GB754508A - Spark gap system - Google Patents

Spark gap system

Info

Publication number
GB754508A
GB754508A GB25174/54A GB2517454A GB754508A GB 754508 A GB754508 A GB 754508A GB 25174/54 A GB25174/54 A GB 25174/54A GB 2517454 A GB2517454 A GB 2517454A GB 754508 A GB754508 A GB 754508A
Authority
GB
United Kingdom
Prior art keywords
gap
condenser
electrodes
electrode
insulator
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
GB25174/54A
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.)
Bendix Aviation Corp
Original Assignee
Bendix Aviation Corp
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 Bendix Aviation Corp filed Critical Bendix Aviation Corp
Publication of GB754508A publication Critical patent/GB754508A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02PIGNITION, OTHER THAN COMPRESSION IGNITION, FOR INTERNAL-COMBUSTION ENGINES; TESTING OF IGNITION TIMING IN COMPRESSION-IGNITION ENGINES
    • F02P15/00Electric spark ignition having characteristics not provided for in, or of interest apart from, groups F02P1/00 - F02P13/00 and combined with layout of ignition circuits
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01JELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
    • H01J17/00Gas-filled discharge tubes with solid cathode
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01JELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
    • H01J2893/00Discharge tubes and lamps
    • H01J2893/0059Arc discharge tubes

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Spark Plugs (AREA)

Abstract

754,508. Ignition systems. BENDIX AVIATION CORPORATION. Aug. 30, 1954 [Sept. 30, 1953], No. 25174/54. Class 7(4) [Also in Group XL(a)] An ignition system comprises a sealed two-electrode spark gap 30 and a threeelectrode spark gap assembly 35, 37, 40 (see Group XL(a)) mounted in an insulator casing 10 and provided with three terminal strips 18, 24 and 46. Electrodes 37 and 40 are bridged by an insulator 39 provided with a semi-conductive surface coating, or may be bridged by a resistor of the order of 0.1 to 10 megohms, and electrode 40 is connected to electrode 25 of the control gap 30. Condenser 47 is charged through a rectifier 48 to a voltage sufficient to break down the control gap 30 whereupon condenser 47 partially discharges into condenser 49. The current flowing through the semiconductive surface coating on insulator 39 ionizes the gap between electrodes 37 and 40 which breaks down and ionizes the gap between electrodes 35 and 37 so that the remainder of the charge in condenser 47 is: passed to a surface discharge spark plug 50.
GB25174/54A 1953-09-30 1954-08-30 Spark gap system Expired GB754508A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US754508XA 1953-09-30 1953-09-30

Publications (1)

Publication Number Publication Date
GB754508A true GB754508A (en) 1956-08-08

Family

ID=22125843

Family Applications (1)

Application Number Title Priority Date Filing Date
GB25174/54A Expired GB754508A (en) 1953-09-30 1954-08-30 Spark gap system

Country Status (1)

Country Link
GB (1) GB754508A (en)

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