CA1145727A - Four stage gas compressor - Google Patents

Four stage gas compressor

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Publication number
CA1145727A
CA1145727A CA000361522A CA361522A CA1145727A CA 1145727 A CA1145727 A CA 1145727A CA 000361522 A CA000361522 A CA 000361522A CA 361522 A CA361522 A CA 361522A CA 1145727 A CA1145727 A CA 1145727A
Authority
CA
Canada
Prior art keywords
stage
piston
chamber
face
cylindrical body
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
Application number
CA000361522A
Other languages
French (fr)
Inventor
Antonio Gozzi
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to CA000361522A priority Critical patent/CA1145727A/en
Application granted granted Critical
Publication of CA1145727A publication Critical patent/CA1145727A/en
Expired legal-status Critical Current

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  • Compressor (AREA)

Abstract

ABSTRACT
A four stage hydraulically operated gas compressor is disclosed.
It includes a double-acting piston operable by pressurised oil and provided with first and second hollow opposed piston rods the first of which is con-nected to a first-stage piston and the second of which is connected to a second-stage piston. The first and second-stage pistons are arranged to slide in first and second jackets respectively and are in a sliding fit upon first and second cylindrical bodies respectively which are fixed to first and second opposed heads. The compressor also includes a first axial suction and delivery duct leading to an end face of the first cylindrical body, a third stage chamber being defined between the end face and one face of the double-acting piston; and a second axial suction and delivery duct leading to an end face of the second cylindrical body, a fourth stage chamber being defined between the end face of said second cylindrical body and the other face of the double-acting piston.

Description

~45727 This invention concerns a four-stage gas compressor, i.e. a machine which compresses gaseous substances such as air, nitrogen or methane and raises them from atmospheric pressure (or from any other pressure whether higher or lower) to a much higher pressure through said machine's four compression stages.
The prior art includes four-stage compressors operated by electric motors or internal combustion engines through crank mechanisms with heavy and cumbersome flywheels to prevent angular speed oscillations. Said prior art also includes one and two stage linear compressors hydraulically operated from the inside of the compressor itself: the two-stage compressors consist of two one-stage linear compressors interconnected with each other.
An object of the present invention is the provision of a relatively compact, single assembly machine which is both four-stage and hydraulically operated.
The present invention provides a four-stage gas compressor including:
a double-acting piston operable by pressurised oil and provided with first and second hollow opposed piston rods the first of which is connected to a first-stage piston and the second of which is connected to a second-stage piston;
said first- and second-stage pistons being arranged to slide in first and second jackets respectively; said first and second hollow piston rods being coupled with a sliding fit to first and second cylindrical bodies acting as fixed pistons of the third and fourth stage respectively; said first and second cylindrical bodies being fixed to first and second opposed heads; said first cylindrical body being axially provided with a first suction and delivery duct; said second cylindrical body being axially provided with a second suction and delivery duct; a third stage chamber being defined between said first cylindrical body and one face of said double-acting piston; said first suction ~457Z7 and delivery duct leading into said third stage chamber; a fourth stage chamber being defined between said second cylindrical body and the other face of said double-acting piston; said second suction and delivery duct leading into said fourth stage chamber.
The invention described herein employs a single mobile element, axially equipped with a double-action hydraulic engine piston, and, in addi-tion, with two pistons for the first and second gas-compression stages, with the gas-compression chambers for the third and fourth stages situated inside the rods of these two pistons, and with the compression itself occurring by means of these same rods. The machine itself has an aligned, coaxial overall design.
The advantages of such a machine are: simplicity and compactness and reduced overall radial and longitudinal dimensions, despite the existence of four stages in a single unit.
By way of example only, a preferred embodiment of the present invention is described in detail with reference to the accompanying drawing, which shows a schematic longitudinal sectional view through a compressor in accordance with the present invention.
Referring to the drawing, a head disc 1 is connected to an intermediate head disc 2 by means of a 3ac~et 3 equipped with a liquid or air cooling sys-tem and centred and fixed to the head disc 1 by screws 4. A cylindrical body 5 acts as a :

~;

.

~5~7'2~ . 4 fixed third stage piston, and is equipped with a head 6 connecting it to the outside of the head di~c ~ by means of screws 7. A cylindrical tubular element 8 coupled with a sliding fit to the body 5 forms the rod of a piston 9, which is fixed to the tubular element 8, to compress the gas in the first stage. A bush 10 is fixed to the intermediate disc 2 by screws 11 and it is internally coupled to the external surface of the tubular element 8 and acts as an oil seal. An end face 12 of the cylindrical body 5 compresses the gas in its third stage.
A double-action piston 13 is internally screwed to the end of the tubular element 8 on the side opposite to the piston 9; this piston 13 creates the alternating motion deriving from the action of the oil contained in the chambers 14 and 15, said oil being pressurised by a hydr~ulic power unit. A jacket 16 surrounds the hydraulic element in which the piston 13 slides and, on one side, it is centred in an annular projection 17 of the disc 2; on the other side, it it centred in an annular projection 18 of ~n intermediate head 19. A cooling jacket 21, equipped with liquid or air cooling system, is centred in the annular projection of the head 19, opposite to the projection 18, and in a head disc 22, and houses the second compression stage~
The assembly consisting of the jacket 16, the head 19, the jacket 21 and the head 22 is all axially joined to the disc 2 by tie rods 23. A cylindrical tubular element 24, analogous and opposite to the cylindrical body 5, acts as the fixed piston of the fourth stage and has a head 25 for connection to the disc 22 by means of scre~Js 26. A cylindrical tubular element 27 is coupled with a sliding fit to the body .

~ ~145~27 5 24 and constitutes the rod of a piston 28 o~ the second compression stageO A bush 29, analogous to the bush 10, is fixed to the disc 19 by means of screws 30 and is internally coupled to the exterior surface of the tubular element 27, to act also as an oil seal. An interior end face 31 of the cylindrical body 24, analogous and opposite to the face 12, compresses the gas in the fourth stage. A reduced diameter threaded end 32 of the piston 13, opposite to the end to which the cylindrical element 8 is screwed, is screwed to the end of the cylindrical tubular element 27, opposite to the end screwed to the piston 28.
A first-stage suction valve 33 connects the tank of gas to be compressed (not shown) to a chamber 34. A first-stage delivery valve 35 connects the chamber 34 to a second_stage chamber 36, via a cooling coil 37, through a suction valve 38. A second-stage delivery valve 39 connects the chamber 36 to a thir~-stage chamber 40, via a cooling coil 41, through a suction valve 42 and an axial suction delivery duct 43.
located in the bod~ 5. A third stage delivery valve 44 connects the chamber 40 to a fourth-stage chamber 45, via cooling coil 46, through a fourth-stage suction valve 47 and an axial suction and delivery duct 48, located in the cylindrical body 24. A delivery valve 49 connects the chamber 45, via a cooling coil 51, to a user 50 which can be a tank.
~ he chamber 52, opposite to the first_stage chamber 34, has an outlet port 53 in the disc 2, which vents into the atmosphere any leakage of gas, and an outlet port 54 to discharge any leakage of oil from the bush 10. A chamber 55 is opposite to the second-stage chamber 36 and has an outlet ., .

.
;.

1:145~7;27 ..
port 56 in the head 19, to vent into the atmosphere any leaka~e Or gas, and a port 57 to discharge an~ leakage of oil from the bush 29~ Gas seals 5~ are secured to the piston 28 and oil seals 59 are inserted into the piston 13.
The piston 9 is provided with a locking nut 60 to be used if the piston has to be screwed to the tubular element 8.
A locking nut 61, analogous to the locking nut 60, fixes the piston 28 to the tubular element 27. The numbers 62 and 63 indicate the oil inlet and drain ports of the chambers 14 and 15 respectively.
The compressor operates as follows: once the oil i6 delivered under pressure to the chamber 14, the piston 13 moves, lowering the volume of the chamber 15, pulling the first-stage piston 9 and pushing the second-stage piston 28.
The movement of the piston 9 increases the volume of the chamber 34 and causes gas to be compressed to be sucked into it th~gh the valve 33. ~he movement of the piston 28 reduces the volume of the chamber 36 and causes the , compression necessary to feed the third-stage chamber 40, through the valves 39 and 42. At the same time, the volu~e of the fourth_stage chamber 45 is reduced, causing the gas . to be compressed to pass through the valve 49 and into the user.
If, on the contrary, the oil is delivered under pressure to the chamber 15, the volume of the chamber 14 is reduced, pushing the first-stage piston 9 and pulling the second . stage piston 28~ ~he movement of the piston 9 reduces the volume of the chamber 34, compressing the gas therein which . . then is fed into the second-stage chamber 36 through the _ 6 --- .

:. ,. ' ' :
. . ~ ' ' ~

fll4~727 valves 35 and 38. Likewise, the volume of the third_star~e chamber 40 is reduced, compressing the gas therein which then is fed into the fourth stage chamber 45 through the valves 44 and 47~ '~his sequence is repeated in the following cycles.
It will be appreciated that the compression ratios of the above compressor stages may be varied if necessary:-for example, each stage may have a compression ratio of 1:~, resulting in an overall compression ratio of 44=256.

., ,7 , .

Claims (2)

THE EMBODIMENTS OF THE INVENTION IN WHICH AN EXCLUSIVE
PROPERTY OR PRIVILEGE IS CLAIMED ARE DEFINED AS FOLLOWS:
1. A four-stage gas compressor including: a double-acting piston operable by pressurised oil and provided with first and second hollow opposed piston rods the first of which is connected to a first-stage piston and the second of which is connected to a second-stage piston; said first- and second-stage pistons being arranged to slide in first and second jackets respectively; said first and second hollow piston rods being coupled with a sliding fit to first and second cylindrical bodies acting as fixed pistons of the third and fourth stage respectively; said first and second cylindrical bodies being fixed to first and second opposed heads; said first cylindrical body being axially pro-vided with a first suction and delivery duct; said second cylindrical body being axially provided with a second suction and delivery duct; a third stage chamber being defined between said first cylindrical body and one face of said double-acting piston; said first suction and delivery duct leading into said third stage chamber; a fourth stage chamber being defined between said second cylindrical body and the other face of said double-acting piston; said second suction and delivery duct leading into said fourth stage chamber.
2, A compressor as claimed in claim 1 wherein said first and second hollow opposed piston rods comprise jackets around the first and second cylindrical bodies respectively.
CA000361522A 1980-10-03 1980-10-03 Four stage gas compressor Expired CA1145727A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CA000361522A CA1145727A (en) 1980-10-03 1980-10-03 Four stage gas compressor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CA000361522A CA1145727A (en) 1980-10-03 1980-10-03 Four stage gas compressor

Publications (1)

Publication Number Publication Date
CA1145727A true CA1145727A (en) 1983-05-03

Family

ID=4118058

Family Applications (1)

Application Number Title Priority Date Filing Date
CA000361522A Expired CA1145727A (en) 1980-10-03 1980-10-03 Four stage gas compressor

Country Status (1)

Country Link
CA (1) CA1145727A (en)

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