CN103498727A - Vane type engine - Google Patents
Vane type engine Download PDFInfo
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- CN103498727A CN103498727A CN201310500044.6A CN201310500044A CN103498727A CN 103498727 A CN103498727 A CN 103498727A CN 201310500044 A CN201310500044 A CN 201310500044A CN 103498727 A CN103498727 A CN 103498727A
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- 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
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Abstract
The invention relates to a vane type engine which comprises an outer shell, a rotor, a plurality of vanes, a rotating shaft supporting piece, a gas inlet valve component, an exhaust valve component and a rotating shell placed between the outer shell and the rotor. According to the vane type engine, rolling friction replaces sliding friction, energy loss is lowered, the temperature and the pressure of exhausted gas are low, energy is fully used, a plurality of containing cavities work together and efficiency is high. Accordingly, the engine is high in energy using rate and efficiency and capable of generating high economic benefit.
Description
Technical field
The present invention relates to a kind of novel motor, especially there is the vane motor of transcapsidation.
Background technique
What existing market extensively generally adopted is four-stroke cylinder type motor; What by the power generating equipment of coal and nuclear power, adopt is steam turbine set, and what water generating adopted is turbines.
For the four-stroke cylinder engine, by its characteristics determined, following defect is arranged: (1) four-stroke engine expansion stroke equals compression stroke, when the pressurized gas after the energy burning is discharged motor, gas still has uniform temperature and certain pressure, and these energy have been wasted; (2) be sliding friction between the piston of motor and cylinder, in order to guarantee that pressurized gas are not revealed, also increased seal ring, such sliding friction is off-energy also.(3) only have a stroke for acting in four of four-stroke engine strokes, other three strokes all do not do work, and efficiency is low.
For steam turbine and turbo machine, because being produces moment of torsion by impacting, need medium to there is very high speed and could produce enough impact forces, and medium velocity is from zero to needing at a high speed energy, these energy have been wasted, so steam turbine and turbine efficiency are not high yet.
Owing to there being above-mentioned shortcoming, cause that current engine efficiency is low, energy loss is large, bring thus energy dissipation large, all kinds of problems such as environmental pollution.Reduce energy waste, the transformation efficiency that improves the energy is the whole society, global emphasis research topic always.Along with the whole society is more and more higher to the requirement of engine energy-saving performance, if the more high efficiency energy machine that turns is arranged, existing motor will be eliminated gradually because energy consumption is higher.If efficiency doubles, just be equivalent to adopt now the energy of half can drive existing all machinery.Therefore, it is current problem demanding prompt solution that a kind of motor that can improve capacity usage ratio, energy-conserving and environment-protective is provided, and has great Social benefit and economic benefit.
Summary of the invention
In order to solve the problems of the technologies described above, improve capacity usage ratio, the present invention, by the setting of " transcapsidation " additional bearing structure, by the setting of rotor and blade special construction, has realized that the almost identical angular velocity between rotor, blade and transcapsidation rotates.On the one hand, rolling friction replaces the sliding friction in traditional product, has reduced frictional loss; On the other hand, because slippage between blade and transcapsidation is little, contact force can be strengthened, then, by the cooperation of " blade " and " transcapsidation ", sealing effect preferably can be realized.Simultaneously due to the mutual eccentric setting of " rotor " gyration center and " transcapsidation " gyration center, realized the cavity volume be comprised of a plurality of volume spaces that vary in size on a circumference, each cavity volume can be realized from big to small more regular change procedure from small to large in rotation process.Coordinate suction port, relief opening, the various processes such as that motor can be realized realizing is air-breathing, pressurized gas, burning, expansion acting, exhaust in a circulation.
A kind of vane motor, comprise shell, rotor, a plurality of blade, rotating shaft support part, suction valve assembly and exhaust valve component, and rotor is rotationally connected by rotating shaft support part and shell, it is characterized in that:
Also comprise the transcapsidation between shell and rotor, transcapsidation and shell are rotationally connected by rotatable support;
The rotor side surface circumference forms groove, and a plurality of blades along the circumferential direction are distributed in rotor recesses, and each blade is along the rotor radial setting;
The mutual eccentric setting of the gyration center of the gyration center of rotor, rotating shaft support part and rotatable support, transcapsidation;
The end of adjacent two blades, described groove and sidewall and transcapsidation internal surface form cavity volume, thereby make whole vane motor have a plurality of cavity volumes that vary in size;
Suction valve assembly and exhaust valve component are positioned on the sidewall of the rotor recesses that forms cavity volume.
Further, in rotor recesses, along rotor radial, form a plurality of radial grooves, blade is arranged on respectively in chute; When rotor rotates, blade is along the chute slippage of rotor, and its outside is pressed together on the transcapsidation internal surface.
Further, the blade outside has spill Ji mouth, and transcapsidation partly or entirely is placed in above-mentioned spill Ji mouth.
Further, transcapsidation partly or entirely is arranged in the groove of rotor and matches with it.
Further, transcapsidation, blade and rotor all adopt tightness to contact each other.
Further, rotor is one-body molded, or assembly and connection forms.
Further, add lubricated oil by rotor center oil sump and/or suction port to cavity volume, and be thrown in transcapsidation under the effect of centrifugal force, make transcapsidation, blade, rotor kinematic pair each other all exist oil to be sealed.
Further, when rotor rotates, drive a plurality of blades and rotate in transcapsidation, each blade moves along rotor radial simultaneously, makes each blade outside contact with the transcapsidation tightness;
Further, the suction valve assembly comprises air inlet moving runner, Intake shaft, air inlet link, air inlet spring, suction valve; Exhaust valve component comprises exhaust moving runner, exhaust shaft, exhaust link, exhaust spring, outlet valve.
Further, the shell inner side surface has ring cam set, the air inlet of air inlet side cam operated inlet valve assembly; Exhaust side cams drives the exhaust valve component exhaust.
Further, outlet valve is opened when cavity volume reaches maximum, carries out exhaust; Reach fiery of minimum time point at cavity volume; Between above-mentioned two stages, certain starts to guarantee that outlet valve and suction valve are closed condition constantly, carries out compression process; After outburst, Ji begins externally to do work, until outlet valve turns to when cavity volume reaches maximum, opens, and carries out exhaust, to complete one-period.
Further, there is the suction valve assembly on a sidewall of the rotor recesses that forms cavity volume; There is exhaust valve component on another sidewall of the rotor recesses that forms cavity volume; There is air-inlet cavity and exhaust cavity between shell and rotor, sealing mutually between air-inlet cavity and exhaust cavity; The suction valve assembly connects air-inlet cavity, and exhaust valve component connects exhaust cavity.
Further, air-inlet cavity air pressure is greater than exhaust cavity air pressure.
Further, in one or more at volume in larger several cavity volumes, taken a breath, the process of ventilation is first to beat the Ji outlet valve to carry out exhaust, opens after a while suction valve and carries out air inlet, through ventilation final vacuum valve and suction valve successively or sealing simultaneously; The process that the volume of cavity volume diminishes is the compression process to combustion gas; Reach fiery of minimum time point at cavity volume; Then the volume of cavity volume becomes large, and gas expansion externally does work.
Technique effect: motor of the present invention adopts rolling friction to replace sliding friction, has reduced energy loss; Effluent air temp, pressure are less, take full advantage of energy; A plurality of cavity volumes do work together, and efficiency is high.Therefore, engine power utilization ratio of the present invention is high, efficiency is high, can produce huge economic benefit.
The accompanying drawing explanation
The sectional view that Fig. 1 is motor C-C section
Fig. 2 is engine body structure A-A section sectional view
Fig. 3 is engine body structure B-B section sectional view
The sectional view that Fig. 4 is motor P-P section
The sectional view that Fig. 5 is the transcapsidation main cross section
The plan view that Fig. 6 is blade
The sectional view that Fig. 7 is blade E-E section
Fig. 8 is the side view that rotor removes half
The sectional view that Fig. 9 is rotor F-F section
Figure 10 is suction valve assembly ssembly drawing
Embodiment
1, mechanical structure
Fig. 1 is the sectional view of motor main cross section C-C, shows the situation of change of each cavity volume size; Fig. 2 is the agent structure A-A section sectional view of engine breathing, shows the intake and exhaust situation of air-valve assembly; Fig. 3 is engine body structure B-B section sectional view, shows the relation of transcapsidation, blade, rotor; Fig. 4 is the sectional view of motor P-P section, shows order and the cavity volume situation of engine exhaust and air inlet.Motor is by parts or spatial composings such as shell, rotational support, transcapsidation, blade, rotor, cam, air-inlet cavity, air-valve assembly, Sealing, exhaust cavitys; Its critical piece is shell, rotatable support, transcapsidation, rotor from outside to inside successively; Blades installation is on rotor, and two rotational support are arranged on shell, and rotational support supports respectively transcapsidation and rotor.
Shell 1 is basic component, and outside is connected with the basis of motor, and inside provides respectively the support to transcapsidation, rotor by rotatable support 2, rotating shaft support part 6.Rotatable support 2, rotatable support 6 have bias.The inboard of shell and also being installed with or directly processing gas inlet side cam and exhaust side cams.
Rotatable support 2 is the supporting elements between transcapsidation 3 and shell 1, and its structure can be that bearing, ball, ball add the various structures such as retainer, as long as can realize that transcapsidation rotates under shell supports.
As shown in Figure 6 and Figure 7, N altogether, blade, have spill Ji mouth outside blade to blade 4 structures, and part or all of transcapsidation is placed in above-mentioned spill opening.The overall width of blade is a+2b, the intermediate portion that the edge section that two width of its middle concave opening are b is a higher than intermediate width; Spill A/F a is just in time identical with the width of cavity volume and transcapsidation; The end of two ends width b is arranged in the chute of rotor 5, and transcapsidation, rotor and blade all adopt airtight giving birth to contact each other; Its cross section of the part that width is a has circular arc, and radius is r (as shown in Figure 7), during rotation, withstands in transcapsidation 3 and tangent with transcapsidation 3 inner circles; And the interior edge face of the part that the two ends width is b is stuck on transcapsidation 3 sides; 3. 2. two surfaces of blade be two surfaces that can change in six surfaces of cavity volume.
The structure of rotor 5 as shown in Figure 8 and Figure 9, is comprised of the cylindrical body of 1 two diameter phi 2 of a diameter phi and the axle at rear portion, and φ 2 > φ 1.For the convenience of manufacturing and assembling, generally all be made into two body structures, with bolt two-part tightly together.Certainly both also can be one-body molded.7. rotor radially forms a plurality of chutes by the circumferential center of circle, blade be arranged on respectively chute 7. in, after assembling, rotor 5 is clamped on the width direction of transcapsidation 3 together with blade 4, rotor and blade relative position is different when rotating, under the acting in conjunction of centrifugal force and/or center oil pressure and/or transcapsidation pressure, blade stretches out or the slip (as shown in Figure 1) of retracting from the radial groove of rotor, thereby, while making rotor rotate, guarantees the tightness of cavity volume.6. the surface of rotor 5 forms the internal surface of cavity volume, and 5. 4. the surface of rotor 5 form two side surfaces of cavity volume.The outer end diameter of rotor is greater than on the flange of φ 1, every two chutes 7. between, all process the profiled holes of, suction valve assembly and exhaust valve component are arranged in this hole, the U of air-valve assembly and V section (U, V are respectively two mounting holes) are arranged on the strong point in hole, past polyslip under the driving of cam; And gas carries out the actions such as air inlet, exhaust and sealing under the effect of air-valve assembly by profiled holes.N the hole that is less than φ 1 is bolt hole.The center hole of rotor 5 is oil sumps, the high pressure oil of auxiliary system adds this oil sump, pressure oil lubricates the sliding pair between rotor 5 and blade 4 on the one hand, and be penetrated in cavity volume by this sliding pair, under the effect of centrifugal force, lubricant oil is thrown in transcapsidation 4, and certain thickness arranged, make like this transcapsidation 3, blade 4, rotor 5 kinematic pair each other that the existence of sealing oil is arranged, make hermetic seal make oil seal into, further improve the sealability of motor; The pressure of high pressure oil also acts on the interior edge face of blade on the other hand, increases the contact force between blade 4 and transcapsidation 3, increases the sealing between cavity volume.
Rotational support 6 can be the various structures such as bearing, ball, roller, roller, as long as can realize axle rotation under shell supports.Rotating shaft support part 6 is for being rotationally connected shell 1 and rotor 5.
The effect of cam 7 as shown in Figure 4.Cam 7 is arranged on the inner side surface of shell 1.Intake cam and exhaust cam are arranged.Cam is the order element of air intake-exhaust, it is totally the part of a ring-type, when the position that does not need air inlet and exhaust (for example, in RQ14-RQ18 and RQ1-RQ9 period), cam is flat, for example, when the position that needs air inlet and exhaust (RQ10-RQ13 period), cam lobe, the amount of projection is ascending descending again, the starting point of projection and terminal determine the opening and closing points of air intake-exhaust, and the amount of projection determines the size of air inlet and air displacement.
Air-inlet cavity 8 is between shell and rotor, by sealed at both ends 10 space surrounded.Air-inlet cavity 8 is for holding combustible gas, and combustible gas refers to the mixed gas of air and fuel, and fuel refers to gasoline, diesel oil, rock gas etc.Except combustible gas, lubrication and seal cavity volume oil also enters from air-inlet cavity.The independent import that free G&O gas is arranged of air-inlet cavity, the amount that enters the G&O of air-inlet cavity is weight feed.
Air-valve assembly 9 is shown in Figure 10, by moving runner 9-1, axle 9-2, link 9-3, spring 9-4, air valve 9-5 etc., formed, it is upper that moving runner 9-1, axle 9-2 are arranged on link 9-3, and it is upper that spring 9-4 is sleeved on air valve 9-5, and air valve 9-5 is threaded connection on link 9-3.Air-valve assembly is arranged on rotor 5, and its U and V section are installation positions; Under the pressure of spring 9-4 moving runner 9-1 all the time with the cam pressing; Under the acting in conjunction of cam and spring, the air-valve assembly to-and-fro motion, realize opening the purpose of closing cavity volume.Air valve 9-5 can regard an one-way valve as, only could air intake-exhaust under the action of beating Ji, under the condition of not opening, though the pressure in cavity volume far above the pressure of air-inlet cavity and exhaust cavity, also must not reverse leakage.Moving runner 9-1 is cone structure, and its purpose has two, first can guarantee moving runner 9-1 and the cam member pure rolling fricton-tight, second can guarantee that the rotation centerline direction of moving runner 9-1 points to the center line of rotor 5 all the time.2N altogether of air-valve assembly 9, wherein the air-valve assembly N of air inlet, the air-valve assembly N of exhaust.
Air-inlet cavity 11 is cavity volumes of inflammable gas, and between shell, rotor and Sealing 10, the pressure of combustion gas body is higher than the pressure of exhaust cavity.
Exhaust cavity 12 is cavity volumes of gas after combustion, and the gas that the air-valve assembly of exhaust is discharged enters this chamber, and then is discharged in atmosphere environment and goes by this chamber.
The gyration center B of the gyration center A of rotor 5, rotational support 6 and rotational support 2, transcapsidation 3 has an eccentric e, has formed N cavity volume after N blades installation between rotor and transcapsidation.The outside of the cavity volume that each is independent be the transcapsidation internal surface 1., the inside be rotor 5 groove floor 6., also have 4 sides, left and right be respectively blade side 2. 3., the both sides, front and back be rotor 5 the groove side 4. 5..Suppose as shown in Figure 1 totally ten eight cavity volumes (concrete cavity volume number and size can be set according to actual needs), use respectively RQ1, RQ2, RQ3 ... RQ18 means.
In the process of rotation, (transcapsidation 3 likely throws switch when rotating with the angular velocity rotation for transcapsidation 3, blade 4, rotor 5, but measure very little), each blade 4 often turns around and transcapsidation 3, rotor 5 between the slippage summation roughly equal two offset 2e, amount of friction reduces greatly, reduce wearing and tearing, improved efficiency.
Motor has an air intlet.The air inflow of the single cavity volume of every forwarding motivation is to determine like this, and when suction valve and the outlet valve of cavity volume are closed moment simultaneously, the volume of cavity volume can be defined as the air inflow of single cavity volume, and the air pressure of cavity volume is between air-inlet cavity and exhaust cavity.The air inflow of air-inlet cavity, by a metering pump supply with the engine speed associated, often turns air inflow and equals the long-pending of cavity volume number and single cavity volume air inflow, just maintains and gets rid of the rear gas of combustion, finishes changing inflammable gas.Except air intlet, motor also has the import of fuel, for fuel, enters cavity volume.
Due to the needs of the lubricated of cavity volume and sealing, need the machinery oil of certain lubrication and seal in cavity volume, these oil generally add from following two channels one of (or both).1,, at suction port, add appropriate lubrication and seal oil to cavity volume; 2, from rotor center, add,, there is an oil sump at the center of rotor, and the lubrication and seal oil that auxiliary system is supplied with certain pressure and flow enters oil sump, oil sliding pair between lubrication and seal rotor and blade on the one hand under certain pressure, be penetrated among cavity volume by this kinematic pair again.Above-mentioned two lubricant oil that aspect adds, under the effect of centrifugal force, be thrown to the moving shell in oil pocket outside above, and there is certain oil slick thickness; Under oily permeability and centrifugal action, oil is full of among each kinematic pair in rotor to the motor holding cavity structure, transcapsidation, blade, makes hermetic seal be transformed into oil seal.
2, working procedure
The working procedure of the vane motor of moving shell is following (referring to Fig. 1 Fig. 2, motor is totally 18 cavity volumes, suppose that motor is rotated counterclockwise): 1, gas exchange process: when the cavity volume of motor turns to the position in the middle of RQ9 and RQ10, outlet valve is beaten Ji, at this moment the air pressure in cavity volume is still higher than atmospheric gas pressure, opening moment exhaust immediately, making the pressure in cavity volume be reduced to rapidly the atmospheric pressure approached in environment; Arrive RQ10 after a while during position, suction valve is beaten Ji, the air pressure higher than cavity volume of air-inlet cavity now, and the air pressure of cavity volume is higher than the air pressure of exhaust cavity, forwarding RQ10, RQ11 to, RQ12 is the suction valve air inlet, the outlet valve exhaust; Until position suction valve and the outlet valve of RQ13 are closed (or outlet valve first close, close after suction valve) simultaneously, now taken a breath.2, compression process: when the cavity volume of motor turns to the position of RQ14, RQ15, RQ16, RQ17, the cavity volume sealing of motor, volume now progressively dwindles, and now motor is the isentropic Compression process, and inflammable gas raises in this course pressure temperature simultaneously.3, outburst process: RQ18 moment is igniting outburst process, and the igniter ignited flammable gas burns rapidly, emits a large amount of energy, and air pressure, temperature after outburst in cavity volume sharply increase.4, expansion acting process: when turning to the position of RQ1, RQ2, RQ3, RQ4, RQ5, RQ6, RQ7, RQ8, the volume of the single cavity volume of motor progressively increases, now that constant entropy expansion is external acting process, pressurized gas expand and promote blade and externally do work, this pressure process temperature reduces gradually, until exhaust is opened in the position of outlet valve between RQ9 and RQ10, to this movement process, finish.
Above-mentioned process is only a rough process, and different intake and exhaust positions, igniting outburst position also belong in the protection domain of this patent.
3, industrial applicibility
The vane motor of band transcapsidation of the present invention, have essential distinction with the conventional engines structure, will bring revolutionary shadow to.Due to the restriction of the structural principle of available engine own, its all many-sided inferior position is the advantage place of motor of the present invention exactly.Motor advantage of the present invention: 1, turn and can machine can rotate continuously, a plurality of cavity volumes do work simultaneously, fixing air intake-exhaust position, the mixing of inflammable gas.The expansion stroke that 2, can design is greater than compression stroke (four-stroke cylinder engine expansion stroke is substantially equal to compression stroke, and capacity usage ratio is low), to raise the efficiency.3, be mainly rolling friction between the motor associated part, frictional loss is little.4, the requirement of fuel reduces, and can utilize gas, liquid and composition thereof to act as a fuel.
These are only limited enumerating, the application of motor is not limited to this.And the description of above-mentioned principle, effect and application is not as the concrete restriction to the claims in the present invention protection domain.Structure every and of the present invention identical or be contemplated that with the present invention the improvement product carried out on basis all falls into protection domain of the present invention within.
Claims (12)
1. a vane motor, comprise shell, rotor, a plurality of blade, rotating shaft support part, suction valve assembly and exhaust valve component, and rotor is rotationally connected by rotating shaft support part and shell, it is characterized in that:
Also comprise the transcapsidation between shell and rotor, transcapsidation and shell are rotationally connected by rotatable support.
The rotor side surface circumference forms groove, and a plurality of blades along the circumferential direction are distributed in rotor recesses, and each blade is along the rotor radial setting.
The mutual eccentric setting of the gyration center of the gyration center of rotor, rotating shaft support part and rotatable support, transcapsidation.
The end of adjacent two blades, described groove and sidewall and transcapsidation internal surface form cavity volume, thereby make whole vane motor have a plurality of cavity volumes that vary in size.
Suction valve assembly and exhaust valve component are positioned on the sidewall of the rotor recesses that forms cavity volume.
2. a kind of vane motor as claimed in claim 1 is characterized in that: forms a plurality of radial grooves along rotor radial in rotor recesses, blade is arranged on respectively in chute; When rotor rotates, blade is along the chute slippage of rotor, and its outside is pressed together on the transcapsidation internal surface.
3. a kind of vane motor as claimed in claim 1 is characterized in that: the blade outside has the spill opening, and transcapsidation partly or entirely is placed in above-mentioned spill opening.
4. a kind of vane motor as claimed in claim 1 is characterized in that: transcapsidation partly or entirely is arranged in the groove of rotor and matches with it.
5. a kind of vane motor as claimed in claim 1, it is characterized in that: transcapsidation, blade and rotor all adopt tightness to contact each other.
6. a kind of vane motor as claimed in claim 1, it is characterized in that: rotor is one-body molded, or assembly and connection forms.
7. a kind of vane motor as claimed in claim 1, it is characterized in that: by rotor center oil sump and/or suction port, to cavity volume, add lubricated oil, and be thrown in transcapsidation under the effect of centrifugal force, make transcapsidation, blade, rotor kinematic pair each other all exist oil to be sealed.
8. a kind of vane motor as claimed in claim 1, it is characterized in that: the suction valve assembly comprises air inlet moving runner, Intake shaft, air inlet link, air inlet spring, suction valve; Exhaust valve component comprises exhaust moving runner, exhaust shaft, exhaust link, exhaust spring, outlet valve.
9. a kind of vane motor as claimed in claim 1, it is characterized in that: the shell inner side surface has ring cam set, the air inlet of air inlet side cam operated inlet valve assembly; Exhaust side cams drives the exhaust valve component exhaust.
10. a kind of vane motor as claimed in claim 9, it is characterized in that: in one or more at volume in larger several cavity volumes, taken a breath, the process of ventilation is first to open outlet valve to carry out exhaust, open after a while suction valve and carry out air inlet, successively or simultaneously seal through ventilation final vacuum valve and suction valve; The process that the volume of cavity volume diminishes is the compression process to combustion gas; Reach fiery of minimum time point at cavity volume; Then the volume of cavity volume becomes large, and gas expansion externally does work.
11. a kind of vane motor as claimed in claim 1 is characterized in that: on a sidewall of the rotor recesses that forms cavity volume, there is the suction valve assembly; There is exhaust valve component on another sidewall of the rotor recesses that forms cavity volume; There is air-inlet cavity and exhaust cavity between shell and rotor, sealing mutually between air-inlet cavity and exhaust cavity; The suction valve assembly connects air-inlet cavity, and exhaust valve component connects exhaust cavity.
12. a kind of vane motor as claimed in claim 11 is characterized in that: air-inlet cavity air pressure is greater than exhaust cavity air pressure.
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310500044.6A CN103498727A (en) | 2013-10-21 | 2013-10-21 | Vane type engine |
| PCT/CN2014/088593 WO2015058635A1 (en) | 2013-10-21 | 2014-10-14 | Energy conversion device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310500044.6A CN103498727A (en) | 2013-10-21 | 2013-10-21 | Vane type engine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN103498727A true CN103498727A (en) | 2014-01-08 |
Family
ID=49863973
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201310500044.6A Pending CN103498727A (en) | 2013-10-21 | 2013-10-21 | Vane type engine |
Country Status (1)
| Country | Link |
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| CN (1) | CN103498727A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2015058635A1 (en) * | 2013-10-21 | 2015-04-30 | 宋振才 | Energy conversion device |
| CN109477385A (en) * | 2016-06-24 | 2019-03-15 | 龚水明 | Vane type compressed air engine |
| CN109595038A (en) * | 2017-11-24 | 2019-04-09 | 李四屯 | Multipurpose vane gas liquid operated transforming machine |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB596541A (en) * | 1945-07-30 | 1948-01-06 | Edward George Baxter | Improvements in rotary sliding vane internal combustion engines |
| US2969021A (en) * | 1958-04-16 | 1961-01-24 | Acc Emanuel Di G E R Emanuel & | Automatic device for adjusting the output of rotary hydraulic machines |
| US3683694A (en) * | 1970-09-14 | 1972-08-15 | Albert J Granberg | Positive displacement fluid translating device |
| WO1988002438A1 (en) * | 1986-09-26 | 1988-04-07 | H.M.R. Engine Co. Pty. Ltd. | Rotary machine |
| EP0394651A1 (en) * | 1989-04-27 | 1990-10-31 | Schmid & Wezel | Compressed air vane motor |
| CN101506494A (en) * | 2006-08-18 | 2009-08-12 | 中川宗司 | Vane-type internal combustion engine |
-
2013
- 2013-10-21 CN CN201310500044.6A patent/CN103498727A/en active Pending
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB596541A (en) * | 1945-07-30 | 1948-01-06 | Edward George Baxter | Improvements in rotary sliding vane internal combustion engines |
| US2969021A (en) * | 1958-04-16 | 1961-01-24 | Acc Emanuel Di G E R Emanuel & | Automatic device for adjusting the output of rotary hydraulic machines |
| US3683694A (en) * | 1970-09-14 | 1972-08-15 | Albert J Granberg | Positive displacement fluid translating device |
| WO1988002438A1 (en) * | 1986-09-26 | 1988-04-07 | H.M.R. Engine Co. Pty. Ltd. | Rotary machine |
| EP0394651A1 (en) * | 1989-04-27 | 1990-10-31 | Schmid & Wezel | Compressed air vane motor |
| DE3913908A1 (en) * | 1989-04-27 | 1990-10-31 | Schmid & Wezel | COMPRESSED AIR BLADE MOTOR |
| US5064361A (en) * | 1989-04-27 | 1991-11-12 | Schmid U. Wezel | Rotating pneumatic vane motor with air bearing |
| CN101506494A (en) * | 2006-08-18 | 2009-08-12 | 中川宗司 | Vane-type internal combustion engine |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2015058635A1 (en) * | 2013-10-21 | 2015-04-30 | 宋振才 | Energy conversion device |
| CN109477385A (en) * | 2016-06-24 | 2019-03-15 | 龚水明 | Vane type compressed air engine |
| CN109477385B (en) * | 2016-06-24 | 2021-03-19 | 龚水明 | Vane type compressed air engine |
| US11111789B2 (en) | 2016-06-24 | 2021-09-07 | Shuiming GONG | Vane-type air motor |
| CN109595038A (en) * | 2017-11-24 | 2019-04-09 | 李四屯 | Multipurpose vane gas liquid operated transforming machine |
| CN109595038B (en) * | 2017-11-24 | 2021-02-05 | 李四屯 | Multipurpose blade type gas-liquid kinetic energy converter |
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Application publication date: 20140108 |