GB827944A - Improvements in or relating to igniters - Google Patents

Improvements in or relating to igniters

Info

Publication number
GB827944A
GB827944A GB279458A GB279458A GB827944A GB 827944 A GB827944 A GB 827944A GB 279458 A GB279458 A GB 279458A GB 279458 A GB279458 A GB 279458A GB 827944 A GB827944 A GB 827944A
Authority
GB
United Kingdom
Prior art keywords
outer shell
inner portion
semi
sparking
combustion 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
Application number
GB279458A
Inventor
Lawrence Raymond Lentz
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.)
Federal Mogul Ignition LLC
Original Assignee
Champion Spark Plug Co
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 Champion Spark Plug Co filed Critical Champion Spark Plug Co
Priority to GB279458A priority Critical patent/GB827944A/en
Publication of GB827944A publication Critical patent/GB827944A/en
Expired legal-status Critical Current

Links

Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01TSPARK GAPS; OVERVOLTAGE ARRESTERS USING SPARK GAPS; SPARKING PLUGS; CORONA DEVICES; GENERATING IONS TO BE INTRODUCED INTO NON-ENCLOSED GASES
    • H01T13/00Sparking plugs
    • H01T13/02Details
    • H01T13/16Means for dissipating heat

Landscapes

  • Ignition Installations For Internal Combustion Engines (AREA)

Abstract

827,944. Sparking plugs. CHAMPION SPARK PLUG CO. Jan. 28, 1958, No. 2794/58. Class 7(4) A sparking plug for gas turbine engines or jet engines comprises an inner sparking portion having spaced centre and shell electrodes 11, 13 disposed at an end extending into an engine combustion chamber and a heat shielding outer shell 2 surrounding and radially spaced from the inner portion over the length of the end extending into the combustion chamber, the outer shell having a portion 18 in contact with the inner portion when cool and which is moved away from the inner portion by thermal expansion when at normal operating temperatures and the outer shell having an opening 20 for admission of cooling air into the radial space 10 between the inner portion and the outer shell. As shown the central electrode 11 is electrically and physically connected to a body of semi-conductive material 12 but the semi-conductive body will be eliminated in certain types of igniters. Gas leakage around the semi-conductive body may be prevented by tamping masses of granular material 13, 14 in place in known manner. When the engine is at operating temperature cooling air exits largely through the space between the flanges 16 and 18
GB279458A 1958-01-28 1958-01-28 Improvements in or relating to igniters Expired GB827944A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB279458A GB827944A (en) 1958-01-28 1958-01-28 Improvements in or relating to igniters

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB279458A GB827944A (en) 1958-01-28 1958-01-28 Improvements in or relating to igniters

Publications (1)

Publication Number Publication Date
GB827944A true GB827944A (en) 1960-02-10

Family

ID=9746040

Family Applications (1)

Application Number Title Priority Date Filing Date
GB279458A Expired GB827944A (en) 1958-01-28 1958-01-28 Improvements in or relating to igniters

Country Status (1)

Country Link
GB (1) GB827944A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS4893822A (en) * 1972-02-17 1973-12-04
JPS50154610A (en) * 1973-09-17 1975-12-12
FR2990073A1 (en) * 2012-04-26 2013-11-01 Snecma IGNITION CANDLE FOR COMBUSTION CHAMBER OF A GAS TURBINE ENGINE
US20160003150A1 (en) * 2014-07-03 2016-01-07 General Electric Company Igniter tip with cooling passage
CN110107406A (en) * 2019-04-04 2019-08-09 中国人民解放军空军工程大学 A kind of anode self cooled plasma igniter

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS4893822A (en) * 1972-02-17 1973-12-04
JPS5641815B2 (en) * 1972-02-17 1981-09-30
JPS50154610A (en) * 1973-09-17 1975-12-12
JPS5934852B2 (en) * 1973-09-17 1984-08-24 ゼネラル エレクトリツク カンパニイ fuel igniter
FR2990073A1 (en) * 2012-04-26 2013-11-01 Snecma IGNITION CANDLE FOR COMBUSTION CHAMBER OF A GAS TURBINE ENGINE
US9413141B2 (en) 2012-04-26 2016-08-09 Snecma Spark plug for combustion chamber of a gas turbine engine
US20160003150A1 (en) * 2014-07-03 2016-01-07 General Electric Company Igniter tip with cooling passage
CN110107406A (en) * 2019-04-04 2019-08-09 中国人民解放军空军工程大学 A kind of anode self cooled plasma igniter

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