US1897191A - Explosion engine - Google Patents

Explosion engine Download PDF

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US1897191A
US1897191A US469123A US46912330A US1897191A US 1897191 A US1897191 A US 1897191A US 469123 A US469123 A US 469123A US 46912330 A US46912330 A US 46912330A US 1897191 A US1897191 A US 1897191A
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cylinders
wall
mixture
manifold
engine
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US469123A
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Farina Giovanni
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B57/00Internal-combustion aspects of rotary engines in which the combusted gases displace one or more reciprocating pistons
    • F02B57/08Engines with star-shaped cylinder arrangements

Definitions

  • present invention relates to internal combustion engines with star or radially arranged cylinders and comprises means for distributing to engine cylinders an explosive mixture supplied by the engine carbureters in the best condition as to uniformity an d homogeneity.
  • the present invention has for its obJect means securing such result in a simple manner. and wlthout the use of moving parts.
  • this invention comprises a manifold consisting of an annular vided duct divided in sections each other,
  • Figure 1 is a front view of an seven engine with star-arrangedcyhnders having the 1n- Figure 3 is a transverse section of a modified construction.
  • the engine comprises cylinders 1, 2, 3, 4, 5, 6, 7 in which opera-- tive stroke is produced in the succession 1,
  • each of said cylinders has a suction duct 8, and said suction ducts 8 lead to an inlet manifold A communicating with the carbureters 16.
  • said manifold A comprises an annular duct having a substantially square cross section and confined outwardly by an outer cylindrical wall 9 havi tion (1 ng connections 10-for the cylinder sucucts 8; the internal wall of said .duct
  • each of said sections consists of two joined and similar sections 11, 11 each having the contour of a portion of a spiral line and a baffle 12, 12 extending into said duct and ending a small distance are thus provided in said manifold A and each of said sections has across section which is progressively de- 0 creasing from one to the other end, a pocket as 17, 17' being provided at one end of each section 13, 13' by the above described baffles 12, 12 extending thereinto, and in each of said pockets opens a mouth 14, 14 connected as with a duct 15 leading to a carbureter 16.
  • the mixture supplied by the carburetors 16 is caused to flow in a streamwhich is not affected by suction acting thereon, in register with cylinder suction ducts 810, and further, the stream in each section 13, 13 is assisted by the stream coming from the other manifold section, said sections communicating with each other at their ends through restricted passages 18, 18' 'provided by bafiles 12, 12.
  • the shape and arrangement of the described inlet manifold assist in directing to the cylinders the mixture flowing into said manifold through mouths 14,14, and further, they cause the mixture to circulate in a constant direction throughout said manifold, which direction is the same as that of succession ofignitions in engine cylinders.
  • a manifold for internal combustion engines with star-arranged cylinders comprising walls providing an. annular space, the
  • a manifoldfor internal combustion engines with star-arrangedcylinders comprising outer and inner walls providing an annular space, outlets departing from said outer wall and each leading to one of the engine cylinders, intermediate. walls separating said annular pace in compartments communicating through restricted passages, means for supplying fuel mixture and a connection from said means to each of said compartments, said connection terminating in said compartment at a point adjacent to the restricted passage and separated from said passage by said intermediate wall.
  • a manifold for internal combustion engines with star-arranged cylinders comprising an outer wall having a circular profile and an inner wall providing with said outer wall an annular space, outlets departing from said outer wall and each leading to one of the engine cylinders, intermediate walls separating said annular space in compartments communicating through restricted passages, means for supplying fuel mixture and a connection from said means to each of shaped to a plurality of volute arches following each other which separate the annular space in compartments communicating through restricted passages, inlets in said inner wall intermediate the beginning and the end of two subsequent volute arches, said inlets opening tangentially in said annular space, means for supplying fuel mixture and a connection from each of said inlets to saidmeans for supplying fuel mixture.
  • a manifold for internal combustion engines with star-arranged cylinders comprising walls providing an annular space, the outer one of said walls having a regular pr0 file, outlets departing from said outer Wall and each leading to one of the engine cylinders, the inner wall of said space being divided into sections which separate the annular space in compartments communicating through restrlcted passages, inlets in said inner wall intermediate'the beginning and the end of two subsequent sections, said inlets opening tangentially in said annular space, means for supplying fuel mixture and a connection from each'of said inlets to said means for supplying fuel mixture.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Cylinder Crankcases Of Internal Combustion Engines (AREA)

Description

Feb. 14, 1933. G. FARINA EXPLOSION ENGINE Filed July 19, 1930 Patented Feb. 14, 1933 UNITED STATES PATENT OFF The ICE
GIOVANNI FARINA, OF TURIN, ITALY EXPLOSION ENGINE Application filed July 19, 1930, Serial No. 469,123, and in Italy August 8, 1929.
present invention relates to internal combustion engines with star or radially arranged cylinders and comprises means for distributing to engine cylinders an explosive mixture supplied by the engine carbureters in the best condition as to uniformity an d homogeneity.
It is known that difficulties are found in in der form mixture,
supplying the several cylinders of a star-cylengine witha homogeneous and uniand more or less complicated devices and particularly centrifugal fans have been suggested for the purpose of stirring the mixture supplied by the carbureters; The present invention has for its obJect means securing such result in a simple manner. and wlthout the use of moving parts.
For
the above purpose this invention comprises a manifold consisting of an annular vided duct divided in sections each other,
communicating with and each of said sections is proat its end where mixture is introduced with a pocket open in front of, or opposite and tangentially to, the direction in which the mixture stream is caused to flow.
On the annexed drawing is shown by way of example an embodiment of this invention,
and
Figure 1 is a front view of an seven engine with star-arrangedcyhnders having the 1n- Figure 3 is a transverse section of a modified construction.
In Figures 1 and 2, the engine comprises cylinders 1, 2, 3, 4, 5, 6, 7 in which opera-- tive stroke is produced in the succession 1,
3, 5, 7, 2, 4, 6; each of said cylinders has a suction duct 8, and said suction ducts 8 lead to an inlet manifold A communicating with the carbureters 16. v
In the illustrated embodiment said manifold A comprises an annular duct having a substantially square cross section and confined outwardly by an outer cylindrical wall 9 havi tion (1 ng connections 10-for the cylinder sucucts 8; the internal wall of said .duct
consists of two joined and similar sections 11, 11 each having the contour of a portion of a spiral line and a baffle 12, 12 extending into said duct and ending a small distance are thus provided in said manifold A and each of said sections has across section which is progressively de- 0 creasing from one to the other end, a pocket as 17, 17' being provided at one end of each section 13, 13' by the above described baffles 12, 12 extending thereinto, and in each of said pockets opens a mouth 14, 14 connected as with a duct 15 leading to a carbureter 16.
In operation, the mixture supplied by the carburetors 16 is caused to flow in a streamwhich is not affected by suction acting thereon, in register with cylinder suction ducts 810, and further, the stream in each section 13, 13 is assisted by the stream coming from the other manifold section, said sections communicating with each other at their ends through restricted passages 18, 18' 'provided by bafiles 12, 12.
As shown in Figure 1, the shape and arrangement of the described inlet manifold assist in directing to the cylinders the mixture flowing into said manifold through mouths 14,14, and further, they cause the mixture to circulate in a constant direction throughout said manifold, which direction is the same as that of succession ofignitions in engine cylinders.
ssuming the suction is taking place in cylinder 1, this cylinder receives directly .the mixture supplied by mouth 14. and cooperating duct 15 and carbureter 16, the incoming mixture stream being directed thereto by baffie 12; thereafter in the engine cycle the suction takes place in cylinder3 and this cylinder is still supplied by mouth 14:. On) the contrary, the next suction in cylinder 5 is supplied by mouth 14; and thecooperatingflfi carburetor, and at this time the-bafiie 12 prevents the mixture supplied through mouth 14: from being drawn into said cylinder 5, said baflie further assisting the supply to cylinder 7 adjacent thereto.
The same description applies to the suction in other cylinders. As above described, the mixture which enters the manifold through mouths 14, 14 flows permanently in a given direction through sections 3, 3, as shown by arrows, and no reversal may take place in-the flowing mixture which is evenly and uniformly distributed to the several engine cylinders and provides a continuously circulating stream, this fact assisting the filling-in of cylinders.
Of course, the present invention is capable of many embidments other than that 'illustrated by way of example, but falling within the spirit of the appended claims; thus, months 10 for. the'connection of the engine cylinder suction ducts instead of being radial, as in Figures 1 and 2, may be arranged frontally of the manifold and elbow shaped asin the construction of Fig. 3, where said elbow connections are shown by reference 10.
What I claim'as myinvention and desire to secure by United States'Letters Patent 1s:--
1. A manifold for internal combustion engines with star-arranged cylinders, comprising walls providing an. annular space, the
Y outer one of said walls having a cylindrical profile, outlets departing from said outer wall and each leading to one of the engine cylinders, the inner wall of said space being shaped to a plurality of volute arches following each other which separate the annular space in compartments communicating through restricted passages, pockets formed in said inner wall intermediate the beginning and the end of two subsequent volute arches, said pockets opening tangentially in said annular space, means for supplying fuel mixture, and a connection from each of said pockets to said means for supplying fuel mixture.
2. A manifoldfor internal combustion engines with star-arrangedcylinders, comprising outer and inner walls providing an annular space, outlets departing from said outer wall and each leading to one of the engine cylinders, intermediate. walls separating said annular pace in compartments communicating through restricted passages, means for supplying fuel mixture and a connection from said means to each of said compartments, said connection terminating in said compartment at a point adjacent to the restricted passage and separated from said passage by said intermediate wall.
3. A manifold for internal combustion engines with star-arranged cylinders, comprising an outer wall having a circular profile and an inner wall providing with said outer wall an annular space, outlets departing from said outer wall and each leading to one of the engine cylinders, intermediate walls separating said annular space in compartments communicating through restricted passages, means for supplying fuel mixture and a connection from said means to each of shaped to a plurality of volute arches following each other which separate the annular space in compartments communicating through restricted passages, inlets in said inner wall intermediate the beginning and the end of two subsequent volute arches, said inlets opening tangentially in said annular space, means for supplying fuel mixture and a connection from each of said inlets to saidmeans for supplying fuel mixture.
5. A manifold for internal combustion engines with star-arranged cylinders, comprising walls providing an annular space, the outer one of said walls having a regular pr0 file, outlets departing from said outer Wall and each leading to one of the engine cylinders, the inner wall of said space being divided into sections which separate the annular space in compartments communicating through restrlcted passages, inlets in said inner wall intermediate'the beginning and the end of two subsequent sections, said inlets opening tangentially in said annular space, means for supplying fuel mixture and a connection from each'of said inlets to said means for supplying fuel mixture.
In testimony whereof, I aflix my signature.
GIOVANNI FARINA.
US469123A 1929-08-08 1930-07-19 Explosion engine Expired - Lifetime US1897191A (en)

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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2425156A (en) * 1943-03-12 1947-08-05 Lloyd O Knight Internal-combustion engine
US2511248A (en) * 1941-12-27 1950-06-13 Wright Aeronautical Corp Internal-combustion engine lubrication
US2578875A (en) * 1947-06-13 1951-12-18 New Britain Machine Co Valve actuating mechanism for multiple-row radial engines
US3166059A (en) * 1961-02-13 1965-01-19 Bendix Corp Aircraft fuel injection system

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2511248A (en) * 1941-12-27 1950-06-13 Wright Aeronautical Corp Internal-combustion engine lubrication
US2425156A (en) * 1943-03-12 1947-08-05 Lloyd O Knight Internal-combustion engine
US2578875A (en) * 1947-06-13 1951-12-18 New Britain Machine Co Valve actuating mechanism for multiple-row radial engines
US3166059A (en) * 1961-02-13 1965-01-19 Bendix Corp Aircraft fuel injection system

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