US2241957A - Motor compressor of the free piston type - Google Patents

Motor compressor of the free piston type Download PDF

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Publication number
US2241957A
US2241957A US282906A US28290639A US2241957A US 2241957 A US2241957 A US 2241957A US 282906 A US282906 A US 282906A US 28290639 A US28290639 A US 28290639A US 2241957 A US2241957 A US 2241957A
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Prior art keywords
compressor
motor
pistons
piston
stage
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Expired - Lifetime
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US282906A
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Pescara Raul Pateras
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Societe dEtudes et de Participations Eau Gaz Electricite Energie SA
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Societe dEtudes et de Participations Eau Gaz Electricite Energie SA
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B71/00Free-piston engines; Engines without rotary main shaft
    • F02B71/04Adaptations of such engines for special use; Combinations of such engines with apparatus driven thereby

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  • the present invention relates to motor compressors of the free piston type having several stages of compression, that is to say to multiple stage motor compressors the pistons of which are of freelywvariable stroke.
  • the chief object of the present invention is to provide a compressor'of this type which is better adapted to meet the' requirements of practice,
  • I provide all the compression stages on the same side of the motor element of the generator, and at least one energy accumulator on the other side of said motor element, and, on the other hand, I provide means for applying, on the non-active face of at least one of the compressor pistons of the machine, a pressure higher than atmospheric pressure, this pres sure being, for instance, supplied, for each compression stage, by the next lower stage of compression.
  • Fig. l is an axial section diagrammatically showing a multiple stage motor compressor with free pistons made according to thepresent invention
  • Figs. 2 to 4 inclusive are diaphragms illustrating the operation of the various stages of this motor compressor, these diagrams being intended According to the present invention, inorder to provide a multiple stage motor compressor of the free piston type, I proceedim the following manner:
  • the motor element of this machine is made in any suitable usual manner, for instance including at least one motor cylinder I, surrounded by a fluidtight casing 2, and two pistons 31 and 32 synchronized by means of a system of connecting rods 4 and lever 5. When nearing the outer end of their outward stroke, these pistons open inlet ports 6 and outlet ports 1.
  • scavenging pump adapted to ensure the feed and scavenging of the motor cylinder.
  • I further provide means for subjecting the non-active face of at least one of the three pistons P1, P2, P3 to the action of a compensating pressure higher than the atmospheric pressure.
  • section .91 of the low pressure piston must be so chosen that it is inversely proportional to the number of stages, that is to say that $1 is equal to with the compressor element independent of the taken of the fact that the'two faces of pistons- P3 are not of the same free section, a portion.
  • the discharge pressure of the first stage will be caused to act upon the inactive face of piston I: and the discharge pressure. of the second stage will act on the inr active face of piston P3.
  • account should be piston of a compressor element having a single stage of compression capable of being substituted for the three stage element that has been considered, the section of this single piston being then three times the section of the low pressure piston Pi.
  • each compressor stage includes at least one section valve I31, I32 or I33, and at least one discharge valve I41, I42, M3. I provide, respectively between the low pressure stage and the intermediate pressure stage.
  • I connect the whole of the compressor portion to the remainder of the machine in such manner that these two'elements can easily be separated when it is desired to change said compressor portion in order to obtain another discharge pressure, for which purpose, for instance, I provide in casing 2, for the passage 'of the low pressure cylinder, a circular hole 2' against the edge of which I apply a flange I8 integral or rigid with said low pressure cylinder. 1
  • this chamber can be disposed either behind the low pressure piston of the compressor element or behind the piston of the energy accumulator as above mentioned.
  • the first solution will be reserved to the case of compressors having one or two stages in which the size of the low pressure compressor piston is generally suflicient for sucking in a sufficient volume of scavenging air.
  • the size of the low pressure compressor piston would be insufiicient for sucking in a sumcient volume i of scavenging air.
  • a motor compressor which comprises, in combinatio a motor cylinder, at least two motor pistons freely movable in opposed relation in said cylinder, synchronizing means for coupling said pistons with each other, an energy accumulator coupled with one of said motor pistons only, and a multiple stage compressor system coupled entirely with the other motor piston, sald'compressor system; including a plurality of compressor pistons and means for applying to the inactive face of at least one; of said compressor pistons a pressure higher than atmospheric pressure.
  • a motor compressor which comprises, in combination, a motor cylinder, at least two motor pistons with each other, an energy accumulator coupled with one of said motor pistons only, and a multiple stage compressor system coupled entirely with the other motor-piston, said compressor system including a plurality of compressor pistons, and means for applying to the inactive face of each compressor piston the inlet pressure of the corresponding stage.
  • a motor compressor which comprises, in combination, a motor cylinder, at leasttwo motor pistons freely movable in opposed relation to each other in said cylinder, synchronizing means for coupling said pistons with each other, an energy accumulator coupled with one of said pistons including an accumulator piston coupled with said last mentioned motor piston only, and a cylinder cooperating with said accumulator piston, means adapted to cooperate with said accumulator piston for forming a scavenging pump connected with said motor cylinder, and a multiple stage compressor system coupled entirely with the other motor piston, said compressor'system including a plurality of compressor pistons and means for applying to the inactive face of said-compressor pistons a pressure higher than atmospheric pressure.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Compressors, Vaccum Pumps And Other Relevant Systems (AREA)

Description

R. PATERAS PESCARA MOTOR COMPRESSOR OF THE FREE PISTON TYPE Filed July 5, 1939 v Inventor.- ideal)" aierzs 2%.; Cara,
v Affornega Patented May 13, 1941 Raul Pateras Pescara, Paris, France, assignor of one-tenth to Societc dEtudes et de Participa- 'tions Eau, Gaz, Electricite, Energie S. A., Geneva, Switzerland, a society of Switzerland Application July 5, 1939, Serial No. 282,906 In Luxemburg July 16,1938
-40laims.
The present invention relates to motor compressors of the free piston type having several stages of compression, that is to say to multiple stage motor compressors the pistons of which are of freelywvariable stroke.
The chief object of the present invention is to provide a compressor'of this type which is better adapted to meet the' requirements of practice,
than those used up to this time.
According to an essential feature of the present invention, I provide all the compression stages on the same side of the motor element of the generator, and at least one energy accumulator on the other side of said motor element, and, on the other hand, I provide means for applying, on the non-active face of at least one of the compressor pistons of the machine, a pressure higher than atmospheric pressure, this pres sure being, for instance, supplied, for each compression stage, by the next lower stage of compression.
Other features of the present invention will result from the following detailed description of some specific embodiments thereof.
A preferred embodiment of the present invention will be hereinafter described, with reference to the accompanying drawing, given merely by way of example, and in which: I
Fig. l is an axial section diagrammatically showing a multiple stage motor compressor with free pistons made according to thepresent invention;
Figs. 2 to 4 inclusive are diaphragms illustrating the operation of the various stages of this motor compressor, these diagrams being intended According to the present invention, inorder to provide a multiple stage motor compressor of the free piston type, I proceedim the following manner:
The motor element of this machine is made in any suitable usual manner, for instance including at least one motor cylinder I, surrounded by a fluidtight casing 2, and two pistons 31 and 32 synchronized by means of a system of connecting rods 4 and lever 5. When nearing the outer end of their outward stroke, these pistons open inlet ports 6 and outlet ports 1.
According to the essential feature of the present invention, all the compressor pistons to be provided in the different stages of compression, thatisto say the three pistons, P1, P2, P3 in the case of the three stage motor compressorgiven to facilitate the understandingof the invention.
by way of example, are controlled by the same 7 motor piston. For instance these compressor other side of said last mentioned piston, owing to the action of valves l I and II, a scavenging pump adapted to ensure the feed and scavenging of the motor cylinder. I further provide means for subjecting the non-active face of at least one of the three pistons P1, P2, P3 to the action of a compensating pressure higher than the atmospheric pressure. It will be readily understood that, with such an arrangement, by suitably choosing the characteristics of the compressor portion of this machine, and in particularjthe values of sections s1, s2, and $3 of the compressor pistons same as the values of the compensating pressure or pressures, the algebraic sum of the stresses acting upon the active and non active faces of said compressor pistons can be made substantially equal to the resultant of the efforts exerted on the two faces of the compressor piston of a motor compressor of the same power havinga single stage of compression and the motor portion and the energy' accumulator of which would be identical to those of the machine that is being considered. Therefore, it will be possible, with a machine madeaccording to the present invention, to obtain a satisfactory'coaction of the motor and accumulator elements of said machine with any of a plurality of single or multiple-stage compressor to the condition of equality of the resultant efforts above mentioned, for instance by complying with this condition with an approximation of about 20%. 1
I will now indicate, by way of example, a solution which permits of obtaining, with compressor elements having different numbers of stages,
the constancy of the resultant efiorts applied to the rod of the corresponding motor piston.-
Designating by po the feed pressure of the machine (pa being, as a rule, and as it will beassumed, equal to 1) and by p. the discharge pressure of the last stage, I may arrange that the compression effort developed in each stage is identical.
By choosing, for' the intennediate'pressures 91, 212, p3 Pn-l values which comply with the following condition.
l fi=fi=h P P1 Z 2 Pn-i v that is to say p2=p1, 1213:111 etc., and by giving the compressor pistons sections .91, 82, ss inversely proportional to their discharge pressures, this condition is As a matter of fact the compression efforts developed in the successive compression stages are then:
The sum of these elementary compressor. efforts being equal to n.p1 s1.
If it is desired to have this sum independent of the number of stages of compression, the
section .91 of the low pressure piston must be so chosen that it is inversely proportional to the number of stages, that is to say that $1 is equal to with the compressor element independent of the taken of the fact that the'two faces of pistons- P3 are not of the same free section, a portion.
of the inactive face of said piston being covered' by rod 81. This might be compensated in many different ways, for instance by applying on the inactive faces of one of the pistons, P2
, for instance, a pressure slightly higher than the discharge pressure of the first stage.
I have shown in solid lines, on diagrams m, b1, 01, di, as, 122, c2, d2, as, ba, 03, d3 of Figs. 2 to 4 the resultant efforts as a function of the respective strokes for each of the pistons P1, P2,
P3. I have further shown, in dotted lines, on the diagram aibiCD of Fig. 2 the sum of these three diagrams, which are identical to one another. This resultant diagram would represent the resultant of the efforts on the faces of the number n of stages, it suflices, since the sum of the compression efiortsfis independent of n, to arrange in order that the sum of the efforts exerted on the non-active faces of the pistons may be also independent of n, which result can be obtained, for instance, by applying on the non-active face of each piston the discharge pressure of the next lower stage.
As a matter of fact, in this case, the efforts acting respectively on the non-active faces of each of the pistons have thefollowing values:
f'n pn1 a 1 I and the sum of these eiforts has the following value:
I 11.81 s'i which value is truly independent of the number of stages of the compressor element of the machine.
In particular, for the three stage compressor which is considered, the discharge pressure of the first stage will be caused to act upon the inactive face of piston I: and the discharge pressure. of the second stage will act on the inr active face of piston P3.
As a matter of fact, in order to obtain a wholly accurate compensation, account should be piston of a compressor element having a single stage of compression capable of being substituted for the three stage element that has been considered, the section of this single piston being then three times the section of the low pressure piston Pi.
I might also, taking into account the above explanations, proceed in many different ways for designing the compressor part of a machine,
according to the invention, and, in particular, have recourse to the embodiment illustrated by the drawing.
In this embodiment, each compressor stage includes at least one section valve I31, I32 or I33, and at least one discharge valve I41, I42, M3. I provide, respectively between the low pressure stage and the intermediate pressure stage.
on the one hand, and between the intermediate pressure stage and the high pressure stage, on the other hand, two intermediate reservoirs C1, C2 in which the compressed air is advantageous- ,ly cooled,'for instance by means of refrigerating tubes I5.
7 I connect reservoir Crwith a fluidtight casing I6 surrounding the intermediate pressure cylinder in such manner that the pressure existing in said reservoir can act upon the nonactive face of piston P2, the high pressure cylinder being similarly surrounded by a casing I! connected to reservoir C2. 4 1
And preferably, I connect the whole of the compressor portion to the remainder of the machine in such manner that these two'elements can easily be separated when it is desired to change said compressor portion in order to obtain another discharge pressure, for which purpose, for instance, I provide in casing 2, for the passage 'of the low pressure cylinder, a circular hole 2' against the edge of which I apply a flange I8 integral or rigid with said low pressure cylinder. 1
Concerning the arrangement of the chamber for the compression of the scavenging air, ac-
motor portion of the machine, this chamber can be disposed either behind the low pressure piston of the compressor element or behind the piston of the energy accumulator as above mentioned.
Advantageously, the first solutionwill be reserved to the case of compressors having one or two stages in which the size of the low pressure compressor piston is generally suflicient for sucking in a sufficient volume of scavenging air.
On the contrary, in the case of compressors having more than two stages of compression, the size of the low pressure compressor piston would be insufiicient for sucking in a sumcient volume i of scavenging air.
, second solution and care will be taken to dimension the piston of the energy accumulator so that Use will then be made of the it can suck in through its rear face, a sumcient volume of scavenging air.
Anyway, whatever he the particular embodipractical and eiilcient embodiments of the present I invention it should be well understood that I do not wish to be limited thereto as there might be pistons freely movable in opposed relation in said cylinder, synchronizing means for coupling said changes made in the arrangement, disposition and form of the parts without departing from the principle of the present invention as comprehended within the scope of the appended claims. I I
What I claim is:
1. A motor compressor which comprises, in combinatio a motor cylinder, at least two motor pistons freely movable in opposed relation in said cylinder, synchronizing means for coupling said pistons with each other, an energy accumulator coupled with one of said motor pistons only, and a multiple stage compressor system coupled entirely with the other motor piston, sald'compressor system; including a plurality of compressor pistons and means for applying to the inactive face of at least one; of said compressor pistons a pressure higher than atmospheric pressure.
2. A motor compressor according to claim 1 in which the last mentioned means are so devised that the pressure acting on the inactive face of at least one of the compressor pistons is of such a value that the sinn of the absolute pres sures acting on the whole of the inactive faces of the compressor pistons of the respective stages is equal to the absolute pressure which would act' on the inactive face of the compressor piston of a single stage compressor of the same power as the multiple stage compressor that is considered and working with a discharge pressure equal to n the discharge pressure of the first stage'of the multiple stage compressor.
-3. A motor compressor which comprises, in combination, a motor cylinder, at least two motor pistons with each other, an energy accumulator coupled with one of said motor pistons only, and a multiple stage compressor system coupled entirely with the other motor-piston, said compressor system including a plurality of compressor pistons, and means for applying to the inactive face of each compressor piston the inlet pressure of the corresponding stage.
- 4. A motor compressor which comprises, in combination, a motor cylinder, at leasttwo motor pistons freely movable in opposed relation to each other in said cylinder, synchronizing means for coupling said pistons with each other, an energy accumulator coupled with one of said pistons including an accumulator piston coupled with said last mentioned motor piston only, and a cylinder cooperating with said accumulator piston, means adapted to cooperate with said accumulator piston for forming a scavenging pump connected with said motor cylinder, and a multiple stage compressor system coupled entirely with the other motor piston, said compressor'system including a plurality of compressor pistons and means for applying to the inactive face of said-compressor pistons a pressure higher than atmospheric pressure.
RAUL PA'rERAs PESCARA.
US282906A 1938-07-16 1939-07-05 Motor compressor of the free piston type Expired - Lifetime US2241957A (en)

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Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2420426A (en) * 1945-04-30 1947-05-13 Herbert W Harrer Compressor
US2466255A (en) * 1940-11-23 1949-04-05 Mercier Ernest Frederic Balanced double-acting engine
US2470231A (en) * 1942-06-25 1949-05-17 Alan Muntz & Co Ltd Internal-combustion operated free-piston machine
US2578439A (en) * 1940-11-23 1951-12-11 Moore Inc Balanced double-acting engine
US2667300A (en) * 1949-06-14 1954-01-26 Participations Soc Et Free piston machine the compressor portion of which includes at least two stages
US3172596A (en) * 1962-01-15 1965-03-09 Arthur S King Free piston engine compressor
US4111609A (en) * 1975-10-22 1978-09-05 Anton Braun Multistage gas compressor
US4115037A (en) * 1975-01-03 1978-09-19 Direct Power Limited Opposed piston internal combustion engine-driven pump
US4516913A (en) * 1977-11-30 1985-05-14 Techniques Girodin Multistage drum compressor
US4705460A (en) * 1985-02-26 1987-11-10 Anton Braun Bounce chambers for multi-cylinder linear engine compressors
US5525044A (en) * 1995-04-27 1996-06-11 Thermo Power Corporation High pressure gas compressor
US20100192764A1 (en) * 2009-02-05 2010-08-05 Ries James D Variable-displacement piston-cylinder device
US20170016387A1 (en) * 2015-07-17 2017-01-19 Tonand Inc. Internal Combustion Engine with Integrated Air Compressor
CN117108476A (en) * 2023-10-24 2023-11-24 自贡诺力斯百盛压缩机有限公司 Variable-frequency gas compressor

Cited By (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2466255A (en) * 1940-11-23 1949-04-05 Mercier Ernest Frederic Balanced double-acting engine
US2578439A (en) * 1940-11-23 1951-12-11 Moore Inc Balanced double-acting engine
US2470231A (en) * 1942-06-25 1949-05-17 Alan Muntz & Co Ltd Internal-combustion operated free-piston machine
US2420426A (en) * 1945-04-30 1947-05-13 Herbert W Harrer Compressor
US2667300A (en) * 1949-06-14 1954-01-26 Participations Soc Et Free piston machine the compressor portion of which includes at least two stages
US3172596A (en) * 1962-01-15 1965-03-09 Arthur S King Free piston engine compressor
US4115037A (en) * 1975-01-03 1978-09-19 Direct Power Limited Opposed piston internal combustion engine-driven pump
US4111609A (en) * 1975-10-22 1978-09-05 Anton Braun Multistage gas compressor
US4516913A (en) * 1977-11-30 1985-05-14 Techniques Girodin Multistage drum compressor
US4705460A (en) * 1985-02-26 1987-11-10 Anton Braun Bounce chambers for multi-cylinder linear engine compressors
WO1989000245A1 (en) * 1985-02-26 1989-01-12 Anton Braun Bounce chambers for multi-cylinder linear engine compressors
US5525044A (en) * 1995-04-27 1996-06-11 Thermo Power Corporation High pressure gas compressor
US20100192764A1 (en) * 2009-02-05 2010-08-05 Ries James D Variable-displacement piston-cylinder device
US7779627B1 (en) 2009-02-05 2010-08-24 Ries James D Variable-displacement piston-cylinder device
US20170016387A1 (en) * 2015-07-17 2017-01-19 Tonand Inc. Internal Combustion Engine with Integrated Air Compressor
CN117108476A (en) * 2023-10-24 2023-11-24 自贡诺力斯百盛压缩机有限公司 Variable-frequency gas compressor
CN117108476B (en) * 2023-10-24 2024-01-23 自贡诺力斯百盛压缩机有限公司 Variable-frequency gas compressor

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