GB717755A - Improvements in and relating to ignition systems - Google Patents
Improvements in and relating to ignition systemsInfo
- Publication number
- GB717755A GB717755A GB15875/51A GB1587551A GB717755A GB 717755 A GB717755 A GB 717755A GB 15875/51 A GB15875/51 A GB 15875/51A GB 1587551 A GB1587551 A GB 1587551A GB 717755 A GB717755 A GB 717755A
- Authority
- GB
- United Kingdom
- Prior art keywords
- windings
- electrodes
- circuit
- condenser
- spark
- 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
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02P—IGNITION, OTHER THAN COMPRESSION IGNITION, FOR INTERNAL-COMBUSTION ENGINES; TESTING OF IGNITION TIMING IN COMPRESSION-IGNITION ENGINES
- F02P15/00—Electric 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
- F02P15/001—Ignition installations adapted to specific engine types
- F02P15/003—Layout of ignition circuits for gas turbine plants
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/26—Starting; Ignition
- F02C7/264—Ignition
- F02C7/266—Electric
Landscapes
- 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)
Abstract
717,755. Ignition systems; sparking plugs. BRITISH THOMSON-HOUSTON CO., Ltd. July 4, 1951 [July 6, 1950], No. 15875/51. Class 7(4) In an ignition system comprising two separate spark-electrode units 3, 4 each having a single electrode 5, 9, respectively, and means for energizing the electrodes simultaneously with potentials of opposite polarity to cause a spark to jump therebetween, the energizing means includes two separate but inter-connected H.T. windings 13, 16 which are connected in series between the electrodes, two separate but interconnected L.T. windings 12, 15 and a source of sparking voltage, such as a battery 19, connected to the L.T. windings. The L.T. windings 12 and 15, are connected in series through a common point 18, the circuit including a condenser 21 and a switch 20; the H.T. windings 13, 16 are also connected in series through the point 18, the outer end of each winding being connected to one of the electrodes 5, 9 in the combustion chamber 1 of a jet engine, the two electrodes forming between them a spark gap of about half-an-inch in length. Each electrode is located in a ceramic insulator 6 within a metal housing 7 which has a flange 8 whereby it is secured to the chamber 1. Connected across the condenser 21 is a vibrator 22 so that when switch 20 is closed and the circuit of the L.T. windings is interrupted by the vibrator 22 the condenser 21 is charged by the voltage induced in the L.T. windings, the cables and electrodes of the H.T. circuit also being charged by the voltage induced in the H.T. windings 13, 16. When the voltage between the electrodes 5, 9 reaches the breakdown value a high-frequency spark will jump the gap and dissipate the energy stored in the capacitance of the H.T. circuit after which the condenser 21 discharges through the gap at a lower frequency to be followed by the discharge of the inductive energy of circuit. Due to the arrangement of coils and electrodes the sparking voltage is about double the usual value as is the capacitive and inductive energy in the circuit. The system is used for starting purposes.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US717755XA | 1950-07-06 | 1950-07-06 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB717755A true GB717755A (en) | 1954-11-03 |
Family
ID=22103506
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB15875/51A Expired GB717755A (en) | 1950-07-06 | 1951-07-04 | Improvements in and relating to ignition systems |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB717755A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1064293B (en) * | 1957-03-09 | 1959-08-27 | Smitsvonk Nv | Sliding spark plug for internal combustion engines |
EP1936149A1 (en) * | 2006-12-22 | 2008-06-25 | Siemens Aktiengesellschaft | Gas turbine burner |
EP2813683A1 (en) * | 2013-06-13 | 2014-12-17 | Delavan Inc. | Continuous ignition systems |
US9080772B2 (en) | 2013-06-13 | 2015-07-14 | Delavan Inc | Continuous ignition |
-
1951
- 1951-07-04 GB GB15875/51A patent/GB717755A/en not_active Expired
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1064293B (en) * | 1957-03-09 | 1959-08-27 | Smitsvonk Nv | Sliding spark plug for internal combustion engines |
EP1936149A1 (en) * | 2006-12-22 | 2008-06-25 | Siemens Aktiengesellschaft | Gas turbine burner |
EP2813683A1 (en) * | 2013-06-13 | 2014-12-17 | Delavan Inc. | Continuous ignition systems |
US9080772B2 (en) | 2013-06-13 | 2015-07-14 | Delavan Inc | Continuous ignition |
US9567912B2 (en) | 2013-06-13 | 2017-02-14 | Delavan Inc | Continuous ignition systems |
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