US3625188A - Glow ignition device for rotary piston engines - Google Patents

Glow ignition device for rotary piston engines Download PDF

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Publication number
US3625188A
US3625188A US878403A US3625188DA US3625188A US 3625188 A US3625188 A US 3625188A US 878403 A US878403 A US 878403A US 3625188D A US3625188D A US 3625188DA US 3625188 A US3625188 A US 3625188A
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Prior art keywords
rotary piston
rotary
chamber
valve
internal combustion
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US878403A
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Stanislaw Jarnuskiewicz
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Priority claimed from PL130161A external-priority patent/PL63680B1/pl
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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
    • F02B53/00Internal-combustion aspects of rotary-piston or oscillating-piston engines
    • F02B53/12Ignition
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23QIGNITION; EXTINGUISHING-DEVICES
    • F23Q7/00Incandescent ignition; Igniters using electrically-produced heat, e.g. lighters for cigarettes; Electrically-heated glowing plugs
    • F23Q7/001Glowing plugs for internal-combustion engines
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B1/00Engines characterised by fuel-air mixture compression
    • F02B1/02Engines characterised by fuel-air mixture compression with positive ignition
    • F02B1/04Engines characterised by fuel-air mixture compression with positive ignition with fuel-air mixture admission into cylinder
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B53/00Internal-combustion aspects of rotary-piston or oscillating-piston engines
    • F02B2053/005Wankel engines
    • 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

Definitions

  • Lavine ABSTRACT A rotary piston engine is provided with a chamber in which is a glow plug: a pair of passages, controlled by a rotary valve, communicate that chamber with the piston chamber or hollow, the passages entering the piston chamber or hollow substantially at the median plane of rotation of the rotary piston and at circumferentially spaced points.
  • a primary object of this invention is to provide an effective ignition system for trochoidal rotary piston engines, ensuring the correct ignition of the mixture at high engine speeds by means of a simple and inexpensive device.
  • This object has been achieved by providing a glow-type ignition device constructed so that the operating space of the engine is connected through one or more channels in the engine body with a rotary gate that uncovers or screens a glowing glow plug and enables igniting of the mixture by the glow plug.
  • the glow plug is heated electrically from a low-tension installation.
  • the rotary gate is drivenfrom the engine shaft through suitable gearing.
  • the ignition device according to the invention does not have the disadvantages of the spark plug-type ignition as the life of the glow plug does not depend on the frequency of igniting, since the intensity of igniting of the glow plug is constant and independent of the engine speed.
  • the ignition control is etfected mechanically, forcedly.
  • the gate is a simple fail-safe element. Providing of several channels connecting the glow plug with the combustion space permits the achieving of ignition at several points of the combustion chamber simultaneously. Further, the location of the channels inlets, being approximately in the median plane of rotation of the rotary piston, and circumferentially spaced, causes the flow of the combustible mixture in these channels at the moment they are connected by the rotary valve gear and there is thereby effected scavenging of the remaining combustion gases in the proximity of the glow plug.
  • HO. 2 is a cross section taken on the line A--A of FIG. 1.
  • the device shown in F105. 1 and 2 comprises two channels I and 2 in the engine body 3 and conducted to the rotary gate valve 4 driven from the engine shaft by suitable gearing.
  • a cutout 5 is provided connecting in a first position thereof channels 1 and 2 with the electrode 6 of the glow plug 7:
  • glow plug 7 is mounted in a chamber in the engine body 3. In a second position, the connection is closed.
  • the channels 1 and 2, as shown in FIG. 1, enter the engine hollow 8, defining the combustion chamber, substantially at v the median plane of rotation of the rotary piston as shown in FIG. 2; these points are circumferentially spaced, thereby enabling scavenging of changer .in which is located the electrode 6.
  • Operation of the ignition device enables the rotary gate valve 4 to connect through the cutout 5 the channels 1 and 2 with the glowing electrode of the glow plug 7 at the predetermined moment for ignition.
  • a part of the compressed combustible mixture rushes into the chamber and is ignited by the electrode of the glow plug.
  • the combustible mixture also scavenges the chamber as a result of the pressure difference at both sides of the contraction of the trochoid.
  • An increase is pressure follows the ignition and part of the burning mixture is blown through the channels 1 and 2 into the operating chamber of the engine and causes ignition of the mixture compressed therein.
  • a rotary piston internal combustion engine of the trochoidal type comprising a hollow body and a rotary piston therein,
  • valve means in said passage means for alternately opening and closing said passage means.
  • passage means comprising a pair of passages each connected to said chamber and entering said hollow at spaced points.
  • valve means comprising a rotary valve, and means for drivingly connecting said rotary valve to a rotating element of said engine.
  • valve means comprising a rotary valve, and means for drivingly connecting said rotary valve to a rotating element of said engine.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Ignition Installations For Internal Combustion Engines (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)

Abstract

A rotary piston engine is provided with a chamber in which is a glow plug: a pair of passages, controlled by a rotary valve, communicate that chamber with the piston chamber or hollow, the passages entering the piston chamber or hollow substantially at the median plane of rotation of the rotary piston and at circumferentially spaced points.

Description

United States Patent Inventor Stanislaw Jarnuskiewicz Krakow, Swierczewskiego 29, Poland Appl. No. 878,403 Filed Nov. 20, 1969 Patented Dec. 7, 1971 Priority Nov. 21, 1968 Poland P 130.161
GLOW IGNITION DEVICE FOR ROTARY PISTON ENGINES 6 Claims, 2 Drawing Figs.
U.S.'Cl 123/8.l9, 123/809, 123/8.ll,60/39.82, 123/146 Int. Cl F02b 53/08 Field of Search 123/819,
[56] References Cited UNITED STATES PATENTS 1,310,459 7/1919 Walkos 60/3976 X 1,933,442 10/1933 Maxwell 60/3978 X 2,907,307 10/1959 Striegel 123/809 3,196,852 7/1965 Bentele 123/809 FOREIGN PATENTS 947,284 1/1964 Great Britain 123/809 Primary Examiner-Clarence R. Gordon Atlorney-lrvin A. Lavine ABSTRACT: A rotary piston engine is provided with a chamber in which is a glow plug: a pair of passages, controlled by a rotary valve, communicate that chamber with the piston chamber or hollow, the passages entering the piston chamber or hollow substantially at the median plane of rotation of the rotary piston and at circumferentially spaced points.
PATENTED DEC 7191:
WNW
l HIIHIIWIIIHH GLOW IGNITION DEVICE FOR ROTARY PISTON ENGINES Hitherto there were used in rotary piston engines conventional spark ignition systems with high-tension coils and makebrake devices.
The drawback of such devices when applied to rotary piston engines is rapid wear of the spark plugs and the difficulty of obtaining a correct spark at high speeds, as usually in engines of such type a single spark plug operates all chambers and sparking must occur at a frequency equal to the number of chambers, i.e. several times higher than that occuring in conventional engines.
Therefore, a primary object of this invention is to provide an effective ignition system for trochoidal rotary piston engines, ensuring the correct ignition of the mixture at high engine speeds by means of a simple and inexpensive device.
This object has been achieved by providing a glow-type ignition device constructed so that the operating space of the engine is connected through one or more channels in the engine body with a rotary gate that uncovers or screens a glowing glow plug and enables igniting of the mixture by the glow plug. The glow plug is heated electrically from a low-tension installation. The rotary gate is drivenfrom the engine shaft through suitable gearing.
The ignition device according to the invention does not have the disadvantages of the spark plug-type ignition as the life of the glow plug does not depend on the frequency of igniting, since the intensity of igniting of the glow plug is constant and independent of the engine speed.
The ignition control is etfected mechanically, forcedly.
The gate is a simple fail-safe element. Providing of several channels connecting the glow plug with the combustion space permits the achieving of ignition at several points of the combustion chamber simultaneously. Further, the location of the channels inlets, being approximately in the median plane of rotation of the rotary piston, and circumferentially spaced, causes the flow of the combustible mixture in these channels at the moment they are connected by the rotary valve gear and there is thereby effected scavenging of the remaining combustion gases in the proximity of the glow plug.
IN THE DRAWINGS HO. 1 is a cross-sectional view taken along the axis of a rotary piston engine provided with the glow ignition apparatus of the present invention.
HO. 2 is a cross section taken on the line A--A of FIG. 1.
The device shown in F105. 1 and 2 comprises two channels I and 2 in the engine body 3 and conducted to the rotary gate valve 4 driven from the engine shaft by suitable gearing. In the said gate valve controlling the channels 1 and 2 to the electrode 6 of the glow plug 7 a cutout 5 is provided connecting in a first position thereof channels 1 and 2 with the electrode 6 of the glow plug 7: glow plug 7 is mounted in a chamber in the engine body 3. In a second position, the connection is closed. The channels 1 and 2, as shown in FIG. 1, enter the engine hollow 8, defining the combustion chamber, substantially at v the median plane of rotation of the rotary piston as shown in FIG. 2; these points are circumferentially spaced, thereby enabling scavenging of changer .in which is located the electrode 6.
Operation of the ignition device according to this invention enables the rotary gate valve 4 to connect through the cutout 5 the channels 1 and 2 with the glowing electrode of the glow plug 7 at the predetermined moment for ignition. At the said ignition moment a part of the compressed combustible mixture rushes into the chamber and is ignited by the electrode of the glow plug. The combustible mixture also scavenges the chamber as a result of the pressure difference at both sides of the contraction of the trochoid. An increase is pressure follows the ignition and part of the burning mixture is blown through the channels 1 and 2 into the operating chamber of the engine and causes ignition of the mixture compressed therein.
What IS claimed is:
l. A rotary piston internal combustion engine of the trochoidal type comprising a hollow body and a rotary piston therein,
a chamber in said body,
a glow plug in said body having the electrodes thereof in said chamber,
passage means connecting said chamber and the hollow of said body wherein said rotary piston is located,
and valve means in said passage means for alternately opening and closing said passage means.
2. The rotary piston internal combustion engine of claim I, said passage means comprising a pair of passages each connected to said chamber and entering said hollow at spaced points.
3. The rotary piston internal combustion engine of claim 2, wherein said points are located substantially at the median plane of rotation of said rotary piston.
4. The rotary piston internal combustion engine of claim 2, wherein said points are circumferentially spaced.
5. The rotary piston internal combustion engine of claim 2, said valve means comprising a rotary valve, and means for drivingly connecting said rotary valve to a rotating element of said engine.
6. The rotary piston internal combustion engine of claim I, said valve means comprising a rotary valve, and means for drivingly connecting said rotary valve to a rotating element of said engine.
a a: r t a

Claims (6)

1. A rotary piston internal combustion engine of the trochoidal type comprising a hollow body and a rotary piston therein, a chamber in said body, a glow plug in said body having the electrodes thereof in said chamber, passage means connecting said chamber and the hollow of said body wherein said rotary piston is located, and valve means in said passage means for alternately opening and closing said passage means.
2. The rotary piston internal combustion engine of claim 1, said passage means comprising a pair of passages each connected to said chamber and entering said hollow at spaced points.
3. The rotary piston internal combustion engine of claim 2, wherein said points are located substantially at the median plane of rotation of said rotary piston.
4. The rotary piston internal combustion engine of claim 2, wherein said points are circumferentially spaced.
5. The rotary piston internal combustion engine of claim 2, said valve means comprising a rotary valve, and means for drivingly connecting said rotary valve to a rotating element of said engine.
6. The rotary piston internal combustion engine of claim 1, said valve means comprising a rotary valve, and means for drivingly connecting said rotary valve to a rotating element of said engine.
US878403A 1968-11-21 1969-11-20 Glow ignition device for rotary piston engines Expired - Lifetime US3625188A (en)

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PL130161A PL63680B1 (en) 1968-11-21

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AT (1) AT302735B (en)
DE (1) DE1958577A1 (en)
FR (1) FR2023799A1 (en)
GB (1) GB1285612A (en)
SE (1) SE351263B (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4077366A (en) * 1975-11-28 1978-03-07 Ford Motor Company Internal combustion engine control system
US4202312A (en) * 1977-03-17 1980-05-13 Toyota Jidosha Kogyo Kabushiki Kaisha Ignition device for rotary piston engine
JP2010043635A (en) * 2008-08-13 2010-02-25 Yoshio Abe Moistureproof cover for plug
EP2211799A1 (en) * 2007-08-01 2010-08-04 The Board of Regents of The University of Texas System Portable fluid warming system
US20140374660A1 (en) * 2013-06-25 2014-12-25 Massachusetts Institute Of Technology Engine Chemical Reactor With Catalyst

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1310459A (en) * 1919-07-22 Botary gas-engine
US1933442A (en) * 1931-11-10 1933-10-31 Henry B Kistler Rotary motor
US2907307A (en) * 1958-08-27 1959-10-06 Striegl George Combined motor and/or motor apparatus
GB947284A (en) * 1961-11-16 1964-01-22 Daimler Benz Ag Improvements relating to rotary-piston diesel engines
US3196852A (en) * 1962-11-02 1965-07-27 Curtiss Wright Corp Rotating combustion engine with direct fuel injection

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1310459A (en) * 1919-07-22 Botary gas-engine
US1933442A (en) * 1931-11-10 1933-10-31 Henry B Kistler Rotary motor
US2907307A (en) * 1958-08-27 1959-10-06 Striegl George Combined motor and/or motor apparatus
GB947284A (en) * 1961-11-16 1964-01-22 Daimler Benz Ag Improvements relating to rotary-piston diesel engines
US3196852A (en) * 1962-11-02 1965-07-27 Curtiss Wright Corp Rotating combustion engine with direct fuel injection

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4077366A (en) * 1975-11-28 1978-03-07 Ford Motor Company Internal combustion engine control system
US4202312A (en) * 1977-03-17 1980-05-13 Toyota Jidosha Kogyo Kabushiki Kaisha Ignition device for rotary piston engine
EP2211799A1 (en) * 2007-08-01 2010-08-04 The Board of Regents of The University of Texas System Portable fluid warming system
EP2211799B1 (en) * 2007-08-01 2013-12-18 The Board of Regents of The University of Texas System Portable fluid warming system
JP2010043635A (en) * 2008-08-13 2010-02-25 Yoshio Abe Moistureproof cover for plug
US20140374660A1 (en) * 2013-06-25 2014-12-25 Massachusetts Institute Of Technology Engine Chemical Reactor With Catalyst

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FR2023799A1 (en) 1970-08-21
GB1285612A (en) 1972-08-16
DE1958577A1 (en) 1970-07-30
SE351263B (en) 1972-11-20
AT302735B (en) 1972-10-25

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