US673109A - Gas-engine. - Google Patents

Gas-engine. Download PDF

Info

Publication number
US673109A
US673109A US67046498A US1898670464A US673109A US 673109 A US673109 A US 673109A US 67046498 A US67046498 A US 67046498A US 1898670464 A US1898670464 A US 1898670464A US 673109 A US673109 A US 673109A
Authority
US
United States
Prior art keywords
valve
cylinder
air
power
piston
Prior art date
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
Application number
US67046498A
Inventor
Gaston A Bronder
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to US67046498A priority Critical patent/US673109A/en
Application granted granted Critical
Publication of US673109A publication Critical patent/US673109A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • 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
    • F02B75/02Engines characterised by their cycles, e.g. six-stroke
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M9/00Carburettors having air or fuel-air mixture passage throttling valves other than of butterfly type; Carburettors having fuel-air mixing chambers of variable shape or position
    • F02M9/02Carburettors having air or fuel-air mixture passage throttling valves other than of butterfly type; Carburettors having fuel-air mixing chambers of variable shape or position having throttling valves, e.g. of piston shape, slidably arranged transversely to the passage
    • 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
    • F02B75/02Engines characterised by their cycles, e.g. six-stroke
    • F02B2075/022Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle
    • F02B2075/025Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle two

Definitions

  • This invention relates'to that class of gasengines known as compression explosive gas-engines, in which pistons are actuated by the pressure produced by the explosive combustion of a mixture of compressed air compression and power cylinders, and a valve deriving motion from the engine and serving the two purposes of controlling the admission of the explosive mixture of air and vapor or gas from the explosion-chamber to the power cylinder and the evacuation of the spent gases from the said cylinder.
  • compression explosive gas-engines in which pistons are actuated by the pressure produced by the explosive combustion of a mixture of compressed air compression and power cylinders, and a valve deriving motion from the engine and serving the two purposes of controlling the admission of the explosive mixture of air and vapor or gas from the explosion-chamber to the power cylinder and the evacuation of the spent gases from the said cylinder.
  • Figure 1 is a side elevation; Fig. 2, a front Fig. 3 is a vertical section parallel elevation. with Fig. l in the line 3 3 ofFig. 2 as viewed from the left of that figure.
  • Fig. 4 is a vertical section parallel with Fig. 2 in the line 4 4 of Figs. 1 and 3 as viewed from the right of those figures, the valve-gear and governor beingomitted.
  • Fig. P isadetail view, which will be hereinafter explained.
  • Fig. 5 is a plan view; Fig. 6, a vertical section of the carbureter and 'air-heater;-Fig. 7, a verticalsectiou corresponding with Figr3of the explosionchamber,the valve-box and valves of the compression-cylinder, and the valve for control ling the admission of the explosive mixture 'open to the atmosphere.
  • Fig. 9 is a detail view, which will be-hereinafter explained. Figs. 6, 7, and 8 are on a larger scale than Figs. 1 to 5, and Fig. 9 is on a still larger scale.
  • the engine represented is a double one-- that is to say, it has two similar power or explosion cylinders A A*, fitted with pistons E E*, and two similar compression-cylinders B, fitted with pistons F, onecompressiou-cylinder for each explosion-cylinder, the piston E'of the one explosion-cylinder A and the piston F of the corresponding compressioncylinder B being connected by rods G H with one, C, of two cranks set in opposite directions on the main or power transmitting shaft G of the engine, and the piston E* of the power-cylinder A* and the piston of the corresponding air-compression cylinder being connected by similar rods G H with the other one, (3*, of said cranks.
  • the said cylinders and shaft may besupported in any suitable manner.
  • the cylinders are represented as all erected upon a hollow base 0, in which are also provided the bearends of all the cylinders being opento the cavity of the base 0' may be considered as
  • the two engines of which this double engine is composed each comprising one compression-cylinder and piston and one explosion or power cylinder and piston, one crank and its piston connections, and one set of valves, are both alike, it will be sufficient to describe in detail, as follows, one of said engines:
  • the upper end of the explosion-cylinderA is closed by a head a and the upper end of the compression-cylinder is closed by a head 1), the last-mentioned head being made hollow to constitute a valve-box to contain the inletvalve 0 for the admission of the explosive mixture to the compression-cylinder and the ings O for the crank-shaft D.
  • the lower cylindrical valve J which controls the ad mission of the explosive mixture from the explosion-chamber to the explosion-cylinder and also controls the final evacuation of the spent gases from the said cylinder.
  • the said jacket f is supplied with cooling water through a side passage g (see Figs. 3 and 7) from a jacket f, which surrounds the power-cylinder and which is supplied with water through a pipe t, the water passing through both jackets and escaping by a pipe 72. at the top of the jacketf.
  • the induction-pipe K through which the mixture of air and vapor is admitted to the engine, communicates with the inlet-compartment of the valve-box in the compression-cylinder head I).
  • the inlet and discharge valves 0 din the said head may be such as are common in air-compressors. They are represented as puppet-valves with closingsprings c d.
  • the valve J is of hollow cylindrical form and derives an oscillating motion from one of two separate eccentrics J (see Figs. 1 and 2) on the crank-shaft D, the rod J of said eccentric being connected with an arm J" on a part of the valve-spiudlej,-which projects through one side of the casting I, in which the cylindrical seat of the said valve is formed.
  • the valve J has in its outer circumference a coved port j,which by the oschamber e and the cylinder-A through aport- 5 9' in the cylinder-head, just below which port there is an inlet is through one side of the cylinder-head from an igniting-tube 7c.
  • valve also has a second port j which will be hereinafter described as a supplemental exhaust-port, and through which by the oscillating movement of the valve comm unication is opened and closed between the cylin der A and the internal cylindrical cavity of the valve.
  • the valves J Jof the two engines opposite and in line with each other, as shown in Fig. 4, and their internal cylindrical cavities are both in constant communication, through a cross-passage j, (see Figs.
  • the body of the carbureter consists of a tight vessel P for containing the gasolcne or carbureting liquid and in which there is an opening m at one side for the entrance of fresh-heated air from the heater N and an opening at at the top for the exit of the carbureted air.
  • this vessel P From the top of this vessel P there is dependent a dipping cylinder or petticoat P, extending about half-way down, and within this petticoat there is contained in the said vessel a float P Attached to the top of the float within the petticoat there is an annular tray or trough P over which in the head of the vessel P there is a small opening 19, through which a suitable hydrocarbon liquid, as gasolene, drops into said trough or tray by a pipe 19 from any suitable reservoir under the control of a valve 19, fitted to said opening.
  • This valve is attached to a lever P which is so connected with the float as to be closed by the ascent and opened by the descent thereof.
  • the tray P is perforated near its outer edges, as indicated at 10 in Fig.
  • the communication between the outlet n and the passage q is controlled, as shown in Figs. 6 and 8, by a hollow conical valve Q,Which is fitted to acorresponding seat in the valve-box Q and adjustable by a handlever Q the ports in said seat and valve being so arranged, as shown in Fig. 6, as to be capable of opening and closing communication between 12 and (1 while opening or closing communication between the said passage q and an inlet-opening (1 through which fresh cold air may be admitted to the valvebox from the surrounding atmosphere to mix with the carbureted air when it may be ascertained that the latter is too highly carbureted.
  • the inlet g is fitted with an inwardlyopening check-valve g which is self-closing, to prevent any escape of carbureted air.
  • the air is drawn through the carbureter by the suction of the compression-cylinder piston during every downstroke of the latter, the said suction causing the air entering at m to the space between the petticoat and the walls of the vessel P to be drawn down-in the said space and to depress the level of the liquid therein below the edges of the petticoat under which it passes through the liquid within the latter, thence passing between the float and inner surface of the petticoat and absorbing the vapor from the thinly-distributed liquid on the said surface passing out at n.
  • valve Q be turned to a proper position to open communication between the fresh-air inlet g the suction of the compression-cylinder piston will also cause the opening of the valve (1 and the entrance of fresh air to mix with the carbureted air passing out at q.
  • a governorvalve R controlled, through a lever S, by a governor S on the crank-shaft, so that when the highest desired speed is exceeded the said valve cuts off the supply of air and vapor entirely from the engine and causes a vacuum in the compression-cylinder, thereby retarding the engine until it resumes its normal speed.
  • the heater represented is of multitubular construction, consisting of a cylinder or shell N, across which, near the ends thereof, are tube sheets or diaphragms r, which receive the air-tubes s.
  • the said shell N is connected at one end with the carbureter Pat the inlet m of the latter, and its other end is open to the atmosphere and has connected with it the air-suction pipe 'I, through which the air to be carbureted is supplied.
  • the said shell is connected between the tube-sheets r with the outlets L L of the two power-cylinders, so that the hot spent-gases escaping from said cylinders through said outlets into said shell will circulate around and between said tubes and heat the air which is drawn throughsaid tubes in the carbureter by the suction of the compression-cylinder.
  • the said shell has an outlet at N to the exhaust-pipe N through which the final escape of the spent gases takes place.
  • the supplemental exhaust-pipe M hereinbefore mentioned, through which the final exhaust from the power-cylinder through the ports 7' j and the valve J takes place, is connected with the heater-shell N at M, so that all of the escaping hot spent gases from the engine are utilized for heating the incoming air.
  • Fig. 3 The arrangement of the power-cylinder A and the compression-cylinderB and their connection with a single crank, which constitute important features of my invention, are best illustrated in Fig. 3.
  • the two cylinders, placed one before the other and as near together as practicable, are set at such inclination to each other and the crank-shaft is arranged in such relation to them that lines coincident with the axes of the two cylinders would meet approximately in the axis of the crank-shaft, and hence that the two connecting-rods G and H of their respective pistons operate in connection with the crank-pin with approximately equal directness, each in lines as nearly as practicable parallel with its respective cylinder.
  • the connecting-rod H of the power-piston E is connected directly with the crank-pin, but the connecting-rod G of the compression-piston instead of being so directly connected is connected with the said rod H as nearly as practicable to the crankpin by means of a separate pin t, (see Fig. 3,) and by this means, while the connection between the crank-pin and the compressionpiston' is made in a nearly straight line, a
  • crank-pin bearing is obtained for the power-piston rod without a very long crank-pin.
  • the revolution of the crank being in the direction of the arrows shown near it in Figs. 1 and 3, which is such that the crank-pin passes the compression-piston before it passes the power-piston, causes the former piston first to complete its stroke and fill the explosion-chain her a with the fully-compressed gasbefore the power-piston is required to start on its working stroke.
  • the eccentric J 2 should be so set on the crank-shaft as to so operate the Valve J that the said valve will not open the communication between the two cylinders until after the termination of the upward stroke of the compression-piston and the completion of the compression, and that it will leave the power-cylinder port 3' open to the valve-portj for the final escape of the spent gas from the power-cylinder until the powerpiston has made all but a small fraction of its complete stroke.
  • the valve J so operating insures the evacuation of the power-cylinder of all-but an exceedingly small portipn of the spent gases before the advent of a fresh charge of air and gas or vapor.
  • a metal packing-ring 4 instead of being formed in the body of the valve is formed in the outer face of a metal packing-ring 4), which is fitted lo a seat countersunk in the exterior of the valve, and the opening tt is formed in a thimble 22', which is screwed into the said ring from the interior of the valve.
  • a ring Q12 of a suitable more or less elastic substance, as asbestos packing, of sufficient thickness to form not only a gastightpackingaround the thimble,buta spring by which the margin of the outer face of the metal ring 1; is held gas-tight against the interior of the valve-seat J.
  • a part of the reted is arranged over the lamp and above the igniting-tubes and within an arch formed by ⁇ the cross-passage j, as shown in Figs. 2 and 4, so that it may be heated to someextent by the wasteheat from the same lamp .U, the heat from which is .reverberated upon the said pipe T and theJigniting-tubes by the said arch.
  • Thepower-piston has completed its downward stroke and is just commencing to move upward and is exhaust ing through its ports Z.
  • the compression-piston havingstarted on its upward strokein advance of the power-piston has not yet moved upward far enough to cause the opening of its valve d by the compression of the mixture of air and vaporwith which its-cylinder was filled by the downward stroke.
  • the oscillating valve J ismoving in the direction of the arrow shown near it in Fig. 3, but the portj in the power-cylinderhead is closed both to the explosion-chamber and to the valve-port 9'
  • the valve J willhave moved far enough to open its port j to the port 7 as shown in Fig. 9, and so permit the spent gas remaining in the power-cylinder to be forced out therefrom by the upward movement of its piston through the interior of the valve J, and hence through the heater and carbureter to the exhaust-pipe.
  • the com- is
  • a single engine, organized ashereinabove described, having a heavy fly-wheel D on the crank-shaft would form aneifective motor, for
  • the-carburetor willbe dispensed with and :the inductionpipeK maybe connected with the outletm ofvthe heater, and-the gasmay be introduced into the induction-pipe-in a continuous jet or .sheaniat anysuitable distance fromthe compression-cylinder.
  • What.I claim as my invention is 1.
  • a compressionrcylinder a powercylinder, an explosion-chamber between said cylinders, and a hollow oscillating valve the internal cavity of which is in constant communication with an exhaust-outlet and in the exterior of which there is a coved port for forming communication between the powercylinder and explosive-chamberand through one side-of which there is a port for communication between the said power-cylinder. and the said internal cavity, substantially as herein described.
  • a compression explosive gas-engine having two power-cylinders arranged side by side and an arched exhaust-passage between and common to both cylinders, the combination of two igniting-tubes arranged side by sideone for each cylinder under the archrof said passage, a heating-lamp arranged under lating valve for controlling the admission ofthe explosive mixture to the power-cylinder and the explosion of spent gases therefrom having a port 9' through one side and opposite said port an open seat, of a metal packing-ring 'u fitted to said seat and having in its outer face a cavity of an area equal to said port, an elastic packing-ring Q12 fitted to said 15 seat within said metal packing-ring and a shouldered thirnble 'v screwed into said metal ring from the interior of the valve, all substantially as herein described.

Description

No. 673,|o9. Patented Apr. 30, I901;
a. snounen.
GAS' ENGINE.
(Application filed Feb. 16, 1898.) (No l odol.) 3 Sheats$heat 2.
un)" "I.
Inna. "0/1,"
- :"HE Nam-us pzrzns 00 monxu'rua, WASHINGTON, a. c.
Patented Apr. 30, l90l.
G. A. BRUNDER.
GAS ENGINE.
(Application filed Feb. 16, 1898.)
3 Sheets-Shoat 3.
(No ducal.)
UNITED STATES PATENT OFFICE.
GASTON A. BRONDER, OF BROOKLYN, NEW YORK.
GAS-ENGlNE.
SPECIFICATION forming part of Letters Patent No. 673,109, dated April 30, 1901.
Application filed February 16, 1898. Serial No. 670,464. (No model.)
To all whom it may concern.-
Be it known that I, GASTON A. BRONDER, a citizen of the United States, and a resident of the borough of Brooklyn, in the city of New York and State of New York, have invented a' new and useful Improvement in Gas-Engines, of which the following is a specification.
This invention relates'to that class of gasengines known as compression explosive gas-engines, in which pistons are actuated by the pressure produced by the explosive combustion of a mixture of compressed air compression and power cylinders, and a valve deriving motion from the engine and serving the two purposes of controlling the admission of the explosive mixture of air and vapor or gas from the explosion-chamber to the power cylinder and the evacuation of the spent gases from the said cylinder.
My invention also includes certain details to be hereinafter described, and pointed out in claims.
The accompanying drawings represent an engine embodying all the features of my invention.
Figure 1 is a side elevation; Fig. 2, a front Fig. 3 is a vertical section parallel elevation. with Fig. l in the line 3 3 ofFig. 2 as viewed from the left of that figure. Fig. 4 is a vertical section parallel with Fig. 2 in the line 4 4 of Figs. 1 and 3 as viewed from the right of those figures, the valve-gear and governor beingomitted. Fig. P isadetail view, which will be hereinafter explained. Fig. 5 is a plan view; Fig. 6, a vertical section of the carbureter and 'air-heater;-Fig. 7, a verticalsectiou corresponding with Figr3of the explosionchamber,the valve-box and valves of the compression-cylinder, and the valve for control ling the admission of the explosive mixture 'open to the atmosphere.
of air and gas or vapor from the combustiom chamber to the power-cylinder and the evacuation of the spent gas from the latter cylinder; Fig; 8, a horizontal section of thehandcontrolled valve hereinbefore mentioned and of the governor-valve and communicating passages, taken in the line 88 of Fig. 6. Fig. 9 is a detail view, which will be-hereinafter explained. Figs. 6, 7, and 8 are on a larger scale than Figs. 1 to 5, and Fig. 9 is on a still larger scale.
Similar-letters of reference designate corresponding parts in all the figures.
The engine represented is a double one-- that is to say, it has two similar power or explosion cylinders A A*, fitted with pistons E E*, and two similar compression-cylinders B, fitted with pistons F, onecompressiou-cylinder for each explosion-cylinder, the piston E'of the one explosion-cylinder A and the piston F of the corresponding compressioncylinder B being connected by rods G H with one, C, of two cranks set in opposite directions on the main or power transmitting shaft G of the engine, and the piston E* of the power-cylinder A* and the piston of the corresponding air-compression cylinder being connected by similar rods G H with the other one, (3*, of said cranks. These connections will be hereinafter more fully described. The said cylinders and shaft may besupported in any suitable manner. The cylinders are represented as all erected upon a hollow base 0, in which are also provided the bearends of all the cylinders being opento the cavity of the base 0' may be considered as As the two engines of which this double engine is composed, each comprising one compression-cylinder and piston and one explosion or power cylinder and piston, one crank and its piston connections, and one set of valves, are both alike, it will be sufficient to describe in detail, as follows, one of said engines:
The upper end of the explosion-cylinderA is closed by a head a and the upper end of the compression-cylinder is closed by a head 1), the last-mentioned head being made hollow to constitute a valve-box to contain the inletvalve 0 for the admission of the explosive mixture to the compression-cylinder and the ings O for the crank-shaft D. The lower cylindrical valve J, which controls the ad mission of the explosive mixture from the explosion-chamber to the explosion-cylinder and also controls the final evacuation of the spent gases from the said cylinder. The said jacket f is supplied with cooling water through a side passage g (see Figs. 3 and 7) from a jacket f, which surrounds the power-cylinder and which is supplied with water through a pipe t, the water passing through both jackets and escaping by a pipe 72. at the top of the jacketf.
The induction-pipe K, through which the mixture of air and vapor is admitted to the engine, communicates with the inlet-compartment of the valve-box in the compression-cylinder head I). The inlet and discharge valves 0 din the said head may be such as are common in air-compressors. They are represented as puppet-valves with closingsprings c d. The valve J is of hollow cylindrical form and derives an oscillating motion from one of two separate eccentrics J (see Figs. 1 and 2) on the crank-shaft D, the rod J of said eccentric being connected with an arm J" on a part of the valve-spiudlej,-which projects through one side of the casting I, in which the cylindrical seat of the said valve is formed. The valve J has in its outer circumference a coved port j,which by the oschamber e and the cylinder-A through aport- 5 9' in the cylinder-head, just below which port there is an inlet is through one side of the cylinder-head from an igniting-tube 7c. The
said valve also has a second port j which will be hereinafter described as a supplemental exhaust-port, and through which by the oscillating movement of the valve comm unication is opened and closed between the cylin der A and the internal cylindrical cavity of the valve. The valves J Jof the two engines opposite and in line with each other, as shown in Fig. 4, and their internal cylindrical cavities are both in constant communication, through a cross-passage j, (see Figs. 2, 4, and 5,) with a pipe M, which will be hereinafter described as the supplemental exhaust-pipe, and through which the finalevacuation of the hot spent gases from the cylinder A is efiected, the greater portion of said gases being intended to escape through portsl in the lower part of the said cylinder, which are opened and closed by the movement of its piston E, and through said ports to an outlet L (see Figs. 1, 2, 3, 5, and 6) to the heaterN, wherein the said hot gases are employed to heat the air on its way to the carbureter p.
The body of the carbureter, the location of which is shown in Figs. 1, 2, and 5, but which is shown in section in Fig. 6, consists of a tight vessel P for containing the gasolcne or carbureting liquid and in which there is an opening m at one side for the entrance of fresh-heated air from the heater N and an opening at at the top for the exit of the carbureted air. From the top of this vessel P there is dependent a dipping cylinder or petticoat P, extending about half-way down, and within this petticoat there is contained in the said vessel a float P Attached to the top of the float within the petticoat there is an annular tray or trough P over which in the head of the vessel P there is a small opening 19, through which a suitable hydrocarbon liquid, as gasolene, drops into said trough or tray by a pipe 19 from any suitable reservoir under the control of a valve 19, fitted to said opening. This valve is attached to a lever P which is so connected with the float as to be closed by the ascent and opened by the descent thereof. The tray P is perforated near its outer edges, as indicated at 10 in Fig. 6, for the escape of the liquid therefrom in numerous small streams against the internal surface of the petticoat P in a thinly-distributed condition. The float is so balanced and its lever connection with the valve 19 is such that the opening and closing of the said valve 19 is so controlled as to keep the liquid in the reservoir at a normal level only slightly above the lower edge of the petticoat. From the outlet n for the carbureted air a communication is provided to the induction -pipe K, which leads to the inlet-compartment of the valve box of the compression cylinder through a valve-box Q on the top of the carbureter, the said valve-box having an outletpassage q, Figs. 1, 2, 5, 6, and 8, which leads to said pipe K. The communication between the outlet n and the passage q is controlled, as shown in Figs. 6 and 8, bya hollow conical valve Q,Which is fitted to acorresponding seat in the valve-box Q and adjustable by a handlever Q the ports in said seat and valve being so arranged, as shown in Fig. 6, as to be capable of opening and closing communication between 12 and (1 while opening or closing communication between the said passage q and an inlet-opening (1 through which fresh cold air may be admitted to the valvebox from the surrounding atmosphere to mix with the carbureted air when it may be ascertained that the latter is too highly carbureted. The inlet g is fitted with an inwardlyopening check-valve g which is self-closing, to prevent any escape of carbureted air.
The air is drawn through the carbureter by the suction of the compression-cylinder piston during every downstroke of the latter, the said suction causing the air entering at m to the space between the petticoat and the walls of the vessel P to be drawn down-in the said space and to depress the level of the liquid therein below the edges of the petticoat under which it passes through the liquid within the latter, thence passing between the float and inner surface of the petticoat and absorbing the vapor from the thinly-distributed liquid on the said surface passing out at n.
If the valve Q be turned to a proper position to open communication between the fresh-air inlet g the suction of the compression-cylinder piston will also cause the opening of the valve (1 and the entrance of fresh air to mix with the carbureted air passing out at q.
Between the passage (1 and the pipe K there is provided in the valve-box Q a governorvalve R, controlled, through a lever S, by a governor S on the crank-shaft, so that when the highest desired speed is exceeded the said valve cuts off the supply of air and vapor entirely from the engine and causes a vacuum in the compression-cylinder, thereby retarding the engine until it resumes its normal speed.
The heater represented is of multitubular construction, consisting of a cylinder or shell N, across which, near the ends thereof, are tube sheets or diaphragms r, which receive the air-tubes s. The said shell N is connected at one end with the carbureter Pat the inlet m of the latter, and its other end is open to the atmosphere and has connected with it the air-suction pipe 'I, through which the air to be carbureted is supplied. The said shell is connected between the tube-sheets r with the outlets L L of the two power-cylinders, so that the hot spent-gases escaping from said cylinders through said outlets into said shell will circulate around and between said tubes and heat the air which is drawn throughsaid tubes in the carbureter by the suction of the compression-cylinder. The said shell has an outlet at N to the exhaust-pipe N through which the final escape of the spent gases takes place. The supplemental exhaust-pipe M, hereinbefore mentioned, through which the final exhaust from the power-cylinder through the ports 7' j and the valve J takes place, is connected with the heater-shell N at M, so that all of the escaping hot spent gases from the engine are utilized for heating the incoming air.
The arrangement of the power-cylinder A and the compression-cylinderB and their connection with a single crank, which constitute important features of my invention, are best illustrated in Fig. 3. The two cylinders, placed one before the other and as near together as practicable, are set at such inclination to each other and the crank-shaft is arranged in such relation to them that lines coincident with the axes of the two cylinders would meet approximately in the axis of the crank-shaft, and hence that the two connecting-rods G and H of their respective pistons operate in connection with the crank-pin with approximately equal directness, each in lines as nearly as practicable parallel with its respective cylinder. The connecting-rod H of the power-piston E is connected directly with the crank-pin, but the connecting-rod G of the compression-piston instead of being so directly connected is connected with the said rod H as nearly as practicable to the crankpin by means of a separate pin t, (see Fig. 3,) and by this means, while the connection between the crank-pin and the compressionpiston' is made in a nearly straight line, a
comparatively long crank-pin bearing is obtained for the power-piston rod without a very long crank-pin. The revolution of the crank being in the direction of the arrows shown near it in Figs. 1 and 3, which is such that the crank-pin passes the compression-piston before it passes the power-piston, causes the former piston first to complete its stroke and fill the explosion-chain her a with the fully-compressed gasbefore the power-piston is required to start on its working stroke. It will be understood that the eccentric J 2 should be so set on the crank-shaft as to so operate the Valve J that the said valve will not open the communication between the two cylinders until after the termination of the upward stroke of the compression-piston and the completion of the compression, and that it will leave the power-cylinder port 3' open to the valve-portj for the final escape of the spent gas from the power-cylinder until the powerpiston has made all but a small fraction of its complete stroke. The valve J so operating insures the evacuation of the power-cylinder of all-but an exceedingly small portipn of the spent gases before the advent of a fresh charge of air and gas or vapor.
To provide for the balancing of the valve J hereinbefore described against the pressure of the gas which is admitted into its interior through its port 7' I provide in its exterior opposite the said port a cavity to of an area equal to that of the said port j and provide an opening 41 to said cavity to from the interior of the valve. In order to prevent any leakage around the valve through the port and opening u, I have made the special provision fully represented in Fig. 9, which is a transverse section of the valve and its seat on a larger scale than Fig. 7. The said, cavity 1/. instead of being formed in the body of the valve is formed in the outer face of a metal packing-ring 4), which is fitted lo a seat countersunk in the exterior of the valve, and the opening tt is formed in a thimble 22', which is screwed into the said ring from the interior of the valve. Under the said ring at the bottom of its seat there is placed around the thimble o a ring Q12 of a suitable more or less elastic substance, as asbestos packing, of sufficient thickness to form not only a gastightpackingaround the thimble,buta spring by which the margin of the outer face of the metal ring 1; is held gas-tight against the interior of the valve-seat J.
pipe T which supplies the air to be carbu this reservoir oil their-own crank-pins and" cylinders are located in thespaces between; said cylinders, as shown in Figs. 2 and 4:, but more clearly in Fig. 4*, which is a horizontal? section of said tubes and parts of the two cyl-i inders anda plan of the single lamp bywhichl both of said tubes are keptheated sufficiently; to inflame the mixture of air and vapor or gas? which enters them from the explosion-cham-g ber. The said tubes are arranged side by side, and the lamp U is so arranged below them; that it will heat them both. A part of the reted is arranged over the lamp and above the igniting-tubes and within an arch formed by} the cross-passage j, as shown in Figs. 2 and 4, so that it may be heated to someextent by the wasteheat from the same lamp .U, the heat from which is .reverberated upon the said pipe T and theJigniting-tubes by the said arch.
.It has been hereinbefore mentioned that thebase O of the engineis hollow. Its bottom beingclosedtightly makesit serve as-an oil-reservoir-for containing oil for the lubrication of the-crank-shaftand crank-pin bearings. The cranks during the lower portions of their revolutions dipping into the oil in pickup a certain-portionot' said oil,-which during the upper portions of; their revolutionsi is-thrown bythem against and into catchers; 10, which conduct it to the oil-holes of the shaft-bearings G The operation of either of thetwo engines? is as follows: First, suppose the partsto :be in the relative positions shown in Fig. 1, the crank moving in the direction of the arrow; shown near it in Fig. 3. Thepower-piston has completed its downward stroke and is just commencing to move upward and is exhaust ing through its ports Z. The compression-piston havingstarted on its upward strokein advance of the power-piston has not yet moved upward far enough to cause the opening of its valve d by the compression of the mixture of air and vaporwith which its-cylinder was filled by the downward stroke. The oscillating valve J ismoving in the direction of the arrow shown near it in Fig. 3, but the portj in the power-cylinderhead is closed both to the explosion-chamber and to the valve-port 9' By the time the power-piston has moved upward far enough to close the exhaust-ports Z the valve J willhave moved far enough to open its port j to the port 7 as shown in Fig. 9, and so permit the spent gas remaining in the power-cylinder to be forced out therefrom by the upward movement of its piston through the interior of the valve J, and hence through the heater and carbureter to the exhaust-pipe. In the meantime the com-.
pression of the air and vapor which is going on in the compression-cylinder will have caused the opening of the valve 61, and the compressed mixture will be forced into the explosion-chamber-e, which continues to be closed to the power-cylinder by the valve J until the upward stroke of the compressioncylinder has been 'completed, when the valve J, the movement of which has been reversed, opens communication through .the cove j between the explosion-chamber: and the powercylinder, as shown in Fig. 7. The explosive :mixture entering the power-cylinder is at once ignited at'the opening 7c and the whole charge in thechamber 6 is exploded into gas,
which entering'the power-cylinder through .theport j producesthe downwardunovement of the piston E and a half-revolution of the crank, thedownward movement of the compression-piston B, which takes place at the same'time, drawing a new charge of explosivemixture into the compression-cylinder.
A single engine, organized ashereinabove described, having a heavy fly-wheel D on the crank-shaft would form aneifective motor, for
light work. In such an engine the upward .stroke of the pistonwould ,be' produced by .and the fresh charge of the explosive mixture is being drawn intothe co npressionrcylinder of the other ,Bngine, oneexplosion taking place in each power-cylinder during every half-revolution or two during each revolution.
.I-n an engine having its compressionand power cylinders, explosion-chain ber, .valves, and piston connections like thoseofithe engine herein described, but intendedto be actuated by an explosive-mixture of air and a permanent combustible gas, the-carburetor willbe dispensed with and :the inductionpipeK maybe connected with the outletm ofvthe heater, and-the gasmay be introduced into the induction-pipe-in a continuous jet or .sheaniat anysuitable distance fromthe compression-cylinder.
What.I claim as my invention is 1. In'an explosive gas-engine, the combination of a compressionrcylinder, a powercylinder, an explosion-chamber between said cylinders, and a hollow oscillating valve the internal cavity of which is in constant communication with an exhaust-outlet and in the exterior of which there is a coved port for forming communication between the powercylinder and explosive-chamberand through one side-of which there is a port for communication between the said power-cylinder. and the said internal cavity, substantially as herein described.
2. In a compression explosive gas-engine having two power-cylinders arranged side by side and an arched exhaust-passage between and common to both cylinders, the combination of two igniting-tubes arranged side by sideone for each cylinder under the archrof said passage, a heating-lamp arranged under lating valve for controlling the admission ofthe explosive mixture to the power-cylinder and the explosion of spent gases therefrom having a port 9' through one side and opposite said port an open seat, of a metal packing-ring 'u fitted to said seat and having in its outer face a cavity of an area equal to said port, an elastic packing-ring Q12 fitted to said 15 seat within said metal packing-ring and a shouldered thirnble 'v screwed into said metal ring from the interior of the valve, all substantially as herein described.
In testimony that I claim the foregoing as 20 my invention I have signed my name, in presence of two witnesses, this 7th day of February, 1898.
GASTON A. BRONDER.
Witnesses:
FREDK. HAYNES, L. M. EGBERT.
US67046498A 1898-02-16 1898-02-16 Gas-engine. Expired - Lifetime US673109A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US67046498A US673109A (en) 1898-02-16 1898-02-16 Gas-engine.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US67046498A US673109A (en) 1898-02-16 1898-02-16 Gas-engine.

Publications (1)

Publication Number Publication Date
US673109A true US673109A (en) 1901-04-30

Family

ID=2741661

Family Applications (1)

Application Number Title Priority Date Filing Date
US67046498A Expired - Lifetime US673109A (en) 1898-02-16 1898-02-16 Gas-engine.

Country Status (1)

Country Link
US (1) US673109A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2420454A (en) * 1945-08-10 1947-05-13 Viel Edmond Pierre Robert Two-cycle engine
US2769435A (en) * 1951-02-28 1956-11-06 Charles E Cass Two stroke cycle internal combustion engine with pump compression

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2420454A (en) * 1945-08-10 1947-05-13 Viel Edmond Pierre Robert Two-cycle engine
US2769435A (en) * 1951-02-28 1956-11-06 Charles E Cass Two stroke cycle internal combustion engine with pump compression

Similar Documents

Publication Publication Date Title
US4879974A (en) Crankcase supercharged 4 stroke, 6 cycle engine
US673109A (en) Gas-engine.
US676523A (en) Gas-engine.
US348998A (en) place
US1127810A (en) Internal-combustion engine.
US1582241A (en) Internal-combustion engine
US658367A (en) Explosive-engine.
US880704A (en) Gas-engine.
US1174765A (en) Two-cycle combustion-engine.
US736224A (en) Gas-engine.
US745704A (en) Gas-engine.
US975651A (en) Thermodynamic motor.
US620941A (en) Explosive-engine
US806125A (en) Rotary explosive-engine.
US322477A (en) place
US334041A (en) Method of operating explosive vapor engines
US1403736A (en) Internal-combustion motor
US758943A (en) Balanced valveless two-cycle gas-engine.
US1292942A (en) Internal-combustion engine.
US642706A (en) Gas-engine.
US419806A (en) Carl w
US576604A (en) Gas engine
US868202A (en) Internal-combustion engine.
US584282A (en) Gas-engine
US332447A (en) Gas-engine