US2046631A - Multistage free piston motor compressor - Google Patents
Multistage free piston motor compressor Download PDFInfo
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- US2046631A US2046631A US725749A US72574934A US2046631A US 2046631 A US2046631 A US 2046631A US 725749 A US725749 A US 725749A US 72574934 A US72574934 A US 72574934A US 2046631 A US2046631 A US 2046631A
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- 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
- F02B71/00—Free-piston engines; Engines without rotary main shaft
- F02B71/04—Adaptations of such engines for special use; Combinations of such engines with apparatus driven thereby
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- My invention relates to free piston motorcompressors and more particularly to apparatus comprising two pistons arranged in a cylinder a the dimensions of the coupling gear care must be taken to avoid a transfer of mechanical energy by means of the coupling gear from one side of the apparatus to the other.
- free piston multi-stage compressors the two halves have been designed symmetrically to each other, for instance by providing on each side a threestage compressor, so that the apparatus comprises six stages.
- Such a device has a very large overall length and is composed of a large number of parts. Even the scavenging pump'must be made in two parts, one on each side, in order to avoid a unilateral load on the engine.
- the coupling gear will transfer mechanical energy from one side to the other during the working stroke and the return stroke, so that the members of the gear must be made relatively strong and heavy.
- the weight of the reciprocating masses is increased, the building cost is high and owing to the increased friction losses occurring in the coupling gear the efiiciency is reduced.
- a device according to my invention involves the advantage that the overall length is considerably smaller than in symmetrically designed devices, while the coupling gear may consist of light members.
- the pressure ratios or the volume ratios or both in the single compressor chambers in a suitable manner.
- the ratios were so chosen that the amount of energy fed to the compressor chambers during the working stroke or fed back to the free pistons during the return stroke is uniformly distributed over the single stages.
- these energies are distributed over the stages in a non-uniform manner, the sum of the energies, however, on one side being equal to the sum of the energies on the other side during the working stroke as well as during the return stroke.
- Figs. 1 to 3 are pressure-volume diagrams in which the abscissae designate the volume v and the ordinates the pressure p of the gas in a compressor stage.
- Fig. 4 is an axial section of an apparatus according to my invention.
- the point B corresponds to the inner dead centre position of the piston of the stage.
- the gas is compressed from the pressure 111 to the pressure pa.
- the compressed gas is discharged.
- the energy fed to the compressor stage during the working stroke may be calculated from the area of the surface A-BC--EF-A.
- a gas body remains in the dead space or at the pressure 7):, in which is stored a portion of the energy fed to the stage during the working stroke, this energy being re-fed to the piston of the stage during the return stroke in order to return the piston to its inner dead centre position and to compress the charge of fuel in the motor cylinder of the engine.
- the return stroke is indicated in the diagram by the curve E-GB.
- E-GB The return stroke is indicated in the diagram by the curve E-GB.
- the gas body is expanded from the pressure p: to the pressure p1.
- the second portion GB gas is sucked into the cylinder of the stage.
- the total amount of energy fed back to the pistons during the return stroke may be calculated from the area of the surface A-B-GEF-A.
- the energy delivered by the stage together with the discharged gas is rendered by the area of the surface enclosed by thecycle B-C-EG-B.
- the energy fed to the stage during the working 5 stroke and the feed-back energy fed back to the pistons during the return stroke, which are rendered by the surfaces AB-c-E-F-A and ABGE-F A, respectively, are ,fimctions of the pressure ratio I andotthevolumeratio on being the stroke volume.
- Fig. 2 illustrates the diagram of a stage operatingatthe samepressureratioandthesame stroke volume, the volume ratio being however increased by increasing the dead space from 01 to ur-I-v'r.
- the cycle of this stage is illustrated by the curve BC'EG'.
- the energy ifed tothis stage during the working stroke is reduced with respect to the corresponding value of Fig. 1 by the area of the surface BO-C'B, while the feed-back energy is increased by the area of the surface E-G-GE.
- the energy fed by the stage together with the discharged gas is indicated by the area of the cycle BC'-EG' and is reduced with respect to the corresponding vaiueoithediagramshowninFig. lbythesum of the areas of the surfaces B -OC 'B and EG'-G-E.
- the energy fed to the stage during the working stroke is increased by the area of the surface CC" "-E and the feed-back energy is increased by the surface of the area E"-G"GE".
- the energies fed to the compressor stage during the working stroke and fed back by it during the retina stroke and the difierence V of these energies may be varied within wide limitsby suitably choosing the premure ratio and the volume ratio.
- the pressure ratios and the volume ratios of the single stages are so chosen as to obtain equal sums of energies on each side during the working sh'oke as well as during the return stroke, so that the coupling gear securing syn-' chronous reciprocation of the pistons in opposite senses is relieved from transfer of energy exceptmg the energy required for driving auxiliary devices such as fuel pinnps or cooling water pumps.
- the side of the apparatus comtwo stages would operate at two thirds, the other side at one third of the total load, so that the coupling gearing must transfer one sixth of the total load from one side to the other. If however, according to my invention the pressure ratios on the side of the engine comprising two stagw i. e. in. the embodiment shown in Fig. 4 onthelefthandside of the motorcylinder I are made smaller than the pressure ratio on the other side comprising only one stage, the energy canoiriformlyoverbothsides.
- the volume ratios of the single stages may be varied in a similar sense as discussedaboveinconnectionwiththepressure ratio.
- the suction stroke 6-8 is reduced to GB (see Fig. 2). thusreducingtheamountotgcssuckedinduring thesuckingstroke.
- the amount of the forces exerted by the pis- 30 tons at the end of the working stroke may be further controlled within certain limits by changing thedischargeprossurem.
- pz hasaconstant value only, if the chamber into which the gas is discharged, has an infinite volume, so that the pressureexistingthereinisnotbydisc arging the gas into the If, however, the chamber into which the gas is discharged from the stage, is suitably dimensioned, the discharge pressure pz will increase during the discharge stroke, so that the corresponding portion of the diagram will be indicated by a more or less inclined curve, as shown by CK in Fig. l, in which the discharge increases from in to p"z.
- air ed from a low pressure stage during the portion of the working stroke in the manner described may be 60 added to the scavenging air conveyed by a scavenging pump.
- the pump may be formed by the rear faces of one or a plurality of compressor pistons. If a separate sca pump is provided,itshouldbe c f stages or energy storage chambers should be so chosen that the energy amounts fed to, and refed by, such chambers in addition to the energy amountsof the other compressor stages amount to equal sums on the two sides of the structure.
- My invention may be used in connection with any free piston engine comprising a multistage energy consumer, for instance a compressor, in which the stages are non-uniformly distributed over the sides of the apparatus.
- a multistage energy consumer for instance a compressor
- An example of such an apparatus is a three stage compressor, in which two stages are arranged on one side and one stage on the other side.
- the invention may however be advantageously used also in connection with compressors with an even number of stages, since in devices of this kind the areas of the diagram curves of the single stages need not be equal, so that a compensation according to my invention may involve considerable advantages in connection with these devices.
- Fig. 4 showing a three stage free piston motor-compressor
- I is the motor cylinder and 2 and 3 are the motor pistons arranged in the cylinder I for synchronous reciprocation in opposite directions.
- 4 and 5 are scavenging and exhaust ports arranged in the .wall of the cylinder and controlled by the pistons 2 and 3, respectively.
- the rod 6 of piston 2 is connected to the piston 3 of the first compressor stage, piston 8 being connected to the piston 2I of the third stage.
- 9 and 22 are the cylinders, in which the pistons 8 and 2
- Piston 3 is connected by means of rod I to the piston III of the second compressor stage, which reciprocates in the cylinder I I.
- the freely moving bodies of the two sides of the apparatus are coupled with each other by means of a coupling gear.
- a coupling gear comprising racks I2 and I2 and a pinion I3 rotataby securedto the casing of the motor cylinder by means of suitable bearings (not shown) or the like.
- II are the suction valves of the first compressor stage, from which compressed gas is discharged through exhaust valves I5 into a connecting pipe I5, from which it is sucked by the second compressor stage through suction valves II.
- the air compressed in the second stage is discharged through valves I8 into a connecting pipe I9, from which it is sucked through valve 20 into the third stage.
- the air compressed in the third stage is discharged through a pressure valve 23.
- the pressure ratio and the volume ratio are chosen higher in the second stage II, than in the other stages, in the manner discussed above.
- the forces exerted by the pistons, particularly at the end of the working stroke, are equalized by making the diameter of piston III relatively large.
- a portion of the gas sucked in is discharged again during the initial portion of the working stroke as described above,
- valves 24 being provided in the wall of the cylinders II, through which during the initial portion of the working stroke a portion of the gas sucked in through the valves I1 is re-fed into the pipe I5, until the piston III has passed the valves 24.
- Similar valves 25 may be provided in the first compressor stage.
- the air discharged through valves 25 is used as additional scavenging air by providing a pipe 26 connecting the valves 25 to the interior of the motor casing 33 used as a scavenging air container.
- the scavenging pump is' formed by the rear side of the piston 3 and by the portion of the cylinder 9 closed'by an end wall 29 provided with pressure valves 28.
- the scavenging pump sucks in air and discharges it during the return stroke into the scavenging air container 33.
- the energy input and output of the scavenging pump is balanced on the opposite side of the engine by a storage chamber connected with the second compressor stage and formed by the left-hand portion 32 of the cylinder II, which is closed by an end wall 3I.
- the air present in the chamber 32 is compressed and the energy amount therefor required may be so chosen as to balance the energy demand of the scavenging pump. partial balancing may be obtained, if the wall 3
- the pressure ratios and the volume ratios in the compressor stages 9, II and 22 and in the rear chambers 30 and 32 are so chosen that during the working stroke as well as during the return stroke the sums of the energies are substantially equal on both sides of the engine, so
- Fig. 4 The operation of the device shown in Fig. 4 is substantially the same as that of known free piston devices. Fuel mixture is periodically delivered to the cylinder I through a fuel inlet 34 and burnt therein so that the motor pistons 2 and 3 excute a working stroke, during which the air in the compressor chambers is compressed and partly discharged in the manner above described. The pistons are returned to their inner dead centre positions by the energy stored in the gas or air bodies remaining over in the dead spaces of the compressor chambers, scavenging being eflected in the manner above described. It should, however, be understood, that in an apparatus according to my invention the pressure ratios and the volume ratios are chosen in the manner described above so as to relieve the coupling gear from any substantial transfer of energy in spite of the fact, that the structure is not symmetrically designed.
- a free piston multi-stage motor compressor comprising in combination a motor cylinder, a pair of pistons arranged in said cylinder and adapted to reciprocate therein in opposite directions, a coupling gear substantially free from transmitting mechanical energy connecting said pistons for synchronizing the movements thereof, a plurality of compression cylinders, asymmetrically arranged on both sides of said motor cylinder, a compressor piston in each compression cylinder, each compressor piston and each compression' cylinder so determining the ratios of the volumes and pressures prevailing in each compression cylinder at the outer and inner dead center positions of said compressor piston that, for the working stroke as well as for the return stroke, the sum of the work yielded in all compression cylinders on one side of said motor cylinder is substantially equal to the sum or the work yielded in all compression cylinders on the other side of said motor cylinder.
- a free piston multi-stage motor compressor comprising in combination a motor cylinder, a pair of pistons arranged in said cylinder and adapted to reciprocate therein in opposite directions, :1 coupling gear substantially free from transmitting mechanical energy connecting said pistons for synchronizing the movements thereof,
- a plurality of compression cylinders arranged asymmetrically on both sides of said motor cylinder, a compressor piston in each compression cylinder, rigid connections connecting each motor piston with the compressor pistons on its side of the motor cylinder, each compressor piston and each compression cylinder so determining the ratios of the volumes available in each compression cylinder at the outer and inner dead center positions.
- said compressor piston that, for the working stroke as well as for the return stroke, the sum of the work yielded in all compression cylinders on one side of said motor cylinder is substantially equal to the sum of the work yielded in all compression cylinders on the other side of said motor cylinder.
- a free piston multi-stage motor compressor comprising in combination a motor cylinder, a pair of pistons arranged in said cylinder and adapted to reciprocate therein in opposite directions, a coupling gear substantially free from transmitting mechanical energy connecting said pistons for synchronizing the movements thereof, a plurality of compression cylinders arranged asymmetrically on both sides of said motor cylinder, a compressor piston in each compression cylinder, means connecting each motor piston with the compressor pistons on its side oi.
- a free piston multi-stage motor compressor in which the ratios of the initial and end pressures prevailing in said compression cylinder at the outer and inner dead center positions of said compressor'piston are substantially higher on the side oi. the motor cylinder comprising the smaller number of stages than on the other side.
- a free piston multi-stage motor compressor in which the ratios of the initial and end volumes available in said compression cylinder at the outer and inner dead center positions of said compressor piston are substantially higher on the side of the motor cylinder comprising the smaller number of stages than on the other side.
- a freepiston multi-stage motor compressor comprising in combination a motor cylinder, a pair of pistons arranged in said cylinder and adapted to reciprocate therein in opposite directions, means substantially free from transmitting the motor cylinder,
- a plurality of compression cylinders arranged asymmetrically on both sides or said motor cylinder, a compressor piston in each compression cylinder, valve means associated with at least one of said compression cylinders for discharging, during the initial portion of the compression stroke, a portion of the gas contained in said compression cylinder, rigid connections connecting each motor piston with the compressor pistons on its side of each compressor pistonand each compression cylinder so determining the ratios of the volumes and pressures prevailing in each compressor cylinder at the outer and inner dead center positions of said compressor piston that, for the working stroke as well as for the return stroke, the sum of the work yielded in all compression cylinders on one side of said motor cylinder is substantially equal to the sum of the work yielded in' all compression cylinders on the other side of said motor cylinder.
- a free piston multi-stage motor compressor comprising in combination a motor cylinder, a pair of pistons arranged in said cylinder and adapted to reciprocate therein in opposite directions, a coupling gear substantially free. from transmitting mechanical energy connecting said pistons for synchronizing the movements thereof, a plurality of compression cylinders arranged asymmetrically on both sides of said motor cylinder, a compressor piston in each compression cylinder, said compression cylinders comprising high pressures and low pressures stages, means in at least one low pressure cylinder for discharging, during the initial portion of the compression stroke, a portion of the gas contained in said cylinder and for delivering said portion to said ,motor cylinder for scavenging purposes, rigid connections connecting each motor piston with the compressor pistons on its side of the motor cylinder, each compressor piston and each compression cylinder so determining the ratios of the volumes and pressures prevailing in each compressor cylinder at the outer and inner dead center positions of said compressor piston that, for the working stroke as well as for the return stroke, the sumof the work yielded in
- a free piston multi-stage motor compressor which comprises in combi-- nation a motor cylinder, a plurality of compression cylinders and pistons provided therein, at least one of said cylinders being adapted to be used, on one side of the piston reciprocating therein, as a compressor chamber and on the other side as a scavenging pump, and valves connecting said pump with said motor cylinder.
- a free piston multi-stage motor compressor comprising a motor cylinder and a plurality of compression cylinders
- the improvement which comprises means for adapting a compression cylinder on one side of said motor cylinder to act as a scavenging pump, and means for adapting a compression cylinder on the other side thereof to act as an energy storage chamber.
- a free piston multi-stage motor compressor comprising a plurality of compression cylinders, the improvement which comprises a discharging chamber, valves connecting at least one of said compression cylinders to said chamber for discharginggas thereto during the compression stroke, said chamber being adapted to gradually increase the pressure of the gas contained in said compression cylinder during the discharge.
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Description
July 7, 1936- H. JANICKE MULTISTAGE FREE PISTON MOTOR COMPRESSOR Filed May 15, 1934 2 Shee ts-Sheet 1 In venfol:
July 7, 1936. H. JANICKE 2,046,631
MULTISTAGE FREE PISTON MOTOR COMPRESSOR Filed May 15, 1954 2 Sheets-Sheet 2 Fig. 4-
ln ventor:
atented July 7, 1936 UNITED STATES MULTISTAGE FREE PISTON MOTOR COMPRESSOR Hermann Jinicke, Dessau, Germany, asslgnor to Hugo Junkers, Bayrisch-Zell, Oberbayern,
Germany Application May 15, 1934, Serial No. 725,749 In Germany May 20, 1933 '11 Claims.
My invention relates to free piston motorcompressors and more particularly to apparatus comprising two pistons arranged in a cylinder a the dimensions of the coupling gear care must be taken to avoid a transfer of mechanical energy by means of the coupling gear from one side of the apparatus to the other. To this end in free piston, multi-stage compressors the two halves have been designed symmetrically to each other, for instance by providing on each side a threestage compressor, so that the apparatus comprises six stages. Such a device, however, has a very large overall length and is composed of a large number of parts. Even the scavenging pump'must be made in two parts, one on each side, in order to avoid a unilateral load on the engine. If on the other hand the structure is designed unsymmetrically, for instance by arranging the scavenging pump at one side, or by providing different numbers of compressor stages on the two sides, the coupling gear will transfer mechanical energy from one side to the other during the working stroke and the return stroke, so that the members of the gear must be made relatively strong and heavy. Hereby the weight of the reciprocating masses is increased, the building cost is high and owing to the increased friction losses occurring in the coupling gear the efiiciency is reduced.
It is an object of my invention to provide an unsymmetrical multistage free piston motorcompressor of the kind referred to, in which the coupling gear is substantially relieved from transferring mechanical energy from one side of the structure to the other. A device according to my invention involves the advantage that the overall length is considerably smaller than in symmetrically designed devices, while the coupling gear may consist of light members. In order to accomplish this I choose the pressure ratios or the volume ratios or both in the single compressor chambers in a suitable manner. In the multistage free piston motor-compressors hitherto known the ratios were so chosen that the amount of energy fed to the compressor chambers during the working stroke or fed back to the free pistons during the return stroke is uniformly distributed over the single stages. In contradistinction thereto in a structure according to my invention these energies are distributed over the stages in a non-uniform manner, the sum of the energies, however, on one side being equal to the sum of the energies on the other side during the working stroke as well as during the return stroke.
Other objects of my invention will appear from the following description.
In the drawings afiixed to this specification and forming part thereof some diagrams illustrating the operation of a motor-compressor according to my invention and an embodiment of such apparatus are shown diagrammatically by way of example.
In the drawings:
Figs. 1 to 3 are pressure-volume diagrams in which the abscissae designate the volume v and the ordinates the pressure p of the gas in a compressor stage.
Fig. 4 is an axial section of an apparatus according to my invention.
Referring first to Fig. 1, in which the curve B--CEG illustrates an operating cycle of a compressor stage, the point B corresponds to the inner dead centre position of the piston of the stage. During the initial portion of the working stroke, indicated by the curve BC, the gas is compressed from the pressure 111 to the pressure pa. During the last portion of the working stroke, indicated by the horizontal straight line CE, the compressed gas is discharged. The energy fed to the compressor stage during the working stroke may be calculated from the area of the surface A-BC--EF-A. At the end of the working stroke a gas body remains in the dead space or at the pressure 7):, in which is stored a portion of the energy fed to the stage during the working stroke, this energy being re-fed to the piston of the stage during the return stroke in order to return the piston to its inner dead centre position and to compress the charge of fuel in the motor cylinder of the engine. The return stroke is indicated in the diagram by the curve E-GB. During the initial portion E-G of the return stroke the gas body is expanded from the pressure p: to the pressure p1. During the second portion GB gas is sucked into the cylinder of the stage. The total amount of energy fed back to the pistons during the return stroke may be calculated from the area of the surface A-B-GEF-A. The energy delivered by the stage together with the discharged gas is rendered by the area of the surface enclosed by thecycle B-C-EG-B.
The energy fed to the stage during the working 5 stroke and the feed-back energy fed back to the pistons during the return stroke, which are rendered by the surfaces AB-c-E-F-A and ABGE-F A, respectively, are ,fimctions of the pressure ratio I andotthevolumeratio on being the stroke volume.
Fig. 2 illustrates the diagram of a stage operatingatthe samepressureratioandthesame stroke volume, the volume ratio being however increased by increasing the dead space from 01 to ur-I-v'r. The cycle of this stage is illustrated by the curve BC'EG'. The energy ifed tothis stage during the working stroke is reduced with respect to the corresponding value of Fig. 1 by the area of the surface BO-C'B, while the feed-back energy is increased by the area of the surface E-G-GE. The energy fed by the stage together with the discharged gas is indicated by the area of the cycle BC'-EG' and is reduced with respect to the corresponding vaiueoithediagramshowninFig. lbythesum of the areas of the surfaces B -OC 'B and EG'-G-E.
Fig.3sbows adlagramofastageoperatingat a higher ratio and at the same volume ratio and the same stroke volume as the cycle shown in Fig. l. The energy fed to the stage during the working stroke is increased by the area of the surface CC" "-E and the feed-back energy is increased by the surface of the area E"-G"GE".
Aswillbeseen fromthediagramsshownin Figs. 1 to 3, the energies fed to the compressor stage during the working stroke and fed back by it during the retina stroke and the difierence V of these energies may be varied within wide limitsby suitably choosing the premure ratio and the volume ratio. Now in an unsymmetrically designed motor-compressor according to my invention the pressure ratios and the volume ratios of the single stages are so chosen as to obtain equal sums of energies on each side during the working sh'oke as well as during the return stroke, so that the coupling gear securing syn-' chronous reciprocation of the pistons in opposite senses is relieved from transfer of energy exceptmg the energy required for driving auxiliary devices such as fuel pinnps or cooling water pumps.
This shall be still further explained by discussing a three stage free piston compressor comprising three compressor chambers, two of which are arranged on the same side of the structutre.
If the load is uniformly distributed over the stages by providing equal pressure ratios and vol- 'ume ratios therein, the side of the apparatus comtwo stages would operate at two thirds, the other side at one third of the total load, so that the coupling gearing must transfer one sixth of the total load from one side to the other. If however, according to my invention the pressure ratios on the side of the engine comprising two stagw i. e. in. the embodiment shown in Fig. 4 onthelefthandside of the motorcylinder I are made smaller than the pressure ratio on the other side comprising only one stage, the energy canbeimiformlyoverbothsides. In consequence thereof a simple construction comprising the minimum number of cylinders is obtained with a coupling gear relieved of transferofenergyandwhichmaybeconstmctedwith 5 low weight members, the efliciency of the apparatus being increased by avoiding friction losses in the coupling gear. Instead of or besides varying the presure ratios, the volume ratios of the single stages may be varied in a similar sense as discussedaboveinconnectionwiththepressure ratio. By varying the volume ratio the suction stroke 6-8 is reduced to GB (see Fig. 2). thusreducingtheamountotgcssuckedinduring thesuckingstroke. 'Ihis,however,maybeeasily compensated for by gly increasing the diameter of the piston, which involves the further advantage that the diiference between theforcesexertedbyoronthepistonawhichis amaximumat theendoftheworkingstroke, is Ieducedbecausethisfomeise uaItotheproductofthespeciflcpressure (p1 orpi) andthe area of the piston surface. In order to reduce this difference, the diameter; of the pistons of the stagesarrangedonthesidecom thesmaller number ofstagesshouldbeenlargedasfaras possible,andthiscanbedonebychoosingthe volume ratiointhesestageshigherthaninthe stages on the other side.
The amount of the forces exerted by the pis- 30 tons at the end of the working stroke may be further controlled within certain limits by changing thedischargeprossurem. pzhasaconstant value only, if the chamber into which the gas is discharged, has an infinite volume, so that the pressureexistingthereinisnotbydisc arging the gas into the If, however, the chamber into which the gas is discharged from the stage, is suitably dimensioned, the discharge pressure pz will increase during the discharge stroke, so that the corresponding portion of the diagram will be indicated by a more or less inclined curve, as shown by CK in Fig. l, in which the discharge increases from in to p"z.
In some cases it may be desirable to increase the working surface of the piston of a stage beyond the limit corresponding to the increase of the volume ratio. In order to avoid in such cases an undesirable increase of the stroke volume and the'input and output of the stage, whereby the uniform distribution of energy would be disturbed, a portion of the gas sucked in may be discharged during the portion of the working stroke, so that the point 3 indicating the beginning of the compression is shifted to the left along the line B-G shown inFig. i.
In an air compressor air ed from a low pressure stage during the portion of the working stroke in the manner described may be 60 added to the scavenging air conveyed by a scavenging pump. The pump may be formed by the rear faces of one or a plurality of compressor pistons. If a separate sca pump is provided,itshouldbe c f stages or energy storage chambers should be so chosen that the energy amounts fed to, and refed by, such chambers in addition to the energy amountsof the other compressor stages amount to equal sums on the two sides of the structure.
My invention may be used in connection with any free piston engine comprising a multistage energy consumer, for instance a compressor, in which the stages are non-uniformly distributed over the sides of the apparatus. An example of such an apparatus is a three stage compressor, in which two stages are arranged on one side and one stage on the other side. The invention may however be advantageously used also in connection with compressors with an even number of stages, since in devices of this kind the areas of the diagram curves of the single stages need not be equal, so that a compensation according to my invention may involve considerable advantages in connection with these devices.
Referring now to Fig. 4 showing a three stage free piston motor-compressor, I is the motor cylinder and 2 and 3 are the motor pistons arranged in the cylinder I for synchronous reciprocation in opposite directions. 4 and 5 are scavenging and exhaust ports arranged in the .wall of the cylinder and controlled by the pistons 2 and 3, respectively. The rod 6 of piston 2 is connected to the piston 3 of the first compressor stage, piston 8 being connected to the piston 2I of the third stage. 9 and 22 are the cylinders, in which the pistons 8 and 2| reciprocate, respectively. Piston 3 is connected by means of rod I to the piston III of the second compressor stage, which reciprocates in the cylinder I I. The freely moving bodies of the two sides of the apparatus are coupled with each other by means of a coupling gear. comprising racks I2 and I2 and a pinion I3 rotataby securedto the casing of the motor cylinder by means of suitable bearings (not shown) or the like. II are the suction valves of the first compressor stage, from which compressed gas is discharged through exhaust valves I5 into a connecting pipe I5, from which it is sucked by the second compressor stage through suction valves II. The air compressed in the second stage is discharged through valves I8 into a connecting pipe I9, from which it is sucked through valve 20 into the third stage. The air compressed in the third stage is discharged through a pressure valve 23.
In order to equalize the energy amounts occurring on the two sides of the structure during the working stroke and during the return stroke, the pressure ratio and the volume ratio are chosen higher in the second stage II, than in the other stages, in the manner discussed above. The forces exerted by the pistons, particularly at the end of the working stroke, are equalized by making the diameter of piston III relatively large. In order to avoid an undesirably large input of energy at the second stage, a portion of the gas sucked in is discharged again during the initial portion of the working stroke as described above,
that the coupling gear I2, I2, I3is relieved from 35 transfer of energy.
The operation of the device shown in Fig. 4 is substantially the same as that of known free piston devices. Fuel mixture is periodically delivered to the cylinder I through a fuel inlet 34 and burnt therein so that the motor pistons 2 and 3 excute a working stroke, during which the air in the compressor chambers is compressed and partly discharged in the manner above described. The pistons are returned to their inner dead centre positions by the energy stored in the gas or air bodies remaining over in the dead spaces of the compressor chambers, scavenging being eflected in the manner above described. It should, however, be understood, that in an apparatus according to my invention the pressure ratios and the volume ratios are chosen in the manner described above so as to relieve the coupling gear from any substantial transfer of energy in spite of the fact, that the structure is not symmetrically designed.
I wish it to be understood that I do not desire to be limited to the exact details of construction shown and described for obvious modifications will occur to a person skilled in the art.
I claim:
1. A free piston multi-stage motor compressor comprising in combination a motor cylinder, a pair of pistons arranged in said cylinder and adapted to reciprocate therein in opposite directions, a coupling gear substantially free from transmitting mechanical energy connecting said pistons for synchronizing the movements thereof, a plurality of compression cylinders, asymmetrically arranged on both sides of said motor cylinder, a compressor piston in each compression cylinder, each compressor piston and each compression' cylinder so determining the ratios of the volumes and pressures prevailing in each compression cylinder at the outer and inner dead center positions of said compressor piston that, for the working stroke as well as for the return stroke, the sum of the work yielded in all compression cylinders on one side of said motor cylinder is substantially equal to the sum or the work yielded in all compression cylinders on the other side of said motor cylinder.
2. A free piston multi-stage motor compressor comprising in combination a motor cylinder, a pair of pistons arranged in said cylinder and adapted to reciprocate therein in opposite directions, :1 coupling gear substantially free from transmitting mechanical energy connecting said pistons for synchronizing the movements thereof,
a plurality of compression cylinders arranged asymmetrically on both sides of said motor cylinder, a compressor piston in each compression cylinder, rigid connections connecting each motor piston with the compressor pistons on its side of the motor cylinder, each compressor piston and each compression cylinder so determining the ratios of the volumes available in each compression cylinder at the outer and inner dead center positions. of said compressor piston that, for the working stroke as well as for the return stroke, the sum of the work yielded in all compression cylinders on one side of said motor cylinder is substantially equal to the sum of the work yielded in all compression cylinders on the other side of said motor cylinder.
3. A free piston multi-stage motor compressor comprising in combination a motor cylinder, a pair of pistons arranged in said cylinder and adapted to reciprocate therein in opposite directions, a coupling gear substantially free from transmitting mechanical energy connecting said pistons for synchronizing the movements thereof, a plurality of compression cylinders arranged asymmetrically on both sides of said motor cylinder, a compressor piston in each compression cylinder, means connecting each motor piston with the compressor pistons on its side oi. the motor cylinder, said compressor piston and said compression cylinder so determining the ratios of the pressures prevailing in each compression cylinder at the outer and inner dead center positions of said compressor piston that, for the working stroke as well as for the return stroke, the sum of the work yielded in all compression cylinders on one side of said motor cylinder is substantially equal to the sum of the work yielded in all compression cylinders on the other side of said motor cylinder.
4. A free piston multi-stage motor compressor according to claim 2, in which the ratios of the initial and end pressures prevailing in said compression cylinder at the outer and inner dead center positions of said compressor'piston are substantially higher on the side oi. the motor cylinder comprising the smaller number of stages than on the other side.
5. A free piston multi-stage motor compressor according to claim 2, in which the ratios of the initial and end volumes available in said compression cylinder at the outer and inner dead center positions of said compressor piston are substantially higher on the side of the motor cylinder comprising the smaller number of stages than on the other side.
6. A freepiston multi-stage motor compressor comprising in combination a motor cylinder, a pair of pistons arranged in said cylinder and adapted to reciprocate therein in opposite directions, means substantially free from transmitting the motor cylinder,
mechanical energy connecting said pistons for synchronizing the movements thereof, a plurality of compression cylinders arranged asymmetrically on both sides or said motor cylinder, a compressor piston in each compression cylinder, valve means associated with at least one of said compression cylinders for discharging, during the initial portion of the compression stroke, a portion of the gas contained in said compression cylinder, rigid connections connecting each motor piston with the compressor pistons on its side of each compressor pistonand each compression cylinder so determining the ratios of the volumes and pressures prevailing in each compressor cylinder at the outer and inner dead center positions of said compressor piston that, for the working stroke as well as for the return stroke, the sum of the work yielded in all compression cylinders on one side of said motor cylinder is substantially equal to the sum of the work yielded in' all compression cylinders on the other side of said motor cylinder.
7. A free piston multi-stage motor compressor comprising in combination a motor cylinder, a pair of pistons arranged in said cylinder and adapted to reciprocate therein in opposite directions, a coupling gear substantially free. from transmitting mechanical energy connecting said pistons for synchronizing the movements thereof, a plurality of compression cylinders arranged asymmetrically on both sides of said motor cylinder, a compressor piston in each compression cylinder, said compression cylinders comprising high pressures and low pressures stages, means in at least one low pressure cylinder for discharging, during the initial portion of the compression stroke, a portion of the gas contained in said cylinder and for delivering said portion to said ,motor cylinder for scavenging purposes, rigid connections connecting each motor piston with the compressor pistons on its side of the motor cylinder, each compressor piston and each compression cylinder so determining the ratios of the volumes and pressures prevailing in each compressor cylinder at the outer and inner dead center positions of said compressor piston that, for the working stroke as well as for the return stroke, the sumof the work yielded in all compression cylinders on one side of said motor cylinder is substantially equal to thesum of the work yielded in all compression cylinders on the other side of said motor cylinder.
8. A free piston multi-stage motor compressor according to claim 1 which comprises in combi-- nation a motor cylinder, a plurality of compression cylinders and pistons provided therein, at least one of said cylinders being adapted to be used, on one side of the piston reciprocating therein, as a compressor chamber and on the other side as a scavenging pump, and valves connecting said pump with said motor cylinder.
'9. In a free piston multi-stage motor compressor according to claim 1, comprising a motor cylinder and a plurality of compression cylinders, the improvement which comprises means for adapting a compression cylinder on one side of said motor cylinder to act as a scavenging pump, and means for adapting a compression cylinder on the other side thereof to act as an energy storage chamber.
10. In a free piston multi-stage motor compressor according to claim 1 comprising a plurality of compression cylinders, the improvement which comprises a discharging chamber, valves connecting at least one of said compression cylinders to said chamber for discharginggas thereto during the compression stroke, said chamber being adapted to gradually increase the pressure of the gas contained in said compression cylinder during the discharge.
11. In a, free piston multi-stage motor compressor' according to claim 1, comprising a motor cylinder and a plurality of compression cylinders, the improvement which comprises means for adapting a compression cylinder on one side of saidmotor cylinder to act as an energy storage 5 chamber.
HERMANN JAmcKE.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE2046631X | 1933-05-20 |
Publications (1)
Publication Number | Publication Date |
---|---|
US2046631A true US2046631A (en) | 1936-07-07 |
Family
ID=7982453
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US725749A Expired - Lifetime US2046631A (en) | 1933-05-20 | 1934-05-15 | Multistage free piston motor compressor |
Country Status (1)
Country | Link |
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US (1) | US2046631A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2554762A (en) * | 1945-01-25 | 1951-05-29 | English Electric Co Ltd | Free piston type internalcombustion compressor |
US3125282A (en) * | 1964-03-17 | Janicke | ||
US20170016387A1 (en) * | 2015-07-17 | 2017-01-19 | Tonand Inc. | Internal Combustion Engine with Integrated Air Compressor |
-
1934
- 1934-05-15 US US725749A patent/US2046631A/en not_active Expired - Lifetime
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3125282A (en) * | 1964-03-17 | Janicke | ||
US2554762A (en) * | 1945-01-25 | 1951-05-29 | English Electric Co Ltd | Free piston type internalcombustion compressor |
US20170016387A1 (en) * | 2015-07-17 | 2017-01-19 | Tonand Inc. | Internal Combustion Engine with Integrated Air Compressor |
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