US2454600A - Compressor - Google Patents

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US2454600A
US2454600A US557161A US55716144A US2454600A US 2454600 A US2454600 A US 2454600A US 557161 A US557161 A US 557161A US 55716144 A US55716144 A US 55716144A US 2454600 A US2454600 A US 2454600A
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cylinders
cylinder
faces
crankcase
face
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US557161A
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William V Fischer
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AIR FLO COMPRESSOR Co
AIR-FLO COMPRESSOR Co
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AIR FLO COMPRESSOR Co
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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
    • F04B27/00Multi-cylinder pumps specially adapted for elastic fluids and characterised by number or arrangement of cylinders
    • F04B27/04Multi-cylinder pumps specially adapted for elastic fluids and characterised by number or arrangement of cylinders having cylinders in star- or fan-arrangement
    • F04B27/0404Details, component parts specially adapted for such pumps
    • F04B27/0423Cylinders
    • 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
    • F04B27/04Multi-cylinder pumps specially adapted for elastic fluids and characterised by number or arrangement of cylinders having cylinders in star- or fan-arrangement
    • F04B27/0404Details, component parts specially adapted for such pumps
    • 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
    • F04B27/04Multi-cylinder pumps specially adapted for elastic fluids and characterised by number or arrangement of cylinders having cylinders in star- or fan-arrangement
    • F04B27/053Multi-cylinder pumps specially adapted for elastic fluids and characterised by number or arrangement of cylinders having cylinders in star- or fan-arrangement with an actuating element at the inner ends of the cylinders
    • F04B27/0536Multi-cylinder pumps specially adapted for elastic fluids and characterised by number or arrangement of cylinders having cylinders in star- or fan-arrangement with an actuating element at the inner ends of the cylinders with two or more series radial piston-cylinder units

Definitions

  • changeable parts which are Adesigned for modifled aggroupment to produce either va two, four, or six cylinder machine with delivery rates proportionate to the number of cylinders.
  • a further object is provided by the lower unit costs realized in the manufacture of standard parts adaptable for interchangeable usage in each of three sizes of compressors.
  • FIG. 3 is a transverse'section on line S-Ivof Fig. 2 illustrating the offset relation of the cylinders and the mounting flanges thereof;
  • Fig. 4 is a view similar to Fig. 2 showing the arrangement of the parts when organized to produce a four cylinder compressor; v
  • Fig. 5 is a transverse sectional view of a portion of a four cylinder compressor embodying modified forms of crankcase and cylinders;
  • Fig. 6 is similar to Fig. 5 illustrating the use of the modified form of cylinder in a six cylinder compressor
  • Fig. 'l is a transverse section through a cylinder showing an alternate flange design
  • Fig. 8 is a transverse sectional view of a crankcase of further modified form with cylinders o prises a crankcase III of prismoidal form with inclined sides inthe upper portion thereof and a vflanged mounting base II.
  • the upper face I2 of the crankcase is substantially parallel to the base II, while the oblique or inclined faces I2--Il are disposed in transverse section at angles of 521/2 degrees relative to the face I2.
  • Elliptical openings IQ are provided in the faces I2 and vII--Il to accommodate the reception of elliptical mounting flanges I5 in the cylinders I8, each of which is identical in form and configuration.
  • the cylinders I6 are secured to the crankcase by mounting bolts or studs I 1 which engage bolt holes in the elliptical flanges I5.
  • the elliptical openings ⁇ I4 and the flanges of the cylinders on oblique faces Il-II have their minor axes parallei to the longitudinall axis of the crankcase I0.'
  • the axes of the cylinders I 8 are disposed normal to the minor axes oi' the ellipses of the flanges I5 and at 71/2 degree angles from the normal to the maior axes of ⁇ said ellipses.
  • rotation of the cylinders through one hundred and eighty degrees will alter the position of the cylinder radially by fteen degrees.
  • the cylinders are offset on the major axes of the elliptical mounting flanges I5 as shown in Fig.
  • the cylinders I6 when mounted on faces I3I3, will be disposed at angles of 45 degrees or 30 degrees to the face I2 depending upon the rotational position of said cylinders, since the faces I3-I3 are inclined at 521/2 degree angles to the face I2 and the cylinder mounting flanges I5 are inclined at l1/2 degree angles to a plane normal to the medial axis oi the cylinders.
  • the upper face I2 of the crankcase I0 is formed in complementa] configuration to the mounting flanges I5 to accommodate the securement of the cylinders I5 in perpendicular relation to said face.
  • the cylinders I8 are mounted on the up per face I2 in quarter-turned relation to the cylinders on faces I3--I3 and the face I2 is inclined at 'Z1/2 degree angles yfrom the center to the forward and rearward ends thereof.
  • the drive shaft IB is machined for the keyed support of the cams Il which transmit their rotary motion to the master connecting rod sleeves 20 Journalled thereon.
  • Each sleeve 2li is provided with a pair of apertured bosses 2I in I equi-spaced relation with the master rod 22. for connecting articulate links as shown ln the six cylinder compressor illustrated in Fig. 2.
  • sleeves 20 are further provided with a second pair 5 of apertured bosses 22 for use in the four cylinder modification shown in Fig. 4.
  • the two master rods 22 reciprocate in the upper or central cylinders in the two or the six cylinder compressor; however, in the four cylinder arrangement,
  • one master rod 22 operates in each bank of cylinders as shown in Fig. 4.
  • the cylinder heads 24 and valve plates 25 are secured to the cylinders by symmetrically Aspaced studs allowing the rotative adjustment of parts to facilitate the connectioxof conduits.
  • Figs. 5 and 6 which illustrate a modification of cylinder design
  • the flange 30 on the cylinder 3i is disposed perpendicularly to 50 the medial axis of lsaid cylinder, and said cylinder is unequally spaced from the ends of said flange and from the holes for the bolts I1: thus rotation of the cylinder through an angle of 180 degrees will effect a translational change of position of the cylinder.
  • the cylinders on the oblique faces I3-I3 are positioned closer to the face I2 (Fig. 5) than they are in the six cylinder machine (Fig. 6).
  • FIG. 7 is a view illustrating a modified cylinder ange.
  • the slots 33 in the ange engage with the studs I1 on the faces of the compressor to accommodate the repositioning of the cylinders, said slots being disposed to locate the cylinders properly at the opposed limits of travel.
  • crankcase 34 having three adjaouter faces 2l and 21 are disposed at angles of 52%, degrees relative to'base 38, and the intermediate face 25 is disposed at Z1/2 degrees to said base.
  • the outer faces 35 and 21 function, as in the heretofore described preferred embodiment. to accommodate the support of the cylinders I6 in either a 45 or a 60 degree relation to the cylinders mounted on the intermediate face. Since the 'I1/2 degree inclination of the intermediate face 38 conforms to the angle of the cylinder flanges, said cylinders may be mounted thereon in perpendicular relation to the base 2l.
  • This form of crankcase provides an intermediate face having a plane surface and thus simplifies the machining thereof.
  • An air compressor comprising a crankcase, a plurality of similar cylinders, flanges thereon having bolt holes therein arranged in a symmetrical pattern eccentric to the axes o f the cylinders, one horizontal cylinder-receiving face on said crankcase, two oblique cylinder-receiving faces adjacent to said horizontal face disposed downwardly Y in angular relation thereto, cylinder supporting studs on said faces arranged in a symmetrical pattern to receivesaid cylinders, a drive shaft in said crankcase, eccentric cams thereon, sleeves journalled on said cams, pistons in said cylinders,
  • a ⁇ compressor 4a plurality of similar cylinders formed with elongated flanges, a crankcase having a major axis and formed with three angularly disposed adjacent cylinder-receiving faces having oval openings therein for the reception of the flanges on said cylinders, the outer cylinder-receiving faces of said crankcase being disposed at angles of 521/2 degrees to the line of intersection of a plane perpendicular to the major axis withthe plane of the intermediate face, the
  • openings in said intermediate cylinder-receiving ⁇ of which are disposed at 521/2 degree angles to the line of intersection of the intermediate face and a plane perpendicular to the major axis, said three faces having openings therein, flanges on said cylinders disposed at angles of 'I1/2 degrees to planes perpendicular to the axes of the cylinders, whereby the cylinders may be mounted on said outer faces at either 120 or 90 degree angles to each other, said intermediate face of the crankcase being inclined at a 'l1/2 degree angle to the major axis to accommodate the securement of the cylinder thereon in normal relation to the major axis of the crankcase, and means mounting the cylinders on the crankcase.
  • An air compresso-r comprising a plurality of similar cylinders, flanges thereon having bolt holes therein arranged in equi-spaced relation in a path eccentric to the axis of the cylinders, a
  • crankcase for the support of said cylinders
  • a crankcase formed with three adjacent faces adapted to receive cylinders, the cylinder-receiving portions of the faces being disposed, with respect to the crankshaft axis of the crankcase and a reference Y plane containing the said axis as follows: the cylinder-receiving portion of the intermediate one of the faces substantially coinciding with a plane intersecting the reference plane at an angle of seven and one-half degrees in 4a line perpendicular to the axis, and the cylinder-receiving portions of the outer two faces substantially coinciding with planes intersecting the reference plane at angles of fifty-two and one-half degrees in lines parallel to the axis, and at least two cylinders formed with flanges disposed at an angle of approximately 821/2 degrees to the cylinder axis mounted on the least two of the said cylinder receiving portions.
  • a compressor a plurality of cylinders, a crankcase therefor, said crankcase being formed with three faces intersecting at angles of approximately 521/2 degrees relative to each other, said faces having openings therein, the intermediate face being inclined at an angle of 71/2 l flanges conforming to said openings and being f degrees from its lcenter to its ends, flanges on said cylinders inclined at l1/2 degree angles to a transverse plane through said cylinders, said offset eccentric to the axes of said cylinders to provide for radial alignment of the cylinders in either of two positions on the two oblique faces, v
  • said flanges constituting means for securement of said cylinders to the crankcase when supported vertically on said center face or at 30 or 45 degree angles to the horizontal on the oblique faces of said crankcase, said cylinders being secured to said crankcase.
  • a crankcase for a reciprocating machine formed with three adjacent faces adapted to receive cylinders, the cylinder-receiving portions of the faces being disposed, with respect to Athe crankshaft axis of the crankcase and a reference plane containing the said axis as follows:
  • cylinder-receiving portion of the intermediateV one of the faces substantially coinciding with a I plane intersecting the reference plane at an angle of seven and one-half degrees in a line perpendicular to the axis

Description

Nov. 23, 1948. w. v. FISCHER COMPRESSOR 2 Sheets-Sheet l Filed Oct. 4, 1944 yFigi INVENTOR.
*Vum V -'uscHeR AT1-oa Nava Nov. 23, 1948. w, v F|scHER 2,454,600 i coMPREssoR l Filed 001'.. 4, 1944 2 Sheets-Sheet 2 v INV rok. Wn.|.\AM\/ lscHER By f//M' ATTORNEYS Patented Nov.l 1948 comnassoa William V. Fischer. Akron, Ohio, aalignor` to The AlrFio Compressor Company, Akron, Ohio. a
corporation of Ohio Application October 4, 1944, Serial No. 557,181
8 Claims. (Cl. 23o-172) This invention relates broadly to gas com- I pressors and more specifically to improvements,
in the design and organization of certain of the parts thereof.
changeable parts which are Adesigned for modifled aggroupment to produce either va two, four, or six cylinder machine with delivery rates proportionate to the number of cylinders.
Other objects and advantages of the invention reside in the economies realized by the purchaser of the improved compressor and the convenience attained in the conversion thereof to a machine of low, medium, or high volumetric delivery.
A further object is provided by the lower unit costs realized in the manufacture of standard parts adaptable for interchangeable usage in each of three sizes of compressors. H
Other objects and advantages more or less ancillary to the foregoing and the manner in which all .the various objects are realized will appear Fig. 3 is a transverse'section on line S-Ivof Fig. 2 illustrating the offset relation of the cylinders and the mounting flanges thereof;
Fig. 4 is a view similar to Fig. 2 showing the arrangement of the parts when organized to produce a four cylinder compressor; v
Fig. 5 is a transverse sectional view of a portion of a four cylinder compressor embodying modified forms of crankcase and cylinders;
Fig. 6 is similar to Fig. 5 illustrating the use of the modified form of cylinder in a six cylinder compressor;
Fig. 'l is a transverse section through a cylinder showing an alternate flange design; and
Fig. 8 is a transverse sectional view of a crankcase of further modified form with cylinders o prises a crankcase III of prismoidal form with inclined sides inthe upper portion thereof and a vflanged mounting base II. The upper face I2 of the crankcase is substantially parallel to the base II, while the oblique or inclined faces I2--Il are disposed in transverse section at angles of 521/2 degrees relative to the face I2. Elliptical openings IQ are provided in the faces I2 and vII--Il to accommodate the reception of elliptical mounting flanges I5 in the cylinders I8, each of which is identical in form and configuration. The cylinders I6 are secured to the crankcase by mounting bolts or studs I 1 which engage bolt holes in the elliptical flanges I5. The elliptical openings `I4 and the flanges of the cylinders on oblique faces Il-II have their minor axes parallei to the longitudinall axis of the crankcase I0.'
The axes of the cylinders I 8, however, are disposed normal to the minor axes oi' the ellipses of the flanges I5 and at 71/2 degree angles from the normal to the maior axes of` said ellipses. Thus rotation of the cylinders through one hundred and eighty degrees will alter the position of the cylinder radially by fteen degrees.
The cylinders are offset on the major axes of the elliptical mounting flanges I5 as shown in Fig.
- 3, the structure being designed to accommodate rotation of the cylinders in the manner heretofore describedV when mounted on faces II--II with the medial axes of the cylinders normal to the drive shaft I 8.
From the foregoing it will readily be recognized that the cylinders I6, when mounted on faces I3I3, will be disposed at angles of 45 degrees or 30 degrees to the face I2 depending upon the rotational position of said cylinders, since the faces I3-I3 are inclined at 521/2 degree angles to the face I2 and the cylinder mounting flanges I5 are inclined at l1/2 degree angles to a plane normal to the medial axis oi the cylinders.
Referring now to Fig. l, the upper face I2 of the crankcase I0 is formed in complementa] configuration to the mounting flanges I5 to accommodate the securement of the cylinders I5 in perpendicular relation to said face. For this purpose the cylinders I8 are mounted on the up per face I2 in quarter-turned relation to the cylinders on faces I3--I3 and the face I2 is inclined at 'Z1/2 degree angles yfrom the center to the forward and rearward ends thereof.
The drive shaft IB is machined for the keyed support of the cams Il which transmit their rotary motion to the master connecting rod sleeves 20 Journalled thereon. Each sleeve 2li is provided with a pair of apertured bosses 2I in I equi-spaced relation with the master rod 22. for connecting articulate links as shown ln the six cylinder compressor illustrated in Fig. 2. The
sleeves 20 are further provided with a second pair 5 of apertured bosses 22 for use in the four cylinder modification shown in Fig. 4. The two master rods 22 reciprocate in the upper or central cylinders in the two or the six cylinder compressor; however, in the four cylinder arrangement,
one master rod 22 operates in each bank of cylinders as shown in Fig. 4.
The cylinder heads 24 and valve plates 25 are secured to the cylinders by symmetrically Aspaced studs allowing the rotative adjustment of parts to facilitate the connectioxof conduits.
faces I3-I2, the base portion thereof being ar- 25 ranged to position the cylinders at 45 degree angles to the face I2 and at 90 degree angles to each other. Two of the four cover plates 28 removed from faces AI3I3 are then installed to close openings I4 in the upper face I2. The two so master rods 22 and the articulate links 20 are then assembled in operative position as shown in Fig. 4.
Further increase in capactiy is obtained by `installing two additional cylinders on the upper face I2. To this end, the master rod and articulate links are repositioned to form the six cylinder compressor illustrated in Fig. 2, the four cylinders on the oblique faces II-II being rotated one half turn in such reassembly. The resulting compress comprises three banks of cylinders'de- 40 fining angles of 60 degrees, each bank embodying two cylinders having the pistons therein disposed in opposed dead center relation (see Fig. l) The use of an even number of opposed cams effectuates an equal distribution of compressive charges throughout each cycle of either the two, four, or
six cylinder machine. Y
Referring now to Figs. 5 and 6 which illustrate a modification of cylinder design, the flange 30 on the cylinder 3i is disposed perpendicularly to 50 the medial axis of lsaid cylinder, and said cylinder is unequally spaced from the ends of said flange and from the holes for the bolts I1: thus rotation of the cylinder through an angle of 180 degrees will effect a translational change of position of the cylinder. In the four cylinder compressor the cylinders on the oblique faces I3-I3 are positioned closer to the face I2 (Fig. 5) than they are in the six cylinder machine (Fig. 6). This provides operative 'clearance of the articulate links so 29 with the bores of the cylinders 3i and also rccommodates the ready interchangeability of parts. The upper face I2 of the modified crankcase 3 2 is a plane surface to accommodate the perpendicular mounting pf the modified cylinders Fig. 7 is a view illustrating a modified cylinder ange. The slots 33 in the ange engage with the studs I1 on the faces of the compressor to accommodate the repositioning of the cylinders, said slots being disposed to locate the cylinders properly at the opposed limits of travel.
The compressor shown in Fig. 8 embodies a modified form of crankcase 34 having three adjaouter faces 2l and 21 are disposed at angles of 52%, degrees relative to'base 38, and the intermediate face 25 is disposed at Z1/2 degrees to said base.. The outer faces 35 and 21 function, as in the heretofore described preferred embodiment. to accommodate the support of the cylinders I6 in either a 45 or a 60 degree relation to the cylinders mounted on the intermediate face. Since the 'I1/2 degree inclination of the intermediate face 38 conforms to the angle of the cylinder flanges, said cylinders may be mounted thereon in perpendicular relation to the base 2l. This form of crankcase provides an intermediate face having a plane surface and thus simplifies the machining thereof.
The inherent advantage of a structure which facilitates the manufacture of three sizes of compressors (substantially three to'one ratio of output) from assemblies of parts of identical typal form is obviously invaluable in an industry in which hundreds of varying sizes and types of compressors are catalogued at the present time. Moreover, the accessibility of parts, the ease of conversion of the machine from one size to another and the broad range of delivery output thereof inures by way of economy to the purchasers and users of such machines.
Although the foregoing descrpition is necessarily of a detailed character, in order that the invention may be completely set forth, it is to be understood that the specific terminology is not intended to be restrictive or conning, and that various rearrangements of parts and modifications of detail may be resorted to without departing from the spirit or scope of the invention as herein claimed. i
I claim:
l. A compressor embodying cylinders, pistons therein, mechanism for reciprocating said pistons, a housing having one face substantially horizontal, two oblique faces adjacent thereto disposed at 52% degree angles to the horizontal, said oblique faces having transversely elongated openingstherein, cylinders having mounting flanges thereon inclined at 'Z1/2 degree angles from planes normal to their medial axes for mounting said cylinders on said oblique faces at either 30 or 45 degree angles to the horizontal, said substantially horizontal face having openings therein, beveled surfaces adjacent said openings for mounting cylinders thereon, the cylinders being mounted on the housing', connecting links coupled with, said pistons, and means in said reciprocating mechanism for mounting said connecting links to form an operative two cylinder compressor when cylinders are mounted on the substantially horizontal surface, a four cylinder compressor when cylinders are mounted on the oblique faces at 45 degree angles, or a six cylinder compressor when cylinders are mounted on the substantially horizontal face and on the oblique faces at 30 degree angles to the horizontal face.
2. An air compressor comprising a crankcase, a plurality of similar cylinders, flanges thereon having bolt holes therein arranged in a symmetrical pattern eccentric to the axes o f the cylinders, one horizontal cylinder-receiving face on said crankcase, two oblique cylinder-receiving faces adjacent to said horizontal face disposed downwardly Y in angular relation thereto, cylinder supporting studs on said faces arranged in a symmetrical pattern to receivesaid cylinders, a drive shaft in said crankcase, eccentric cams thereon, sleeves journalled on said cams, pistons in said cylinders,
cent faces on the upper portion thereof. 'The 75 connecting links intermediate said pistons and said sleeves, unequally spaced apertured bosses ony said sleeves for the support of said connecting links in operative clearance with the bores of said cylinders when the eccentric cylinder fianges are mounted on said studs with the narrow portion of the flanges faced in one direction or in the opposed direction.
3. In a` compressor, 4a plurality of similar cylinders formed with elongated flanges, a crankcase having a major axis and formed with three angularly disposed adjacent cylinder-receiving faces having oval openings therein for the reception of the flanges on said cylinders, the outer cylinder-receiving faces of said crankcase being disposed at angles of 521/2 degrees to the line of intersection of a plane perpendicular to the major axis withthe plane of the intermediate face, the
openings in said intermediate cylinder-receiving `of which are disposed at 521/2 degree angles to the line of intersection of the intermediate face and a plane perpendicular to the major axis, said three faces having openings therein, flanges on said cylinders disposed at angles of 'I1/2 degrees to planes perpendicular to the axes of the cylinders, whereby the cylinders may be mounted on said outer faces at either 120 or 90 degree angles to each other, said intermediate face of the crankcase being inclined at a 'l1/2 degree angle to the major axis to accommodate the securement of the cylinder thereon in normal relation to the major axis of the crankcase, and means mounting the cylinders on the crankcase.
5. An air compresso-r comprising a plurality of similar cylinders, flanges thereon having bolt holes therein arranged in equi-spaced relation in a path eccentric to the axis of the cylinders, a
crankcase for the support of said cylinders,
cylinder receiving faces thereon disposed in ap-4 proximately 521/2" angular relation with each other, cylinder supporting studs therein disposed for engagement with the bolt holes in said flanges, a drive shaft in said crankcase, cams on said shaft, eccentric straps on said cams, pistons in said cylinders, connecting links intermediate said pistons and said straps, and means on said straps for the support of said links in operative position when said cylinders are mounted on said studs with the eccentrically disposed bolt holes arranged in alternate positions 180 degrees apart, whereby rotative adjustment of the cylinders through 180 degrees will eiect chordal variations thereof for the support of a different number of cylinders and accommodate operative driving connections for the pistons therein.
6. In a reciprocating machine, a crankcase formed with three adjacent faces adapted to receive cylinders, the cylinder-receiving portions of the faces being disposed, with respect to the crankshaft axis of the crankcase and a reference Y plane containing the said axis as follows: the cylinder-receiving portion of the intermediate one of the faces substantially coinciding with a plane intersecting the reference plane at an angle of seven and one-half degrees in 4a line perpendicular to the axis, and the cylinder-receiving portions of the outer two faces substantially coinciding with planes intersecting the reference plane at angles of fifty-two and one-half degrees in lines parallel to the axis, and at least two cylinders formed with flanges disposed at an angle of approximately 821/2 degrees to the cylinder axis mounted on the least two of the said cylinder receiving portions.
7. In a compressor, a plurality of cylinders, a crankcase therefor, said crankcase being formed with three faces intersecting at angles of approximately 521/2 degrees relative to each other, said faces having openings therein, the intermediate face being inclined at an angle of 71/2 l flanges conforming to said openings and being f degrees from its lcenter to its ends, flanges on said cylinders inclined at l1/2 degree angles to a transverse plane through said cylinders, said offset eccentric to the axes of said cylinders to provide for radial alignment of the cylinders in either of two positions on the two oblique faces, v
said flanges constituting means for securement of said cylinders to the crankcase when supported vertically on said center face or at 30 or 45 degree angles to the horizontal on the oblique faces of said crankcase, said cylinders being secured to said crankcase.
8. A crankcase for a reciprocating machine formed with three adjacent faces adapted to receive cylinders, the cylinder-receiving portions of the faces being disposed, with respect to Athe crankshaft axis of the crankcase and a reference plane containing the said axis as follows: the
cylinder-receiving portion of the intermediateV one of the faces substantially coinciding with a I plane intersecting the reference plane at an angle of seven and one-half degrees in a line perpendicular to the axis, and the cylinder-receiving portions of the outer two faces substantially coinciding with planes intersecting the reference plane at angles of fifty-two and one-half degrees in lines parallel to the axis, and at least one cylinder formed with a flange disposed at an angle of approximately eighty-two andone-half degrees to the cylinder axis mounted on at least one of the said cylinder-receiving portions.
WILLIAM V. FISCHER.
REFERENCES CITED The following references are of record inJ the file of this patent:
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Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2955750A (en) * 1958-05-09 1960-10-11 Trane Co Multi-cylinder reciprocating compressor
US3136478A (en) * 1962-04-11 1964-06-09 Worthington Corp Multi-stage compressor with annular ring valve service
US5429080A (en) * 1993-12-13 1995-07-04 Evestar Technologies, Inc. Compact internal combustion engine
WO2000065232A2 (en) * 1999-04-22 2000-11-02 Bitzer Kühlmaschinenbau Gmbh Coolant compressor system
US20040031458A1 (en) * 2002-04-15 2004-02-19 Snyder Dale D. Modular internal combustion engines
US20070098580A1 (en) * 2005-06-24 2007-05-03 Dirk Petersen Pump gear
US20120093665A1 (en) * 2009-05-28 2012-04-19 Flanigan Paul J Light Weight Crankcase Casting for Compressor
EP3070332A1 (en) * 2008-07-18 2016-09-21 Allen Jones Radial compressor apparatus

Citations (5)

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Publication number Priority date Publication date Assignee Title
US1677539A (en) * 1927-10-06 1928-07-17 Harry P Wollman Air compressor
US1846656A (en) * 1929-11-15 1932-02-23 Champion Pneumatic Machinery C Single stage compressor
US2202520A (en) * 1938-09-19 1940-05-28 Jesse W Forrester Fluid displacement mechanism
US2255852A (en) * 1940-04-19 1941-09-16 Radial Pump And Compressor Com Pump assembly
US2263786A (en) * 1938-08-12 1941-11-25 Jr Emile T Rumpp Pump

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1677539A (en) * 1927-10-06 1928-07-17 Harry P Wollman Air compressor
US1846656A (en) * 1929-11-15 1932-02-23 Champion Pneumatic Machinery C Single stage compressor
US2263786A (en) * 1938-08-12 1941-11-25 Jr Emile T Rumpp Pump
US2202520A (en) * 1938-09-19 1940-05-28 Jesse W Forrester Fluid displacement mechanism
US2255852A (en) * 1940-04-19 1941-09-16 Radial Pump And Compressor Com Pump assembly

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2955750A (en) * 1958-05-09 1960-10-11 Trane Co Multi-cylinder reciprocating compressor
US3136478A (en) * 1962-04-11 1964-06-09 Worthington Corp Multi-stage compressor with annular ring valve service
US5429080A (en) * 1993-12-13 1995-07-04 Evestar Technologies, Inc. Compact internal combustion engine
WO2000065232A2 (en) * 1999-04-22 2000-11-02 Bitzer Kühlmaschinenbau Gmbh Coolant compressor system
WO2000065232A3 (en) * 1999-04-22 2001-03-22 Bitzer Kuehlmaschinenbau Gmbh Coolant compressor system
US6401472B2 (en) 1999-04-22 2002-06-11 Bitzer Kuehlmaschinenbau Gmbh Refrigerant compressor apparatus
US20040031458A1 (en) * 2002-04-15 2004-02-19 Snyder Dale D. Modular internal combustion engines
US6904883B2 (en) 2002-04-15 2005-06-14 Tecumseh Products Company Modular internal combustion engines
US20070098580A1 (en) * 2005-06-24 2007-05-03 Dirk Petersen Pump gear
US9097249B2 (en) * 2005-06-24 2015-08-04 Bran+Luebbe Gmbh Pump gear
EP3070332A1 (en) * 2008-07-18 2016-09-21 Allen Jones Radial compressor apparatus
US20120093665A1 (en) * 2009-05-28 2012-04-19 Flanigan Paul J Light Weight Crankcase Casting for Compressor

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