US1514280A - Internal-combustion engine - Google Patents

Internal-combustion engine Download PDF

Info

Publication number
US1514280A
US1514280A US592130A US59213022A US1514280A US 1514280 A US1514280 A US 1514280A US 592130 A US592130 A US 592130A US 59213022 A US59213022 A US 59213022A US 1514280 A US1514280 A US 1514280A
Authority
US
United States
Prior art keywords
cylinders
engine
valve
pistons
internal
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
US592130A
Inventor
Fitzhugh B Girvin
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 US592130A priority Critical patent/US1514280A/en
Application granted granted Critical
Publication of US1514280A publication Critical patent/US1514280A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01LCYCLICALLY OPERATING VALVES FOR MACHINES OR ENGINES
    • F01L7/00Rotary or oscillatory slide valve-gear or valve arrangements
    • F01L7/08Rotary or oscillatory slide valve-gear or valve arrangements with conically or frusto-conically shaped valves

Definitions

  • the invention relates to multiple cylinder internal combustion engines, and has for its object to provide a device of thisv character comprising elongated cylinders, in the opposite ends of which pistons are slidably mounted and connected tocrank shafts at opposite sides of the cylinders, which crank shafts have connecting rod connections whereby they will be rotated in unison by the various pistons. Also to provide rotary intake and exhaust valves disposed aboveand below the cylinders intermediate the ends thereof whereby the single charge will operate the pistons at the opposite end of each cylinder.
  • a further object is to provide gear means for controlling the rotation of the valves whereby different speeds of rotation may be obtained, thereby allowing the speed of operation of the engine to be controlled.
  • Figure 1 is a top plan view of the engine showing a portion of the casing broken away to better show the structure.
  • Figure 2 is an end view of the engine, part being broken away to better show the structure.
  • Figure 3 is a transverse sectional view through the engine taken on line 33 of Figure 1.
  • Figure 4 is a perspective view of one of the rotary valves.
  • Figure 5 is a vertical transverse sectional view through one of the cylinders taken on line 55 of Figure 1.
  • the numeral 1 designates the casing of the engine, which casing is provided with a plurality of elongated cylinders 2, in which cylinders, at the opposite ends thereof are slidably mounted pistons 4.
  • the pistons 4 move outwardly and inwardly towards each other and are provided with connecting rods the outer ends of which are connected to crank shafts 6 through the medium of cranks 7. It will be seen that when the pistons are forced outwardly that the cranks 6 will simultaneously rotate thereby imparting rotation to the fly wheels 8.
  • the cranks 6 are connected together adjacent their ends by means of connecting rods 9 which are connected to cranks 10, thereby insuring accurate and simultaneously timed rotation of the shaft.
  • the shafts 6 are pro vided with crank engaging members 11 for the reception of a crank handle 12, whereby the engine may be started in the usual manner.
  • a tapered rotary intake valve 13 Disposed above the cylinders 2 and rotatably mounted in a tapered bearing 12 is a tapered rotary intake valve 13, which valve is provided with a plurality of transversely disposed intake ports 14, which during the rotation of the valve comes into the registration with the ports 15 in the casing 1 and allow passage of fuel through the intake pipe 16 to the cylinders 2, intermediate their ends, and between the pistons 4 therein, where the fuel will be ignited by the spark plugs 17 and the piston simultaneouslyforced outwardly.
  • the valve 13 is provided with a spring 18 for maintaining the same tight within the tapered bearing 12.
  • a rotatably tapered exhaust valve 19 Disposed below the valve 13 and the cylinders 2 is a rotatably tapered exhaust valve 19, similarly shaped as the valve'12 and provided with a plurality of exhaust ports 20 extending therethrough, which exhaust ports, are during the rotation of the valve 19 moved into registration with the exhaust ports 21 in the casing 1, ports 20 being positioned whereby when the pistons 4 start inwardly on their exhaust stroke they will register with the ports 21 and allow the exhaust of the gases through the exhaust pipe 22, which exhaust pipe is provided with a drain cock 23 for allowing drainage of the engine, especially when steam is used instead of an explosive fuel.
  • a bevel gear 25 Secured to the idle gear 24 is a bevel gear 25, which bevelled gear 25 is adapted to be engaged by one of the bevelled gears 26 of the transversely shiftable shaft 27 rotatably mounted in bearings of the easing.
  • the shaft 27 adjacent its outer ends is provided with bevelled gears 28, which are adapted to be moved into and out of mesh with the small bevelled gear 29 carried by one of the crank shafts 6, and a large bevelled gear '30 carried by the other crank shaft 6 for increasing or diminishing the speed of rotation of the bevelled gear 25 thereby allowing the valves to be rotated for operating at a high or a low speed, said shifting of the-shaft 27 being controlled by a lever 31.
  • Valve 19 is provided with a spring 32, similar to the spring 18 for mainlaining the same tightly seated at'all times.
  • an opposed cylinder engine which is simple in construction, one wherein the same combustion chamber is used for opp0- site pistons, cylinder heads are eliminated, and one wherein a speed of operation may be controlled.

Description

F. B. GIRVIN INTERNAL COMBUSTION ENGI NE 1922 2 Shee1sSheet 1 Filed Oct. 5,
QMQMM New. 4 1924. 1,514,289
' Y F. B. GIRVIN INTERNAL COMBUSTION ENGINE Filed Oct. 5, 1922 2 sheets-sheet 2 Patented Nov. 4, 1924.
UNITED STATES FITZHUGH-B. GIRVIN, GEORGETOWN, TEXAS.
INTERNAL-COMBUSTION I ENGINE.
Application filed October 3, 1922. Serial No. 592,130.
To all whom it may concern: I
Be it known that I, FrrzHUGH B. GIRVIN, a citizen of the United States, residing at Georgetown, in the county of Williamson. State of Texas, have invented a new and useful Internal-Combustion Engine; andI do hereby declare the following to be a full, clear, and exact description of the invention, such as will enable others skilled in the art to which it appertains to make and use the same.
The invention relates to multiple cylinder internal combustion engines, and has for its object to provide a device of thisv character comprising elongated cylinders, in the opposite ends of which pistons are slidably mounted and connected tocrank shafts at opposite sides of the cylinders, which crank shafts have connecting rod connections whereby they will be rotated in unison by the various pistons. Also to provide rotary intake and exhaust valves disposed aboveand below the cylinders intermediate the ends thereof whereby the single charge will operate the pistons at the opposite end of each cylinder.
A further object is to provide gear means for controlling the rotation of the valves whereby different speeds of rotation may be obtained, thereby allowing the speed of operation of the engine to be controlled.
\Vith the above and other objects in view the invention resides in the combination and arrangement of parts as hereinafter set forth, shown in the drawing, describedv and claimed, it being understood that changes in the precise embodiment of the invention may be made within the scope of what is claimed without departing from the spirit of the invention.
In the drawings:
Figure 1 is a top plan view of the engine showing a portion of the casing broken away to better show the structure.
Figure 2 is an end view of the engine, part being broken away to better show the structure.
Figure 3 is a transverse sectional view through the engine taken on line 33 of Figure 1.
Figure 4 is a perspective view of one of the rotary valves.
Figure 5 is a vertical transverse sectional view through one of the cylinders taken on line 55 of Figure 1.
Referring to the drawings, the numeral 1 designates the casing of the engine, which casing is provided with a plurality of elongated cylinders 2, in which cylinders, at the opposite ends thereof are slidably mounted pistons 4. The pistons 4 move outwardly and inwardly towards each other and are provided with connecting rods the outer ends of which are connected to crank shafts 6 through the medium of cranks 7. It will be seen that when the pistons are forced outwardly that the cranks 6 will simultaneously rotate thereby imparting rotation to the fly wheels 8. The cranks 6 are connected together adjacent their ends by means of connecting rods 9 which are connected to cranks 10, thereby insuring accurate and simultaneously timed rotation of the shaft. The shafts 6 are pro vided with crank engaging members 11 for the reception of a crank handle 12, whereby the engine may be started in the usual manner. Disposed above the cylinders 2 and rotatably mounted in a tapered bearing 12 is a tapered rotary intake valve 13, which valve is provided with a plurality of transversely disposed intake ports 14, which during the rotation of the valve comes into the registration with the ports 15 in the casing 1 and allow passage of fuel through the intake pipe 16 to the cylinders 2, intermediate their ends, and between the pistons 4 therein, where the fuel will be ignited by the spark plugs 17 and the piston simultaneouslyforced outwardly. The valve 13 is provided with a spring 18 for maintaining the same tight within the tapered bearing 12. Disposed below the valve 13 and the cylinders 2 is a rotatably tapered exhaust valve 19, similarly shaped as the valve'12 and provided with a plurality of exhaust ports 20 extending therethrough, which exhaust ports, are during the rotation of the valve 19 moved into registration with the exhaust ports 21 in the casing 1, ports 20 being positioned whereby when the pistons 4 start inwardly on their exhaust stroke they will register with the ports 21 and allow the exhaust of the gases through the exhaust pipe 22, which exhaust pipe is provided with a drain cock 23 for allowing drainage of the engine, especially when steam is used instead of an explosive fuel.
Secured to the outer ends of the valves 13 and 19 are gears 23, which gears mesh, with anidle gear 24:, therefore the gears 23 will simultaneously rotate when the idle gear 24 is rotated. Secured to the idle gear 24 is a bevel gear 25, which bevelled gear 25 is adapted to be engaged by one of the bevelled gears 26 of the transversely shiftable shaft 27 rotatably mounted in bearings of the easing. The shaft 27 adjacent its outer ends is provided with bevelled gears 28, which are adapted to be moved into and out of mesh with the small bevelled gear 29 carried by one of the crank shafts 6, and a large bevelled gear '30 carried by the other crank shaft 6 for increasing or diminishing the speed of rotation of the bevelled gear 25 thereby allowing the valves to be rotated for operating at a high or a low speed, said shifting of the-shaft 27 being controlled by a lever 31. Valve 19 is provided with a spring 32, similar to the spring 18 for mainlaining the same tightly seated at'all times.
From the above it will be seen that an opposed cylinder engine is provided which is simple in construction, one wherein the same combustion chamber is used for opp0- site pistons, cylinder heads are eliminated, and one wherein a speed of operation may be controlled. It will also be seen that the and at the outer ends of the cylinders, connecting rod connections between the crank shafts and the pistons, a rotary intake valve above the cylinders centrally thereof at a right angle to the cylinders and in a plane at one side thereof and having ports of communication therewith, an exhaust valve below the cylinders at a right angle thereto and in a plane at the other side thereof from the intake valve and having ports of communication therewith and means for simultaneously rotating said intake and exhaust valves, said last named means being controlled at various speeds from either crank shaft and by a single lever between the crank shafts.
In testimony whereof I have signed my name to this specification in the presence of two subscribing witnesses.
. FITZHUGH B. GIRVINQ Witnesses C. H. GEE, H. C. GEE.
[ill
US592130A 1922-10-03 1922-10-03 Internal-combustion engine Expired - Lifetime US1514280A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US592130A US1514280A (en) 1922-10-03 1922-10-03 Internal-combustion engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US592130A US1514280A (en) 1922-10-03 1922-10-03 Internal-combustion engine

Publications (1)

Publication Number Publication Date
US1514280A true US1514280A (en) 1924-11-04

Family

ID=24369410

Family Applications (1)

Application Number Title Priority Date Filing Date
US592130A Expired - Lifetime US1514280A (en) 1922-10-03 1922-10-03 Internal-combustion engine

Country Status (1)

Country Link
US (1) US1514280A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4037572A (en) * 1976-07-28 1977-07-26 Franz Dennis Laverne Paired piston engine with rotary valves
US20090217904A1 (en) * 2007-01-24 2009-09-03 Lee Dae-Hee Crankless reciprocating steam engine

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4037572A (en) * 1976-07-28 1977-07-26 Franz Dennis Laverne Paired piston engine with rotary valves
US20090217904A1 (en) * 2007-01-24 2009-09-03 Lee Dae-Hee Crankless reciprocating steam engine
US7765803B2 (en) * 2007-01-24 2010-08-03 Inje University Industy-Academic Cooperation Foundation Crankless reciprocating steam engine

Similar Documents

Publication Publication Date Title
US1813259A (en) Engine
US1550643A (en) Reciprocatory internal-combustion engine
US2016734A (en) Internal combustion motor
US1514280A (en) Internal-combustion engine
US2457206A (en) Rotary valve for internalcombustion engines
US1539227A (en) Internal-combustion engine
US1764147A (en) Internal-combustion engine
US1398354A (en) wright
US1664150A (en) Double-acting four-cycle internal-combustion engine
US1799759A (en) Valve for internal-combustion engines
US1306639A (en) Internal-combustion engine
US1705638A (en) Internal-combustion engine
US1903511A (en) Engine
US1407336A (en) Internal-combustion engine
US1574686A (en) Engine
US1617792A (en) Internal-combustion engine
US1538208A (en) Internal-combustion motor
US1542765A (en) Internal-combustion engine
US1763460A (en) Valve mechanism for internal-combustion engines
US1672594A (en) Intebnal-combtrstion engine
US1357135A (en) Internal-combustion motor
US1912285A (en) Internal combustion engine
US1750733A (en) Rotary valve mechanism for internal-combustion engines
US1176857A (en) Rotary valve.
US1367825A (en) Internal-combustion engine