CN102536753A - Compressor or turbine device - Google Patents

Compressor or turbine device Download PDF

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Publication number
CN102536753A
CN102536753A CN2012100351206A CN201210035120A CN102536753A CN 102536753 A CN102536753 A CN 102536753A CN 2012100351206 A CN2012100351206 A CN 2012100351206A CN 201210035120 A CN201210035120 A CN 201210035120A CN 102536753 A CN102536753 A CN 102536753A
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CN
China
Prior art keywords
cylinder
gas
piston
anger
turbine installation
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CN2012100351206A
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Chinese (zh)
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汤斌
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Individual
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Abstract

The invention provides a compressor or turbine device which comprises a first cylinder, a second cylinder... and an Nth cylinder, wherein the capacities of the first cylinder, the second cylinder... and the Nth cylinder are increased progressively or decreased progressively; the first cylinder, the second cylinder... and the Nth cylinder are respectively provided with a first piston, a second piston... and an Nth piston, wherein N is a natural number larger than or equal to 0; the first piston, the second piston... and the Nth piston are connected with a transmission mechanism; the exhaust pipe of the former-stage cylinder in the cylinders which are positioned on a cylinder increasing or decreasing sequence is connected with the air inlet pipe of the later-stage cylinder in series; and when one cylinder at the previous stage and one cylinder at the later previous stage which are connected together are in the air compression state, the other cylinder is in the air expansion state, and the air in the cylinder at the previous stage in the compression state enters into the cylinder at the later stage in the expansion state. The compressor or turbine device provided by the invention has the advantages that complete machine material adaptive performance is good, and pressure loss can be avoided when expansion or compression is carried out in a closed space.

Description

Calm the anger or turbine installation
Technical field
The present invention relates to a kind ofly can be used for internal combustion and outer combustion-ing engine compressor, the calming the anger or turbine installation of fields such as air-conditioning.
Background technique
Existing calm the anger or turbine installation mainly is the rotor stator structure, gas constantly is accelerated in the course of the work, the thermal efficiency of gas in compression or the process that expands and the very big relation of structural design existence of gas velocity and rotor.Traditional calm the anger or the gas acting process of turbine installation is open working procedure promptly is not compression or expand in airtight space, has the bigger pressure loss inevitably.And common piston engine is as calming the anger or during turbine installation; Cylinder and piston are in the course of the work not only in low temperature environment work but also almost be operated in hot environment simultaneously; Cylinder will lean on the cooling liquid cooling when the temperature difference is big, thereby bigger heat waste occurs, thereby has reduced the thermal efficiency.
Summary of the invention
In order to overcome the problems referred to above, the present invention provides a kind of gas flow unobstructed to society, and the thermal efficiency is high, and good the calming the anger or turbine installation of complete machine material Adapter Property.
Technological scheme of the present invention is: provide a kind of and calm the anger or turbine installation; Comprise first cylinder, second cylinder to the N cylinder; The volume of said first cylinder, second cylinder to the N cylinder is increasing or decreasing successively; Be respectively equipped with first piston, second piston to the N piston at said first cylinder, second cylinder to the N cylinder, N is the natural number more than or equal to 0; Said first piston, second piston to the N piston are connected with driving mechanism; Be in the outlet pipe of the previous stage cylinder in the cylinder on the cylinder increasing or decreasing sequence and the suction tude polyphone of back one-level cylinder; And when a cylinder in previous stage cylinder that links to each other and the back one-level cylinder is in the gas compression state; Another cylinder is in the gas swelling state, and the gas unidirectional that is in the cylinder of compressive state of previous stage gets among the cylinder of the swelling state that is in the back one-level.
As to improvement of the present invention, in the exhaust of cylinder and gas-entered passageway, be provided with valve by distribution device control.
As to improvement of the present invention, said driving mechanism is connecting rod, planetary gear mechanism, the piston-engined driving mechanism of crank round slider, olivary-rotor engine driving mechanism, Wankel RC configuration driving mechanism, displacement sliding rotary engine driving mechanism or non-at the uniform velocity than driving mechanism etc.
As to improvement of the present invention, when calming the anger or turbine installation when using as gas compressor, said valve is one-way cock and is arranged near the relief opening position that is positioned on cylinder or the cylinder head.
As to improvement of the present invention; When calming the anger or turbine installation when using as turbine installation; On cylinder intake pipe and outlet pipe, be correspondingly provided with air intake valve and drain tap; And air intake valve is arranged near the suction port position that is positioned on cylinder head or the cylinder, and drain tap is arranged near the relief opening position that is positioned on cylinder head or the cylinder, and air intake valve and drain tap are all controlled by distribution device.When cylinder be not first cylinder and cylinder be in compression stroke and when finishing near compression stroke the drain tap of this cylinder close and air intake valve is opened and made the gas that is in compressive state in the cylinder and be compressed with gas in the gas channel that suction port is connected, the drain tap of previous stage cylinder still is in and closes at this moment.When this cylinder compression stroke finished, the gas pressure intensity in the feasible gas channel that is communicated with this cylinder air inlet was near the pressure of previous stage cylinder operation gas this moment.When finishing to transfer expansion stroke to along with this cylinder compression stroke, when with gas channel that this cylinder air inlet is connected in gas pressure intensity be less than or equal to this moment during previous stage cylinder operation gas pressure intensity the drain tap of previous stage cylinder open and make gas from this cylinder of previous stage cylinder entering.
As to improvement of the present invention, also be provided with heat exchange chamber, said heat exchange chamber one end is calmed the anger with one or first cylinder of turbine installation links to each other, and the other end links to each other with first cylinder of another compression or turbine installation.Said heat exchange chamber can be heating pipe, condensation tube or firing chamber etc.
As to improvement of the present invention; When calming the anger or turbine installation makes as gas compressor; The distribution device that control valve is opened or closed can be one-way cock, promptly the gas pressure in the previous stage cylinder greater than in the one-level cylinder of back during gas pressure valve opening make gas get into back one-level cylinder by the previous stage cylinder.
The order of work of gas of the present invention is: gas gets into the previous stage cylinder; The previous stage cylinder is in the expansion stage; The previous stage cylinder got into compression stage gas this moment and gets into back one-level cylinder from the previous stage cylinder after gas expanded and finishes; Back one-level cylinder is in the expansion stage; Thereby because the working volume between previous stage cylinder and the back one-level cylinder does not wait and makes the gas of previous stage cylinder get into behind the one-level cylinder of back the volumetric pressure of gas fully to change gas is done work or gas externally does work; Back one-level cylinder expands and finishes and when getting into compression stage, gas from the back one-level cylinder discharge, the inflation process that the compression process that gas reduces through volume in this process is done negative work or volume to be increased is done positive work.
Piston is a triangle and cylinder is respectively Olive Shape and 8 fonts when driving mechanism adopts olivary-rotor engine driving mechanism, Wankel RC configuration driving mechanism; When driving mechanism adopts displacement sliding rotary engine driving mechanism or non-at the uniform velocity than driving mechanism such as annular cylinder rotor engine driving mechanism; Planetary gear differential power plant (planetary pinion planet wheel eccentric shaft) engine drive mechanism; Number of pistons is 2 or a plurality of during noncircular gear engine drive mechanism etc.; The velocity variations of adjacent pistons makes the volume between the piston constantly change the expansion and the compression of corresponding gas, when the change in location of piston (rotor) or cylinder block rotation can be controlled suction port and exhaust open and close, air intake valve and drain tap can be set.
When the present invention was used to calm the anger device, its pressure ratio was more constant, and pressure leakage is little, can not cause exhaust air pressure to increase rapidly because rotating speed increases simultaneously.When being used for turbine installation, pressure leakage is little, can make to improve heat utilization efficiency by the kinetic energy that is converted into that gas interior can be maximum; And have simple in structure, the advantage of easy processing.When being used for motor, can use pluralities of fuel, various energy resources utilizes mode to comprise internal combustion and external combustion mode, and compression and expansion can both obtain the high thermal efficiency.Can use multiple combustion manner when using fuel, like igniting, pulse, sustained combustion etc.When adopting multistage cylinder operation, the operating temperature range of each grade cylinder is little, the thermal distortion that can reduce material require and few with or improved the thermal efficiency without cooling liquid.
Description of drawings
Fig. 1 is the plane structure schematic representation of an embodiment of the present invention.
Fig. 2 is the another kind of embodiment's of the present invention a plane structure schematic representation.
Fig. 3 is the third embodiment's of the present invention a plane structure schematic representation.
Embodiment
Marginal data:
Bent axle 1
First cylinder 10
First cylinder piston 11
First cylinder, first cylinder head 12
First air cylinder connecting rod 13
The first cylinder bent axle 14
First cylinder, first suction port 15
First cylinder, first relief opening 16
First air intake valve 17
First drain tap 170
Second cylinder 20
Second cylinder piston 21
Second cylinder, first cylinder head 22
Second air cylinder connecting rod 23
The second cylinder bent axle 24
Second cylinder, first suction port 25
Second cylinder, first relief opening 26
Second air intake valve 27
Second drain tap 270
The 3rd cylinder 30
The 3rd cylinder piston 31
The 3rd cylinder first cylinder head 32
The 3rd air cylinder connecting rod 33
The 3rd cylinder bent axle 34
The 3rd cylinder first suction port 35
The 3rd cylinder first relief opening 36
The 3rd air intake valve 37
The 3rd drain tap 370
N cylinder N0
N cylinder piston N1
N cylinder the one N cylinder head N2
N air cylinder connecting rod N3
N cylinder bent axle N4
N cylinder the one N suction port N5
N cylinder the one N relief opening N6
N air intake valve N7
N drain tap N70
Embodiment 1
See also Fig. 1, Fig. 1 is the plane structure schematic representation of an embodiment of the present invention.Present embodiment be with the gas swept volume from first cylinder 10 to N cylinder N0 gradually the mode of increasing sequence arrange, obviously, this enforcement also can be from first cylinder 10 to N cylinder N0 the gas swept volume gradually the mode of descending series arrange.In the present embodiment; Said driving mechanism is a connecting rod; Obviously, said connecting rod also can use the driving mechanism of planetary gear mechanism, crank round slider piston engine, olivary-rotor engine, Wankel RC configuration, displacement sliding rotary engine structure or non-at the uniform velocity ratio engine to replace (down together).
Can know from figure; In first cylinder 10, be provided with first cylinder piston 11; Said first cylinder piston 11 is connected with the first cylinder bent axle 14 through first air cylinder connecting rod 13, on first cylinder, first cylinder head 12, is provided with first cylinder, first suction port 15 and first cylinder, first relief opening 16; In second cylinder 20, be provided with second cylinder piston 21; Said second cylinder piston 21 is connected with the second cylinder bent axle 24 through second air cylinder connecting rod 23; On second cylinder, first cylinder head 22, be provided with second cylinder, first suction port 25 and second cylinder, first relief opening 26, said first cylinder, first relief opening 16 is connected with said second cylinder, first suction port 25; In the 3rd cylinder 30, be provided with the 3rd cylinder piston 31; Said the 3rd cylinder piston 31 is connected with the 3rd cylinder bent axle 34 through the 3rd air cylinder connecting rod 33; On the 3rd cylinder first cylinder head 32, be provided with the 3rd cylinder first suction port 35 and the 3rd cylinder first relief opening 36, said second cylinder, first relief opening 26 is connected with said the 3rd cylinder first suction port 35; And; In N cylinder N0, be provided with N cylinder piston N1; N is the natural number more than or equal to 0; Said N cylinder piston N1 is connected with N cylinder bent axle N4 through N air cylinder connecting rod N3, on N cylinder the one N cylinder head N2, is provided with N cylinder the one N suction port N5 and N cylinder the one N relief opening N6, and said N-1 cylinder first relief opening is connected with said N cylinder the one N suction port N5; The first lower inlet valve door 17 and first time drain tap 170 by distribution device control are set on said first cylinder; The second lower inlet valve door 27 and first time drain tap 270 by distribution device control are set on said second cylinder; The 3rd lower inlet valve door 37 and the 3rd time drain tap 370 by distribution device control are set on said the 3rd cylinder; N lower inlet valve door N7 and first time drain tap N70 by distribution device control are set on said N cylinder, are used for control gaseous and flow to.Certainly also can be on the passage of the relief opening of adjacent cylinder and suction port on the connection cylinder collating sequence only with a valve control (being that air intake valve and drain tap are merged into a valve), as air intake valve or the drain tap in the adjacent cylinder only is set., present embodiment on the relief opening that connects adjacent cylinder and suction port (like the first time drain tap 170 and the second lower inlet valve door 27) passage, only establishes an one-way cock when using as gas compressor; And valve is arranged near the relief opening position on cylinder or the cylinder head, and gas got into and discharged from first cylinder, 10 suction ports 15 from N0 cylinder exhaust port N6 this moment.
The first cylinder bent axle 14, the second cylinder bent axle 24, the 3rd cylinder bent axle 34 to N cylinder bent axle N4 connect into an integral shaft 1; Adjacent two cylinders are configured on the said cylinder collating sequence; When a cylinder in adjacent two cylinders is in the gas compression state; Another cylinder is in the gas swelling state, and the gas unidirectional that is in the cylinder of compressive state of previous stage gets among the cylinder of the swelling state that is in the back one-level.When present embodiment used as gas compressor, when N cylinder N0 was in compressive state, N cylinder piston N1 was in the decline state; Gas gets into the N-1 cylinder from the N0 cylinder, and the N0 air intake valve is closed, and the N0 drain tap is opened; The N-1 cylinder is in swelling state, and the N-1 cylinder piston is in propradation, and the N-1 air intake valve is opened and (also this air intake valve can be set at this moment; The N0 drain tap is set is set to one-way cock); The N-1 drain tap is closed, thus since cylinder N0 gas working volume when getting into cylinder N-1 by cylinder N0 greater than cylinder N-1 gas working volume gas the volume of working gas reduce, working gas is compressed; Gas pressure intensity increases temperature and raises, and the rest may be inferred for the working procedure of remaining cylinders.
When the present invention uses as turbine installation; Distribution device make second cylinder be in compression stroke and when finishing near compression stroke the drain tap 270 of second cylinder close and air intake valve 27 open make the gas that is in compressive state in the cylinder and with gas channel that suction port 25 is connected in the gas of (passage between valve 170 and the suction port 25) be compressed, the drain tap 170 of cylinder 10 still is in and closes at this moment.When cylinder 20 compression strokes finished, the gas pressure intensity of (passage between valve 170 and the suction port 25) was near the pressure of cylinder 10 working gass this moment in the feasible gas channel that is communicated with cylinder 20 suction ports 25.When finishing to transfer expansion stroke to along with cylinder 20 compression strokes, when with gas channel that cylinder 20 suction ports are connected in gas pressure intensity be less than or equal to this moment during cylinder 10 working gas pressure the drain tap 170 of cylinder 10 open and make gas from cylinder 10 entering cylinders 20.Remaining cylinders as 30,40 until the working procedure of N0 according to this type.When the present invention uses as turbine installation; Gas gets into first cylinder 10 from first cylinder, first suction port 15; Progressively be admitted to second cylinder 20, the 3rd cylinder 30 more successively until N cylinder N0, because the volume from first cylinder 10 to N cylinder N0 increases progressively gradually, working gas gets into from first cylinder that the volume of gas increases behind second cylinder; The temperature of working gas reduces pressure and reduces, so the present invention constitutes a turbine installation.Suppose that the gas that gets in first cylinder 10 from first cylinder, first suction port 15 is high-temperature gas; Like 1200 ℃ (this temperature can be produced by unified thermal source); At this moment, people's material of anti-1200 ℃ of high temperature of only needing to make the material selection of first cylinder 10 and first cylinder piston 11 gets final product; The same hot gas of working as gets into second cylinder 20 from first cylinder 10; Because the volume of second cylinder 20 is greater than the volume of first cylinder 10; Gas temperature descends; As drop to 1000 ℃, at this moment, the material of anti-1000 ℃ of high temperature that people only need to make the material selection of second cylinder 20 and second cylinder piston 21 gets final product; The 3rd cylinder 30 is similar up to the situation of N cylinder N0.Like this, the present invention has just overcome the necessary anti-very big temperature difference of existing cylinder, like the temperature difference from 1000 ℃ to tens degrees centigrade; So selection and making to cylinder all require very high; And generally, in order to dwindle the temperature difference also have to adopt cooling system, not only complex structure; And also to lose very big heat, its energy transformation ratio is just low.Therefore, the present invention has the good advantage of complete machine material Adapter Property, and simultaneously the operating temperature of each cylinder is all different, even also do not need all working cylinder all to be cooled to same temperature when cylinder need cool off.The present invention also adopts air cylinder structure, and compression or expansion can be avoided the pressure loss in airtight space.
When the present invention used as the device of calming the anger, its structure need not change, and only need suction port be arranged on the N cylinder N0, and gas gets in N cylinder N0, progressively enters into the N-1 cylinder successively, until to first cylinder 10, exported pressurized gas.Equally, the gas temperature difference in each cylinder is less, makes the present invention have the good advantage of complete machine material Adapter Property.
Embodiment 2
See also Fig. 2, Fig. 2 is second kind of embodiment's of the present invention a plane structure schematic representation.Embodiment illustrated in fig. 2 and embodiment illustrated in fig. 1 comparing, its general structure is identical, and different is: on first cylinder, second cylinder head 121, be provided with first cylinder, second suction port 151 and first cylinder, second relief opening 161; On second cylinder, second cylinder head 221, be provided with second cylinder, second suction port 251 and second cylinder, second relief opening 261, said first cylinder, second relief opening 161 is connected with said second cylinder, second suction port 251; On the 3rd cylinder second cylinder head 321, be provided with the 3rd cylinder second suction port 351 and the 3rd cylinder second relief opening 361, said second cylinder, second relief opening 261 is connected with said the 3rd cylinder second suction port 351; And, on N cylinder the 2nd N cylinder head N21, being provided with N cylinder the 2nd N suction port N51 and N cylinder the 2nd N relief opening N61, said N-1 cylinder second relief opening is connected with said N cylinder the 2nd N suction port N51; Drain tap 172 on being provided with on said first cylinder by the first upper inlet valve door 171 and first of distribution device control; Drain tap 272 on being provided with on said second cylinder by the second upper inlet valve door 271 and first of distribution device control; Drain tap 372 on being provided with on said the 3rd cylinder by the 3rd upper inlet valve door 371 and the 3rd of distribution device control; Drain tap N72 on being provided with by the N upper inlet valve door N71 and first of distribution device control on the said N cylinder is used for control gaseous and flows to.Certainly also can be on the passage of the relief opening of connection adjacent cylinder and suction port only with a valve control, as air intake valve or the drain tap in the adjacent cylinder only is set.
Said adjacent two cylinders are configured to; When a cylinder in adjacent two cylinders is in the gas compression state; Another cylinder is in the gas swelling state cylinder top working space or the cylinder bottom working space of corresponding diagram 2 (unified), and the gas unidirectional that is in the cylinder of compressive state of previous stage gets among the cylinder of the swelling state that is in the back one-level.When being in swelling state like first cylinder 10 among Fig. 2, first cylinder piston 11 is in upper state, and gas gets into gas from first cylinder, first suction port 15; The first lower inlet valve door 17 is closed, and second cylinder 20 is in compressive state, and second cylinder piston 21 is in the next state; Second time drain tap 270 is opened (the 3rd lower inlet valve door 37 is opened); Gas gets into the 3rd cylinder 30, and the 3rd cylinder 30 is in swelling state, and the rest may be inferred for the working procedure of remaining cylinders; Simultaneously, for same cylinder, in cylinder, be boundary with the piston; The interior space of cylinder that is in the piston both sides is in the alternation state again, as, be example with first cylinder 10; When first cylinder piston 11 moved upward, first cylinder piston, 11 underside gas expanded, and first cylinder, first suction port 15 is opened; The first lower inlet valve door 17 is opened and first time drain tap 170 closed, simultaneously, and the 11 upside gas compressions of first cylinder piston; First cylinder, second suction port 151 is closed, and the first upper inlet valve door 171 is closed, and the drain tap 172 and the second upper inlet valve door 271 are opened (when only being provided with one of them valve, making this valve opening) on first.Second cylinder 20, gas three cylinders 30 and N cylinder N0 working state are similar, please the reader analyze voluntarily.
Said structure can make same cylinder in up or folding process, uses all actings simultaneously of piston both sides, has improved working efficiency of the present invention, and under the situation of equal volume, power can double.Simultaneously, the pressure of gas that is in the different operating state in the same cylinder is approaching, the gas leakage of piston both sides during to piston opposite side space the gas pressure loss less, so low to the seal request between piston and the cylinder.
Embodiment 3
See also Fig. 3, Fig. 3 is the third embodiment's of the present invention a plane structure schematic representation.The application that is the present invention as combustion turbine shown in Figure 3.As can beappreciated from fig. 3, the present invention also comprises and also is provided with heat exchange chamber 50, and said heat exchange chamber 50 1 ends link to each other with said first cylinder 10, and the other end links to each other with said first cylinder 10 of another turbine installation of calming the anger.During work; First cylinder, first suction port 15 of the compression set in cool air heat exchange chamber 50 left sides from Fig. 3 and first cylinder, second suction port 151 alternately get into; Through second cylinder 20, the 3rd cylinder 30 after N cylinder N0 compression; Get into heat exchange chamber 50 (being gas combustion chamber in the present embodiment); For heat exchange chamber provides source of the gas, all only be provided with drain tap at second cylinder the 3rd cylinder to the N cylinder in the present embodiment, and drain tap is that one-way cock is arranged near the relief opening position on cylinder or the cylinder head.The hot gas that heat exchange chamber 50 produces gets into first cylinder 10 of the turbine installation on right side among Fig. 3 again, passes through the 2nd cylinder 20 then successively until N cylinder N0, does work.But so just constitute the motor of a complete continuous burning.
Likewise; No matter be the compression set in heat exchange chamber 50 left sides or the turbine installation on its right side; All are calming the anger or turbine installation shown in embodiment 1 or the embodiment 2 among the present invention who adopts, its gas temperature difference that has equally in each cylinder is less, and it is good to make the present invention have a complete machine material Adapter Property; And in airtight space, compress or expansion, can avoid the advantage of the pressure loss.
Piston is a triangle and cylinder is respectively Olive Shape and 8 fonts when driving mechanism adopts olivary-rotor engine driving mechanism, Wankel RC configuration driving mechanism in above embodiment; When driving mechanism adopts displacement sliding rotary engine driving mechanism or non-at the uniform velocity than driving mechanism such as annular cylinder rotor engine driving mechanism; Planetary gear differential power plant (planetary pinion planet wheel eccentric shaft) engine drive mechanism; Number of pistons is 2 or a plurality of during noncircular gear engine drive mechanism etc.; The velocity variations of adjacent pistons makes the volume between the piston constantly change the expansion and the compression of corresponding gas, when the change in location of piston (rotor) or cylinder block rotation can be controlled suction port and exhaust open and close, air intake valve and drain tap can be set.
Compression space volume when the working space compression stroke in the cylinder among the present invention finishes in the cylinder is more than or equal to 0, and preferably this volume is directly infinitely near 0.

Claims (6)

1. calm the anger or turbine installation for one kind; It is characterized in that; Comprise first cylinder, second cylinder to the N cylinder; The volume of said first cylinder, second cylinder to the N cylinder is increasing or decreasing successively, is respectively equipped with first piston, second piston to the N piston at said first cylinder, second cylinder to the N cylinder, and N is the natural number more than or equal to 0; Said first piston, second piston to the N piston are connected with driving mechanism; Be in the outlet pipe of the previous stage cylinder in the cylinder on the cylinder increasing or decreasing sequence and the suction tude polyphone of back one-level cylinder; And when a cylinder in previous stage cylinder that links to each other and the back one-level cylinder is in the gas compression state; Another cylinder is in the gas swelling state, and the gas unidirectional that is in the cylinder of compressive state of previous stage gets among the cylinder of the swelling state that is in the back one-level.
2. according to claim 1 calming the anger or turbine installation is characterized in that, in the exhaust of cylinder and gas-entered passageway, is provided with the valve by distribution device control.
3. according to claim 1 and 2 calming the anger or turbine installation is characterized in that: said driving mechanism is connecting rod, planetary gear mechanism, the piston-engined driving mechanism of crank round slider, olivary-rotor engine driving mechanism, Wankel RC configuration driving mechanism, displacement sliding rotary engine driving mechanism or non-at the uniform velocity than driving mechanism.
4. according to claim 3 calming the anger or turbine installation is characterized in that: when calming the anger or turbine installation when using as gas compressor, said valve is an one-way cock.
5. according to claim 3 calming the anger or turbine installation; It is characterized in that: when calming the anger or turbine installation when using as turbine installation; On cylinder intake pipe and outlet pipe, be correspondingly provided with air intake valve and drain tap; And air intake valve is arranged near the cylinder air inlet position, and drain tap is arranged near the cylinder exhaust port position, and air intake valve and drain tap are all controlled by distribution device; When cylinder be not first cylinder and cylinder be in compression stroke and when finishing near compression stroke the drain tap of this cylinder close and air intake valve is opened and made the gas that is in compressive state in the cylinder and be compressed with gas in the gas channel that suction port is connected, the drain tap of previous stage cylinder still is in and closes at this moment; When this cylinder compression stroke finished, the gas pressure intensity in the feasible gas channel that is communicated with this cylinder air inlet was near the pressure of previous stage cylinder operation gas this moment; When finishing to transfer expansion stroke to along with this cylinder compression stroke, when with gas channel that this cylinder air inlet is connected in gas pressure intensity be less than or equal to this moment during previous stage cylinder operation gas pressure intensity the drain tap of previous stage cylinder open and make gas from this cylinder of previous stage cylinder entering.
6. according to claim 1 and claim 2 is described calms the anger or turbine installation; It is characterized in that: also be provided with heat exchange chamber; Said heat exchange chamber one end is calmed the anger with one or first cylinder of turbine installation links to each other, and the other end is calmed the anger with another or first cylinder of turbine installation links to each other.
CN2012100351206A 2012-02-16 2012-02-16 Compressor or turbine device Pending CN102536753A (en)

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Application Number Priority Date Filing Date Title
CN2012100351206A CN102536753A (en) 2012-02-16 2012-02-16 Compressor or turbine device

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Application Number Priority Date Filing Date Title
CN2012100351206A CN102536753A (en) 2012-02-16 2012-02-16 Compressor or turbine device

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CN102536753A true CN102536753A (en) 2012-07-04

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102878061A (en) * 2012-09-11 2013-01-16 佛山市广顺电器有限公司 Multi-stage gas booster equipment
CN105201556A (en) * 2015-09-11 2015-12-30 武汉广益交通科技股份有限公司 Novel expansion machine
CN109758202A (en) * 2019-02-21 2019-05-17 江苏省人民医院 A kind of radial artery oppressor and its working method

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1118048A (en) * 1994-07-29 1996-03-06 霍尔格阀门工厂股份公司 Device and a method for influencing of a valve
CN2364246Y (en) * 1999-03-24 2000-02-16 郑国泉 Exhausting device for piston air compressor
CN2440122Y (en) * 2000-09-12 2001-07-25 康定睦 Piston-type air compressor with power itself
CN2620109Y (en) * 2003-04-30 2004-06-09 吴小冬 Linkage type air compressor

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1118048A (en) * 1994-07-29 1996-03-06 霍尔格阀门工厂股份公司 Device and a method for influencing of a valve
CN2364246Y (en) * 1999-03-24 2000-02-16 郑国泉 Exhausting device for piston air compressor
CN2440122Y (en) * 2000-09-12 2001-07-25 康定睦 Piston-type air compressor with power itself
CN2620109Y (en) * 2003-04-30 2004-06-09 吴小冬 Linkage type air compressor

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102878061A (en) * 2012-09-11 2013-01-16 佛山市广顺电器有限公司 Multi-stage gas booster equipment
CN102878061B (en) * 2012-09-11 2015-09-09 佛山市广顺电器有限公司 A kind of multi-level gas booster arrangement
CN105201556A (en) * 2015-09-11 2015-12-30 武汉广益交通科技股份有限公司 Novel expansion machine
CN109758202A (en) * 2019-02-21 2019-05-17 江苏省人民医院 A kind of radial artery oppressor and its working method
CN109758202B (en) * 2019-02-21 2023-09-15 江苏省人民医院 Radial artery compressor and working method thereof

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Application publication date: 20120704