CN1104712A - Vortex engine - Google Patents
Vortex engine Download PDFInfo
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- CN1104712A CN1104712A CN 93120586 CN93120586A CN1104712A CN 1104712 A CN1104712 A CN 1104712A CN 93120586 CN93120586 CN 93120586 CN 93120586 A CN93120586 A CN 93120586A CN 1104712 A CN1104712 A CN 1104712A
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- scroll
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- combustion
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Abstract
The vortex engine comprises combustion system, power system composed of dynamic and static vortex disks and connected with combustion system, pressurizing system formed by engagement of dynamic and static vortex disks and lubricating system including rotor pump and lubricant way. The power vortex disk is connected to pressurizing and lubricating systems respectively by more eccentric shafts as power output one. Its advantages include use of different fuels, external combustion, simple structure and small size.
Description
The present invention relates to a kind of motor, particularly a kind of Vortical engine.
At present, in the middle low power scope, the engine structures that use are shuttle in a large number, and the motor of this form is historical long, and manufacturing, use experience are enriched.But reciprocating machine has determined the deficiency of the motor of this form; Complex structure; The intermittent type oil jetting combustion, period of combustion is short, and need complicated combustion system: the inlet and outlet pulsating nature is big for this reason, and inlet and outlet valve complexity needs complicated distribution device; Inertial force is big, vibration and noise are big; Change in torque is big; The limiting factor that improves rotating speed is many; In order to improve horse-power per litre, large and medium-sized motor adopts supercharging technology, pressurization system complex structure etc. (document: " Principles of Internal-Combustion Engine ", Chinese agriculture machinery publishing house, in February, 1981 version).
The objective of the invention is to overcome the shortcoming of above-mentioned prior art, propose a kind of rotary type Vortical engine, it is made up of power system, pressurization system and supplementary equipment, have simple in structure, size is little, characteristics such as component are few, heavy and light amount.
The present invention includes the power system of being made up of moving scroll and fixed scroll that is connected with combustion system, moving scroll utilizes multiple-eccentric shaft to link with pressurization system, lubrication system respectively, and as power output shaft.Said pressurization system comprises one and the joining moving scroll of eccentric shaft and the fixed scroll that is meshed with it.Said lubrication system comprises a rotor pump and lubricating oil path.
Liquid or gaseous fuel and air produce high temperature, high-pressure gas, enter in the power system in combustion system, moving scroll in expansion and the propulsion power system is done plane motion, and drive multiple-eccentric shaft and rotate, drive pressurization system, lubrication system works or external output work with this.Pressurization system is sent into combustion system after sucking compresses fresh air, to improve MAF and horse-power per litre; Lubrication system guarantees the proper functioning of each moving element by oil circuit.
This shows that the present invention has following effect:
1, because when the moving scroll of power system and fixed scroll Plane of action circular movement, form a plurality of active chamber spaced apart from each other, and by core side shifting outside scroll progressively, the volume of active chamber increases gradually, and intake process, inflation process and exhaust process are separated from each other.Therefore, do not need distribution device and inlet and outlet valve; Realize growing continuous burning, period of combustion, realizing complete expansion; But the inertial force complete equilibrium is vibrated little; Combustion gas moves by the central task chamber is outer gradually, reaches complete expansion continuously, therefore pulse little, change in torque is little, noise is low.
2, because pressurization system and power system structural similarity, connect simple, so simplify the structure, component are few, can realize the ultra high speed operation, have improved horse-power per litre.
3, because combustion system is outer burning form, can use pluralities of fuel, as natural gas, petroleum gas, gasoline, diesel oil etc.
Fig. 1 is a sectional structure chart of the present invention.
Fig. 2 is a right elevation of the present invention.
Fig. 3 is the sealed structure chart of pressurization system.
Below in conjunction with accompanying drawing structural principle of the present invention and working principle are done detailed explanation.
Combustion system of the present invention comprises an air preheating chamber 3, configuration one firing chamber 2 reaches the secondary nozzle 4 that is connected with firing chamber 2 in the air preheating chamber 3, dispose primary nozzle 1 and air duct joint 32 on the air preheating chamber 3 respectively, fixed scroll 5 phase configuration of secondary nozzle 4 and power system facing to firing chamber 2.
Said power system comprises one and the fixed scroll 5 of primary nozzle 4 phase configuration, the air outlet of the suction port of fixed scroll 5 and secondary nozzle is connected, dispose moving scroll 6 with fixed scroll 5 engagements, the back side of moving scroll 6 evenly is furnished with multiple-eccentric shaft (being illustrated as three 10,11,12); The back side of moving scroll 6 disposes thermal-protective coating 33 and friction ring 16, and friction ring 16 is embedded on the support 7 by supporting ring 17 and following spring 18 thereof, and support 7 is fixedlyed connected with fixed scroll 5, and eccentric shaft 10,11,12 is bearing on the support 7.
The moving scroll 8 of the other end of eccentric shaft 11 and pressurization system links, dispose the fixed scroll 9 that is fixed on the support 7 with moving scroll 9 engagements, the back side of moving scroll 8 disposes friction ring 41, friction ring 41 is being supported by the supporting ring 27, the spring 28 that are embedded on the support 7, for anti-stop scroll 8 rotations, the back side of moving scroll 8 is furnished with the Oldham's coupling 26 that is bearing on the support 7; The relief opening of fixed scroll 9 is connected with pipe joint 30, and pipe joint 30,32 is connected by pipeline 31.
The oil pump internal rotor 21 of the other end of eccentric shaft 10 and lubrication system links by taper pin 24, said lubrication system comprises an oil pump and corresponding oil circuit, said oil pump comprises that one is fixed on support 7 upper frames 23, the internal rotor 21 that disposes external rotor 22 in the support 23 and be meshed with external rotor 22.Said oil circuit comprises an in-line 19 that is connected with the oil pump oil suction chamber, oil inlet pipe 34, oil inlet pipe 34 (not shown) that is connected with oil cooler, said oil circuit also comprises a flowline connection to subsea 20 that is connected with the oil pump oil-discharging cavity, and oil outlet tube 37, oil outlet tube 37 are connected with lubricating oil path on being arranged in support 7 by pipe joint 28.
In addition, 13,14,15,29 is respectively the needle bearing of corresponding connecting part among the figure, the 35th, the flowline connection to subsea of support 7 lubricating oil paties, the 39th, oil outlet tube also is connected with oil cooler, the 25th, the gland of oil pump, the 36th, the bearing cap of eccentric shaft 12, the 40th, the supporting foot of whole motor, the 41st, the self-lubricating seal ring between moving scroll 8 and the quiet vortex 9.
Burning sprays into firing chamber 2 by primary nozzle 1, fully mix with the air of coming in from air preheating chamber 3, light burning down in the ignition system (not shown), produce high temperature, high-pressure gas, spraying into moving scroll 5 by secondary nozzle 4 is meshing with each other and constitutes a plurality of active chambers, combustion gas is by the central task chamber, move outside expanding gradually, pressure, temperature constantly reduce, side relief opening by fixed scroll 5 enters atmosphere at last, the transformation of energy of combustion gas becomes the kinetic energy of moving scroll 6 and drives multiple-eccentric shaft to rotate output power.In the diagram, three eccentric shafts have identical throw of eccentric, and equal the turning radius of moving scroll 6.Eccentric shaft 10 is the live axle of oil pump, and eccentric shaft 11 is live axles of pressurization system, output power beyond the eccentric shaft 12.
Moving scroll 8 meshes a plurality of active chambers that constitute pressurization systems with fixed scroll 9, by the side air inlet of fixed scroll 9, and progressively moves to the center, and compression discharged by the central row pore of fixed scroll 9 at last, and oil-piping 31 is connected with air preheating chamber 3.
Claims (3)
1, Vortical engine comprises a combustion system, the power system that is connected with combustion system, and the pressurization system and the lubricant passage way system that are driven by power system.The invention is characterized in: said power system comprises one and the fixed scroll (5) of secondary nozzle (4) phase configuration of combustion system, the moving scroll (6) that is meshed with fixed scroll (5), the back side of moving scroll (6) evenly is furnished with the multiple-eccentric shaft that can link with pressurization system, lubrication system respectively and export as power respectively.Said pressurization system comprise one with joining moving scroll of eccentric shaft (8) and the fixed scroll (9) that is meshed with moving scroll (8), the central row gas port of fixed scroll (9) is connected with the air preheating chamber (3) of combustion system by pipeline (31).
2, Vortical engine according to claim 1 is characterized in that, the back of the body of moving scroll (6) disposes thermal-protective coating (33).
3, vortex motor according to claim 1 and 2 is characterized in that, disposes self-lubricating seal ring (41) between moving scroll (8) and the fixed scroll (9).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 93120586 CN1104712A (en) | 1993-11-27 | 1993-11-27 | Vortex engine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 93120586 CN1104712A (en) | 1993-11-27 | 1993-11-27 | Vortex engine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN1104712A true CN1104712A (en) | 1995-07-05 |
Family
ID=4993356
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 93120586 Pending CN1104712A (en) | 1993-11-27 | 1993-11-27 | Vortex engine |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN1104712A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN100532932C (en) * | 2002-09-26 | 2009-08-26 | 创新能量公司 | Combustion method and apparatus |
| CN106232939A (en) * | 2014-04-21 | 2016-12-14 | 全重植 | Inhaler, dynamic force generating unit, utilize the external-combustion engine system of inhaler and dynamic force generating unit, utilize inhaler and the internal-combustion engine system of dynamic force generating unit, utilize the air hybrid generation system of inhaler and dynamic force generating unit |
-
1993
- 1993-11-27 CN CN 93120586 patent/CN1104712A/en active Pending
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN100532932C (en) * | 2002-09-26 | 2009-08-26 | 创新能量公司 | Combustion method and apparatus |
| CN106232939A (en) * | 2014-04-21 | 2016-12-14 | 全重植 | Inhaler, dynamic force generating unit, utilize the external-combustion engine system of inhaler and dynamic force generating unit, utilize inhaler and the internal-combustion engine system of dynamic force generating unit, utilize the air hybrid generation system of inhaler and dynamic force generating unit |
| CN106232939B (en) * | 2014-04-21 | 2019-02-01 | 全重植 | Utilize the system of inhalator and dynamic force generating unit |
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| C06 | Publication | ||
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| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C01 | Deemed withdrawal of patent application (patent law 1993) | ||
| WD01 | Invention patent application deemed withdrawn after publication | ||
| REG | Reference to a national code |
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