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US2002200A - Engine compressor assembly - Google Patents

Engine compressor assembly Download PDF

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Publication number
US2002200A
US2002200A US566631A US56663131A US2002200A US 2002200 A US2002200 A US 2002200A US 566631 A US566631 A US 566631A US 56663131 A US56663131 A US 56663131A US 2002200 A US2002200 A US 2002200A
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Prior art keywords
crosshead
pistons
cylinders
engine
main frame
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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
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US566631A
Inventor
Hewitt A Gehres
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Cooper Bessemer Corp
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Cooper Bessemer Corp
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Publication date
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Priority to US566631A priority Critical patent/US2002200A/en
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Publication of US2002200A publication Critical patent/US2002200A/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
    • F04B35/00Piston pumps specially adapted for elastic fluids and characterised by the driving means to their working members, or by combination with, or adaptation to, specific driving engines or motors, not otherwise provided for
    • 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
    • F04B27/02Multi-cylinder pumps specially adapted for elastic fluids and characterised by number or arrangement of cylinders having cylinders arranged oppositely relative to main shaft
    • 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
    • F04B39/0005Component 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 adaptations of pistons
    • F04B39/0022Component 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 adaptations of pistons piston rods
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T74/00Machine element or mechanism
    • Y10T74/18Mechanical movements
    • Y10T74/18056Rotary to or from reciprocating or oscillating
    • Y10T74/18208Crank, pitman, and slide

Definitions

  • This invention relates to engine compressors and is particularly adapted to internal comlrustion engine compressors, of the type where the engine and compressor units are provided with a common crank shaft and fly Wheel interposed between said units.
  • An object of this invention is to provide means for obviating the above disadvantages and for obtaining the above desired characteristics and advantages.
  • FIG. 1 is a transverse longitudinal section showing such features of the apparatus as are necessary to a complete understanding of the invention
  • Fig. 2 is an enlarged longitudinal section taken through the power pistons, crosshead connected thereto -and the crosshead guide; one of the pistons and its connected piston strut is shown detached in order to more clearly illustrate certain features of the construction.
  • Fig. 3 is a transverse section taken at line 3-3 of Fig. 2 in the direction indicated by the arrows, and
  • Fig. 4 is a transverse section taken at line 4-4 of Fig. 2 in the direction indicated by the arrows.
  • the apparatus is mounted on a suitable base or pedestal I which supports the main frame 2, to the right handend of which is attached a compressorunit 3 and to the left hand end of which is attached the power unit I.
  • the compressor unit is entirely supported from the main frame 2 while the power unit 4 is partially supported by an extension of the pedestal I. 'f
  • a crank shaft 5 is suitably supported on the pedestal I and frame 2 and carries the'fly wheel B.
  • the crank shaft is provided with a crank l carrying a crank pin 8 which is engaged by the connecting rod 9, the other end of which engages a pin IIJ journaled in a crosshead I I which is supported on a suitable crosshead guide I2 formed integral with the main frame 2.
  • the crosshead II connects directly to the compressor piston rod I3 which passes through suitable stuiiing boxes carried jointly by the main frame 2 and the casing of the compressor 3 and the rod I3 carries at its outer end a compressor piston I4.
  • the crosshead II is also connected directly to the ends ofdistance rods I5 and I6. These distance rods extend Within the main frame 2 and for the major portion of their length are substantially entirely enclosed therein; access to the interior vof the main frame 2 being available through the removable cover plate I1, thus permitting access to the moving parts within the main frame 2.
  • the ⁇ distance rods are spaced outwardly from the center of the crank shaft 5, the upper rod being positioned'inside of the crank 'I and the outer rod being positioned outside of thelower balanced end of the crank 1.
  • the distance rods then pass out through the left hand end of the main frame 2 and. connect to a second crosshead I8 by means of suitable nuts such as I9 which serve to rigidly connect the distance rods I5 and I6 to the crosshead I8.
  • the crosshead I8 is supported on a crosshead guide I9 (see also Figs. 2, 3 and 4) which is ⁇ formed integral with the engine base which is supported by the pedestal I.
  • the base 20 carries the opposed tandem power cylinders 2
  • and 22 are provided with cylinder bores 23 and 24 .in which are mounted the power pistons 25 and 26.
  • the power pistons are rigidly attachedrespectively (Fig. 2) to piston struts 21 and 28, the inner ends of which are spaced apart and rigidly attached by means of spacer bolts 29 and suitable nuts such as 30--3 I.
  • the inner ends of the struts 21 and 28 are provided with spherical seats such as 32-33, and these are spaced apart so as to come into cooperative sliding engagement with the cooperating respectively corresponding spherical faces 70 cycle type.
  • this provision also eliminates the wearing of the power pistons and their cylinders due to uneven expansion of the rods I5 and I6. Undue wearing or binding between the power pistons and their cylinders is prevented by supporting the pistons and their interconnected struts from the crosshead I6 which is supported on the guide I9'. It will therefore be seen that the entire Weight of the pistons and their interconnected struts is supported free from any appreciable cngagement with the cylinder bores 22 and 23.
  • the distance rods I 5 and .I6 are positioned with respect to the axis of travel of the crosshead
  • 'Ihe cylinder base 20 substantially entirely encloses the space between the cylinders 2
  • a removable cover plate 39 is provided for access 5 to the movable parts enclosed therein.
  • the interior of the enclosure is in communication with the atmosphere or a suitable supply of air by means of the opening or bore 40 extending vertically upward through the pedestal I and in communication with the interior of the enclosure.
  • Suitable throttle means and adjustment means for the intake mixture are provided in a manner well understood in the art.
  • the exhaust chambers are designated respectively as 41 and 48 and comprise the usual exhaust valves and other features well understood to those skilled in the art. These exhaust chambers are in communication respectively with the exhaust pipes 49 and 50.
  • the connecting rod extends toward the power cylinders instead of away from them and the engine runs under, instead of over, as is usual in common practice in apparatus of this kind. This serves to maintain a downward pressure on the guide I2 of the main crosshead II. 'I'he direction of rotation of the crank shaft 5 and iiy wheel 6 is indicated by arrows in Fig. l.
  • An apparatus of the class described having opposed engine cylinders, pistons for said cylinders, a crosshead interposed between said cylin- Y ders, means connecting said crosshead to reciprocate with said pistons, a second crosshead located beyond one of -said cylinders, means connecting said crossheads to drive the second from the first, a connecting rod extending from said last mentioned crosshead toward said cylinders, a driven element connected to the end of the connecting rod which is so extended toward the cylinders, and a driven rod extending from said last mentioned crosshead in a direction opposed to said connecting rod.
  • An apparatus of the class described having opposed engine cylinders, pistons for said cylinders, a crosshead interposed between said cylinders, means connecting said crosshead to reciprocate with said pistons and coupling said pistons to form a rigid structure, a second crosshead located beyond one of said cylinders, a connecting rod extending from said last mentioned crosshead toward said cylinders, distance rods connecting said crossheads to drive the second from the rst, a driven rod extending from said last mentioned crosshead in a direction opposed to said connecting rod, and said connecting means aiording a slight rocking movement of said first mentioned crosshead in any direction relative to the aforesaid pistcn structure.
  • An apparatus of the class described having opposed engine cylinders, pistons for said cylinders, connecting members extendingbetween said pistons and connecting the same to form a rigid structure, a crosshead interposed between and reciprocable with said connecting members, said crosshead at least partially supporting the aforesaid piston structure, said crosshead 'having a spherically shaped part located between the pistons and said connecting members having spherical bearing seats engaging said spherically shaped part and affording angular rocking of the piston structure in any direction relative to the crosshead during operation, and power transmitting distance rods connected with said crosshead and reciprocating therewith.

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

Description

May 21, 1935. H. A. GEI-IRES ENGINE COMPRESSOR ASSEMBLY Filed Oct. 3, 1951 INVENTOR B-mzzu ArroRNYs Patented May 21, 1935 ENGINE COMPRESSOR ASSEMBLY Hewitt A. Gehres, Mount Vernon, Ohio, asslgnor to Cooper-Bessemer Corporation, Mount Vernon, Ohio, a corporation of Ohio Application October 3, 1931, Serial No. 566,631
3 Claims.` (Cl. 121117) This invention relates to engine compressors and is particularly adapted to internal comlrustion engine compressors, of the type where the engine and compressor units are provided with a common crank shaft and fly Wheel interposed between said units.
In apparatus of this character it has been customary to mount the respective engine or power unit and a compressor unit on respectively opposite ends of a main frame and to provide two crossheads carried in the main frame and interconnected by distance rods. LThe mounting of the cross heads in this manner requires the apparatus to be relatively large in size and this necessitates a corresponding large space for installation.
In apparatus of this character it is desired to provide relatively great power in a single device While keeping the dimensions down to a minimum; and further, to provide a'well balanced device in which reciprocating parts are free from undue wear or binding.
An object of this invention is to provide means for obviating the above disadvantages and for obtaining the above desired characteristics and advantages.
The invention consists in the novel features, arrangements and combinations of parts embodied by way of example in the apparatus hereinafter described as illustrating the preferred form of the invention, and the invention will be moreparticularly pointed out in the appended claims.
Other objects, features and advantages of the invention will appear from the following speciiication and claims taken in connection with the accompanying drawing in which Fig. 1 is a transverse longitudinal section showing such features of the apparatus as are necessary to a complete understanding of the invention,
Fig. 2 is an enlarged longitudinal section taken through the power pistons, crosshead connected thereto -and the crosshead guide; one of the pistons and its connected piston strut is shown detached in order to more clearly illustrate certain features of the construction.
Fig. 3 is a transverse section taken at line 3-3 of Fig. 2 in the direction indicated by the arrows, and
Fig. 4 is a transverse section taken at line 4-4 of Fig. 2 in the direction indicated by the arrows.
Referring to the drawing, which illustrates a present preferred form of the invention, the apparatus is mounted on a suitable base or pedestal I which supports the main frame 2, to the right handend of which is attached a compressorunit 3 and to the left hand end of which is attached the power unit I. The compressor unit is entirely supported from the main frame 2 while the power unit 4 is partially supported by an extension of the pedestal I. 'f
Only such details of the compressor unit and power unit as are comprehended in the present invention will be described, since the construction and operation of other features will be well understood by those skilled in the art.
A crank shaft 5 is suitably supported on the pedestal I and frame 2 and carries the'fly wheel B. The crank shaft is provided with a crank l carrying a crank pin 8 which is engaged by the connecting rod 9, the other end of which engages a pin IIJ journaled in a crosshead I I which is supported on a suitable crosshead guide I2 formed integral with the main frame 2. The crosshead II connects directly to the compressor piston rod I3 which passes through suitable stuiiing boxes carried jointly by the main frame 2 and the casing of the compressor 3 and the rod I3 carries at its outer end a compressor piston I4.
The crosshead II is also connected directly to the ends ofdistance rods I5 and I6. These distance rods extend Within the main frame 2 and for the major portion of their length are substantially entirely enclosed therein; access to the interior vof the main frame 2 being available through the removable cover plate I1, thus permitting access to the moving parts within the main frame 2.
The` distance rods are spaced outwardly from the center of the crank shaft 5, the upper rod being positioned'inside of the crank 'I and the outer rod being positioned outside of thelower balanced end of the crank 1. The distance rods then pass out through the left hand end of the main frame 2 and. connect to a second crosshead I8 by means of suitable nuts such as I9 which serve to rigidly connect the distance rods I5 and I6 to the crosshead I8.
The crosshead I8 is supported on a crosshead guide I9 (see also Figs. 2, 3 and 4) which is `formed integral with the engine base which is supported by the pedestal I. The base 20 carries the opposed tandem power cylinders 2| and 22 which are in axial alignment with the center of the crosshead I8, the center of the crank shaft 5, the center of the crosshead II and the axis of the compressor piston I4. The cylinders 2| and 22 are provided with cylinder bores 23 and 24 .in which are mounted the power pistons 25 and 26. The power pistons are rigidly attachedrespectively (Fig. 2) to piston struts 21 and 28, the inner ends of which are spaced apart and rigidly attached by means of spacer bolts 29 and suitable nuts such as 30--3 I.
The inner ends of the struts 21 and 28 are provided with spherical seats such as 32-33, and these are spaced apart so as to come into cooperative sliding engagement with the cooperating respectively corresponding spherical faces 70 cycle type.
34--35 formed on the sleeve 36 which is rigidly attached to the crosshead I8. The strut spacing bolts such as 29 pass through enlarged openings i 31 formed in the crosshead I8, thereby permitting 5 relative angular movement of the crosshead I8 with respect to the axis of the pistons 25-26. 'I'he nuts 30-3I provide for proper adjustment between the spherical seats formed on the crosshead and those formed on the spaced apart inner ends of the piston struts to thereby permit proper initial setting and to compensate for wear. This provision for relative angular movement between the crosshead I8 and the pistons 25 and 26 permits the pistons to freely reciprocate on their normal axis free of any binding eifect from uneven expansion of the distance rods I5 and I6. 'I'his expansion is quite common in practice and normally results in a binding or wearing between one or more of the crossheads and seats thereof;
and in the particular construction herein provided this provision also eliminates the wearing of the power pistons and their cylinders due to uneven expansion of the rods I5 and I6. Undue wearing or binding between the power pistons and their cylinders is prevented by supporting the pistons and their interconnected struts from the crosshead I6 which is supported on the guide I9'. It will therefore be seen that the entire Weight of the pistons and their interconnected struts is supported free from any appreciable cngagement with the cylinder bores 22 and 23.
The distance rods I 5 and .I6 are positioned with respect to the axis of travel of the crosshead |18 (Fig. 3) so that the distance rods I5 and I6 lie externally of the cylinder 22; the external diameter of the cylinder 22 being indicated on Fig. 3 by the dash and dot line 38.
'Ihe cylinder base 20 substantially entirely encloses the space between the cylinders 2| and 22,
40 and as will be understood from the foregoing description the crosshead guide I9', the crosshead I8 and attached ends of the distance rods I5 and I6 are contained within the said enclosure. A removable cover plate 39 is provided for access 5 to the movable parts enclosed therein. The interior of the enclosure is in communication with the atmosphere or a suitable supply of air by means of the opening or bore 40 extending vertically upward through the pedestal I and in communication with the interior of the enclosure.
'I'his not only permits a proper breather means for the cylinder base but provides for cooling the power unit and more particularly the moving parts therein; it being understood that the air supply vto the combustion spaces of the power unit is taken from the cylinder base as is customary in usual practice.
Such details of the power unit have been referred to with particularity as will enable those skilled in the art to understand the features which I consider to fall particularly within the scope of the present invention; but in order to provide a better understanding of the general form of the power unit shown in the present pre- '65 ferred form of the invention, the general features of the power unit will now be described briefly. 1
Suitable throttle means and adjustment means for the intake mixture are provided in a manner well understood in the art. The exhaust chambers are designated respectively as 41 and 48 and comprise the usual exhaust valves and other features well understood to those skilled in the art. These exhaust chambers are in communication respectively with the exhaust pipes 49 and 50.
It will be particularly noted that in the construction embodied the connecting rod extends toward the power cylinders instead of away from them and the engine runs under, instead of over, as is usual in common practice in apparatus of this kind. This serves to maintain a downward pressure on the guide I2 of the main crosshead II. 'I'he direction of rotation of the crank shaft 5 and iiy wheel 6 is indicated by arrows in Fig. l.
Having thus described my invention with particularity with reference to its preferred form, it will be obvious to those skilled in the art, after understanding my invention, that other changes and modifications may be made therein without departing from the spirit and scope of my invention, and I aim in the appended claims to cover such changes and modications as are within the scope of the invention.
What I claim is:
l. An apparatus of the class described, having opposed engine cylinders, pistons for said cylinders, a crosshead interposed between said cylin- Y ders, means connecting said crosshead to reciprocate with said pistons, a second crosshead located beyond one of -said cylinders, means connecting said crossheads to drive the second from the first, a connecting rod extending from said last mentioned crosshead toward said cylinders, a driven element connected to the end of the connecting rod which is so extended toward the cylinders, and a driven rod extending from said last mentioned crosshead in a direction opposed to said connecting rod.
2. An apparatus of the class described, having opposed engine cylinders, pistons for said cylinders, a crosshead interposed between said cylinders, means connecting said crosshead to reciprocate with said pistons and coupling said pistons to form a rigid structure, a second crosshead located beyond one of said cylinders, a connecting rod extending from said last mentioned crosshead toward said cylinders, distance rods connecting said crossheads to drive the second from the rst, a driven rod extending from said last mentioned crosshead in a direction opposed to said connecting rod, and said connecting means aiording a slight rocking movement of said first mentioned crosshead in any direction relative to the aforesaid pistcn structure.
3. An apparatus of the class described having opposed engine cylinders, pistons for said cylinders, connecting members extendingbetween said pistons and connecting the same to form a rigid structure, a crosshead interposed between and reciprocable with said connecting members, said crosshead at least partially supporting the aforesaid piston structure, said crosshead 'having a spherically shaped part located between the pistons and said connecting members having spherical bearing seats engaging said spherically shaped part and affording angular rocking of the piston structure in any direction relative to the crosshead during operation, and power transmitting distance rods connected with said crosshead and reciprocating therewith.
HEWITT A. GEHRES.
US566631A 1931-10-03 1931-10-03 Engine compressor assembly Expired - Lifetime US2002200A (en)

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Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2558481A (en) * 1947-08-23 1951-06-26 Hartford Nat Bank & Trust Co Combination comprising a hot-gas engine and a piston machine driven thereby
US2678028A (en) * 1948-06-04 1954-05-11 Joy Mfg Co Expansion engine
US2696343A (en) * 1953-06-15 1954-12-07 Mallory Res Co Internal-combustion engine with compressor
US3657972A (en) * 1969-07-04 1972-04-25 Burgkhardt Ag Maschf Crosshead arrangement for the drive mechanism of high-pressure compressors and pumps
US20080108257A1 (en) * 2006-08-24 2008-05-08 Gibbs Technologies Ltd Amphibian
US20090005954A1 (en) * 2006-12-20 2009-01-01 Delphi Technologies, Inc. Combustion control in an internal combustion engine

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2558481A (en) * 1947-08-23 1951-06-26 Hartford Nat Bank & Trust Co Combination comprising a hot-gas engine and a piston machine driven thereby
US2678028A (en) * 1948-06-04 1954-05-11 Joy Mfg Co Expansion engine
US2696343A (en) * 1953-06-15 1954-12-07 Mallory Res Co Internal-combustion engine with compressor
US3657972A (en) * 1969-07-04 1972-04-25 Burgkhardt Ag Maschf Crosshead arrangement for the drive mechanism of high-pressure compressors and pumps
US20080108257A1 (en) * 2006-08-24 2008-05-08 Gibbs Technologies Ltd Amphibian
US20090005954A1 (en) * 2006-12-20 2009-01-01 Delphi Technologies, Inc. Combustion control in an internal combustion engine

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