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US3071309A - Compressor cylinder and unloader apparatus - Google Patents

Compressor cylinder and unloader apparatus Download PDF

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Publication number
US3071309A
US3071309A US812467A US81246759A US3071309A US 3071309 A US3071309 A US 3071309A US 812467 A US812467 A US 812467A US 81246759 A US81246759 A US 81246759A US 3071309 A US3071309 A US 3071309A
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Prior art keywords
cylinder liner
cylinder
assembly
wall
chamber
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Expired - Lifetime
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US812467A
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Reuben J Hackbart
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Trane Co
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Trane Co
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Priority to US812467A priority Critical patent/US3071309A/en
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04BPOSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
    • F04B49/00Control, e.g. of pump delivery, or pump pressure of, or safety measures for, machines, pumps, or pumping installations, not otherwise provided for, or of interest apart from, groups F04B1/00 - F04B47/00
    • F04B49/22Control, e.g. of pump delivery, or pump pressure of, or safety measures for, machines, pumps, or pumping installations, not otherwise provided for, or of interest apart from, groups F04B1/00 - F04B47/00 by means of valves
    • F04B49/24Bypassing
    • F04B49/243Bypassing by keeping open the inlet valve
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04BPOSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
    • F04B27/00Multi-cylinder pumps specially adapted for elastic fluids and characterised by number or arrangement of cylinders
    • F04B27/08Multi-cylinder pumps specially adapted for elastic fluids and characterised by number or arrangement of cylinders having cylinders coaxial with, or parallel or inclined to, main shaft axis
    • F04B27/10Multi-cylinder pumps specially adapted for elastic fluids and characterised by number or arrangement of cylinders having cylinders coaxial with, or parallel or inclined to, main shaft axis having stationary cylinders
    • F04B27/1036Component parts, details, e.g. sealings, lubrication
    • F04B27/1081Casings, housings
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04BPOSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
    • F04B27/00Multi-cylinder pumps specially adapted for elastic fluids and characterised by number or arrangement of cylinders
    • F04B27/08Multi-cylinder pumps specially adapted for elastic fluids and characterised by number or arrangement of cylinders having cylinders coaxial with, or parallel or inclined to, main shaft axis
    • F04B27/10Multi-cylinder pumps specially adapted for elastic fluids and characterised by number or arrangement of cylinders having cylinders coaxial with, or parallel or inclined to, main shaft axis having stationary cylinders
    • F04B27/1036Component parts, details, e.g. sealings, lubrication
    • F04B27/109Lubrication
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04BPOSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
    • F04B39/00Component parts, details, or accessories, of pumps or pumping systems specially adapted for elastic fluids, not otherwise provided for in, or of interest apart from, groups F04B25/00 - F04B37/00
    • F04B39/12Casings; Cylinders; Cylinder heads; Fluid connections
    • F04B39/125Cylinder heads

Definitions

  • An object of the present invention is to provide a cylinder and unloader construction which is inexpensive to manufacture and is easily assembled.
  • Another object of the present invention is to provide a cylinder and unloader construction which can be readily assembled without damage to the sealing members.
  • a third object of the invention is to provide a refrigeration compressor in which the cylinder liner is located and supported by the casting between the crankcase and the suction chamber and the unloading cylinder is located around the cylinder liner.
  • Another object of the invention is to provide a refrigeration compressor which may readily be serviced in the field in case of damage to the compressor.
  • FIG. 1 is a cross-sectional view of a compressor cylinder and unloader constructed in accordance with my invention.
  • FIG. 2 is a partial section view of the unloader assembly, cylinder liner, and oil pin blown up in detail to show the particulars of my invention.
  • reference number 10 represents a compressor housing in which a multiplicity of operating cylinders are located.
  • the number of cylinders within the housing is optional and not considered to be within the scope of the invention.
  • the compressor housing is closed at the top by cylinder heads 12.
  • Casting or wall 14 separates the discharge chamber 16 from the suction chamber 13.
  • Casting or wall 2i? with integral flange wall 22 separates suction chamber 18 from the crankcase chamber 24.
  • An oil pin 26 is located within flange wall 22 to provide a connection for passage of oil from the unloader control valve (not shown) to the unloading assembly 28.
  • Unloading assembly 23 consists of seal ring 3%, rings 32 and 34.- of neoprene or other suitable material, piston 36, cylinder 38, and unloader springs 4b. The above mentioned unloader assembly is pre-assembled before installation within the compressor.
  • cylinder liner assembly Located within the unloader assembly 23 and abutting the flange wall 22 is the cylinder liner assembly consisting of a liner 4-2, suction valve plate 44, suction valve springs 46, suction valve 43, O-rings 5t), 52, and 64 of neoprene or other suitable material, retaining ring 56, lift pins 53, lift pin springs 60, suction valve lift ring 62, and snap ring 64.
  • Discharge valve cage '70 containing discharge valve 72 within is held into engagement with the cylinder liner assembly by spring means 74.
  • Spring means 74 further provides a safeguard against damage to the compressor if a Slug of liquid refrigerant should pass into the compression chamber.
  • gaseous refrigerant passes from the suction chamber 18, thru suction valve 48 via suction port 61 and into the cylinder liner 42 on the downstroke of piston 76.
  • the gaseous refrigerant is compressed until the refrigerant pressure overcomes the tension of the discharge valve springs and then the compressed refrigerant passes thru dischrage valve 72 into discharge chamber 16.
  • the compressed refrigerant from a multiplicity of discharge cham- 5 hers is then manifolded and discharged from the compressor.
  • the unloading piston assembly 28 surrounding the cylinder liner 42 is oil pressure actuated in a manner shown and described in the patent'of Otto A. Labus et al.,
  • casting 20 is provided with a flange 2.2 integral therewith which supports both the unloader assembly 28 and the cylinder liner assembly.
  • the unloader assembly is first located on the oil pin 26 and then projected towards the casting until the unloader assembly abutts flange wall 22.
  • the cylinder liner assembly is positioned in the unloader as- 20 sembly and moved forward toward-s the casting 20 until the flange 78 on the cylinder liner 42 abutts the flange wall 22 adjacent the base of the unloader assembly.
  • the flange wall 22 provides a supporting surface for both the unloader assembly and the 25 cylinder liner assembly.
  • the inner diameter of the cylinder 38 adjacent the O-ring 52 is greater than the inner diameter of cylinder 38 adjacent the O-ring 54 since the inner surface 53 of cylinder 38 between the chamfers 80 and 82 forms a cylinder of constant radius. Therefore, the outer-diameter of the cylinder liner 42. adjacent the O-ring 52 is greater than the outer diameter of the cylinder liner 42 adjacent O-ring 54-. This construction in conjunction with the chamfers 80 and 82 on the cylinder 3!; prevents destruction of the O-rings 52 and 54 upon assembly of the compressor.
  • My invention provides obvious advantages and eliminates several problem areas found in compressors.
  • My construction allows the unloader assembly to be assembled and placed in position before the liner assembly is Previous to this time, the unloader assembly and the cylinder liner assembly were assembled as a unit and then placed in position in the compressor. Obviously, this type of construction would make it very diflicult to correctly position the unit on the oil pin.
  • a compressor comprising; a housing, a common suction chamber and a common discharge chamber in said housing, first wall means separating said suction chamber from said discharge chamber, a crankcase chamber in said housing, second Wall means separating said suction chamber from said crankcase chamber, means forming openings for a cylinder liner assembly in said first and in said second wall means, oil conducting means in said second Wall means, an annular unloading assembly means connected to said oil conducting means and abutting said second Wall means around said opening in said second wall means, a cylinder liner assembly positioned in said opening in said first wall means and extending through said annular unloading assembly means and abutting said second wall, said cylinder liner assembly including a cylinder liner, said cylinder liner having a first annular sealing member in and surrounding the outer lower diameter portion of said cylinder liner and a second annular sealing member in and surrounding the outer upper diameter portion of said cylinder liner, said unloading assembly means including a cylinder adjacent and surrounding said cylinder liner, said cylinder being in

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Compressor (AREA)

Description

Jan. 1, 1963 R. J. HACKBART 3,071,309
COMPRESSOR CYLINDER AND UNLOADER APPARATUS Filed May 11, 1959 2 Sheets-Sheet l 44 I4 I 46 7 '50 v 66 R I '64 62 \452 32 52 w INVENTOR REUBEN J HACKBART M y W ATTORNEYS Jan. 1, 1963 R. J. HACKBART COMPRESSOR CYLINDER AND UNLOADER APPARATUS Filed May 11, 1959 li -J FIG. 2
2 Sheets-Sheet 2 INVENTOR REUBE'N J HACKBART /W v Zak/sent,-
ATTORNEYS United States Patent Oflfice 3,071,309 Patented Jan. 1, 1963 assignor to The a corporation of This invention relates generally to reciprocating compressors and more particularly to a new and novel cylinder and unloader construction for refrigeration compressors.
An object of the present invention is to provide a cylinder and unloader construction which is inexpensive to manufacture and is easily assembled.
Another object of the present invention is to provide a cylinder and unloader construction which can be readily assembled without damage to the sealing members.
A third object of the invention is to provide a refrigeration compressor in which the cylinder liner is located and supported by the casting between the crankcase and the suction chamber and the unloading cylinder is located around the cylinder liner.
Another object of the invention is to provide a refrigeration compressor which may readily be serviced in the field in case of damage to the compressor.
Other objects and advantages of my invention will be clearly apparent as the specification proceeds to describe the invention with reference to the accompanying drawings, in which:
FIG. 1 is a cross-sectional view of a compressor cylinder and unloader constructed in accordance with my invention; and
FIG. 2 is a partial section view of the unloader assembly, cylinder liner, and oil pin blown up in detail to show the particulars of my invention.
Referring now to the drawings, reference number 10 represents a compressor housing in which a multiplicity of operating cylinders are located. The number of cylinders within the housing is optional and not considered to be within the scope of the invention.
The compressor housing is closed at the top by cylinder heads 12. Casting or wall 14 separates the discharge chamber 16 from the suction chamber 13. Casting or wall 2i? with integral flange wall 22 separates suction chamber 18 from the crankcase chamber 24. An oil pin 26 is located within flange wall 22 to provide a connection for passage of oil from the unloader control valve (not shown) to the unloading assembly 28.
Unloading assembly 23 consists of seal ring 3%, rings 32 and 34.- of neoprene or other suitable material, piston 36, cylinder 38, and unloader springs 4b. The above mentioned unloader assembly is pre-assembled before installation within the compressor.
Located within the unloader assembly 23 and abutting the flange wall 22 is the cylinder liner assembly consisting of a liner 4-2, suction valve plate 44, suction valve springs 46, suction valve 43, O-rings 5t), 52, and 64 of neoprene or other suitable material, retaining ring 56, lift pins 53, lift pin springs 60, suction valve lift ring 62, and snap ring 64.
Discharge valve cage '70 containing discharge valve 72 within is held into engagement with the cylinder liner assembly by spring means 74. Spring means 74 further provides a safeguard against damage to the compressor if a Slug of liquid refrigerant should pass into the compression chamber.
In operation, gaseous refrigerant passes from the suction chamber 18, thru suction valve 48 via suction port 61 and into the cylinder liner 42 on the downstroke of piston 76. On the compression or upstroke of piston 76 the gaseous refrigerant is compressed until the refrigerant pressure overcomes the tension of the discharge valve springs and then the compressed refrigerant passes thru dischrage valve 72 into discharge chamber 16. The compressed refrigerant from a multiplicity of discharge cham- 5 hers is then manifolded and discharged from the compressor.
The unloading piston assembly 28 surrounding the cylinder liner 42 is oil pressure actuated in a manner shown and described in the patent'of Otto A. Labus et al.,
Looking now more particularly at the internal compressor construction, it is seen that casting 20 is provided with a flange 2.2 integral therewith which supports both the unloader assembly 28 and the cylinder liner assembly. In assembly, the unloader assembly is first located on the oil pin 26 and then projected towards the casting until the unloader assembly abutts flange wall 22. After the unloader assembly has been positioned, the cylinder liner assembly is positioned in the unloader as- 20 sembly and moved forward toward-s the casting 20 until the flange 78 on the cylinder liner 42 abutts the flange wall 22 adjacent the base of the unloader assembly. It can readily be seen that the flange wall 22 provides a supporting surface for both the unloader assembly and the 25 cylinder liner assembly.
It should be noted that the inner diameter of the cylinder 38 adjacent the O-ring 52 is greater than the inner diameter of cylinder 38 adjacent the O-ring 54 since the inner surface 53 of cylinder 38 between the chamfers 80 and 82 forms a cylinder of constant radius. Therefore, the outer-diameter of the cylinder liner 42. adjacent the O-ring 52 is greater than the outer diameter of the cylinder liner 42 adjacent O-ring 54-. This construction in conjunction with the chamfers 80 and 82 on the cylinder 3!; prevents destruction of the O- rings 52 and 54 upon assembly of the compressor.
The basic problem solved by the above construction was that the O-rings as they pass an opening upon assembly tend to bulge outwardly and are broken as the cylinder liner passes the particular opening. Looking at FIG. 2, it is seen that Q-ring 54 attached to the cylinder liner must pass openings 84 and 86 in the cylinder 38 before the cylinder liner 42 abutts the flange wall 22. Since the outer diameter of the liner 42 adjacent the 45 O-ring 54 is less than the inner diameter of the cylinder 38 adjacent the O-ring 52, it is obvious that O-ring 54 will pass opening 84- without being'broken. Further, since the inner diameter of the cylinder 38 adjacent openiug as is the same as the diameter adjacent opening 84, it is also obvious that O-ring 54 will also pass opening $6 without damage. Chamfer 82 is provided to guide the O-ring into final position without damage. Chamfer St) is provided to lead O-ring 54 upon initial insertion of the liner 42 into the unloader assembly and also to guide the O-ring 52 into position without damage. If chamfers Sit and 82 were not provided, the O- rings 52 and 54 would be cut by the sharp edge of the casting. Snap ring 64 in conjunction with spring 74 prevents the unloader assembly from lifting off the oil pin.
65 inserted therein.
My invention provides obvious advantages and eliminates several problem areas found in compressors. My construction allows the unloader assembly to be assembled and placed in position before the liner assembly is Previous to this time, the unloader assembly and the cylinder liner assembly were assembled as a unit and then placed in position in the compressor. Obviously, this type of construction would make it very diflicult to correctly position the unit on the oil pin.
Further, the construction of the unloader assembly has virtually eliminated breakage of O-rings upon assembly. Constant breakage of D-rings upon assembly causes a serious labor loss which may cause an increase in the market price of the compressor.
Although I have described in detail the preferred embodiments of my invention, I contemplate that many changes may be made without departing from the scope or spirit of my invention, and I desire to be limited only by the claims.
I claim:
1. A compressor comprising; a housing, a common suction chamber and a common discharge chamber in said housing, first wall means separating said suction chamber from said discharge chamber, a crankcase chamber in said housing, second Wall means separating said suction chamber from said crankcase chamber, means forming openings for a cylinder liner assembly in said first and in said second wall means, oil conducting means in said second Wall means, an annular unloading assembly means connected to said oil conducting means and abutting said second Wall means around said opening in said second wall means, a cylinder liner assembly positioned in said opening in said first wall means and extending through said annular unloading assembly means and abutting said second wall, said cylinder liner assembly including a cylinder liner, said cylinder liner having a first annular sealing member in and surrounding the outer lower diameter portion of said cylinder liner and a second annular sealing member in and surrounding the outer upper diameter portion of said cylinder liner, said unloading assembly means including a cylinder adjacent and surrounding said cylinder liner, said cylinder being in direct contact with said sealing members in said cylinder liner, said cylinder having an inner diameter portion adjacent said second sealing member greater than the inner diameter portion adjacent said first sealing member, and piston means slidably mounted in said cylinder assembly means to draw gaseous refrigerant into said cylinder liner as sembly means from said suction chamber and discharge compressed gaseous refrigerant into said discharge chamber.
2. The structure of claim 1 wherein said cylinder has means forming an opening therethrough for passage of oil into said unloader assembly, said cylinder being chamfered on the inner diameter below said opening to lead the first sealing member into sealing relationship between said unloader assembly and said cylinder liner assembly.
References Cited in the file of this patent UNITED STATES PATENTS 2,156,943 Heller May 2, 1939 2,555,004 Rinehart May 29, i 2,555,005 Warneke May 29, 1951 2,673,025 Labus et a1 Mar. 23, 1954 2,751,146 Moseley June 19, 1956 2,836,345 Gerteis May 27, I958 2,948,461 Frank Aug. 9, I960 2,955,751 Hackbart Oct. 11, 1960 2,971,690 Nicholas Feb. 14, 1961 3,1 2 Hirsch Feb, 28, 196i

Claims (1)

1. A COMPRESSOR COMPRISING; A HOUSING, A COMMON SUCTION CHAMBER AND A COMMON DISCHARGE CHAMBER IN SAID HOUSING, FIRST WALL MEANS SEPARATING SAID SUCTION CHAMBER FROM SAID DISCHARGE CHAMBER, A CRANKCASE CHAMBER IN SAID HOUSING, SECOND WALL MEANS SEPARATING SAID SUCTION CHAMBER FROM SAID CRANKCASE CHAMBER, MEANS FORMING OPENINGS FOR A CYLINDER LINER ASSEMBLY IN SAID FIRST AND IN SAID SECOND WALL MEANS, OIL CONDUCTING MEANS IN SAID SECOND WALL MEANS, AN ANNULAR UNLOADING ASSEMBLY MEANS CONNECTED TO SAID OIL CONDUCTING MEANS AND ABUTTING SAID SECOND WALL MEANS AROUND SAID OPENING IN SAID SECOND WALL MEANS, A CYLINDER LINER ASSEMBLY POSITIONED IN SAID OPENING IN SAID FIRST WALL MEANS AND EXTENDING THROUGH SAID ANNULAR UNLOADING ASSEMBLY MEANS AND ABUTTING SAID SECOND WALL, SAID CYLINDER LINER ASSEMBLY INCLUDING A CYLINDER LINER, SAID CYLINDER LINER HAVING A FIRST ANNULAR SEALING MEMBER IN AND SURROUNDING THE OUTER LOWER DIAMETER PORTION OF SAID CYLINDER LINER AND A SECOND ANNULAR SEALING MEMBER IN AND SURROUNDING THE OUTER UPPER DIAMETER PORTION OF SAID CYLINDER LINER, SAID UNLOADING ASSEMBLY MEANS INCLUDING A CYLINDER ADJACENT AND SURROUNDING SAID CYLINDER LINER, SAID CYLINDER BEING IN DIRECT CONTACT WITH SAID SEALING MEMBERS IN SAID CYLINDER LINER, SAID CYLINDER HAVING AN INNER DIAMETER PORTION ADJACENT SAID SECOND SEALING MEMBER GREATER THAN THE INNER DIAMETER PORTION ADJACENT SAID FIRST SEALING MEMBER, AND PISTON MEANS SLIDABLY MOUNTED IN SAID CYLINDER ASSEMBLY MEANS TO DRAW GASEOUS REFRIGERANT INTO SAID CYLINDER LINER ASSEMBLY MEANS FROM SAID SUCTION CHAMBER AND DISCHARGE COMPRESSED GASEOUS REFRIGERANT INTO SAID DISCHARGE CHAMBER
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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3166236A (en) * 1961-06-23 1965-01-19 Vilter Manufacturing Corp Reciprocating piston type gas compressor
US3403847A (en) * 1966-10-17 1968-10-01 Lennox Ind Inc Cylinder and valve assembly
US3613719A (en) * 1968-10-16 1971-10-19 Hoerbiger Ventilwerke Ag Compressor valve arrangement
EP0103423A1 (en) * 1982-09-02 1984-03-21 F.L. Smidth & Co. A/S Apparatus for burning pulverulent raw material

Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2156943A (en) * 1934-07-28 1939-05-02 Baldwin Southwark Corp Compressor-unloader structure
US2555005A (en) * 1948-01-31 1951-05-29 Gen Electric Reciprocating compressor with unloading and capacity modulating control
US2555004A (en) * 1948-01-31 1951-05-29 Gen Electric Reciprocating compressor with unloading and capacity modulating control
US2673025A (en) * 1949-11-14 1954-03-23 Trane Co Compressor unloading means
US2751146A (en) * 1951-10-29 1956-06-19 Dalmo Victor Company Air compressor
US2836345A (en) * 1954-02-26 1958-05-27 Capacity control for compressors
US2948461A (en) * 1958-02-06 1960-08-09 Trane Co Reciprocating compressor
US2955751A (en) * 1958-08-26 1960-10-11 Trane Co Reciprocating piston compressor
US2971690A (en) * 1958-10-24 1961-02-14 Worthington Corp Unloading means for a reciprocating compressor
US2973132A (en) * 1958-10-20 1961-02-28 Worthington Corp Unloading means for reciprocating compressor

Patent Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2156943A (en) * 1934-07-28 1939-05-02 Baldwin Southwark Corp Compressor-unloader structure
US2555005A (en) * 1948-01-31 1951-05-29 Gen Electric Reciprocating compressor with unloading and capacity modulating control
US2555004A (en) * 1948-01-31 1951-05-29 Gen Electric Reciprocating compressor with unloading and capacity modulating control
US2673025A (en) * 1949-11-14 1954-03-23 Trane Co Compressor unloading means
US2751146A (en) * 1951-10-29 1956-06-19 Dalmo Victor Company Air compressor
US2836345A (en) * 1954-02-26 1958-05-27 Capacity control for compressors
US2948461A (en) * 1958-02-06 1960-08-09 Trane Co Reciprocating compressor
US2955751A (en) * 1958-08-26 1960-10-11 Trane Co Reciprocating piston compressor
US2973132A (en) * 1958-10-20 1961-02-28 Worthington Corp Unloading means for reciprocating compressor
US2971690A (en) * 1958-10-24 1961-02-14 Worthington Corp Unloading means for a reciprocating compressor

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3166236A (en) * 1961-06-23 1965-01-19 Vilter Manufacturing Corp Reciprocating piston type gas compressor
US3403847A (en) * 1966-10-17 1968-10-01 Lennox Ind Inc Cylinder and valve assembly
US3613719A (en) * 1968-10-16 1971-10-19 Hoerbiger Ventilwerke Ag Compressor valve arrangement
EP0103423A1 (en) * 1982-09-02 1984-03-21 F.L. Smidth & Co. A/S Apparatus for burning pulverulent raw material

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