US1541207A - Internal-combustion engine - Google Patents

Internal-combustion engine Download PDF

Info

Publication number
US1541207A
US1541207A US629296A US62929623A US1541207A US 1541207 A US1541207 A US 1541207A US 629296 A US629296 A US 629296A US 62929623 A US62929623 A US 62929623A US 1541207 A US1541207 A US 1541207A
Authority
US
United States
Prior art keywords
cylinders
cylinder
combustion
chamber
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
US629296A
Inventor
Everett R Burtnett
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.)
AUTOMOTIVE VALVES CO
Original Assignee
AUTOMOTIVE VALVES CO
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 AUTOMOTIVE VALVES CO filed Critical AUTOMOTIVE VALVES CO
Priority to US629296A priority Critical patent/US1541207A/en
Application granted granted Critical
Publication of US1541207A publication Critical patent/US1541207A/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
    • F02B25/00Engines characterised by using fresh charge for scavenging cylinders
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B2720/00Engines with liquid fuel
    • F02B2720/13Two stroke engines with ignition device
    • F02B2720/131Two stroke engines with ignition device with measures for removing exhaust gases from the cylinder

Definitions

  • My invention relates to an internal combustion engine and has for its principal ob ject, the provision of asiX cylinder unit engine wherein the six cylinders are arranged in two series of three cylinders each, with each cylinder of each series performing a different function and the three cylinders of each series forming a cycle unit.
  • Fig. 1 is a top plan view of an internal combustion engine of my improved con- .struction.
  • crank case part 10 Suitably supported in the upper portion of crank case part 10, and preferabl ditaken on the lot , rectly above thecrankshaft is a pair of disposed substantially parallel with the axis of the crank shaft.
  • crank 13 The piston within cylinder 15 is connected to crank 13 by a pitman or connecting rod 18'and, in like manner, the piston in cylinder 15 is connected to crank 14 by a connecting rod 18 Crank shaft 12 is arranged to rotate clockwise as designated by the arrow in Fig. 3.
  • crank case member Arranged in crank case member and to the side of cylinders 15, and are inert volume pumping cylinders 19 and 19*, the axes of-which are radially disposed with respect to the axis of the crank shaft.
  • pistons such as 20', and the latter are connected, respectively, to the lower portions of the connecting rods 18 and 18 by connecting rods 21 and 21.
  • the upper portion of the chamber within cylinder 19 is connected to the intermediate portion of the chamber within cylinder 15 by a duct such as 22 and a similar duct 22 connects the upper portionof the chamber within cylinder 19 with the intermediate portion of the chamber within cylinder '15.
  • Cooling and scavenging volumes of inert air or cooled products of combustion are admitted into the upper ends of the chambers within the cylinders 19 and 19 through inlet ports such as 23, and which latter are enclosed by suitable valve housings 2i and 24, that are formed respectively, on the upper portions of cylinders 19 and 19
  • suitable valve housings 2i and 24 that are formed respectively, on the upper portions of cylinders 19 and 19
  • the passage of the inert vohimes through .the valve housings and to the ports 23 is controlled by valves such as 25, that are arranged on the upper ends of suitable springheld push rods 26 and 26.
  • Push rod '26 is arranged for operation in suitable bearings adjacent to cylinder 19 and its carried by the upper end of a push rod 41 lower end bears on the periphery of a cam 27, that is carried by crank shaft 12 and said cam having a lobe 28 that is approximately 135 or 'l l-O degrees-in length.
  • Push rod 26 is arranged for operation in suitable bearings adjacent to cylinder 19 and its lower end bears on a cam 29 that is identical with cam 27 and which is carried. by the crank shaft.
  • cams 27 and 29 are set so that their lobes are directly oppositeto each other.
  • crank case member 10 On top of crank case member 10 and to the side of cylinders 15 and 15 opposite from the side on which cylinders i 19 are located, are gaseous fuel cornpz eion cylinders and 30 'lhus, cylinders 15 1.5 and 30 are dis posed in one row and the cylinders 15 19 and 30 form another row, said rows being parallel with each other and disposed transversely or at right angles to the axis of the crank shaft.
  • the piston 31wvithin cylinder 30 is connected to the'lower portion of rod 18 by a connecting rod 32, and a similar piston within cylinder 3O is connected to the lower portion of rod 18 by a connecting rod 32.
  • the upper portions of the walls of the cylinders 30 and 30 are formed with chambers 33 and leading thereto from exhaust ports such as 34 that are formed in the intermediate portions of the chambers inner ends of the inert volume ducts 22 and 22 but said exhaust ports are slightly wider than said inlet'ports so that they will open or be uncovered an instant earlier than the inlet ports, during the downward travel of the pistons 16.
  • valve housings 36 and 36 Formed on the upper portions of the cyl inders 30 and 30* are, respectively, valve housings 36 and 36 and leading from these housings into the 'upper portions of the chambers within said cylinders are gaseous fuel inlet ports such as 37. 7
  • housings are connected by suitable ducts 38 to a suitable source of gaseous fuel supply and the passage. of the gaseous fuel through said housings and to the ports 37 is controlled by valves such as 39.
  • valve in housing 36 is carried by the upper end of a springheld push rod 40. that operates in suitable bearings, and the lower end of said rod bears on the periphery of cam 27. l
  • the inlet valve within housing 36 is that is identical with rod 40 and the lower end of said rod 41 bearing on the periphery of cam 29.
  • each combustion cylinder is extt-xnded upwardly to form a head 4C2. and formed in each head is a concentrically arranged annular chamber -13 in. which gaseous fuel is adapted to be compressed aud ignited.
  • Each chamber is connected to the piston clearance chamber 4:4: of the corresponding combustion cylinder by a relatively short, concentrically arranged throat 45 that tapers gradually toward its upper end. thereby forming, in effect, a. Venturi chamber or passageway from the center of the chamber as to the upper end of chamber 44.
  • each head 42 is a spark Removably seated inthe top of each head 42 is a valve cage 46 having acentrally ar-v
  • the lower end of each cage is provided with a suitable seat for a valve 49 that is .carried by the corresponding valve being substantially conical in form and provided in its under face with a recess 50.
  • valve stem Carried by the valve stem, and located a short distance above the valve 49 is a short piston 51, carrying in its face a series of packing rings.
  • This piston reciprocates within the upper portion of chamber 47. Seated in the head 42 above each chamber plug 52, and the inner ends of the electrodes thereof, project into said chamber.
  • a compressed gaseous fuel duct 53 leads from the upper end of cylinder to the chamber 47 above combustion cylinder 15 and a similar duct 54 leads from the upper portion of cylinder 30 to the valve chamber 47 that is located above cylinder 15.
  • Suitable springs co-operate with the valve stems 48 to normally hold the valves 49 upon their seats and said valves are unseated by rocker arms 55 that are actuated by push krods 56, and the latter being arranged in 1' suitable bearings to the sides of cylinders 15 and 15.
  • a housing 58 Formed on the upper portions of the walls 4 of cylinders 15 and 15 are heat disseminating webs or fins and surrounding said fins is a housing 58 that is mounted on the heads 42.
  • an air'duct 59 Leading from a suitably located fan to housing 58 is an air'duct 59.
  • My-in1prove'd,engine operates on the two stroke cycle principle and each time the power pistons pass theirhigh centers,:the compressed gaseous fuel charges above said pistons will be ignited in the usual manner 0 by the respective spark plugs, thereby driving said pistons downward on their power strokes.
  • Exhaust port 34 is uncovered an instant before the top of piston 16 passes below the inlet port at the lower end of duct 22 and as said last mentioned inlet port is uncovered, a charge of air or cooled products of combustion that was compressed on thepreceding upward stroke of the piston in cylinder 19, will discharge from the lower end of said duct 22 into chamber 44 directly over the top of the piston 16.
  • Pistons 20 and 31 move with piston 16 inasmuch as all of said pistons are connected to the same crank of sha 12 and on the upward strokes, piston 20 forces compressed air through duct 22 to the piston clearance phamber in cylinder 15 and piston 3L fdrces a compressed charge of gaseQus fuel through duct 50 into the annular chamber above the piston clearance chamber in said cylinder 15.
  • inlet valves 50 operate alternately in proper time relation with the movements of the corresponding sets of pistons and further that the valves and 89 are opened at the proper time to admit air or cooled products of combustion to the cylinders 19 and 19 and gaseous fuel to the cylinders and 30.
  • An internal combustion engine having six cylinders arranged in two rows of three cylinders each and the individual cylinders of each row being radially disposed, a crank shaft having a fixed direction of rotation, the two first cylinders of each row in the direction of crank rotation being adapted to the function of pumping an inert scavenging and cooling volume, the two second cylinders of each row in the direction of crank rotation being adapted for internal combustion, the two third cylinders of each row in the d'section of crank rotation being adapted to the function of gaseous fuel pumping, the first cylinder of each row in the direction of crank rotation functioning to provide the inert volume to the second cylinder of the other row, the third cylinder of each row in the direction of crank rotation functioning to pump the gaseous fuel to the second cylinder of the opposite row, means for supplying an inert volume to the inert volume pumping cylinders, 'means for supply- :ing gaseous fuel to the gaseous fuel pump- 1ng cylinders, cross ducts
  • An internal combustion engine having six radially arranged cylinders disposed in two rows, the two intermediate cyliiulcrs functioning as combustion cylinders, the two cylinders on one side of the intermediate cylinders functioning for the pumping of inert scavenging volumes into the lower portions of the combustion cylinders when the pistons therein pass the low or outer centers thereof, the two. cylinders of the other side of the intermediate cylinders functioning to pump gaseous fuel into said combustion cylinders, a crank shaft about which the cylinders are arranged, pistons within all of said cylinders, all three of the pistons in one row of cylinders being connected to one crank of the shaft, and all three of the pistons in the other row being connected to another crank of said shaft.
  • a pair of combustion cylinders a pair of inert volume pumping cylinders arranged to one side of said combustion cylinders, inert scavenging volume ducts leading from. the pumping cylinders to the lower portions of the chambers within the combustion cylinders, the discharg ends of said inert volume ducts being located so that they are uncovered and openonly' while the pistons in the combustion chambers are at their low centers, a pair of gaseous fuel pumping cylinders arranged on the other side of said combustion cylinders, a shaft having two cranks, pistons within all of said cylinders, the pistons in one of the combustion cylinders, pne of the inert volume pumping cyl-' inders and one of the gaseous fuel pumping cylinders being connected to one of the cranks and the pistons in the other combustion cylinder, inert volume pumping cylinder, and gaseous fuel pumping cylinder being connected to the other crank.
  • An internal combustion engine having six radially arranged cylinders disposed in two rows, the two intermediate cylinders of. the two rows functioning as combustion cylinders, the two cylinders on one side of the intermediate cylinders functioning for the 0 pumping of inert scavenging volumes into the lower portions of the combustion cylinders, and while the pistons therein are at their outer or low centers the two cylinders on the other side of the combustion cylinders functionoring to pump gaseous fuel into said combustion cylinders, exhaust ducts- EVERETT R. BURTNETT.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Output Control And Ontrol Of Special Type Engine (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)

Description

June 9,1925v E. BURTNETT INTERNAL, CONBUSTION ENGINE 1923 Sneeis-Sheet i Filed April 5:,
E. R. BURTNETT INTERNAL COMBUSTION ENGIN E Filed April. 3, 1923 2 Sheets-Sheet 2 v jfme Patented June 9, 1925.
UNITED STATES time earner EVERETT R. BURTNETT, OF LOS ANGELES, CALIFORNIA, ASSIGNOBI, BY DIRECT AND MESNE ASSIGNMENTS, TO THE AUTOMOTIVE VALVES 80., 0E LOS ANGELES, CALI- FORNI A, A VOLUNTARY TRUST.
IlINTERNAL-COMBUSTION ENGINE.
Application filed April 2,
To all whom it may concern:
Be it known that I, EVERETT R. BURTNETT, a citizen. of theUnited States, residing at Los Angeles, in the county of Los Angeles, State of California, have invented new and useful Improvements in Internal- Combustion Engines, of which the following is a specification.
My invention relates to an internal combustion engine and has for its principal ob ject, the provision of asiX cylinder unit engine wherein the six cylinders are arranged in two series of three cylinders each, with each cylinder of each series performing a different function and the three cylinders of each series forming a cycle unit.
Further objects of my invention are to provide a two cycle, two unit internal combustion engine wherein the cylinders of one unit or series function in co-ordination with the functions of the three cylinders forming the other cycle unit, to provide an internal combustion engine having six cylinders arranged in two radial rows that are parallel with each other and with the plane of crank rotation, with the three pistons of the three cylinders in one radial row connected to one crank of the crank shaft by one main or master connecting rod and two auxiliary connecting rods, and aviththe three pistons of the three cylinders in the second or other radial row connected by like means to a second crank of the crank shaft, and further, to provide a six cylinder unitinternal combustion engine having two cylinders adapted to function for internal combustion, two cylinders adapted for pumping a cool, inert volume as a scavenging function to the products of combustion within the combustion cylinders and two cylinders adapted for pumping a gaseous fuel mixture as a function of induction to the combustion cylinders. 1
Further objects of my invention are to provide a six cylinder unit internal combustion engine having a two throw crank dial rows of three cylinders each, each radial row being in a line with the plane of the rotation of the crank to which the pistons of the three respective cylinders are connected, the first. of the three cylinders of each row in the direction of crank rotation 1923. Serial No. 629,296.
being the inert scavenging volume pumping cylinder, the second, the internal combustion cylinder, the third, the gaseous fuel pumping cylinder and the first and third cylthe hot cylinder, cooling the and scavenging the chamber, the resid ou-tlet and inert volume inlet ports closing soon after the piston of the respective cylinder passes over the crank end dead center and the gaseous mixture inlet port, means being opened immediately thereafter and remaining open for a time corresponding to the piston travel for the first part ofthe cont pression stroke after the closing of the outlet and inert volume inlet ports, thereby allowing the induction of gaseous mixture as a throttle of variable quantity, in addition to a constant inert volume initial combus,
tion cylinder content.
lVith the foregoing and other objects in view my invention consists in certain novel features of construction and arrangement of parts that will be hereinafter more fully described and claimed and illustrated in the accompanying drawings, in which Fig. 1 is a top plan view of an internal combustion engine of my improved con- .struction.
stantiallv 180 degrees apart.
Suitably supported in the upper portion of crank case part 10, and preferabl ditaken on the lot , rectly above thecrankshaft is a pair of disposed substantially parallel with the axis of the crank shaft.
The piston within cylinder 15 is connected to crank 13 by a pitman or connecting rod 18'and, in like manner, the piston in cylinder 15 is connected to crank 14 by a connecting rod 18 Crank shaft 12 is arranged to rotate clockwise as designated by the arrow in Fig. 3.
Arranged in crank case member and to the side of cylinders 15, and are inert volume pumping cylinders 19 and 19*, the axes of-which are radially disposed with respect to the axis of the crank shaft.
Arranged for operation within these cylinders are pistons such as 20', and the latter are connected, respectively, to the lower portions of the connecting rods 18 and 18 by connecting rods 21 and 21.
The upper portion of the chamber within cylinder 19 is connected to the intermediate portion of the chamber within cylinder 15 by a duct such as 22 and a similar duct 22 connects the upper portionof the chamber within cylinder 19 with the intermediate portion of the chamber within cylinder '15.
Cooling and scavenging volumes of inert air or cooled products of combustion are admitted into the upper ends of the chambers within the cylinders 19 and 19 through inlet ports such as 23, and which latter are enclosed by suitable valve housings 2i and 24, that are formed respectively, on the upper portions of cylinders 19 and 19 The passage of the inert vohimes through .the valve housings and to the ports 23 is controlled by valves such as 25, that are arranged on the upper ends of suitable springheld push rods 26 and 26. Push rod '26 is arranged for operation in suitable bearings adjacent to cylinder 19 and its carried by the upper end of a push rod 41 lower end bears on the periphery of a cam 27, that is carried by crank shaft 12 and said cam having a lobe 28 that is approximately 135 or 'l l-O degrees-in length.
Push rod 26 is arranged for operation in suitable bearings adjacent to cylinder 19 and its lower end bears on a cam 29 that is identical with cam 27 and which is carried. by the crank shaft.
Obviously the cams 27 and 29 are set so that their lobes are directly oppositeto each other..
.trrangcd on top of crank case member 10 and to the side of cylinders 15 and 15 opposite from the side on which cylinders i 19 are located, are gaseous fuel cornpz eion cylinders and 30 'lhus, cylinders 15 1.5 and 30 are dis posed in one row and the cylinders 15 19 and 30 form another row, said rows being parallel with each other and disposed transversely or at right angles to the axis of the crank shaft. The piston 31wvithin cylinder 30 is connected to the'lower portion of rod 18 by a connecting rod 32, and a similar piston within cylinder 3O is connected to the lower portion of rod 18 by a connecting rod 32.
The upper portions of the walls of the cylinders 30 and 30 are formed with chambers 33 and leading thereto from exhaust ports such as 34 that are formed in the intermediate portions of the chambers inner ends of the inert volume ducts 22 and 22 but said exhaust ports are slightly wider than said inlet'ports so that they will open or be uncovered an instant earlier than the inlet ports, during the downward travel of the pistons 16.
Formed on the upper portions of the cyl inders 30 and 30* are, respectively, valve housings 36 and 36 and leading from these housings into the 'upper portions of the chambers within said cylinders are gaseous fuel inlet ports such as 37. 7
These housings are connected by suitable ducts 38 to a suitable source of gaseous fuel supply and the passage. of the gaseous fuel through said housings and to the ports 37 is controlled by valves such as 39.
The valve in housing 36 is carried by the upper end of a springheld push rod 40. that operates in suitable bearings, and the lower end of said rod bears on the periphery of cam 27. l
The inlet valve within housing 36 is that is identical with rod 40 and the lower end of said rod 41 bearing on the periphery of cam 29.
The upper portion of each combustion cylinder is extt-xnded upwardly to form a head 4C2. and formed in each head is a concentrically arranged annular chamber -13 in. which gaseous fuel is adapted to be compressed aud ignited.
"Each chamber is connected to the piston clearance chamber 4:4: of the corresponding combustion cylinder by a relatively short, concentrically arranged throat 45 that tapers gradually toward its upper end. thereby forming, in effect, a. Venturi chamber or passageway from the center of the chamber as to the upper end of chamber 44.
43 is a spark Removably seated inthe top of each head 42 is a valve cage 46 having acentrally ar-v The lower end of each cage is provided with a suitable seat for a valve 49 that is .carried by the corresponding valve being substantially conical in form and provided in its under face with a recess 50.
Carried by the valve stem, and located a short distance above the valve 49 is a short piston 51, carrying in its face a series of packing rings.
This piston reciprocates within the upper portion of chamber 47. Seated in the head 42 above each chamber plug 52, and the inner ends of the electrodes thereof, project into said chamber.
A compressed gaseous fuel duct 53 leads from the upper end of cylinder to the chamber 47 above combustion cylinder 15 and a similar duct 54 leads from the upper portion of cylinder 30 to the valve chamber 47 that is located above cylinder 15.
Suitable springs co-operate with the valve stems 48 to normally hold the valves 49 upon their seats and said valves are unseated by rocker arms 55 that are actuated by push krods 56, and the latter being arranged in 1' suitable bearings to the sides of cylinders 15 and 15.
The lower ends of these push rods bear on cams 57 that are located on the crank shaft adjacent to the cams 27 and 28.
Formed on the upper portions of the walls 4 of cylinders 15 and 15 are heat disseminating webs or fins and surrounding said fins is a housing 58 that is mounted on the heads 42.
Leading from a suitably located fan to housing 58 is an air'duct 59.
The construction just described provides means for disseminating the greater portion of the heat developed within the heads 42 and the upper portions ofthe combustion cylinders. v
My-in1prove'd,engine operates on the two stroke cycle principle and each time the power pistons pass theirhigh centers,:the compressed gaseous fuel charges above said pistons will be ignited in the usual manner 0 by the respective spark plugs, thereby driving said pistons downward on their power strokes.
For instance, as piston 16 passes high center, a spark produced between the terminals of plug 52,; ignites the compressed fuel charge in chamber 43, thereby driving said piston downwardly and AS the piston approaches its low center the corresponding exhaust port 34, will be uncovered, thereby ermitting the internal pressure to instantly drop and the greater portion of the products of combustion will discharge through said. port, the corresponding duct and chamber 33, which latter surrounds the gaseous fuel pumping cylinders 30 and 30.
Exhaust port 34 is uncovered an instant before the top of piston 16 passes below the inlet port at the lower end of duct 22 and as said last mentioned inlet port is uncovered, a charge of air or cooled products of combustion that was compressed on thepreceding upward stroke of the piston in cylinder 19, will discharge from the lower end of said duct 22 into chamber 44 directly over the top of the piston 16.
This blast of air of cooled products of combustion will strike against the adjacent curved face of rib 17 and thereby be deflected upwardly through the corresponding. side of I chamber 44 and consequently driving the burnt products of combustion out through exhaust port 34.
As piston 16 starts to move upwardly and before any considerable degree of internal pressure has been developed in the clearance charge of gaseous fuel that hasjust beenv compressed in cylinder30 will pass through duct 53 and chamber 47 and discharge over the conical upper surface of valve 50, into the annular chamber 43.
After passing downward through the o'uter portion of this chamber 43, the com pressed gaseous fuel will flow upwardly from the edge around the upper end of throat and after striking against the recess in the under side of the valve, said gas eous fuel will flow axially downward through throat or venturi opening 45 into piston clearance 44; and in so doing said compressed fuel charge will force before it, the residual products of combustion left within said chamber after the closing of exhaust port 34.
Thus as the piston moves upward the charge of gaseous fuel admitted to the combustion cylinder will be compressed in a stratum within annular chamber 43 and the residual products of combustion diluted with the air admitted through duct 22 will be compressed ina stratum in throat 45.
Thus on the subsequent ignition of the charge of compressed gaseous fuel, the resulting expansion will act through the stratum of residual products of combustion and air against the head of piston 16 to drive the same downward on its power stroke.
Pistons 20 and 31 move with piston 16 inasmuch as all of said pistons are connected to the same crank of sha 12 and on the upward strokes, piston 20 forces compressed air through duct 22 to the piston clearance phamber in cylinder 15 and piston 3L fdrces a compressed charge of gaseQus fuel through duct 50 into the annular chamber above the piston clearance chamber in said cylinder 15. I l i As will be understood, inlet valves 50 operate alternately in proper time relation with the movements of the corresponding sets of pistons and further that the valves and 89 are opened at the proper time to admit air or cooled products of combustion to the cylinders 19 and 19 and gaseous fuel to the cylinders and 30.
*Air pumped into duct 59 discharge downwardly over the fins or ribs on the upper portions of the cylinders 15 and 15 thereby exerting acooling effect upon the latter and also upon the walls surrounding the chamber Obviously the construction of the engine may be modified in minor details without departing from the spirit of my invention, the scope of which is set forth in the appended claims.
c I claim as my invention:
1. An internal combustion engine having six cylinders arranged in two rows of three cylinders each and the individual cylinders of each row being radially disposed, a crank shaft having a fixed direction of rotation, the two first cylinders of each row in the direction of crank rotation being adapted to the function of pumping an inert scavenging and cooling volume, the two second cylinders of each row in the direction of crank rotation being adapted for internal combustion, the two third cylinders of each row in the d'section of crank rotation being adapted to the function of gaseous fuel pumping, the first cylinder of each row in the direction of crank rotation functioning to provide the inert volume to the second cylinder of the other row, the third cylinder of each row in the direction of crank rotation functioning to pump the gaseous fuel to the second cylinder of the opposite row, means for supplying an inert volume to the inert volume pumping cylinders, 'means for supply- :ing gaseous fuel to the gaseous fuel pump- 1ng cylinders, cross ducts from the inert volume pumping cylinders to ports that are located in the lower portions of the combustion cylinders, and ports which are uncovered and open only when the pistons in the combustion chambers are at the outer ends of their travel, cross ducts from the gaseous fuel pumping cylinders to the combustion cylinders and ignition means within said combustion cylinders.
2. An internal combustion engine having six radially arranged cylinders disposed in two rows, the two intermediate cyliiulcrs functioning as combustion cylinders, the two cylinders on one side of the intermediate cylinders functioning for the pumping of inert scavenging volumes into the lower portions of the combustion cylinders when the pistons therein pass the low or outer centers thereof, the two. cylinders of the other side of the intermediate cylinders functioning to pump gaseous fuel into said combustion cylinders, a crank shaft about which the cylinders are arranged, pistons within all of said cylinders, all three of the pistons in one row of cylinders being connected to one crank of the shaft, and all three of the pistons in the other row being connected to another crank of said shaft.
3. In an internal combustion engine, a pair of combustion cylinders, a pair of inert volume pumping cylinders arranged to one side of said combustion cylinders, inert scavenging volume ducts leading from. the pumping cylinders to the lower portions of the chambers within the combustion cylinders, the discharg ends of said inert volume ducts being located so that they are uncovered and openonly' while the pistons in the combustion chambers are at their low centers, a pair of gaseous fuel pumping cylinders arranged on the other side of said combustion cylinders, a shaft having two cranks, pistons within all of said cylinders, the pistons in one of the combustion cylinders, pne of the inert volume pumping cyl-' inders and one of the gaseous fuel pumping cylinders being connected to one of the cranks and the pistons in the other combustion cylinder, inert volume pumping cylinder, and gaseous fuel pumping cylinder being connected to the other crank.
4. An internal combustion engine having six radially arranged cylinders disposed in two rows, the two intermediate cylinders of. the two rows functioning as combustion cylinders, the two cylinders on one side of the intermediate cylinders functioning for the 0 pumping of inert scavenging volumes into the lower portions of the combustion cylinders, and while the pistons therein are at their outer or low centers the two cylinders on the other side of the combustion cylinders functioring to pump gaseous fuel into said combustion cylinders, exhaust ducts- EVERETT R. BURTNETT.
which all of the cylinders
US629296A 1923-04-02 1923-04-02 Internal-combustion engine Expired - Lifetime US1541207A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US629296A US1541207A (en) 1923-04-02 1923-04-02 Internal-combustion engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US629296A US1541207A (en) 1923-04-02 1923-04-02 Internal-combustion engine

Publications (1)

Publication Number Publication Date
US1541207A true US1541207A (en) 1925-06-09

Family

ID=24522408

Family Applications (1)

Application Number Title Priority Date Filing Date
US629296A Expired - Lifetime US1541207A (en) 1923-04-02 1923-04-02 Internal-combustion engine

Country Status (1)

Country Link
US (1) US1541207A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2433111A (en) * 1945-06-20 1947-12-23 Cooper Bessemer Corp Two-cycle gas engine
US2511405A (en) * 1946-04-27 1950-06-13 Harmer G Hoover Gas fuel two-cycle internal-combustion engine
US2672854A (en) * 1949-04-02 1954-03-23 Jacob Z Brubaker Air-cooled valve
US3113561A (en) * 1961-01-10 1963-12-10 Ralph M Heintz Stratified charge two-cycle engine
CN114508414A (en) * 2020-11-17 2022-05-17 沃尔沃卡车集团 Internal combustion engine system

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2433111A (en) * 1945-06-20 1947-12-23 Cooper Bessemer Corp Two-cycle gas engine
US2511405A (en) * 1946-04-27 1950-06-13 Harmer G Hoover Gas fuel two-cycle internal-combustion engine
US2672854A (en) * 1949-04-02 1954-03-23 Jacob Z Brubaker Air-cooled valve
US3113561A (en) * 1961-01-10 1963-12-10 Ralph M Heintz Stratified charge two-cycle engine
CN114508414A (en) * 2020-11-17 2022-05-17 沃尔沃卡车集团 Internal combustion engine system
US11519305B2 (en) * 2020-11-17 2022-12-06 Volvo Truck Corporation Internal combustion engine system

Similar Documents

Publication Publication Date Title
US1541207A (en) Internal-combustion engine
US1540286A (en) Internal-combustion engine
US1664091A (en) Internal-combustion engine
US1638287A (en) Internal-combustion engine
US1638288A (en) Internal-combustion engine
US1833445A (en) Combustion chamber for internal combustion engines
US1555807A (en) Internal-combustion engine
US1596398A (en) Internal-combustion engine
US1633921A (en) Internal-combustion engine
US1626387A (en) Internal-combustion engine
US1640958A (en) Internal-combustion engine
US2139266A (en) Two-cycle combustion engine
US1356576A (en) Internal-combustion engine
US1907354A (en) Two-cycle internal combustion engine
US1596401A (en) Internal-combustion engine
US1645797A (en) Internal-combustion engine
US1210286A (en) Internal-combustion engine.
US1621634A (en) Internal-combustion engine
US1390572A (en) Internal-combustion engine
US1623391A (en) Internal-combustion engine
US1431188A (en) Internal-combustion engine
US1508260A (en) Internal-combustion engine
US1528002A (en) Internal-combustion engine
US1511705A (en) Internal-combustion engine
USRE22863E (en) Internal-combustion engine