US963788A - Air-compressor. - Google Patents
Air-compressor. Download PDFInfo
- Publication number
- US963788A US963788A US36264407A US1907362644A US963788A US 963788 A US963788 A US 963788A US 36264407 A US36264407 A US 36264407A US 1907362644 A US1907362644 A US 1907362644A US 963788 A US963788 A US 963788A
- Authority
- US
- United States
- Prior art keywords
- piston
- crank
- compressor
- engine
- shaft
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04B—POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
- F04B17/00—Pumps characterised by combination with, or adaptation to, specific driving engines or motors
- F04B17/05—Pumps characterised by combination with, or adaptation to, specific driving engines or motors driven by internal-combustion engines
Definitions
- This invention relates to direct-connected four-cycle gas engine actuated air. compressors.
- the object of thisinvention is to provide means whereby an air compressor may be actuated by four-cycle gas engines and in such a manner that for each excursionof the com ession piston or each compression stroke thereof there will be a drivin impulse from the engine; in other words, anexplosion will be produced to exert its driving power on the crank-shaft each time work is applied to it from the compressor.
- a pair of four cycle engines are coupled up to the crank shaft of the compressor and the explosions are so timed that there will be an explosion to each rotation of the shaft, the explosions taking place alternately in the cylinders. The explosions will take place at such times that the expansive force of each explosion will give a working impulse to the crank shaft at the time the compressor piston is making.
- the piston, pitman and theconnections of the compressor may be made double the weight of the piston, pitman and con'pections for each of the engines, that is, the
- Fig. 2 is a lon itudinal section 9 the device illustrated in ig. 1.
- Fig. 3 is a cross section through the compressor takenon a plane in about the line 3-'3 of Fig. 2. Fig.
- the crank shaft designated by 10
- the crank shaft is shown sup orted bya number of bearlngs 11 carried y the framing member 12, which framing member constitutes the lower portion of the crank casing.
- This framing member .12 may be mounted upon a sub-base 13 when it is desired to use the structure as a stationary device.
- the caps 14 of the end bearings for the crank shaft are carried by the up er framing member 15 which constitutes t e upper portion of the crank case, and the caps 140 for the intermediate bearings are free from the casing.
- Two four cycle gas engine cylinders 40 and 60 are shown mounted uponthe framing and opening at their back ends into the crank casing.
- Pistons 41 and .61 are mounted within the respective cylinders and-carry pins 42 62 connected by pitmen 4363 with crank pins 44 64 upon the crank shaft 10.
- the supply for each ofthese cylinders is drawn in through a valve -4565,' receiving suppl from supply pipes, designated without pre exhaust from the respective cylinders willbe through valves 4666, the valve stems 4767 being controlled by cams 48-68 upon a cam shaft 18, which cam shaft has a gear wheel 19 meshing with an idler 20 which engages a pinion 21 fast'with the crank shaft and with the fly wheel 22 which is carried by the crank shaft.
- This gearing is two to one.
- the compression cylinder 80 isshown in the present instance mounted upon the framing and opening into the crank case and situated between the cy1inders 40 and 60. Its piston 81 carries a pin 82 pivoted to the pitman 83 which is articulated to the wrist pin 84 upon the crank shaft 10. It will be seen that the piston, pitman and crank pin for the compressor are heavier than those for the engine cylinders. This is for providing equal weight so that the combined weight of these parts of the engines will equal the weight of the similar parts connected with the compressor. This is for the purpose of balancing.
- the crank pins 44-64 are shown upon one side of the shaft and the crank pin 84 is in the present instance disposed diametrically opposite upon the other side.
- crank shaft 10 adjacent to the cranks carrying the wrists 44-64 is shown as carrying projections 23 projecting toward the side carrying the crank pin 84 for the purpose of, bringing as much weight upon. one side of the crank shaft as there is upon the other side.
- the two engine cranks will balance these projections and the compressor crank. It will thus be seen that the structure is mechanically balanced by having the various parts properly proportioned; it is balanced as to power by having the parts made so that an explosion occurs for each working stroke of the compressor, and it is also balanced as to power and to structure by having the compressor located between two power cylinders.
- the engine cylinders are provided with sparking devices 4969 respectively, and each of these is connected up with a spark coil 5070 by circuit wires 517 1, both of which are grounded on the frame at 100 by a common wire 101 in the circuits 517 1.
- the current for the primary circuit is shown as being derived from a battery 102 which is grounded at 100 by being connected to the wire 101 by means of a wire 103, switch 104 and wire 105 at one end and the other 1 end having a wire 106 which is connected to the primary coils of the spark coils by means of wires 55-75.
- the other terminals a set screw 110 is provided for fastening it in its adjusted position.
- the contacting member 11 of the commutator is carried by a frame 113 secured to the shaft 18.v Since the gearing between the shaft 18 and the crank shaft is one to two the primary circuit of each of the spark coils will be closed at each second rotation of the crank shaft, and at each rotation of the crank shaft one or the other of the circuits will be closed. In the positions illustrated the primary circuit for the spark coil 50 is closed and this primary circuit may be traced as follows: circuit closer contact 111, contact 53, wire 52, the primary coil, not illustrated, for the sparking 'COll 50, wire 55, wire 106, battery 102', wire 105, switch 104, wires 103 and 101 to the casing at 100, shaft 18, frame 118. At different times in the running of a gas engine the sparking will take place at dif ferent periods of the piston movement and at different times relative to the exhaust valve action. In the illustration in Fig. 5
- the crank pin 44 is shown on its dead center, the supply valve is shown as closed and the sparking device in operation, so that the primary coil having been closed in the manner described the secondary circuit will carry the high tension current from the sparking coil 50 by means of the wire 51 to the spark plug 49, causing a spark to jump from one point to the other of said sparking plug and ground on the casing of the engine unit and find its way by the various parts to the point 100 and then return by the wire 101 to the sparking coil 50.
- the exhaust valve 66 communicating with the cylinder 60 is in this illustration shown as open; it, however, will be permitted to close at the proper time and the sparking to take place at the spark plug 69 at the proper time for this.
- one of the engine pistons, as 41 will have an expansive impulse given to it during the time that the other, as 61, is drawing in its supply of gas which supply when compressed will be exploded and-the expansive force of the explosion will be communicated to the wrist pin 64 on the crank shaft while the other piston, as 41, is drawing in its supply.
- the air for supplying the compressor may be brought to it through a pipe 85 entering, in the present instance, the lower portion of a chamber 86, the upper portion of which chamber 86 communicates by means of a port 87 with the cylinder 80, v
- valve 88 may be held from its seat when it is desired to run the engines for power and out out the air compressmg feature.
- the end of the crank shaft is shown as projectin at 24 and provided with akeyway 25 to which a pulley or some other power transmission device may be attached.
- a port 96 is provided between .the limits of stroke of the compres- 1 sion piston which is normally closed by a valve 97 controlled by a screw 98 and hand wheel'99. If now it is. desired to decrease the amount of air'delivered, either for the purpose of having that which is delivered under a higher state of compression, or if it is desiredto take off some of the power from the engine in another form, this port will be opened and'the first portion of the working excursion of the piston will necessarily'be rendered idle, the second portion will be compressing.
- the momentum acquired by the parts while the compressor is idle will be utilized with the workmg force that is still being expended upon to the representation of the electrical devices, that the explosive mixture has been compressed in the cylinder 40 and exploded and that the piston 41 is moving downward responsive to the expansion following such explosion and that the driving impulse thereof is being imparted tov the crank shaft 10 through the wrist pin 44 and that the wrist pin 84 will be raised by the crank shaft 10, which will force the piston 81 into the cylinder 80 thereby first closing the port 93 and forcing the charge of air, when this has been compressed to a certain amount, past the back pressure valve 94 and into the service pipe 95.
Landscapes
- 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
I 1 H. MERRILL.
AIR COMPRESSOR.
APPLICATION FILED MAR. 16, 1907.
963,788o Patented July 12, 1910 5 SHEETS-SHEET 1.
WITNESSES: INVENTOR Franklfiierrill,
4K4Me/ (/UTORIVH P. H. MERRILL.
AIR COMPRESSOR.
APPLIOATION FILED MAR. 16, 1907.
Patented July 12, 1910..
5 SHEETS-SHEET 2.
' ATTORNEY INVE/VTUR Hank hf filer/ill W/TIVESSES: v
F. 'H. MERRILL. AIR COMPRESSOR. APPLICATION FILED mm. 16, 1907.
Patented July 12, 1910.
5 SHEETS-SHEET 8.
I WIT NESSE 8:
Mfia
we mm mfi k M H hrromvEr F. H. MERRILL.
AIR COMPRESSOR.
APPLICATION FILED MAR.16, 1907.
Patented July 12, 1910.
6 SHEETS-SHEET 4.
145!!! IIIIIIIIIIIAAJ 1 ATTORNEY.
m/yHvmR Frank h. errz'll,
. WITNESSES.
mzfl
F. H. MERRILL.
AIR COMPRESSOR. I APPLICATION FILED MAK.16,1907'.
963,788. Patented July 12,1910.
5 SHEETSSHEBT 5.
WITNESSES. INVENTOR v v flank if Merrill, ma @5 Br C v JUTOR/VEY U IT STATES PATE FRANK HEATH MERRILL, F PLAINFIELD, NEW JERSEY, ASSIGNORBY MESNE AS- SIGNMENTS, TO GAS ENGINE PNEUMATIC COMPANY, OF PLAINFIELD, NEW JERSEY,
engine piston t A CORPORATION OF NEW: JERSEY.
am-comrnnsson.
Specification of Letters ratent. Application filed March 16, 1907. Serial No. 362,644.
I Patented July 12, 1910.
- .This invention relates to direct-connected four-cycle gas engine actuated air. compressors.
' The object of thisinvention is to provide means whereby an air compressor may be actuated by four-cycle gas engines and in such a manner that for each excursionof the com ession piston or each compression stroke thereof there will be a drivin impulse from the engine; in other words, anexplosion will be produced to exert its driving power on the crank-shaft each time work is applied to it from the compressor. To accomplish this a pair of four cycle engines are coupled up to the crank shaft of the compressor and the explosions are so timed that there will be an explosion to each rotation of the shaft, the explosions taking place alternately in the cylinders. The explosions will take place at such times that the expansive force of each explosion will give a working impulse to the crank shaft at the time the compressor piston is making.
its working stroke or outward excursion.
In the use of a single four cycle engine,
that is one-cylinder and piston, for driving" an air compressor, it has been found that an undue amount of vibration is produced owing to the fact that the parts are not evenly balanced, and also to the further'factthat during the. sup ly o'r suction stroke of the he fly wheel and other parts must have momentum enough to carry the air compressor iston to the full extent of its working stro e. The compressor piston will make two working strokes to one workgiston. Thevibra tion of such engines has een so great as to preclude the construction of the samein a portable form; they have had to be built upon heavy foundations; but by my present im rovement it will be feasible to construct a evice in portable form ow ng to the fact that the vibration is minimized.
The piston, pitman and theconnections of the compressor -may be made double the weight of the piston, pitman and con'pections for each of the engines, that is, the
combined weight if the pistons of the engines and the parts which connect these to QFFICE' I the cranks will be equal to the weight of the piston of the compressor and .the parts which connect it to the crank, so thatthe mechanism will be evenly balanced. In the drawings accompanyin and formn a part of this specification 'gurel is a si e elevation of a practicable embodiment.
of a form of my present im rovement. Fig. 2 is a lon itudinal section 9 the device illustrated in ig. 1. Fig. 3 is a cross section through the compressor takenon a plane in about the line 3-'3 of Fig. 2. Fig.
at is a cross section of one of the engines. lane inabout the line 4-4 of taken on a Fig. 2; and ig. 5 shows the lower portion plane illustrated in Fig. '1 and the upper portion of the crank case at a plane forward of such plane and in the plane of the valve of the crank case in' section on the same View since it is intended as a diagrammatic view for illustrating-the electrical circuits ton-the spark lugs together with a form of commutator or closing the circuits in proper timing.
The crank shaft, designated by 10, is shown sup orted bya number of bearlngs 11 carried y the framing member 12, which framing member constitutes the lower portion of the crank casing. This framing member .12 may be mounted upon a sub-base 13 when it is desired to use the structure as a stationary device. The caps 14 of the end bearings for the crank shaft are carried by the up er framing member 15 which constitutes t e upper portion of the crank case, and the caps 140 for the intermediate bearings are free from the casing. Two four cycle gas engine cylinders 40 and 60 are shown mounted uponthe framing and opening at their back ends into the crank casing. Pistons 41 and .61 are mounted within the respective cylinders and-carry pins 42 62 connected by pitmen 4363 with crank pins 44 64 upon the crank shaft 10. The supply for each ofthese cylinders is drawn in through a valve -4565,' receiving suppl from supply pipes, designated without pre exhaust from the respective cylinders willbe through valves 4666, the valve stems 4767 being controlled by cams 48-68 upon a cam shaft 18, which cam shaft has a gear wheel 19 meshing with an idler 20 which engages a pinion 21 fast'with the crank shaft and with the fly wheel 22 which is carried by the crank shaft. This gearing is two to one. The compression cylinder 80 isshown in the present instance mounted upon the framing and opening into the crank case and situated between the cy1inders 40 and 60. Its piston 81 carries a pin 82 pivoted to the pitman 83 which is articulated to the wrist pin 84 upon the crank shaft 10. It will be seen that the piston, pitman and crank pin for the compressor are heavier than those for the engine cylinders. This is for providing equal weight so that the combined weight of these parts of the engines will equal the weight of the similar parts connected with the compressor. This is for the purpose of balancing. The crank pins 44-64 are shown upon one side of the shaft and the crank pin 84 is in the present instance disposed diametrically opposite upon the other side. The crank shaft 10 adjacent to the cranks carrying the wrists 44-64 is shown as carrying projections 23 projecting toward the side carrying the crank pin 84 for the purpose of, bringing as much weight upon. one side of the crank shaft as there is upon the other side. The two engine cranks will balance these projections and the compressor crank. It will thus be seen that the structure is mechanically balanced by having the various parts properly proportioned; it is balanced as to power by having the parts made so that an explosion occurs for each working stroke of the compressor, and it is also balanced as to power and to structure by having the compressor located between two power cylinders.
The engine cylinders are provided with sparking devices 4969 respectively, and each of these is connected up with a spark coil 5070 by circuit wires 517 1, both of which are grounded on the frame at 100 by a common wire 101 in the circuits 517 1. The current for the primary circuit is shown as being derived from a battery 102 which is grounded at 100 by being connected to the wire 101 by means of a wire 103, switch 104 and wire 105 at one end and the other 1 end having a wire 106 which is connected to the primary coils of the spark coils by means of wires 55-75. The other terminals a set screw 110 is provided for fastening it in its adjusted position. The contacting member 11 of the commutator is carried by a frame 113 secured to the shaft 18.v Since the gearing between the shaft 18 and the crank shaft is one to two the primary circuit of each of the spark coils will be closed at each second rotation of the crank shaft, and at each rotation of the crank shaft one or the other of the circuits will be closed. In the positions illustrated the primary circuit for the spark coil 50 is closed and this primary circuit may be traced as follows: circuit closer contact 111, contact 53, wire 52, the primary coil, not illustrated, for the sparking 'COll 50, wire 55, wire 106, battery 102', wire 105, switch 104, wires 103 and 101 to the casing at 100, shaft 18, frame 118. At different times in the running of a gas engine the sparking will take place at dif ferent periods of the piston movement and at different times relative to the exhaust valve action. In the illustration in Fig. 5
the crank pin 44 is shown on its dead center, the supply valve is shown as closed and the sparking device in operation, so that the primary coil having been closed in the manner described the secondary circuit will carry the high tension current from the sparking coil 50 by means of the wire 51 to the spark plug 49, causing a spark to jump from one point to the other of said sparking plug and ground on the casing of the engine unit and find its way by the various parts to the point 100 and then return by the wire 101 to the sparking coil 50. The exhaust valve 66 communicating with the cylinder 60 is in this illustration shown as open; it, however, will be permitted to close at the proper time and the sparking to take place at the spark plug 69 at the proper time for this. Since the circuits are substantially the same for both spark plugs it will be unnecessary to describethe same in detail for each. By this means one of the engine pistons, as 41, will have an expansive impulse given to it during the time that the other, as 61, is drawing in its supply of gas which supply when compressed will be exploded and-the expansive force of the explosion will be communicated to the wrist pin 64 on the crank shaft while the other piston, as 41, is drawing in its supply.
The air for supplying the compressor may be brought to it through a pipe 85 entering, in the present instance, the lower portion of a chamber 86, the upper portion of which chamber 86 communicates by means of a port 87 with the cylinder 80, v
This is particularly useful when the apparatus is used for construction or repa1r work, as for instance it may be desired to use the compressor for supplymg the power forpneumatic 'riveters, and it may at times be necessary to use the engine for performing other work on the job, so' that all it will be required to do when 1t 1s deslred to I cut out the compression feature and use the air in its movement, and to avoid this detraction of the efficiency ofthe device a port 93 from the supply chamber 86 is prov ded, so that it will be uncovered by the-piston 81 in its extreme downward stroke or its recession movement. This, of course, will permit the cylinder to fill'and upon the inauguration of the upward stroke of the piston the port will be closed and the compressed charge will be forced out through a valve, designated in a general way by 94, from which the compressed charge will pass I through a pipe 95 tosome convenient point of storage or utilization. The back pressure supply valve and the back pressure valve through which the compressed charge is forced form no part of my-present improvement, and, therefore, will not be described in detail since the' form illustrated isnow well known in the art.
At times it may be desired'to compress a smaller amount of air -than the full capacity of the cylinder, but with a higher degree of compression, without increasing the power'which is driving thev compressor. For this purpose a port 96 is provided between .the limits of stroke of the compres- 1 sion piston which is normally closed by a valve 97 controlled by a screw 98 and hand wheel'99. If now it is. desired to decrease the amount of air'delivered, either for the purpose of having that which is delivered under a higher state of compression, or if it is desiredto take off some of the power from the engine in another form, this port will be opened and'the first portion of the working excursion of the piston will necessarily'be rendered idle, the second portion will be compressing. If the engine has not had other work thrown upon it the momentum acquired by the parts while the compressor is idle will be utilized with the workmg force that is still being expended upon to the representation of the electrical devices, that the explosive mixture has been compressed in the cylinder 40 and exploded and that the piston 41 is moving downward responsive to the expansion following such explosion and that the driving impulse thereof is being imparted tov the crank shaft 10 through the wrist pin 44 and that the wrist pin 84 will be raised by the crank shaft 10, which will force the piston 81 into the cylinder 80 thereby first closing the port 93 and forcing the charge of air, when this has been compressed to a certain amount, past the back pressure valve 94 and into the service pipe 95. And while the piston 41 is moving downward responsive to the expansion following the explosion the piston 61 will also be moving downward but will be drawing in a sup ly of explosive mixture, generally gas and air, which upon themovement of the crank shaft, which will bring down the piston 81 to draw in its supply of air, both engine pistons will be moving idly up, the engine piston 41 for expelling the. products of combustion and scavenging the cylinder 40 and the piston 61 for compressing its supply of explosive mixture preparatory to the explosion thereof.
By the means just described it is possible to employ in connection with an air compressor gas engines of the four cycle type and to have an explosion exert its force upon the compressor at each compression stroke thereof which will afford even running and balancmg of the apparatus and avoid much vlbration which takes place when'but one four cycle engine cylinder is employed for dr ving a compressorwhich is coupled to it 1n such a manner that two compression strokes take place at each explosion.
Havingdescribed my invention I claim: 1'. In an air compressor, the combination with a crank shaft, of a compressor cylinder, a piston in the'compressor cylinder directly connected to one side of the crank shaft, a pair of four-cycle gas-engine cylinders situated-upon opposite sides of said compressor piston, pistons in said gas engine cylinders of the driven piston and pitman being double a piston in the compressor cylinder directly connected to one side of the crank shaft,.a
pair of four-cycle gas-engine cylinders situated upon opposite sides of said com ressor piston, pistons in said gas engine cy inders directly connected to the other side of said crank shaft, spark devices in said engine cylinders, and commutators for alternately effecting explosions in said cylinders.
3. The combination with a pair of power pistons, of "a driven piston, a crank shaft, two cranks and crank wrists on one side of the shaft for the power pistons, and balancing extensions and a crank and wrist for the driven piston on the other side of the shaft, the two cranks and the one crank and extensions being substantially equal in weight, pitinen connecting the respective pistons to the crank wrists, the crank wrist for the driven piston being double the weight of the wrists for the power pistons, and the weight the weight of each of the power pistons and pitmen.
t. The combination with a pair of power pistons, of a driven piston located between these and having a weight equal to their combined weight, a crank shaft, two cranks and crank wrists on one side of the shaft for the power pistons, and a balancing extension from each of said cranks and a crank and wrist for the driven piston on the other side of the shaft, the two cranks and wrists and the one crank, wrist and extensions being substantially equal in weight, pitmen connecting the respective pistons to the crank wrists, the weight of the driven pitman being equal to the combined weight of the power pitmen.
5. The combination in an air compressor, of a compressor piston, a crank shaft having a crank upon one side, a pitman connecting this crank to the piston, a pair of gas-engine cylinders located upon respective sides of said compressor piston, a pair of cranks upon the other side of said crank shaft, pitmen connecting these cranks respectively to the engine pistons, each of said engine pistons and pitmen being substan tially half the weight of the compressor piston and pitman.
6. In an air compressor, the combination with a cylinder and a piston therein, of a supply chamber, a supply port at the head of the cylinder and in communication with the supply chamber, a back pressure valve controlling the said port, port in the cylinder positioned to be normally covered by the piston and to be uncovered by the piston at its extreme outward stroke, and an escape valve opening into the said supply" chamber for reducing the efficient length of the cylinder.
Signed at Nos. 9-15 Murray street, New York, N. Y., this 13th day of March, 1907.
FRANK HEATH'MERRILL.
Witnesses: I
CHAS. LYON RUssELL, FRED. J. Donn.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US36264407A US963788A (en) | 1907-03-16 | 1907-03-16 | Air-compressor. |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US36264407A US963788A (en) | 1907-03-16 | 1907-03-16 | Air-compressor. |
Publications (1)
Publication Number | Publication Date |
---|---|
US963788A true US963788A (en) | 1910-07-12 |
Family
ID=3032185
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US36264407A Expired - Lifetime US963788A (en) | 1907-03-16 | 1907-03-16 | Air-compressor. |
Country Status (1)
Country | Link |
---|---|
US (1) | US963788A (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2545793A (en) * | 1947-06-23 | 1951-03-20 | Ricardo & Co Engineers | Internal-combustion engine operating on the four-stroke cycle with compression ignition |
US2614497A (en) * | 1947-02-15 | 1952-10-21 | Ingersoll Rand Co | Combined compressor and engine |
US4509474A (en) * | 1981-03-13 | 1985-04-09 | Johann Schmuck | Piston machine |
US6318977B1 (en) * | 1997-10-06 | 2001-11-20 | Worksmart Energy Enterprises, Inc. | Reciprocating compressor with auxiliary port |
US20060201171A1 (en) * | 2005-03-10 | 2006-09-14 | Sunpower, Inc. | Dual mode compressor with automatic compression ratio adjustment for adapting to multiple operating conditions |
-
1907
- 1907-03-16 US US36264407A patent/US963788A/en not_active Expired - Lifetime
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2614497A (en) * | 1947-02-15 | 1952-10-21 | Ingersoll Rand Co | Combined compressor and engine |
US2545793A (en) * | 1947-06-23 | 1951-03-20 | Ricardo & Co Engineers | Internal-combustion engine operating on the four-stroke cycle with compression ignition |
US4509474A (en) * | 1981-03-13 | 1985-04-09 | Johann Schmuck | Piston machine |
US6318977B1 (en) * | 1997-10-06 | 2001-11-20 | Worksmart Energy Enterprises, Inc. | Reciprocating compressor with auxiliary port |
US20060201171A1 (en) * | 2005-03-10 | 2006-09-14 | Sunpower, Inc. | Dual mode compressor with automatic compression ratio adjustment for adapting to multiple operating conditions |
US7409833B2 (en) | 2005-03-10 | 2008-08-12 | Sunpower, Inc. | Dual mode compressor with automatic compression ratio adjustment for adapting to multiple operating conditions |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US2639699A (en) | Two-cycle engine and improved crankcase induction means therefor | |
US963788A (en) | Air-compressor. | |
US5303679A (en) | Rotary internal combustion engine | |
US2345056A (en) | Internal combustion engine | |
US1146864A (en) | Internal-combustion engine. | |
US773206A (en) | Gas-engine. | |
US719547A (en) | Explosive-engine. | |
US2696343A (en) | Internal-combustion engine with compressor | |
US1614867A (en) | Two-stroke-cycle opposed-piston internal-combustion engine | |
US928405A (en) | Internal-combustion engine. | |
US1436434A (en) | Internal-combustion engine | |
US809451A (en) | Double-acting explosive-engine. | |
US1039704A (en) | Internal-combustion engine. | |
US2474631A (en) | Internal-combustion engine | |
US1368359A (en) | Rotary internal-combustion engine | |
US1439958A (en) | Internal-combustion engine | |
US931531A (en) | Gas-engine. | |
US1335324A (en) | Internal-combustion engine | |
US1211950A (en) | Internal-combustion engine. | |
US990082A (en) | Internal-combustion engine. | |
US758943A (en) | Balanced valveless two-cycle gas-engine. | |
US640672A (en) | Gas-engine. | |
US1109518A (en) | Internal-combustion engine. | |
US2306217A (en) | Internal combustion engine | |
US1429078A (en) | Two-cycle internal-combustion engine |