US2262264A - Internal combustion engine - Google Patents

Internal combustion engine Download PDF

Info

Publication number
US2262264A
US2262264A US283606A US28360639A US2262264A US 2262264 A US2262264 A US 2262264A US 283606 A US283606 A US 283606A US 28360639 A US28360639 A US 28360639A US 2262264 A US2262264 A US 2262264A
Authority
US
United States
Prior art keywords
cylinder
pistons
air
compression
compression chamber
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
US283606A
Inventor
Amos I Addison
Howard B Cheshire
Leroy E Caveriy
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 US283606A priority Critical patent/US2262264A/en
Application granted granted Critical
Publication of US2262264A publication Critical patent/US2262264A/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
    • F02B75/28Engines with two or more pistons reciprocating within same cylinder or within essentially coaxial cylinders
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01BMACHINES OR ENGINES, IN GENERAL OR OF POSITIVE-DISPLACEMENT TYPE, e.g. STEAM ENGINES
    • F01B7/00Machines or engines with two or more pistons reciprocating within same cylinder or within essentially coaxial cylinders
    • F01B7/02Machines or engines with two or more pistons reciprocating within same cylinder or within essentially coaxial cylinders with oppositely reciprocating pistons
    • F01B7/04Machines or engines with two or more pistons reciprocating within same cylinder or within essentially coaxial cylinders with oppositely reciprocating pistons acting on same main shaft
    • F01B7/12Machines or engines with two or more pistons reciprocating within same cylinder or within essentially coaxial cylinders with oppositely reciprocating pistons acting on same main shaft using rockers and connecting-rods

Definitions

  • Another object of our invention is to provide a novel and e'ective means of reciprocating the opposed pistons in the air cylinders from the pivotally mounted arms, said arms being actuated by the power pistons.
  • Still another object of our invention is to provide a novel 'scavenging means for each power cylinder, consisting of pairs o1' air cylinders, each pair o! cylinders having a common compression chamber.
  • a feature of our invention resides in the novell means whereby the volume of the air compression chamber may be easily and effectively altered to change-the pressure of the compressed air to suit various operating conditions of the engine.
  • Figure 2 is a sectional view taken on line 2-2 o! Figure 1.
  • FIG. 1 is a vertical,I sectional view o! our enour engine comprises a ⁇ frame I, in which a crank shaft 2 is journaled.
  • the crank shaft is provided with a separate throw for each piston in the engine, and we have here disclosed a single cylinder with two pistons and, therefore, the crank shaft is'provided with two throws.
  • a cylinder 3 is iixedly mounted in the Vupper part of the frame I ⁇ , and is arranged substantially as shown.
  • a pair of pistons l, i are mounted in the cylinder 3 and these pistons move simultaneously in the cylinder-that is, they are of the usual opposed
  • a pair oi rocker arms S, l are pivotaily journaledinthe frame I, theupper ends of the arms beingconnectedtothepistonslandibymeans ot the connecting rods 3, 3 respectively.
  • the iowerendsoitherockerarmsand'l areconnected to the throws of the crankshaft 2 through the pitmans III and II, respectively.
  • the cylinder 3 may be e. separate part or it may ⁇ be integrally cast with the frame I or the cylinder assembly. We have here shown the cylinder 3 as separate from the water jacket I2.
  • an ignition type of engine may also be used and include substantially the same construction.
  • the usual injection nozzle I3 extends into the cylinder 3 between the pistons l and 5.
  • the usual pressure pump Il compresses the fuel for the purpose of injecting this fuel into the cylinder on the compression stroke, all of which is usual and wellknown.
  • the drive for the pistons is very effective, and also simple and compact, as will ⁇ be subsequently described.
  • the compresser I5 consists of a pair of cylinders I6 and I1. These cylinders may be integrally cast with the water jacket I2, or may be separate and attached thereto, and are arranged immediately adjacent the cylinder 3.
  • the cylinders I6 and I1 are in the same vertical plane as the rocker arms i and 1, and are inclined at an angle, as shown in Figure 1.
  • The'pistons I8 and I9 are mounted in the cylinders Il and I1 respectively, and these pistons are reciprocated through links 20 and 2I ⁇ , which are pivotally attached to said pistons and to the rocker arms 6 and 1, as shown in Figure 1.
  • the links 20 and 2I are connected to' the arms 6 and 1 below the pivot point oi said arms, thereby causing the pistons I8 and I9 to move upwardly on the compression stroke, as the pistons 4 and 5 are moving outwardly on the power stroke.
  • the cylinders I6 and I1 are provided with a common oompression chamber 22, which is immediately adjacent the cylinder 3, and the dividing wall oi' this compression chamber may consist of a part of the wall oi the water jacket I2.
  • scavenging ports 23 and 24 extend from the compression under pressure into the cylinder 3, thus clearing this' cylinder of the burnt gases.
  • Within the compression chamber 22 there is an unobstructed space around the mouth portions ci the ports 2l and 2l, allowing the compression-heated air to pass directly through them without reduction in temperature. l
  • blocks 25 can be placed in the compression chamber 22, and these blocks are held in position by the bolt 26.
  • the blocks reduce the volumetric capacity of the compression chamber and thus the compression is increased.l
  • a frame a power cylinder mounted on said frame, a pair or opposed plstons in said cylinder, an opposed'piston air compressor having a compression chamber in controlled communication with the cylinders oi* said opposed pistons, said compression chamber havingl adjusting blocks therein to vary its capacity, and air compression means operated by the engine to produce in said air compression chamber the air pressures required :or scavenging and ignition purposes.
  • compresser i being integrally formed with the power cylinder, a piston in each cylinder, a com pression chamber common to both cylinders, a
  • said compression chamber l being formed by said water Jacket said air com'- presser having a pair of scavenging DOrts extending from the common compression chamber diand air compression means operated by the eiigine to produce in said air compression chamber the air pressures required :or scavenging and ignition purposes. there a compression block in ⁇ each of opposite end portions oi said chamber, and a threaded bolt connecting said blocks for adjustingV them toward and away from eachother.

Landscapes

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

Description

NOV- 11, 1941 A. l. ADDISON E-rAL 2,252,264
INTERNAL COMIBUSTION ENGINE Filed July 10, 1959 2 Sheets-Sheet 1 I N VE N T0195.
A //fos .l inn/son. How/w CMS/11H5. may E. Cave/wu.
www
/T TOR/VEX A. l. ADDISON ETAL 2,262,264
INTERNAL COMBUSTION ENGINE Filed July 10, 1959 Nov. 11, 1941.
2 'sheets-Shen 2 IN VE /V TORS.
' Patented Nev. 11,1941 y UNITED STATE s PATENT I OFFICE rivrEaNsLcoMnUsrIoN ENGINE A'mol I. Addison, Long Beach, Howard B.
Cheshire Long Beach, Calif.
, Wilmington,
and Leroy E. Caveriy,
Application July 10, 1939, Serial No. 283,606 Claims. (CL 12351) posed pistons in air cylinders arranged immediately adjacent the power cylinder.
" Another object of our invention is to provide a novel and e'ective means of reciprocating the opposed pistons in the air cylinders from the pivotally mounted arms, said arms being actuated by the power pistons.
Still another object of our invention is to provide a novel 'scavenging means for each power cylinder, consisting of pairs o1' air cylinders, each pair o! cylinders having a common compression chamber.
A feature of our invention resides in the novell means whereby the volume of the air compression chamber may be easily and effectively altered to change-the pressure of the compressed air to suit various operating conditions of the engine. l
Other objects, advantages and features of invention may appear from the accompanying drawings, the subjoined detailed description, and
the appended claims.
In the drawings:
gine.
Figure 2 is a sectional view taken on line 2-2 o! Figure 1.
Referring more particularly tothe drawings,
. Figure 1 is a vertical,I sectional view o! our enour engine comprises a `frame I, in which a crank shaft 2 is journaled. The crank shaft is provided with a separate throw for each piston in the engine, and we have here disclosed a single cylinder with two pistons and, therefore, the crank shaft is'provided with two throws. A cylinder 3 is iixedly mounted in the Vupper part of the frame I`, and is arranged substantially as shown. A pair of pistons l, i are mounted in the cylinder 3 and these pistons move simultaneously in the cylinder-that is, they are of the usual opposed A pair oi rocker arms S, l are pivotaily journaledinthe frame I, theupper ends of the arms beingconnectedtothepistonslandibymeans ot the connecting rods 3, 3 respectively. The iowerendsoitherockerarmsand'l areconnected to the throws of the crankshaft 2 through the pitmans III and II, respectively. The cylinder 3 may be e. separate part or it may` be integrally cast with the frame I or the cylinder assembly. We have here shown the cylinder 3 as separate from the water jacket I2.
Our engine is here shown as the Diesel type.
Howeven an ignition type of engine may also be used and include substantially the same construction. For the Diesel type. the usual injection nozzle I3 extends into the cylinder 3 between the pistons l and 5. The usual pressure pump Il compresses the fuel for the purpose of injecting this fuel into the cylinder on the compression stroke, all of which is usual and weilknown. For the purpose of scavenging the cylinder 3, we -provide an opposed piston air compressor adjacent the cylinder 3. In placing the compressor close to the cylinder with consequent short circuits, a greater eiliciency is obtained ldueto the fact that the heat of compression oi the air is conserved. Furthermore. in so positioning the compressor, the drive for the pistons is very effective, and also simple and compact, as will` be subsequently described.
The compresser I5 consists of a pair of cylinders I6 and I1. These cylinders may be integrally cast with the water jacket I2, or may be separate and attached thereto, and are arranged immediately adjacent the cylinder 3. The cylinders I6 and I1 are in the same vertical plane as the rocker arms i and 1, and are inclined at an angle, as shown in Figure 1. The'pistons I8 and I9 are mounted in the cylinders Il and I1 respectively, and these pistons are reciprocated through links 20 and 2I`, which are pivotally attached to said pistons and to the rocker arms 6 and 1, as shown in Figure 1. The links 20 and 2I are connected to' the arms 6 and 1 below the pivot point oi said arms, thereby causing the pistons I8 and I9 to move upwardly on the compression stroke, as the pistons 4 and 5 are moving outwardly on the power stroke. The cylinders I6 and I1 are provided with a common oompression chamber 22, which is immediately adjacent the cylinder 3, and the dividing wall oi' this compression chamber may consist of a part of the wall oi the water jacket I2. scavenging ports 23 and 24 extend from the compression under pressure into the cylinder 3, thus clearing this' cylinder of the burnt gases. Within the compression chamber 22 there is an unobstructed space around the mouth portions ci the ports 2l and 2l, allowing the compression-heated air to pass directly through them without reduction in temperature. l
If it is the desire to raise the compression in the compresser, blocks 25 can be placed in the compression chamber 22, and these blocks are held in position by the bolt 26. The blocks reduce the volumetric capacity of the compression chamber and thus the compression is increased.l
is preferably of the type having a fabric or me' tallic nlter pad,l which is usual and well-known.
Having described our invention, we claim:
1. Incombination with an engine, including a frame, a-cylinder, a pair of opposed pistonsin the cylinder. a pair of rocker arms journaled in the frame. and drive means extending from the pistons to the rocker arms, of lan opposed piston air compresser arranged immediately adiacent the power cylinder. said compresser comprising a pair of cylinders, a piston in each cylinder, and a driving link extending from each piston to a rocken arm, whereby said pistonsl are recipro cated, said air compresser having a compression chamber common to both o! said cylinders, and compression pressure adjusting blocks removably mounted in the compression chamber'.
2. In combination with an engine, including a frame, a horizontal power cylinder, a pair of opposed pistons in the cylinder, a pair of rocker arms iournaled in the frame, and drive means extending from' the pistons tothe rocker' arms. ofan opposed piston air compresser arranged immediately adjacent the power cylinder, said rectly through said water jacket into the power cylinder, and a driving link connecting each of the. 4pisirins in the air compresser to a rocker arm, whereby the pistons in the compresser are reciprocated.
3. In. combination with an engine, includinga frame. a horizontal power cylinder, a pair of opposed pistons in the cylinder, a pair of rockerv arms icurnaied in the frame, and drive means extending from the pistons to the rocker arms, of an opposed piston air compresser arranged immediately adjacent the power cylinder, said compresser being integrally formed with the water jacket of the power cylinder, said com -rocker arm, whereby the pistons in the compresser are reciprocated, and compression pressure adjusting blocks removably mounted in the compression chamber.
4. In an-engine, a frame, a power cylinder mounted on said frame, a pair or opposed plstons in said cylinder, an opposed'piston air compressor having a compression chamber in controlled communication with the cylinders oi* said opposed pistons, said compression chamber havingl adjusting blocks therein to vary its capacity, and air compression means operated by the engine to produce in said air compression chamber the air pressures required :or scavenging and ignition purposes.
5. In an engine. a frame. a power cylindermounted on said frame, a pair o! opposed piaf tons in said cylinder, an opposed piston air com'- pressor having a compression chamber in controlledl communication with cylinders of said opposed pistons, said compression chamber havina adjusting blocks therein to vary its capacity,
compresser i being integrally formed with the power cylinder, a piston in each cylinder, a com pression chamber common to both cylinders, a
' portion o! the'wall o! said compression chamber l being formed by said water Jacket said air com'- presser having a pair of scavenging DOrts extending from the common compression chamber diand air compression means operated by the eiigine to produce in said air compression chamber the air pressures required :or scavenging and ignition purposes. there a compression block in` each of opposite end portions oi said chamber, and a threaded bolt connecting said blocks for adjustingV them toward and away from eachother. t AMOS I. ADDISON.
HOWARDB. CHESHIRE. LEROY E. CAVERLY.
US283606A 1939-07-10 1939-07-10 Internal combustion engine Expired - Lifetime US2262264A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US283606A US2262264A (en) 1939-07-10 1939-07-10 Internal combustion engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US283606A US2262264A (en) 1939-07-10 1939-07-10 Internal combustion engine

Publications (1)

Publication Number Publication Date
US2262264A true US2262264A (en) 1941-11-11

Family

ID=23086815

Family Applications (1)

Application Number Title Priority Date Filing Date
US283606A Expired - Lifetime US2262264A (en) 1939-07-10 1939-07-10 Internal combustion engine

Country Status (1)

Country Link
US (1) US2262264A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2530884A (en) * 1945-12-15 1950-11-21 Auxiliaire Ind L Internal-combustion engine with opposed pistons
US2730087A (en) * 1952-05-02 1956-01-10 Digby B Morton Internal-combustion engines

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2530884A (en) * 1945-12-15 1950-11-21 Auxiliaire Ind L Internal-combustion engine with opposed pistons
US2730087A (en) * 1952-05-02 1956-01-10 Digby B Morton Internal-combustion engines

Similar Documents

Publication Publication Date Title
US2844131A (en) Reciprocating piston machine
US2262264A (en) Internal combustion engine
US1771335A (en) Internal-combustion engine
US3338137A (en) Piston power units
US2405016A (en) Piston and cylinder device
US2127758A (en) Internal combustion engine
US1149142A (en) Internal-combustion engine.
US1638288A (en) Internal-combustion engine
US1639165A (en) Internal-combustion engine
US2136293A (en) Internal combustion engine
SU13564A1 (en) Vertical double internal combustion engine
US2130529A (en) Internal combustion engine
US2099371A (en) Diesel engine
US1845862A (en) Internal combustion engine with staged compression and expansion
US2383432A (en) Internal-combustion engine
US1390572A (en) Internal-combustion engine
US1491410A (en) Internal-combustion engine
US1779596A (en) Internal-combustion engine
US2545793A (en) Internal-combustion engine operating on the four-stroke cycle with compression ignition
US1546008A (en) Internal-combustion engine
US2058505A (en) Internal combustion engine
RU2174603C2 (en) Positive-displacement double-acting piston machine (design versions)
SU12432A1 (en) Internal combustion engine with auxiliary piston
SU49652A1 (en) Internal combustion engine compound with the introduction of compressed air into the combustion products
US1440154A (en) Two-stroke-cycle engine