US719855A - Stroke-varying mechanism for explosive-engines. - Google Patents

Stroke-varying mechanism for explosive-engines. Download PDF

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US719855A
US719855A US9091302A US1902090913A US719855A US 719855 A US719855 A US 719855A US 9091302 A US9091302 A US 9091302A US 1902090913 A US1902090913 A US 1902090913A US 719855 A US719855 A US 719855A
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stroke
pair
piston
explosive
crank
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US9091302A
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Albert F Parks
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B75/00Other engines
    • F02B75/04Engines with variable distances between pistons at top dead-centre positions and cylinder heads
    • F02B75/048Engines with variable distances between pistons at top dead-centre positions and cylinder heads by means of a variable crank stroke length
    • 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
    • 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
    • Y10T74/21Elements
    • Y10T74/211Eccentric
    • 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
    • Y10T74/21Elements
    • Y10T74/2173Cranks and wrist pins
    • Y10T74/2181Variable

Definitions

  • Figure l is a central vertical ⁇ section of a duplex explosive-engine of the vertical type embodying my present invention.
  • Fig. 2 is an enlarged detailillustrating the mode of mounting the eccentrics on the crank-shaft.
  • Fig. 3 is an ideal indicator-diagram, illustrating the cycle of such explosive-engine.
  • Fig. 4 is adiagrammatic view showing the four principal positions of the pistons and the mechanism controlling the movements thereof.
  • My invention is illustrated in the drawings as embodied in a duplex explosive-engine of the vertical type, the main casting of which is designated by 2 and has the usual bearings 3, suitably bushed, as shown at 4, for the reception of an engine-shaft or crank-shaft 5,
  • crank-pin constitutes an orbitally-movable carrier, the orbital axis of which is shown in Fig. 4 by the line 5', and the center of connection of the same with the cranks 6 and 6' is designated by the line 7'.
  • This member will usually be so mounted as to turn about aV rotary axis (indicated here bythe line 7') and in this case hasa circular working surface eccentric to such rotary axis. It will be evident, therefore, that this member or eccentric will be orbitally movable with the crank-pin and will l also be capable of turning about the axis of suchcrank-pin for the purpose of varying the position of the periphery of the eccentric relative toits axis of rotation, and thus lengthening or shortening the stroke of the piston or "other member governed by it.
  • the devices just described are sufficient for the purpose of varyingthe stroke of a single piston of an explosive-en gine, but for the purpose of operating pistons of a duplex engine differentially; but in similar cycles provision must be made for balancing the movements 'of the pistons and also for effecting the shifting of the working surface of each orbitallymovable controller or eccentric in a simple and eective manner and so that the parts will coperate to form an easy-running engine.
  • a pair of orbitally-movable members or eccentrics having differential Working surfaces each surrounding and disposed at dilferent distances from a center of connection or rotary axis located at one side of the Vorbital axis should be employed, and in this construction the differential working surfaces have a iXed relation to each other, -two eccentrics being shown in the drawings located in differentangular positions and so connectedas to move irl-unison.”
  • said eccentrics are disposed oppositely .with respect to the axis of the crank-pin-that 4is to say, they are one hundred and eighty degrees apart-and hence the movements in the cycle of one piston will have a lead of one hundred and eighty degrees over the corresponding movements in the cycle of the other piston.
  • the sleeve and the eccentrics thereon may be formed in two main parts, as indicated in Fig. 2, they being divided in this case in a plane intersecting the axis of the crank-pin and perpendicular to the line of throw ot' the crank, as shown at 18.
  • One of the elements or strap-rods connecting an eccentric with a piston has been hereinbefore referred to.
  • the other is similar thereto and connects the eccentric 12 with the piston IO and is designated by 13'.
  • All of the parts hereinbefore described may be embodied in an explosive-engine of any suitable type, that shown herein being of the duplex type, having at the upper end thereof parallel twin cylinders 2O and 20', preferably of the same size and located in like positions.
  • Fuel charges may be supplied to the compression spaces behind the pistons in these cylinders in any suitable manner-as, for example, through inlet-ports controlled by admission valves 2l and 2l'-and the burned products of combustion may be swept out through exhaust-openings controlled by exhaust-valves, such as 22 and 22.
  • exhaust-valves such as 22 and 22.
  • These valves may be operated by means of any wellknown valve-gear, (not shown,) it being apparent that each exhaust-valve may remain open until the piston corresponding thereto is almost in contact with the face of such valve.
  • Igniting devices, such as 25, of any suitable construction may be employed, and these may be operatedin any well-known manner to ignite and explode each charge.
  • Fig. 4 I have illustrated diagrammatically the positions which the various operating parts assume at four principal points in a complete cycle of operations, the heavy lines indicating the positions. of the parts when the piston 10 has reached the end of its compression-stroke and the piston 10 the end of i-ts expulsion-stroke.
  • the light full lines indicate the corresponding positions when the piston 10 reaches the end of its compression-stroke and the piston IO the end of its expulsion-stroke, the difference in the lengths of the compression and expulsion strokes being clearly indicated by the positions of these parts.
  • the heavy dotted lines indicate the positions of the parts at the end of the instroke corresponding to the heavy lines in this View, while the light dotted lines show the positions at the end of the instroke which correspond to the positions shown by light full lines.
  • each piston in turn accomplishes a cycle of operations consisting of four strokes of unequal lengths,'two of these strokes being of the same length, but occupying diierent portions of the cycle, while the other two are respectively'shorter and longer than said iirst two movements.
  • the two strokes of substantially equal lengths are the induction and expansion strokes,l While the compressionstroke is somewhat shorter and the expulsionstroke considerably longer than either 'the induction or the compression stroke.
  • Fig. 3 The cycle of the engine is shown graphically in Fig. 3, from which diagram it will be seen that the piston draws in its charge at or slightly below atmospheric pressure and on the outstroke moves in compressing the charge to a point considerably in the rear of the extreme limit of its outstroke, whereupon the charge is ignited and exploded, and during the returning instroke the gases are expanded substantially in the usual manner, except that the extreme limit of the expansion-stroke is considerably beyond the corresponding point of the induction-stroke.
  • a piston-stroke equal to either the induction-stroke ct b or the expansion-stroke d e plus the distance b e, which represents the amount of displacement of the extreme points of the expansion-stroke as compared with those of the induction-stroke.
  • crank-shaft having a double crank, of a sleeve mounted to turn on said crank and having a pair of eccentrics fixed thereto in dierent ⁇ angular positions, and a pair of elements coacting respectively with said eccentrics and controlled thereby.

Description

(No. 719,855. V PATENT-ED FEB. a, y190e..
' A. r. PARKS.
STROKE VARYING MEGHANISM POR EXPLdsIvB ENGINES.
` APPLIATIOFILEQ JAN. 23, `1902.
No MODEL.
7 Iren STATE-sf PATENT OFFICE.
ALBERT F. PARKS, F'BROOKLYN, NEW YORK.
STROKE-VARYING VMECHANISIVI FOR EXPLOSIVE-ENGINES.
SPECIFICATION formingpart of Letter'ratent No. 719,855, dated February e, 1903;
Application filed January 23. 1902. Serial No. 90,913. (No model.)
To @ZZ whom it may concern.:
Be it known that I, ALBERT F. PARKS, a citizen of the United States, anda resident of Brooklyn, in the county of Kings andState of New York, have invented certain new and useful Improvements in Stroke-Varying Mechanism for Explosive-Engines, of which the following is a specification.
In theI drawings accompanying this speciiication and forming part of this application, Figure l is a central vertical `section of a duplex explosive-engine of the vertical type embodying my present invention. Fig. 2 is an enlarged detailillustrating the mode of mounting the eccentrics on the crank-shaft. Fig. 3 is an ideal indicator-diagram, illustrating the cycle of such explosive-engine. Fig. 4 is adiagrammatic view showing the four principal positions of the pistons and the mechanism controlling the movements thereof.
Similar characters designate like parts in all the figures of the drawings.
My invention is illustrated in the drawings as embodied in a duplex explosive-engine of the vertical type, the main casting of which is designated by 2 and has the usual bearings 3, suitably bushed, as shown at 4, for the reception of an engine-shaft or crank-shaft 5,
which in this case has a double crank, somewhat .wide and made up in the usual Way of a pair of crank-arms 6 and 6', connected by a long crank-pin 7. This crank-pin constitutes an orbitally-movable carrier, the orbital axis of which is shown in Fig. 4 by the line 5', and the center of connection of the same with the cranks 6 and 6' is designated by the line 7'. For the purpose of regulating the movements of the piston or other member I make use of a member having a working surface surrounding and disposed at different distances from such center of connection y7' and shift the position of said working surface relatively to the orbital axis, a suitable element coacting with this working surface being interposed between the same and such piston. This member will usually be so mounted as to turn about aV rotary axis (indicated here bythe line 7') and in this case hasa circular working surface eccentric to such rotary axis. It will be evident, therefore, that this member or eccentric will be orbitally movable with the crank-pin and will l also be capable of turning about the axis of suchcrank-pin for the purpose of varying the position of the periphery of the eccentric relative toits axis of rotation, and thus lengthening or shortening the stroke of the piston or "other member governed by it. When a piston, such as 10, is mechanically connected with such an eccentric, as 12, in the ordinary manner-that is, by means of a strap-rod 13 it will be evident that the connections to .the piston from the crank-shaft will cause the piston to travel in a manner determined solely by the movements of the mechanically-connected parts and that the piston will have a positive cycle of mechanical movements invariable by any forces other than those due to the movements of elements coacting in a purely mechanical manner.
The devices just described are sufficient for the purpose of varyingthe stroke of a single piston of an explosive-en gine, but for the purpose of operating pistons of a duplex engine differentially; but in similar cycles provision must be made for balancing the movements 'of the pistons and also for effecting the shifting of the working surface of each orbitallymovable controller or eccentric in a simple and eective manner and so that the parts will coperate to form an easy-running engine. In order to enable the pistons or other members to operate differentially, so that, for instance, one will have its compression-stroke while the other isexpelling burned gases or so that one will have its ind notion-stroke while the other is expanding a charge, a pair of orbitally-movable members or eccentrics having differential Working surfaces each surrounding and disposed at dilferent distances from a center of connection or rotary axis located at one side of the Vorbital axis should be employed, and in this construction the differential working surfaces have a iXed relation to each other, -two eccentrics being shown in the drawings located in differentangular positions and so connectedas to move irl-unison."
In this case said eccentrics are disposed oppositely .with respect to the axis of the crank-pin-that 4is to say, they are one hundred and eighty degrees apart-and hence the movements in the cycle of one piston will have a lead of one hundred and eighty degrees over the corresponding movements in the cycle of the other piston. The sleeve and the eccentrics thereon may be formed in two main parts, as indicated in Fig. 2, they being divided in this case in a plane intersecting the axis of the crank-pin and perpendicular to the line of throw ot' the crank, as shown at 18. One of the elements or strap-rods connecting an eccentric with a piston has been hereinbefore referred to. The other is similar thereto and connects the eccentric 12 with the piston IO and is designated by 13'.
All of the parts hereinbefore described may be embodied in an explosive-engine of any suitable type, that shown herein being of the duplex type, having at the upper end thereof parallel twin cylinders 2O and 20', preferably of the same size and located in like positions. Fuel charges may be supplied to the compression spaces behind the pistons in these cylinders in any suitable manner-as, for example, through inlet-ports controlled by admission valves 2l and 2l'-and the burned products of combustion may be swept out through exhaust-openings controlled by exhaust-valves, such as 22 and 22. These valves may be operated by means of any wellknown valve-gear, (not shown,) it being apparent that each exhaust-valve may remain open until the piston corresponding thereto is almost in contact with the face of such valve. Igniting devices, such as 25, of any suitable construction may be employed, and these may be operatedin any well-known manner to ignite and explode each charge.
In Fig. 4 I have illustrated diagrammatically the positions which the various operating parts assume at four principal points in a complete cycle of operations, the heavy lines indicating the positions. of the parts when the piston 10 has reached the end of its compression-stroke and the piston 10 the end of i-ts expulsion-stroke. The light full lines indicate the corresponding positions when the piston 10 reaches the end of its compression-stroke and the piston IO the end of its expulsion-stroke, the difference in the lengths of the compression and expulsion strokes being clearly indicated by the positions of these parts. The heavy dotted lines indicate the positions of the parts at the end of the instroke corresponding to the heavy lines in this View, while the light dotted lines show the positions at the end of the instroke which correspond to the positions shown by light full lines. From this View it will be apparent that each piston in turn accomplishes a cycle of operations consisting of four strokes of unequal lengths,'two of these strokes being of the same length, but occupying diierent portions of the cycle, while the other two are respectively'shorter and longer than said iirst two movements. The two strokes of substantially equal lengths are the induction and expansion strokes,l While the compressionstroke is somewhat shorter and the expulsionstroke considerably longer than either 'the induction or the compression stroke.
The cycle of the engine is shown graphically in Fig. 3, from which diagram it will be seen that the piston draws in its charge at or slightly below atmospheric pressure and on the outstroke moves in compressing the charge to a point considerably in the rear of the extreme limit of its outstroke, whereupon the charge is ignited and exploded, and during the returning instroke the gases are expanded substantially in the usual manner, except that the extreme limit of the expansion-stroke is considerably beyond the corresponding point of the induction-stroke. After expansion is complete the burned products of combustion are expelled substantially at atmospheric pressure by a piston-stroke, e a, equal to either the induction-stroke ct b or the expansion-stroke d e plus the distance b e, which represents the amount of displacement of the extreme points of the expansion-stroke as compared with those of the induction-stroke.
1. The combination with a pair of connected cranks, of a pair of connected diuferential eccentrics loosely mounted on said cranks, and a pair of elements coacting respectively with said eccentrics and controlled thereby.
2. The combination with a pair of connected cranks, of a pair of connected eccentrics loosely mountedon said cranks in dierent angular positions, and a pair of elements coacting respectively with said eccentrics and controlled thereby.
3. The combination with a crank-shaft having a double crank, of a sleeve mounted to turn on said crank and having a pair of eccentrics fixed thereto in dierent` angular positions, and a pair of elements coacting respectively with said eccentrics and controlled thereby.
4. In an explosive-engine, the combination with a pair of cylinders, and with a pair of variable-stroke pistons movable therein, of a pair of connected cranks, a pair of differential connected eccentrics shiftable on said cranks, and connections between said eccentrics and said pistons.
5. In an explosive-engine, the combination with a pair of cylinders, and with a pair of variable-stroke pistons movable therein, of a crank-shaft having a double crank, a pair of ,connected dierential eccentrics shiftable on said crank, and a pair of strap-rods connecting said respective eccentrics with said pistons.
6. In an explosive-engine, the combination with a pair of cylinders, and with a pair of variable-stroke pistons movable therein, of a crank-shaft having a double crank, a sleeve mounted to turn on said crank and having a IOO IIO
pair of eccentrics fixed thereto in different, connected thereto and also connected with angular positions, and a pair of strap-rods saidpistons.
connecting said respective eccentrios with Signed at New York, in the county of New said pistons. York and State of New York, this 22d day of 5 7. In an explosive-engine, the combination January, A. D. 1902.
with a pair of cylinders, and with a pair of variable-stroke pistons movable therein, of ALBERT F PARKS an orbitally-movable shaft, and a pair ot con- Witnesses: nected differential crankmiotions located at C. S. CHAMPION,
Io dierent points in the length of said shaft and R. OHAMPIQN.
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