US782597A - Equalizing mechanism for air-compressors. - Google Patents

Equalizing mechanism for air-compressors. Download PDF

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US782597A
US782597A US20326804A US1904203268A US782597A US 782597 A US782597 A US 782597A US 20326804 A US20326804 A US 20326804A US 1904203268 A US1904203268 A US 1904203268A US 782597 A US782597 A US 782597A
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air
shaft
cylinders
crank
valve
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US20326804A
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Edward Cheshire
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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
    • F04B49/16Control, 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 adjusting the capacity of dead spaces of working chambers

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  • This invention is an improvement in doublecylinder air-compressors, and is of especial value in those double-cylinder air-compressors Whose pistons are directly connected with and driven concurrently in opposite directions by the same crank-shaft.
  • the invention is especially adapted to the motor air-compressor which is disclosed in my pending application, Serial No. 193,361.
  • Such motor-driven air-conipressors have no fly-wheel, and consequently when each piston concludes its compressionstroke and the crank-shaft passes the deadcenter the compressed air in the clearancespace expands and the piston is pushed backward, so as to take up all the backlash or lost motion with a hammer-blow. This causes objectionable noise and wear and tear.
  • the object of this invention is to prevent the described action and its objectionable results and to increase the volumetric efliciency of the machine, and these results are effected by opening up an air-passage between the clearance-spaces in the two cylinders just as the crank-shaft is passing the dead center, whereby the air compressed in the clearancespace in one cylinder will flow into the opposite cylinder, thereby equalizing the pressure against both pistons.
  • Figure 1 is a sectional plan view of a double-cylinder air-compressor equipped with my invention, said section being partly in the plane indicated by line 1 1 of Fig. 2.
  • Fig. 2 is a side View for most part in central vertical section in the plane indicated by line 2 2 of Fig. 1.
  • Fig. 3 is an enlargement of the rock-shaft and adjacent parts in the same plane as Fig. 1.
  • Fig. 4 is an enlarged front view of that part of the mechanism which is between the two air-cylinders when the cylinder 'head plate is removed.
  • Fig. 5 is an enlarged side elevation, partly in section, of the mechanism shown in Fig. 4.
  • A represents the two air-compressor cylinders, which are preferably formed in a single casting.
  • B represents the headplate, by which both cylinders may be-closed at their front ends.
  • 0 U are the pistons, which are moved in reverse directions by the crank-shaft D, to which they are connected by the connectingrods FF.
  • a worm-wheel I-l, attached to the crank-shaft, is turned by the motor-driven worm K, thereby turning the crank-shaft.
  • the clearancespaces mu. at the front end of the two cylinders are connected by a port M, which, as shown, is a narrow groove milled in the front end of the metal between the two cylinders. This groove crosses a tapered valve-seat m, to which the tapered valve G is fitted.
  • This valve normally prevents communication between the two ends of this port M.
  • the valve has an axial recess g in its front end, in which is a spring J, and this spring when the head-plate B is secured in place is compressed, so that it will hold the valve snugly against its seat.
  • a cross-port g which when the valve is in the position shown in Fig. & connects the two ends of the port M.
  • a rockshaft E is mounted in suitable bearings substantially parallel with the axes of the cylinders.
  • the flattened front end of this shaft enters a groove y in therear end of the valve G.
  • On the rear end of this rock-shaft is a wheel H.
  • the lost motion is taken up gradually and without substantial noise or jar.
  • the flow of the compressed air into the suction-cylinder from the clearance-space in the compression-cylinder increases the volumetric efficiency of the compressor, because this transference of air takes place at about the time when the piston in the suction-cylinder has completed its suction-stroke.
  • the volume of air in the suction-cylinder is therefore increased by the volume of air which flows into it from the clearance-space of the other cylinder. Except for this transference of air from one cylinder to the other the air left in the clearance would represent a loss of elficiency, while with the construction described it results in an increase of efficiency.
  • I claim 1 In atwo-cylinderair-compressor,the co1nbination with the two cylinders, their pistons, and means for concurrently moving said pistons in opposite directions, of a port connecting the clearance-spaces in said cylinders, a valve in said port, and means for moving said valve so as to temporarily open it just as each piston is about to terminate its compression-stroke.
  • crank-shaft having diametrically-opposed crank-pins which are respectively connected with said pistons, of a portconnecting the clearance-spaces in said cylinders, a valve in said port, a rock-shaft operatively engaging said valve, and cams secured to the crankshaft for operating said rock-shaft.
  • a two-eylinder air-compressor the combination with two parallel cylinders formed in the same casting, there being in themetal between said cylinders a groove connecting the front open ends of said cylinders, and there being also a conical valve-seat across said groove, a tapered valve fitted to said seat and having a transverse port and a substantially axial recess in its front end, with a head-plate closing the front ends of said cylinders and of said connecting groove, a rock shaft which engages with the notch in the rear end of said valve and which has at its opposite end a crank-arm, a spring tending to turn said shaft in one direction, the pump-pistons, a crank shaft having diametrieall y opposed crank-pins which are respectively connected with said pistons, and a wheel secured to said crank shaft having diametrically opposed cams which engage with the crank-arm on the rock-shaft and thereby rock it in opposition to its spring.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Compressors, Vaccum Pumps And Other Relevant Systems (AREA)

Description

No. 782,597 PATENTED FEB. 14, 1905.
. E. CHESHIRE.
EQUALIZING MEGHANISM FOR AIR OOMPRESSORS.
APPLICATION FILED APE.15.1904.
2 SHEETS -SHEET 1.
a4 a w E -l Win 6 J6 6L5 I Q In vrf0r 67% 521W W 0152070., f )QV'L/ myg PATENTED FEB. 14, 1905..
, E; CHESHIRE.
EQUALIZING MECHANISM FOR AIR GOMPRESSORS.
APPLICATION FILED APR.15.1904.
2 SHEETS-SHEET 2.
UNITED STATES Patented February 14;, I905.
PATENT OFFICE.-
EDl/VARD CHESHIRE, OF MILIVAUKEE, \VISOONSIN.
EQUALIZING MECHANISM FOR AIR-COMPRESSORS.
SPECIFICATION forming part of Letters Patent No. 782,597, dated February 14, 1905,
Application filed April 15, 1904. Serial No. 203,268.
To (all whom it Duty concern:
Be it known that I, EDWARD Giiusninn, a citizen of the United Statearesiding at Milwaukee, in the county of Milwaukee and State of Wisconsin, have invented a certain new and useful Improvement in Equalizing Mechanism for Air-Compressors, of which the fol lowing is a full, clear, and exact description, reference being had to the accompanying drawings.
This invention is an improvement in doublecylinder air-compressors, and is of especial value in those double-cylinder air-compressors Whose pistons are directly connected with and driven concurrently in opposite directions by the same crank-shaft. In the precise form in which the invention is shown it is especially adapted to the motor air-compressor which is disclosed in my pending application, Serial No. 193,361. Such motor-driven air-conipressors have no fly-wheel, and consequently when each piston concludes its compressionstroke and the crank-shaft passes the deadcenter the compressed air in the clearancespace expands and the piston is pushed backward, so as to take up all the backlash or lost motion with a hammer-blow. This causes objectionable noise and wear and tear.
The object of this invention is to prevent the described action and its objectionable results and to increase the volumetric efliciency of the machine, and these results are effected by opening up an air-passage between the clearance-spaces in the two cylinders just as the crank-shaft is passing the dead center, whereby the air compressed in the clearancespace in one cylinder will flow into the opposite cylinder, thereby equalizing the pressure against both pistons.
In the drawings, Figure 1 is a sectional plan view of a double-cylinder air-compressor equipped with my invention, said section being partly in the plane indicated by line 1 1 of Fig. 2. Fig. 2 is a side View for most part in central vertical section in the plane indicated by line 2 2 of Fig. 1. Fig. 3 is an enlargement of the rock-shaft and adjacent parts in the same plane as Fig. 1. Fig. 4 is an enlarged front view of that part of the mechanism which is between the two air-cylinders when the cylinder 'head plate is removed. Fig. 5 is an enlarged side elevation, partly in section, of the mechanism shown in Fig. 4.
Referring to the parts by letters, A represents the two air-compressor cylinders, which are preferably formed in a single casting.
B represents the headplate, by which both cylinders may be-closed at their front ends.
0 U are the pistons, which are moved in reverse directions by the crank-shaft D, to which they are connected by the connectingrods FF. A worm-wheel I-l, attached to the crank-shaft, is turned by the motor-driven worm K, thereby turning the crank-shaft.
The above-named parts are substantially like the corresponding parts as shown and fully described in my prior application referred to.
The present invention is not, of course, limited to the specific construction above described; but in the specific form in which said invention is shown it was especially designed for use with that particular mechanism.
The clearancespaces mu. at the front end of the two cylinders are connected by a port M, which, as shown, is a narrow groove milled in the front end of the metal between the two cylinders. This groove crosses a tapered valve-seat m, to which the tapered valve G is fitted. This valve normally prevents communication between the two ends of this port M. The valve has an axial recess g in its front end, in which is a spring J, and this spring when the head-plate B is secured in place is compressed, so that it will hold the valve snugly against its seat. In the front end of this valve is a cross-port g, which when the valve is in the position shown in Fig. & connects the two ends of the port M. IVhen turned into the position indicated by the dotted lines, communication between the two ends of said port is effectually closed. A rockshaft E is mounted in suitable bearings substantially parallel with the axes of the cylinders. The flattened front end of this shaft enters a groove y in therear end of the valve G. On the rear end of this rock-shaft is a wheel H.
shaft tends to turn it so as to always hold said friction roller in contact with said wormwheel. On that face of the worm-wheel with which said friction-roller engages are two short and rather quick cams it, located at diametrically opposite points. hen these cams engage with said friction-roller, they rock this rock-shaft, and thereby turn valve G, so that the cross-groove g therein connects the two ends of the port M. This engagen'ient takes place just before the crank-shaft reaches the dead-center, and thus the two cylinders are connected through the port M and the airpressure in them is equalized while the cranl shaft is passing said dead-center. hen the worm-wheel has turned to carry these cams out of contact with said friction-roller, the spring N turns the rock-shaft, which turns the valve (1i and closes the port connecting the two cylinders, this port having been open only for a very brief time, as described.
As a result of the above-described construction the lost motion is taken up gradually and without substantial noise or jar. In addition, the flow of the compressed air into the suction-cylinder from the clearance-space in the compression-cylinder increases the volumetric efficiency of the compressor, because this transference of air takes place at about the time when the piston in the suction-cylinder has completed its suction-stroke. The volume of air in the suction-cylinder is therefore increased by the volume of air which flows into it from the clearance-space of the other cylinder. Except for this transference of air from one cylinder to the other the air left in the clearance would represent a loss of elficiency, while with the construction described it results in an increase of efficiency.
Substantially the same mechanism would apply to the opposite ends of single-cylinder double-acting compressors.
Having described my invention, I claim 1. In atwo-cylinderair-compressor,the co1nbination with the two cylinders, their pistons, and means for concurrently moving said pistons in opposite directions, of a port connecting the clearance-spaces in said cylinders, a valve in said port, and means for moving said valve so as to temporarily open it just as each piston is about to terminate its compression-stroke.
2. In a two cylinder air-compressor, the combination with the two cylinders, their pistons, and a single crank-shaft having diametricallydisposed crank-pins which are respectively connected with said pistons, of a port connecting the clearance-spaces in said cylinders, a valve in said port, and mechanism operated by said crank-shaft, for operating said valve.
3. In a two-cylinder air-compressor,the combination with the two cylinders, their pistons,
and a crank-shaft having diametrically-opposed crank-pins which are respectively connected with said pistons, of a portconnecting the clearance-spaces in said cylinders, a valve in said port, a rock-shaft operatively engaging said valve, and cams secured to the crankshaft for operating said rock-shaft.
4. in a two-cylinder air-compressor, the combination with the two cylinders, their pistons, and a crank-shaft having diametrically-opposed erank-pins which are respectively connected with said pistons, of a port connecting the clearance-spaces in said cylinders, an oscillating valve in said port, a rock-shaft operatively connected with said valve and having a crank-arm, a spring operating to turn said rock-shaft in one direction, and a wheel secured to the crank-shaft and having two cam-surfaces engaging with said crank-arm to turn the rock-shaft in the opposite direction.
5. In a two-eylinder air-compressor, the combination with two parallel cylinders formed in the same casting, there being in themetal between said cylinders a groove connecting the front open ends of said cylinders, and there being also a conical valve-seat across said groove, a tapered valve fitted to said seat and having a transverse port and a substantially axial recess in its front end, with a head-plate closing the front ends of said cylinders and of said connecting groove, a rock shaft which engages with the notch in the rear end of said valve and which has at its opposite end a crank-arm, a spring tending to turn said shaft in one direction, the pump-pistons, a crank shaft having diametrieall y opposed crank-pins which are respectively connected with said pistons, and a wheel secured to said crank shaft having diametrically opposed cams which engage with the crank-arm on the rock-shaft and thereby rock it in opposition to its spring.
In testimony whereof I hereunto aiiix my signature in the presence of two witnesses.
EDYVA RI) CHESHIRE.
\Vitnesses:
\V. A. NUSSBAUMER, J. P. Bnusonnn.
US20326804A 1904-04-15 1904-04-15 Equalizing mechanism for air-compressors. Expired - Lifetime US782597A (en)

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Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2654326A (en) * 1948-10-07 1953-10-06 Milton Roy Co Constant delivery pump
US20020059907A1 (en) * 1999-03-23 2002-05-23 Thomas Charles Russell Homogenous charge compression ignition and barrel engines
US20030079715A1 (en) * 1999-03-23 2003-05-01 Hauser Bret R. Integral air compressor for boost air in barrel engine
US20040035385A1 (en) * 1999-03-23 2004-02-26 Thomas Charles Russell Single-ended barrel engine with double-ended, double roller pistons
US20040094103A1 (en) * 2002-04-30 2004-05-20 Hauser Bret R. Radial valve gear apparatus for barrel engine
US7033525B2 (en) 2001-02-16 2006-04-25 E.I. Dupont De Nemours And Company High conductivity polyaniline compositions and uses therefor
US7469662B2 (en) 1999-03-23 2008-12-30 Thomas Engine Company, Llc Homogeneous charge compression ignition engine with combustion phasing
US8046299B2 (en) 2003-10-15 2011-10-25 American Express Travel Related Services Company, Inc. Systems, methods, and devices for selling transaction accounts

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2654326A (en) * 1948-10-07 1953-10-06 Milton Roy Co Constant delivery pump
US6986342B2 (en) 1999-03-23 2006-01-17 Thomas Engine Copany Homogenous charge compression ignition and barrel engines
US20030079715A1 (en) * 1999-03-23 2003-05-01 Hauser Bret R. Integral air compressor for boost air in barrel engine
US6662775B2 (en) 1999-03-23 2003-12-16 Thomas Engine Company, Llc Integral air compressor for boost air in barrel engine
US20040035385A1 (en) * 1999-03-23 2004-02-26 Thomas Charles Russell Single-ended barrel engine with double-ended, double roller pistons
US6698394B2 (en) 1999-03-23 2004-03-02 Thomas Engine Company Homogenous charge compression ignition and barrel engines
US20040163619A1 (en) * 1999-03-23 2004-08-26 Thomas Engine Company Homogenous charge compression ignition and barrel engines
US20020059907A1 (en) * 1999-03-23 2002-05-23 Thomas Charles Russell Homogenous charge compression ignition and barrel engines
US7469662B2 (en) 1999-03-23 2008-12-30 Thomas Engine Company, Llc Homogeneous charge compression ignition engine with combustion phasing
US7033525B2 (en) 2001-02-16 2006-04-25 E.I. Dupont De Nemours And Company High conductivity polyaniline compositions and uses therefor
US20040094103A1 (en) * 2002-04-30 2004-05-20 Hauser Bret R. Radial valve gear apparatus for barrel engine
US6899065B2 (en) 2002-04-30 2005-05-31 Thomas Engine Company Radial-valve gear apparatus for barrel engine
US8046299B2 (en) 2003-10-15 2011-10-25 American Express Travel Related Services Company, Inc. Systems, methods, and devices for selling transaction accounts

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