US2991773A - Free-piston machines - Google Patents
Free-piston machines Download PDFInfo
- Publication number
- US2991773A US2991773A US823396A US82339659A US2991773A US 2991773 A US2991773 A US 2991773A US 823396 A US823396 A US 823396A US 82339659 A US82339659 A US 82339659A US 2991773 A US2991773 A US 2991773A
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- piston
- compressor
- pistons
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- case
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01B—MACHINES OR ENGINES, IN GENERAL OR OF POSITIVE-DISPLACEMENT TYPE, e.g. STEAM ENGINES
- F01B11/00—Reciprocating-piston machines or engines without rotary main shaft, e.g. of free-piston type
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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
-
- 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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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C5/00—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion
- F02C5/06—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion the working fluid being generated in an internal-combustion gas generated of the positive-displacement type having essentially no mechanical power output
- F02C5/08—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion the working fluid being generated in an internal-combustion gas generated of the positive-displacement type having essentially no mechanical power output the gas generator being of the free-piston type
Definitions
- FIGURE 1 is an axial, diagrammatical view showing a free-piston machine constructed according to the teachings of this invention, with a hydraulic operative connection -between the power piston and the compressor pistons; v
- FIGURE 2 illustrates a modified form of embodiment of the machine shown in FIG. 1, wherein the operative connection between the pistons is also efrected by hydraulic means, and
- vFIGURES 3 to 6 illustrate in purely diagrammatical form other modified forms of embodiment of the machine of this invention, which incorporate mechanical connections between the pistons.
- the machine illustrated therein comprises a case 1 having one one side an extension adapted to receive the cylinder 2 in which the power piston 3 is slidably mounted, and on the other side a complementary case 4.
- the compressor piston 5 is movable in the yfirst case 1.
- the combustion chamber is at 21 and the fuel injector at 6.
- the power piston is closed by an annular partition 7 on which is secured at tubular member 8 opening on the one hand into the inner chamber of piston 3 and on the other hand, after extending through the compressor piston 5, into the case 4.
- the compressor piston 5 is rigid with a concentric piston 9 prejecting in the case 4.
- This case 4 is lilled with liquid, for example oil, adapted to flow through the tubular member 8 into the chamber of the power piston 3.
- the cylinder 2 extends within the case 1 and is connected to a suitably shaped ⁇ annular partition 10 connected in turn to the upper portion of the case 1 so as to form a chamber 11 connected in turn through a duct 12 and a non-return valve 13 to the chamber 14 of compressor piston 5.
- the chamber 11 may cornmunicate through ports 15 formed in cylinder 2 with the inner space of this cylinder.
- the exhaust takes place through a port 16 formed on the cylinder 2 and leading into an exhaust pipe 17 connecting this cylinder to the turbine.
- Air inlet ports 18 formed in the wall of case 1 are adapted to be uncovered by the compressor piston 5. The air is compressed at 19 in case 1 by the piston displacements, and forms air-cushions therein.
- This machine operates as follows:
- the explosion produced in chamber 21 forces the power piston 3 down- 2,991,773 Patented July11, ⁇ 1961V wards, that is in the direction of the arrow a, and causes the compressor piston 5 to travel in the opposite direction (arrow b), due to the compression of the liquid column formed inthe case 4, tubular member 8 and inner chamber of piston 3.
- the Vspace 20 located between the two pistons acts as a compressor.
- the power piston 3 and the compressor piston 5 move in the direction of the arrows a and b respectively, so as to compress therebetween in the aforesaid space 20 the air previously introduced through the ports 23 at the end of the preceding stroke.
- a scavenging effect is obtained.
- the pressure exerted on piston 5, plus the vacuum produced at 14, causes the return stroke in the direction of the arrows c, d to begin while stopping the scavenging action, before compressing the fresh air now trapped in chamber 21. It is the kinetic energy of the pistons that enable them to complete their stroke and causes at this time the space 20 (then in underpressure conditions) to communicate through the ports 23 with the surrounding atmosphere.
- the lrst arrangement exemplified in FIG. l corresponds to the conventional generators of the socalled inward compression or return-stroke compression type.
- the arrangement shown in FIG. 2 corresponds to the so-called outward compression or outward-stroke compression type ⁇
- the use of a single compressor piston is not critical, as the most general condition of balance is obtained if:
- a mechanical linkage is provided in the form of connecting-rods and levers between the pistons 3 and 5.
- a rocker 24 fulcrumed on a fixed pivot 25 has its ends pivoted on connecting-rods 26 and 27 connected in turn to these pistons 3 and 5 respectively.
- a lever 28 pivoted at one end on a xed fulcrum 29 has its other end connected to the rod of piston 3, whereas a small lever 30 pivoted intermediate its ends is connected to the end of a rocker 31 pivoted at 32 on a xed fulcrum and connected through its other end to the piston S.
- the rack-forming rod 33 of piston 3 is in meshing engagement with a toothed wheel 34 rigid with another toothed wheel 35 of smaller diameter which meshes with a rack-forming rod 36 of the other piston 5.
- the piston 3 has its rod engaged with a certain clearance in the hollow or tubular rod of piston which acts as a hydraulic cylinder.
- a machine with a free piston comprising a casing, a cylinder in said casing, a motor piston reciprocating in said cylinder, means supplying combustion gas to said cylinder, a compressor piston separated from said free piston and reciprocating in a cylinder coaxial to said first cylinder and means connecting said motor piston with said compressor piston so that said two pistons are displaced in a direction opposite to one another.
- connection between the motor piston and the compressor piston is a hydraulic connection
- the motor piston comprising a hollow rod which opens ⁇ at the interior of a chamber provided in the motor piston and communieating with a chamber provided at the end of the casing, said hollow rod and the two above-mentioned chambers being filled with a liquid so that a displacement of the motor piston corresponds to a displacement in the opposite direction of the compressor piston.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Compressors, Vaccum Pumps And Other Relevant Systems (AREA)
Description
July 11, 1961 J. G. CADIOU 2,991,773
FREE-PISTON MACHINES Filed June 29, 1959 2 Sheets-Sheet l 4 Jean G Cadiou ATTORNEYS July 11, 1961 .1. G. cADloU FREE-PIsToN MACHINES 2 Sheets-Sheet 2 Filed June 29, 1959 INVENTOR Jean G Cadou ATTORNEYS United States Patent O 2,991,773 FREE-PISTON MACHINES Jean Georges Cadiou, Paris, IFrance, assignor to Societe lAnonyme Andre Citroen, Paris, France, a French corporation Filed June 29, 1959, Ser. No. 823,396 Claims priority, application France July 3, 1958 6 Claims. (Cl. 123-46) This invention relates to free-piston machines of the type comprising at least one movable element, and notably to the motor air-compressors and self-generators operating according to the free-piston principle.
It consists essentially in separating the power piston from the compressor piston and in rendering them independent of each other by adequate means, while utiliz- `ing the mass of the compressor piston for compensating the inertia effects caused by the mass of the power piston. r[his invention is also concerned with certain a1'- rangements in connection more particularly with the interdependency of the two power land compressor pistons through hydraulic or mechanical means as will be explained presently in connection Iwith the description of a few forms of embodiment of the invention which are given by way of example with reference to the accompanying drawing in which: J
FIGURE 1 is an axial, diagrammatical view showing a free-piston machine constructed according to the teachings of this invention, with a hydraulic operative connection -between the power piston and the compressor pistons; v
FIGURE 2 illustrates a modified form of embodiment of the machine shown in FIG. 1, wherein the operative connection between the pistons is also efrected by hydraulic means, and
`Referring first to FIG. 1, the machine illustrated therein comprises a case 1 having one one side an extension adapted to receive the cylinder 2 in which the power piston 3 is slidably mounted, and on the other side a complementary case 4. The compressor piston 5 is movable in the yfirst case 1. The combustion chamber is at 21 and the fuel injector at 6. The power piston is closed by an annular partition 7 on which is secured at tubular member 8 opening on the one hand into the inner chamber of piston 3 and on the other hand, after extending through the compressor piston 5, into the case 4. The compressor piston 5 is rigid with a concentric piston 9 prejecting in the case 4. This case 4 is lilled with liquid, for example oil, adapted to flow through the tubular member 8 into the chamber of the power piston 3. The cylinder 2 extends within the case 1 and is connected to a suitably shaped `annular partition 10 connected in turn to the upper portion of the case 1 so as to form a chamber 11 connected in turn through a duct 12 and a non-return valve 13 to the chamber 14 of compressor piston 5. For scavenging purposes, the chamber 11 may cornmunicate through ports 15 formed in cylinder 2 with the inner space of this cylinder. The exhaust takes place through a port 16 formed on the cylinder 2 and leading into an exhaust pipe 17 connecting this cylinder to the turbine. Air inlet ports 18 formed in the wall of case 1 are adapted to be uncovered by the compressor piston 5. The air is compressed at 19 in case 1 by the piston displacements, and forms air-cushions therein.
This machine operates as follows:
During the operation o-f the machine, the explosion produced in chamber 21 forces the power piston 3 down- 2,991,773 Patented July11,`1961V wards, that is in the direction of the arrow a, and causes the compressor piston 5 to travel in the opposite direction (arrow b), due to the compression of the liquid column formed inthe case 4, tubular member 8 and inner chamber of piston 3.
If the cross-sectional areas of the hydraulic pistons are so calculated that the quantities of movement of these pistons are equal, no inertia effect will take place. The air will be compressed at 19 to store up the energy necessary, during the return stroke of the pistons in the direction of the arrows c and d, for compressing the air in the compressor chamber 14, and, through the valve 13 and transfer duct 121, l12, in the annular chamber or accumulator 11. The scavenging action takes place upon completion of the power stroke. The air from Ithe accumulator 11 ows through the inlet ports 15 now uncovered by piston 3 and -scavenges the exhaust gases from chamber 21 through the exhaust ports 16 and pipe 17.
In the modified form of embodiment illustrated in FIG. 2, the component elements similar to those shown in FIG. 1 are designated by the same reference numerals, with a few minor changes. Thus, the air is compressed in the space 20 in case 1 which lies between the pistons 3 and 5. The inlet ports of cylinder 2 are shown at 21 and the exhaust ports at 22. Air is admitted into the aforesaid space 20 through ports 23 uncovered by piston 5. This machine operates as lfollows:
The Vspace 20 located between the two pistons acts as a compressor. Afterthe explosion, the power piston 3 and the compressor piston 5 move in the direction of the arrows a and b respectively, so as to compress therebetween in the aforesaid space 20 the air previously introduced through the ports 23 at the end of the preceding stroke. When the expansion of the burnt or exhaust gas moves the power piston 2 to a position in which firstly the exhaust ports 22 and then the inlet ports 21 are uncovered, a scavenging effect is obtained. The pressure exerted on piston 5, plus the vacuum produced at 14, causes the return stroke in the direction of the arrows c, d to begin while stopping the scavenging action, before compressing the fresh air now trapped in chamber 21. It is the kinetic energy of the pistons that enable them to complete their stroke and causes at this time the space 20 (then in underpressure conditions) to communicate through the ports 23 with the surrounding atmosphere.
Therefore, the lrst arrangement exemplified in FIG. l corresponds to the conventional generators of the socalled inward compression or return-stroke compression type. The arrangement shown in FIG. 2 corresponds to the so-called outward compression or outward-stroke compression type` The use of a single compressor piston is not critical, as the most general condition of balance is obtained if:
(1) The centers of gravity of the power and compressor elements are displaceable along a common axis;
(2) The displacements take place in opposite directions;
(3) The quantities of movement of the power and compressor elements of the machine are constantly equal.
This last requirement (3) may be obtained with a certain approximation by means of rockers or a composite rod-assembly, `and with the maximum accuracy by means of rack-and-pinion assemblies or concentrical hydraulic pistons. Figures 3 to 6 illustrate these forms of embodiment.
In the case shown in FIGS. 3 and 4, a mechanical linkage is provided in the form of connecting-rods and levers between the pistons 3 and 5. In the example shown in FIG. 3, a rocker 24 fulcrumed on a fixed pivot 25 has its ends pivoted on connecting- rods 26 and 27 connected in turn to these pistons 3 and 5 respectively.
Referring now to FIG. 4, a lever 28 pivoted at one end on a xed fulcrum 29 has its other end connected to the rod of piston 3, whereas a small lever 30 pivoted intermediate its ends is connected to the end of a rocker 31 pivoted at 32 on a xed fulcrum and connected through its other end to the piston S.
In the modied form of embodiment illustrated in FIG. 5, the rack-forming rod 33 of piston 3 is in meshing engagement with a toothed wheel 34 rigid with another toothed wheel 35 of smaller diameter which meshes with a rack-forming rod 36 of the other piston 5.
In the last form of embodiment of the invention which is shown in FIG. 6, the piston 3 has its rod engaged with a certain clearance in the hollow or tubular rod of piston which acts as a hydraulic cylinder.
These different forms of embodiment are given only by way of example and should not be construed as limit ing the invention, as many modifications may be brought thereto without departing from the spirit and scope of the invention as set forth in the appended claims.
Thus, in the case of a hydraulic construction, the following alternatives may be contemplated, inter alia:
(i) A regulation of the pressure in the compression chamber, by varying the quantity of oil stored in the case 4.
(ii) A limitation of the piston accelerations by limiting the maximum pressure in case 4.
(iii) The use of oil as a cooling and/or lubricating agent.
(iv) The delivery of power in the form of liquid under pressure issuing from case 4.
The proper timing of the dead centers which is necessary for operating the injection pump may be obtained through mechanical, electrical or other means, for eX- ample as follows:
(a) A rod connected through a fork to the piston 5 so as to be responsive to the movement thereof.
(b) A variable condenser of Which one armature 4 would be the hydraulic piston 9.
(c) A condenser adapted to vary under the influence of the hydraulic pressure, or the direct control of the fuel injection pump by this pressure.
I claim:
l. A machine with a free piston comprising a casing, a cylinder in said casing, a motor piston reciprocating in said cylinder, means supplying combustion gas to said cylinder, a compressor piston separated from said free piston and reciprocating in a cylinder coaxial to said first cylinder and means connecting said motor piston with said compressor piston so that said two pistons are displaced in a direction opposite to one another.
2. A machine as set forth in claim 1 in which the space of the casing comprised between the two pistons, motor and compressor, serves as the compression chamber.
3. A machine as set forth in claim 1 in which the compression chamber is located at the side of the compressor piston opposed to the motor piston.
4. A machine according to claim l in which said connection between the motor piston and the compressor piston is a hydraulic connection, the motor piston comprising a hollow rod which opens `at the interior of a chamber provided in the motor piston and communieating with a chamber provided at the end of the casing, said hollow rod and the two above-mentioned chambers being filled with a liquid so that a displacement of the motor piston corresponds to a displacement in the opposite direction of the compressor piston.
5. In a machine as set -forth in claim 1 wherein said connecting means consist of mechanical elements.
6. In a machine as set forth in claim 1 wherein the mass of the compressor piston is chosen to compensate the inertia effect due to the mass of the motor piston.
References Cited in the Ele of this patent UNITED STATES PATENTS 2,470,231 Beale May 17, 1949 2,473,204 Huber June 14, 1949 2,816,416 French Dec. 17, 1957
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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FR2991773X | 1958-07-03 |
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US2991773A true US2991773A (en) | 1961-07-11 |
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Application Number | Title | Priority Date | Filing Date |
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US823396A Expired - Lifetime US2991773A (en) | 1958-07-03 | 1959-06-29 | Free-piston machines |
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Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3174432A (en) * | 1960-08-12 | 1965-03-23 | Eickmann Karl | Combustion engine for conveying a hydraulic pressure medium |
US3269321A (en) * | 1961-08-01 | 1966-08-30 | Eickmann Karl | Combustion engine for conveying a hydraulic pressure medium |
US3525102A (en) * | 1968-12-17 | 1970-08-18 | Anton Braun | Engine |
US3610214A (en) * | 1970-01-30 | 1971-10-05 | Anton Braun | Unsymmetrical, double-acting free piston engine |
US3610217A (en) * | 1969-10-21 | 1971-10-05 | Anton Braun | Balanced-free piston engine |
US3610216A (en) * | 1969-11-14 | 1971-10-05 | Anton Braun | Balanced-free piston engine |
US3859966A (en) * | 1973-02-16 | 1975-01-14 | Anton Braun | Linear balanced free piston machines |
US4085710A (en) * | 1976-08-03 | 1978-04-25 | Sundar Savarimuthu | Hydraulic engine piston |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2470231A (en) * | 1942-06-25 | 1949-05-17 | Alan Muntz & Co Ltd | Internal-combustion operated free-piston machine |
US2473204A (en) * | 1946-02-05 | 1949-06-14 | Participations Soc Et | Free piston engine control |
US2816416A (en) * | 1955-03-21 | 1957-12-17 | Louis O French | Two cycle internal combustion engine |
-
1959
- 1959-06-29 US US823396A patent/US2991773A/en not_active Expired - Lifetime
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2470231A (en) * | 1942-06-25 | 1949-05-17 | Alan Muntz & Co Ltd | Internal-combustion operated free-piston machine |
US2473204A (en) * | 1946-02-05 | 1949-06-14 | Participations Soc Et | Free piston engine control |
US2816416A (en) * | 1955-03-21 | 1957-12-17 | Louis O French | Two cycle internal combustion engine |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3174432A (en) * | 1960-08-12 | 1965-03-23 | Eickmann Karl | Combustion engine for conveying a hydraulic pressure medium |
US3269321A (en) * | 1961-08-01 | 1966-08-30 | Eickmann Karl | Combustion engine for conveying a hydraulic pressure medium |
US3525102A (en) * | 1968-12-17 | 1970-08-18 | Anton Braun | Engine |
US3610217A (en) * | 1969-10-21 | 1971-10-05 | Anton Braun | Balanced-free piston engine |
US3610216A (en) * | 1969-11-14 | 1971-10-05 | Anton Braun | Balanced-free piston engine |
US3610214A (en) * | 1970-01-30 | 1971-10-05 | Anton Braun | Unsymmetrical, double-acting free piston engine |
US3859966A (en) * | 1973-02-16 | 1975-01-14 | Anton Braun | Linear balanced free piston machines |
US4085710A (en) * | 1976-08-03 | 1978-04-25 | Sundar Savarimuthu | Hydraulic engine piston |
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