.000 claims description 4
- 239000007921 spray Substances 0.000 claims description 3
- 238000009434 installation Methods 0.000 claims description 2
- 238000005461 lubrication Methods 0.000 abstract description 7
- 238000007789 sealing Methods 0.000 abstract description 7
- 230000005611 electricity Effects 0.000 description 5
- 238000000034 method Methods 0.000 description 4
- 230000000694 effects Effects 0.000 description 3
- 238000012423 maintenance Methods 0.000 description 3
- 239000003921 oil Substances 0.000 description 3
- 235000010599 Verbascum thapsus Nutrition 0.000 description 2
- 244000178289 Verbascum thapsus Species 0.000 description 2
- 238000005119 centrifugation Methods 0.000 description 2
- 239000008246 gaseous mixture Substances 0.000 description 2
- 239000000314 lubricant Substances 0.000 description 2
- 230000001050 lubricating effect Effects 0.000 description 2
- 239000003595 mist Substances 0.000 description 2
- 238000005299 abrasion Methods 0.000 description 1
- 238000000889 atomisation Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000002347 injection Methods 0.000 description 1
- 239000007924 injection Substances 0.000 description 1
- 239000011505 plaster Substances 0.000 description 1
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
- F02B53/00—Internal-combustion aspects of rotary-piston or oscillating-piston engines
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01M—LUBRICATING OF MACHINES OR ENGINES IN GENERAL; LUBRICATING INTERNAL COMBUSTION ENGINES; CRANKCASE VENTILATING
- F01M1/00—Pressure lubrication
-
- 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
- F02F11/00—Arrangements of sealings in combustion engines
- F02F11/007—Arrangements of sealings in combustion engines involving rotary applications
-
- 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
- F02M51/00—Fuel-injection apparatus characterised by being operated electrically
- F02M51/06—Injectors peculiar thereto with means directly operating the valve needle
- F02M51/061—Injectors peculiar thereto with means directly operating the valve needle using electromagnetic operating means
-
- 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
- F02M61/00—Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00
- F02M61/04—Fuel-injectors not provided for in groups F02M39/00 - F02M57/00 or F02M67/00 having valves, e.g. having a plurality of valves in series
- F02M61/10—Other injectors with elongated valve bodies, i.e. of needle-valve type
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/12—Improving ICE efficiencies
Abstract
Can axially and radially elastic compensating sealing scribing be made of the two panels scribing that fits together, there is the slot for placing spring above two panels scribing, the spring of the inside supports two scribings simultaneously, the axial elastic force of both direction is provided for scribing, is fitted tightly over scribing axially above rotary engine end cap.There is oilhole on each apex angle of three-apexed rotor, places spring inside oilhole, provide radical elasticity for two panels scribing, two panels scribing is made to can be closely adhered to the inner surface in cylinder body.Can axially and radially elastic compensating sealing scribing, keep rotary engine air-tightness good.Oilhole lubricating oil under the influence of centrifugal force, it guides between the binding face of two scribings, centrifugal force oozes out lubricating oil from the binding face of two panels scribing, provides lubrication for rotor housing and scribing, rotary engine durability can be improved in good lubrication.
Description
Technical field
The present invention relates to one kind can be with the long-life aviation rotary engine of full combustion heavy oil.
Background technique
In currently available technology, for some rotary engine due to poor air-tightness, gas leakage is serious, and rotary engine is caused to light a fire
Difficulty, work efficiency drop.Some and lubricant effect are poor, when running, since insufficient lubrication will cause inner surface of cylinder block and end
The quick frictional dissipation of lid rubbing surface, serious frictional dissipation shorten rotary engine service life, increase use cost.Example
As application No. is described in a kind of end sealing of rotary engine of CN201621059478.2 and lubricating arrangement patent for the patent No.
Diaphragm seal, two pieces of outside is rigid seal piece, and centre is flexible sealing fin, and when engine operation, flexible sealing fin is not wear-resisting
Damage, long time running can lose lubricant effect.It is living with roller that application No. is a kind of rotary engine of CN201520785291.X
Roller described in the patent of plug, due to rotor housing inner wall Zhou Chang great, roller perimeter is small, and roller revolving speed is high, when long
Between operate when roller can be seriously worn, so that engine is lost air-tightness.In above two patents, rotor all can be violent with end cap
Friction makes end cap generate frictional dissipation, leads to end cap damage replacement, increases maintenance and use cost.
Summary of the invention
The object of the present invention is to provide it is a kind of can sufficiently be atomized, combusting heavy oil fuel, energy saving, air-tightness is good, lubrication
Effect is good, the low rotary engine of use, maintenance cost.Solve the above problem present in background technique.
The technical scheme is that this heavy oil aviation rotary engine by rotary engine body, can be axially and radially
Scribing, lubricating oil centrifugation lubricating system, mixed gas heavy oil injector and the end cap patch composition of elastic compensating sealing.
Can axially and radially elastic compensating sealing scribing be made of the two panels scribing that fits together, above two panels scribing
There is the slot for placing spring, the spring of the inside supports two scribings simultaneously, provides the axial elastic force of both direction for scribing, makes to draw
Piece can be axially fitted tightly over above rotary engine end cap.There are oilhole, lubricating oil on each apex angle of three-apexed rotor
Spring is placed inside hole, provides radical elasticity for two panels scribing, two panels scribing is made to can be closely adhered to the inner surface in cylinder body.It can
With the scribing that axially and radially elastic compensating seals, keep rotary engine air-tightness good.Oilhole is being centrifuged lubricating oil
It under the action of power, guides between the binding face of two scribings, centrifugal force oozes out lubricating oil from the binding face of two panels scribing, is
Rotor housing and scribing provide lubrication, and rotary engine durability can be improved in good lubrication.
Mixed gas heavy oil injector is made of gas chamber, air valve, fuel injector.Mixed gas heavy oil injector is mounted on rotary engine
On cylinder body and on end cap, when rotor compression, the air valve for mixing gas heavy oil injector is opened, and gas compressed enters mixed gas heavy oil spray
Emitter gas chamber.Compression finishes, and air valve is closed, and pressure-air is stored in inside the gas chamber of mixed gas heavy oil injector.At this moment, fuel injector
Heavy oil is sprayed into inside toward gas chamber.As rotor continues to rotate, mix gas heavy oil injector entrance again with rotary engine pressure
The connection of contracting chamber, compression chamber the inside air are in low-pressure state, mix gas heavy oil injector air valve and open, the high pressure gas of gas indoor storage
Body is sprayed into rotary engine together with heavy oil therein is mixed in.Under high-speed flow impact, heavy oil is sufficiently atomized, and makes rotor
Heavy oil inside engine chamber being capable of full combustion.The pressurized gas source of mixed gas heavy oil injector is in rotary engine pressure
Contracting stroke itself does not need other auxiliary air compressor, simplifies rotary engine structure, reduces the weight of rotary engine
Amount.
End cap patch is a thin slice for being attached to rotary engine end cap rubbing surface.When rotary polygonal piston engine is done work, end
Lid long-time and three-apexed rotor friction, end cap can be generated and be seriously worn.It is bonded a patch in end cap rubbing surface, rotates rotor
When with patch friction, no longer with end cap direct friction, end cap no longer wears.When patch is worn, end cap patch can be replaced, is not had to
Rotary engine end cap is replaced, rotary engine use cost is reduced.
Detailed description of the invention
Fig. 1 is the front view of rotor apex angle air-tightness scribing.
Fig. 2 is the top view of rotor apex angle air-tightness scribing.
Fig. 3 is the A-A sectional view of rotor apex angle air-tightness scribing.
Fig. 4 is the cross-sectional view of rotor apex angle and air-tightness scribing.
Fig. 5 is the cross-sectional view of rotor and lubricating oil duct.
Fig. 6 is the A-A section of rotor and lubricating oil duct.
Fig. 7 is that high pressure mixes gas heavy oil atomizing injector.
Fig. 8 is that high pressure mixes gas heavy oil atomizing injector and is mounted on course of work when engine end covers.
Fig. 9 is course of work when the mixed gas heavy oil atomizing injector of high pressure is mounted on engine cylinder body.
Figure 10 is wear-resisting patch and the end cover of engine being attached to above end cover of engine.
Figure 11 is that end cover of engine fits together with patch.
Specific embodiment
Invention is further described in detail with reference to the accompanying drawings and detailed description.
Fig. 1 describes the air-tightness scribing 1 on 6 apex angle of three-apexed rotor, and scribing 1 has fluting 3 above, and the inside is equipped with axis
To spring 4.
Fig. 2 describes the scribing 1 and scribing 2 to fit together, and the axle spring 4 of 3 the inside of fluting is scribing 1 and scribing
2 provide negative side's elastic force in the axial direction, contact scribing 1 and scribing 2 closely with end cap 20, make between scribing and end cover of engine 20
Air-tightness is good.
Fig. 3 describes scribing 1 and scribing 2 fits together, and has the gap between two scribing binding faces, and lubricating oil can be with
It flows therethrough, the friction between scribing and cylinder body 17 provides lubrication, and arrow refers to the flow direction of lubricating oil.
Fig. 4 describes an apex angle of three-apexed rotor 6, and scribing 1 and scribing 2 provide axial elastic force by axle spring 4, makes
There is good air-tightness between scribing and end cap.Three-apexed rotor 6 has lubricating oil duct 7 above, after lubricating oil flows therethrough, centrifugation
Power makes lubricating oil flow to the gap between scribing, flows out from scribing top, provides profit between scribing and the inner surface of cylinder body 17
It is sliding, increase rotary engine service life.There is radial spring 5 inside lubricating oil duct 7, provide radical elasticity for scribing, makes to draw
Piece and cylinder body 17 are in close contact, and are made have good air-tightness between scribing and cylinder body 17, are kept rotary engine starting performance good, work
Make high-efficient.
Fig. 5 describes three-apexed rotor 6.
Fig. 6 describes the A-A sectional view of three-apexed rotor 6.The each apex angle of three-apexed rotor 6 has lubricating oil duct 7, the inside
Radial spring 5 is installed.
Fig. 7 describes high pressure and mixes gas heavy oil atomizing injector 18.Needle 9, the top of needle 9 are installed inside shell 8
Portion is male-tapered valve 10, and needle 9 is equipped with return spring 11 above, and 9 tail portion of needle is equipped with dynamic iron 13, moves iron 13 by electromagnetism
Coil 14 controls, and limiting card 24 controls the actuating length of needle 9.It is gas chamber 12 inside shell 8.Shell 8 is equipped with heavy oil above
Fuel injector 15.High pressure is mixed gas heavy oil atomizing injector 18 and is mounted in engine penetrating hole 16.High pressure mixes the injection of gas heavy oil atomizing
Device 18 is mounted on above end cap 20, and required source of high-pressure air has no need to install pneumatics in rotary engine compression stroke
Machine gas supply, simplifies structure, alleviates weight.
Fig. 8 describes high pressure and mixes gas heavy oil atomizing injector 18, is mounted on the work of end cap 20 sprayed into above hole 16
Process.
Fig. 8 a, rotor 6 rotate, and compression chamber enters air and compressed, and high pressure mixes the electromagnetic wire of gas heavy oil injector 18
It enclosing to electricity, moves 13 compression retracteding position spring 11 of iron, male-tapered valve 10 is opened in the movement of needle 9, as three-apexed rotor 6 rotates, compression
Intracavitary air pressure increases, and compressed air enters the gas chamber 12 that high pressure mixes gas heavy oil injector 18.
Fig. 8 b, rotor 6 rotate, and pressure-air enters high pressure and mixes gas heavy oil injector 18, and electromagnetic coil 14 powers off, outer cone
Shape valve 10 is closed, and pressure-air is stored in gas chamber 12.
Fig. 8 c, at this moment, heavy oil fuel injector 15 spray into heavy oil into air storage chamber 12, and heavy oil and pressure-air are atomized mixed for the first time
It closes.
Fig. 8 d, rotor 6 continue to rotate, and engine entrance 16 is connected to compression chamber again, and the air in compression chamber
In low-pressure state, high pressure mixes the electromagnetic coil 14 of gas heavy oil atomizing injector 18 to electricity, moves 13 compression retracteding position spring 11 of iron, valve
Needle 9 moves, and male-tapered valve 10 is opened, and the pressure-air that heavy oil is mixed in gas chamber 12 passes through engine entrance 16, high speed
Engine compresses chamber is sprayed into, when mixed at high speed gas passes through male-tapered valve 10, due to being inner small and outside big taper, pressure-air is fast
Speed is expanded, and the mist of oil in gaseous mixture is atomized for the second time.It is atomized twice, keeps heavy oil atomizing abundant, improve efficiency of combustion.And
It recycles according to this, in cycles.
Fig. 9 describes high pressure and mixes gas heavy oil atomizing injector 18, is mounted on the work of cylinder body 17 sprayed into above hole 16
Process.When the sum that the mixed gas heavy oil atomizing injector 18 of high pressure is mounted on cylinder body 17 is mounted on above end cap 20, course of work phase
Together.
Fig. 9 a is the rotation of rotor 6, and compression chamber enters air and compressed, and high pressure mixes the electricity of gas heavy oil atomizing injector 18
Magnetic coil moves 13 compression retracteding position spring 11 of iron to electricity, and male-tapered valve 10 is opened in the movement of needle 9, as three-apexed rotor 6 rotates,
Air pressure in compression chamber increases, and compressed air enters the gas chamber 12 that high pressure mixes gas heavy oil atomizing injector 18.
Fig. 9 b pressure-air enters high pressure and mixes gas heavy oil atomizing injector 18, and electromagnetic coil 14 powers off, male-tapered valve 10
It closes, pressure-air is by storage gas chamber 12.
At this moment, 15 oil spout of heavy oil fuel injector, atomization mixes heavy oil Fig. 9 c for the first time with pressure-air.
Fig. 9 d rotor 6 continues to rotate, and engine entrance 16 is connected to compression chamber again, and at the air in compression chamber
In low-pressure state, high pressure mixes the electromagnetic coil 14 of gas heavy oil atomizing injector 18 to electricity, moves 13 compression retracteding position spring 11 of iron, valve
Male-tapered valve 10 is opened in the movement of needle 9, the pressure-air of heavy oil is mixed in gas chamber 12 by engine entrance 16, high speed is sprayed
Enter engine compresses chamber, when mixed at high speed gas passes through male-tapered valve 10, due to being inner small and outside big taper, pressure-air is quick
It expands, the mist of oil in gaseous mixture is atomized for the second time.It is atomized twice, keeps heavy oil atomizing abundant, improve efficiency of combustion.And according to this
Circulation, in cycles.
Figure 10 describes the end cap patch 19 and end cap 20 of rotary engine.
The end cap patch 19 of Figure 10 a rotary engine.The end cap of Figure 10 b rotary engine.The end cap of rotary engine pastes
The end cap rubbing surface shape of piece 19 and rotary engine matches, and has air intake duct 21, axis hole 22, screw hole 23.
Figure 11 describes the A-A that the end cap patch 19 of rotary engine and the end cap 20 of rotary engine are bonded together and cuts open
Face figure.The end cap patch 19 of rotary engine can generate abrasion in rotary engine work operating, installation end lid plaster 19 with
Afterwards, the end cap 20 of rotary engine is no longer directly contacted with the side of three-apexed rotor 6, and end cap 20 will not be worn.Three-apexed rotor 6
It can directly be contacted with end cap patch 19, and generate frictional dissipation, after 19 friction damage of end cap patch, so that it may only change end cap
Patch 19 reduces rotary engine use and maintenance cost.
Claims (9)
1. one kind can be with the long-life aviation rotary engine of full combustion heavy oil, the scribing one and scribing two to fit together,
Axle spring (4) inside fluting (3) is that scribing one and scribing two provide negative side's elastic force in the axial direction, keeps scribing one and scribing two tight
It is close to be contacted with end cap (20), keep the air-tightness between scribing and end cover of engine (20) good, has diameter inside lubricating oil duct (7)
To spring (5), radical elasticity is provided for scribing, scribing and cylinder body (17) is in close contact, makes to have between scribing and cylinder body (17)
Good air-tightness is equipped with needle (9) inside shell (8), and the top of needle (9) is male-tapered valve (10), needle (9)
It being equipped with above return spring (11), needle (9) tail portion is equipped with dynamic iron (13), and it moves iron (13) and is controlled by electromagnetic coil (14),
Limiting card (24) controls the actuating length of needle (9), is gas chamber (12) inside shell (8), and shell (8) is equipped with heavy oil spray above
Oily device (15), high pressure are mixed gas heavy oil atomizing injector (18) and are mounted in engine penetrating hole (16), and high pressure mixes gas heavy oil atomizing
Injector (18) is mounted on end cap (20) above, in addition required source of high-pressure air is not needed in rotary engine compression stroke
Air compressor machine gas supply is installed, the end cap patch (19) of rotary engine and the end cap rubbing surface shape of rotary engine match, all
Have air intake duct (21), axis hole (22), screw hole (23), it is characterised in that high pressure mixes gas heavy oil atomizing injector (18) shell (8)
The inside is equipped with needle (9), and the top of needle (9) is male-tapered valve (10), and needle (9) is equipped with return spring above
(11), needle (9) tail portion is equipped with dynamic iron (13), moves iron (13) and is controlled by electromagnetic coil (14), limiting card (24) controls needle
(9) actuating length, shell (8) the inside are gas chamber (12), and shell (8) is equipped with heavy oil fuel injector (15) above, one He of scribing
Scribing two fits together, and the axle spring (4) inside fluting (3), the end cap patch (19) and rotor of rotary engine starts
The end cap rubbing surface shape of machine matches, and has air intake duct (21), axis hole (22), screw hole (23).
2. according to claim 1 can be with the long-life aviation rotary engine of full combustion heavy oil, it is characterised in that turn
Sub (6) have lubricating oil duct (7), and the inside is equipped with radial spring (5), flexibly support scribing one and scribing two, scribing one and scribing
Two provide axial elastic force by axle spring (4).
3. according to claim 1 can be with the long-life aviation rotary engine of full combustion heavy oil, it is characterised in that it is high
It presses and is equipped with needle (9) inside mixed gas heavy oil atomizing injector (18) shell (8), the top of needle (9) is male-tapered valve
(10), needle (9) is equipped with return spring (11) above, and needle (9) tail portion is equipped with dynamic iron (13), moves iron (13) by electromagnetic wire
(14) control is enclosed, it is gas chamber (12) inside shell (8), shell (8) is above that limiting card (24), which controls the actuating length of needle (9),
It is equipped with heavy oil fuel injector (15), high pressure is mixed gas heavy oil atomizing injector (18) and is mounted in engine penetrating hole (16).
4. according to claim 1 can be with the long-life aviation rotary engine of full combustion heavy oil, it is characterised in that it is high
Mixed gas heavy oil atomizing injector (18) is pressed, is mounted on the penetrating hole (16) of end cap (20) above.
5. according to claim 1 can be with the long-life aviation rotary engine of full combustion heavy oil, it is characterised in that it is high
Mixed gas heavy oil atomizing injector (18) is pressed, is mounted on the penetrating hole (16) of cylinder body (17) above.
6. according to claim 1 can be with the long-life aviation rotary engine of full combustion heavy oil, it is characterised in that draw
Piece one and scribing two have the fluting (3) of installation spring (4) above.
7. according to claim 1 can be with the long-life aviation rotary engine of full combustion heavy oil, it is characterised in that shell
It is equipped with needle (9) inside body (8), the top of needle (9) is male-tapered valve (10).
8. according to claim 1 can be with the long-life aviation rotary engine of full combustion heavy oil, it is characterised in that turn
The end cap patch (19) of sub- engine and the end cap rubbing surface shape of rotary engine match, and have air intake duct (21), axis hole
(22), screw hole (23).
9. according to claim 1 can be with the long-life aviation rotary engine of full combustion heavy oil, it is characterised in that turn
The end cap patch (19) of sub- engine and the end cap (20) of rotary engine fit together the mechanical structure of composition.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710310784.1A CN106939830B (en) | 2017-05-05 | 2017-05-05 | Heavy oil aviation rotary engine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710310784.1A CN106939830B (en) | 2017-05-05 | 2017-05-05 | Heavy oil aviation rotary engine |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN106939830A CN106939830A (en) | 2017-07-11 |
| CN106939830B true CN106939830B (en) | 2019-04-05 |
Family
ID=59464090
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710310784.1A Active CN106939830B (en) | 2017-05-05 | 2017-05-05 | Heavy oil aviation rotary engine |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106939830B (en) |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110131036B (en) * | 2019-04-15 | 2021-02-12 | 江苏大学 | Lubricating system of rotary engine |
| CN110318907A (en) * | 2019-07-22 | 2019-10-11 | 西安方霖动力科技有限公司 | Rotary engine end cover structure, spray processes and application |
| US11905836B1 (en) * | 2023-06-08 | 2024-02-20 | Pratt & Whitney Canada Corp. | Rotary engine with single dual-fuel injector |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3807367A (en) * | 1970-03-16 | 1974-04-30 | Daimler Benz Ag | Rotary piston internal combustion engine of trochoidal construction |
| US3958538A (en) * | 1972-05-15 | 1976-05-25 | Nissan Motor Co., Ltd. | Gaseous ignition system for internal combustion engine |
| CN106368809A (en) * | 2016-10-20 | 2017-02-01 | 北京理工大学 | Tiny rotor with radial sealing piece |
-
2017
- 2017-05-05 CN CN201710310784.1A patent/CN106939830B/en active Active
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3807367A (en) * | 1970-03-16 | 1974-04-30 | Daimler Benz Ag | Rotary piston internal combustion engine of trochoidal construction |
| US3958538A (en) * | 1972-05-15 | 1976-05-25 | Nissan Motor Co., Ltd. | Gaseous ignition system for internal combustion engine |
| CN106368809A (en) * | 2016-10-20 | 2017-02-01 | 北京理工大学 | Tiny rotor with radial sealing piece |
Also Published As
| Publication number | Publication date |
|---|---|
| CN106939830A (en) | 2017-07-11 |
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