US2167303A - Exhaust device for internal combustion engines - Google Patents

Exhaust device for internal combustion engines Download PDF

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US2167303A
US2167303A US38826A US3882635A US2167303A US 2167303 A US2167303 A US 2167303A US 38826 A US38826 A US 38826A US 3882635 A US3882635 A US 3882635A US 2167303 A US2167303 A US 2167303A
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cylinder
gases
exhaust
mass
internal combustion
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US38826A
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Kadenacy Michel
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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
    • F02B27/00Use of kinetic or wave energy of charge in induction systems, or of combustion residues in exhaust systems, for improving quantity of charge or for increasing removal of combustion residues
    • F02B27/04Use of kinetic or wave energy of charge in induction systems, or of combustion residues in exhaust systems, for improving quantity of charge or for increasing removal of combustion residues in exhaust systems only, e.g. for sucking-off combustion gases
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/12Improving ICE efficiencies

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  • Theiinvention relates to two-stroke internal combustion engines, wherein the evacuation of the' cylinder by vthebodily displacement of-the burnt gases from jthe cylinder into the exhaust ,system is utilised for the :purpose of. introducing a fresh charge by controlling the inletroriflce to open for the introduction of the said charge when the exhaust gases are moving "outwardly through the exhaust port or duct as a consequence of this 1 9, bodily displacementifromthe cylinder.
  • the exhaust-port is then still open, may cause the charge in the cylinder to be fouled andsome of l 20 this'ch'arge to be forced out of the inlet ports,
  • the object of the invention is to provide means whereby the objectionable actions of an untimely return of the burnt gases or of a prolonged suction in the exhaust system may be minimised.
  • Figure 1 relates to one embodiment of the invention in which the issuing mass of burnt gases is'directed on to a small gaseous mass in the 40 exhaust system and-exerts its pressure on the main atmosphere in a continuous manner.
  • Figure '2 relates to an embodiment in which the explosion gases are constrained to follow an o chamber 3 arrangedas a by-pass on the main the engine cylinder.
  • the faceof the gaseous column ⁇ in the duct 2 in this case forms a reflecting surface on which the gases impinge, and, which yields as the atmospheric column in the duct 2 is put into move-, ment in-the direction'of exhaust.
  • an 1 assembly of fixed guide vanes-or blades I is mounted in the exhaust duct 6 inorder to impart .to the issuing explosion gases a whirling or screw motion.
  • I a This assembly will befittedas closeas possiblev to the cylinder and between the engine and the silencer. The area of passage for the gases-will be made such that the volume of gases dealt with can pass freely.
  • the blades 5 act as deflecting surfaces and,
  • the body of'explosion gases is thus made toact like a screw action upon the atmospheric mass in the duct 6, so as to exert a continuous pressure on the latter, until this atmospheric resistance is broken down and the explosion gases 40 can escape.
  • the exhaust duct opens into the annular chamber 8, forming a closed circuit, situated preferably as close as possible to the latter and having a volume a little larger than the w cylinder volume.
  • the peripheral walls of the chamber I are provided with small orifices 9 leading to the atmosphere and suitably directed to facilitate the &cape of the explosion gases.
  • the devices according to the invention must be placed nearer the cylinder than the point from which the rebound of the gases to the cylinder would occur, as they will otherwise have no infiuence in preventing this rebound.
  • the vacuum is maintained in the "cylinder during a period of time amply sufficient to permit the cylinder to be recharged by atmospheric pressure if desired.
  • I claim: 1. A two stroke cycle internal combustion engine wherein the burnt gases are discharged from the cylinder into an exhaust conduit substantially as a mass whereby the said mass moves outward and thereafter returns towards the cylinder from a point which may be within the said exhaust conduit, and wherein an inlet is opened for the introduction of fresh charge while the exhaust port is still open and when the said issuance of the burnt gases-is in full progress and causes a suction effect to be exerted in the cylinder, the said exhaust conduit providing a tree passage for the burnt gases to the limit of outward travel of said mass and having a chamber in connection with said passage and wherein substantially the whole mass of burnt gases after leaving the cylinder is guided and .is caused to adopt a whirling motion as a compact mass whereby the outward motion of the said mass is prolonged and the rebound of said mass towards the cylinder is delayed and reducedin intensity.
  • a two-stroke cycle internal combustion engine wherein the burnt gases are discharged from the cylinder into an exhaust conduit substantially as a mass whereby the said mass moves outward and thereafter returns towards the cylinder from a pointwhich may be within the said exhaust conduit, and wherein an inlet is opened for the introduction of fresh charge while the exhaust port is still open and when the said is suance of the burnt gases is in full progress and causes a suction eflect to be exerted in the cylinder
  • the said exhaust conduit providing a tree passage for the burnt gases to the limit of outward travel of said mass and having a chamber in connection with said passage into which sub stantially the whole mass of burnt gases is guided after leaving the cylinder, the axis of the chainberbeing in line with that of the exhaust-conduit, said chamber having substantially the same volume as the engine cylinder and having a widened portion in which stationary guiding blades are positioned, which give a spiral motion to the burnt gases, whereby the outward motion of the said mass is prolonged and the rebound of said mass

Description

' July 25, 1939. 2,167,303 11 EXHAUST DEVICE FOR INTERNAL COMBUSTION ENGINES M. KADENACY Filed Aug. 51, 1955 i Patented July 25,1939
' axnaus'r navrcaroa INTERNAL corraus TIONENGINES Michel Kadenacy, Paris, France Application August 31, 1935, v Serial No. 38,826: 71 .I 'In Great Britain Augusta, 1934 v Theiinvention relates to two-stroke internal combustion engines, wherein the evacuation of the' cylinder by vthebodily displacement of-the burnt gases from jthe cylinder into the exhaust ,system is utilised for the :purpose of. introducing a fresh charge by controlling the inletroriflce to open for the introduction of the said charge when the exhaust gases are moving "outwardly through the exhaust port or duct as a consequence of this 1 9, bodily displacementifromthe cylinder.
In such an engine twodisturbing factors occur which may have an objectionable action upon thecharge introduced into thecylinder. 1
when the gaseslhave reached the end of their outwardtravel'as a consequence of their bodily displacement from. the; cylinder "their movement is reversed indirection and the return impact, if:
the exhaust-port is then still open, may cause the charge in the cylinder to be fouled andsome of l 20 this'ch'arge to be forced out of the inlet ports,
Inany case.when this reversal indirection 1 a the cylinder to be drawn into the exhaust system 30 through the open exhaust ports.
The object of the invention is to provide means whereby the objectionable actions of an untimely return of the burnt gases or of a prolonged suction in the exhaust system may be minimised.
I 35 The invention will now be described with reference to the accompanying drawing, in-which:
Figure 1 relates to one embodiment of the invention in which the issuing mass of burnt gases is'directed on to a small gaseous mass in the 40 exhaust system and-exerts its pressure on the main atmosphere in a continuous manner.
Figure '2 relates to an embodiment in which the explosion gases are constrained to follow an o chamber 3 arrangedas a by-pass on the main the engine cylinder.
exhaust pipe I, .2 and in open communication withbothlandi. v H
The body of explosion gases leaving the engine cylinder encounters a refiecting surface .4 on the wall of the duct opposite the entry-tothe chainber 3, which issituated so as, to direct the said body into the annular chamber 3,-,the volume of which will be substantiallythe same as that of The gases then follow by a series of reflectio ns a continuous path in the chamber 3 while. exerting. a component of their force upon the-main mass in the duct 2. v
The faceof the gaseous column {in the duct 2 in this case forms a reflecting surface on which the gases impinge, and, which yields as the atmospheric column in the duct 2 is put into move-, ment in-the direction'of exhaust. n
Inthe arrangement illustrated in Figure 2, an 1 assembly of fixed guide vanes-or blades I is mounted in the exhaust duct 6 inorder to impart .to the issuing explosion gases a whirling or screw motion. I a This assembly will befittedas closeas possiblev to the cylinder and between the engine and the silencer. The area of passage for the gases-will be made such that the volume of gases dealt with can pass freely. v The blades 5 act as deflecting surfaces and,
in combination with the enclosing walls of the so duct 6, impose rotary forward movement on the explosion gases whereby the absolute velocity of the latter is not appreciably reduced but the relative speed of forward motion is reduced but never wholly destroyed.
The body of'explosion gases is thus made toact like a screw action upon the atmospheric mass in the duct 6, so as to exert a continuous pressure on the latter, until this atmospheric resistance is broken down and the explosion gases 40 can escape.
The arrangement shown in Figure 3 differs from the foregoing in that the exhaust duct is no longer, properly speaking, freely open to the atmosphere.
In this case the exhaust duct opens into the annular chamber 8, forming a closed circuit, situated preferably as close as possible to the latter and having a volume a little larger than the w cylinder volume.
The explosion gases project from the cylinder and encounter deflecting surfaces formed by the walls of the duct I which direct them into the chamber 8 and in this chamber they undergo a series of deflections which compel them to follow a continuous closed path in this chamber.
The peripheral walls of the chamber I are provided with small orifices 9 leading to the atmosphere and suitably directed to facilitate the &cape of the explosion gases.
The explosion gases circulating without loss of absolute velocity in the chamber 8 are thus projected gradually into theexternal atmosphere through the orifices 9 and any return to the cylinder by rebounding from the external atmospheric mass is thus prevented.
It will be understood from the foregoing that all the devices described are adapted to cause the issuing mass of burnt gases to travel along an elongated path without thereby increasing the resistance to motion of the gases along this path and that the devices do not obstruct the outflow of the burnt gases in any way or comprise any surfaces which would tend to reflect the mass of burnt gases back towards the cylinder.
It will also be understood from the foregoing that in order to be effective, the devices according to the invention must be placed nearer the cylinder than the point from which the rebound of the gases to the cylinder would occur, as they will otherwise have no infiuence in preventing this rebound.
With all the devices hereinbefore described, the vacuum is maintained in the "cylinder during a period of time amply sufficient to permit the cylinder to be recharged by atmospheric pressure if desired.
The objectionable eil'ect of a return of the burnt gases towards the cylinder is attenuated or wholly destroyed. A loss of charge due to a prolonged suction in the exhaust system is also reduced or avoided completely according to the position in which the device is placed in the exhaust system, since it will be understood that the volume of the void left in the cylinder and in the exhaust system by the issuing mass of burnt gases will depend upon the distance the device 5 cylinder,
I claim: 1. A two stroke cycle internal combustion engine wherein the burnt gases are discharged from the cylinder into an exhaust conduit substantially as a mass whereby the said mass moves outward and thereafter returns towards the cylinder from a point which may be within the said exhaust conduit, and wherein an inlet is opened for the introduction of fresh charge while the exhaust port is still open and when the said issuance of the burnt gases-is in full progress and causes a suction effect to be exerted in the cylinder, the said exhaust conduit providing a tree passage for the burnt gases to the limit of outward travel of said mass and having a chamber in connection with said passage and wherein substantially the whole mass of burnt gases after leaving the cylinder is guided and .is caused to adopt a whirling motion as a compact mass whereby the outward motion of the said mass is prolonged and the rebound of said mass towards the cylinder is delayed and reducedin intensity.
2. A two-stroke cycle internal combustion engine wherein the burnt gases are discharged from the cylinder into an exhaust conduit substantially as a mass whereby the said mass moves outward and thereafter returns towards the cylinder from a pointwhich may be within the said exhaust conduit, and wherein an inlet is opened for the introduction of fresh charge while the exhaust port is still open and when the said is suance of the burnt gases is in full progress and causes a suction eflect to be exerted in the cylinder,'the said exhaust conduit providing a tree passage for the burnt gases to the limit of outward travel of said mass and having a chamber in connection with said passage into which sub stantially the whole mass of burnt gases is guided after leaving the cylinder, the axis of the chainberbeing in line with that of the exhaust-conduit, said chamber having substantially the same volume as the engine cylinder and having a widened portion in which stationary guiding blades are positioned, which give a spiral motion to the burnt gases, whereby the outward motion of the said mass is prolonged and the rebound of said mass towards the cylinder is delayed and reduced in intensity.
MICHEL KADENACY.
US38826A 1934-08-31 1935-08-31 Exhaust device for internal combustion engines Expired - Lifetime US2167303A (en)

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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2583430A (en) * 1945-05-17 1952-01-22 Nina K Guercken Power plant, including a combustion chamber and an impulse turbine driven by exhaustgases from the chamber
US2618925A (en) * 1947-01-31 1952-11-25 Packard Motor Car Co Flow control means for pulse jet combustion units
US2650472A (en) * 1944-07-17 1953-09-01 Whitworth & Co Resonating combustion power gas generator
US4924956A (en) * 1986-10-24 1990-05-15 Rdg Inventions Corporation Free-piston engine without compressor

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2650472A (en) * 1944-07-17 1953-09-01 Whitworth & Co Resonating combustion power gas generator
US2583430A (en) * 1945-05-17 1952-01-22 Nina K Guercken Power plant, including a combustion chamber and an impulse turbine driven by exhaustgases from the chamber
US2618925A (en) * 1947-01-31 1952-11-25 Packard Motor Car Co Flow control means for pulse jet combustion units
US4924956A (en) * 1986-10-24 1990-05-15 Rdg Inventions Corporation Free-piston engine without compressor

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