GB661410A - Improvements in and relating to current pulse generating circuit arrangements - Google Patents
Improvements in and relating to current pulse generating circuit arrangementsInfo
- Publication number
- GB661410A GB661410A GB267549A GB267549A GB661410A GB 661410 A GB661410 A GB 661410A GB 267549 A GB267549 A GB 267549A GB 267549 A GB267549 A GB 267549A GB 661410 A GB661410 A GB 661410A
- Authority
- GB
- United Kingdom
- Prior art keywords
- capacitor
- rectifier
- load
- voltage
- current
- 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
-
- H—ELECTRICITY
- H03—ELECTRONIC CIRCUITRY
- H03K—PULSE TECHNIQUE
- H03K3/00—Circuits for generating electric pulses; Monostable, bistable or multistable circuits
- H03K3/02—Generators characterised by the type of circuit or by the means used for producing pulses
- H03K3/53—Generators characterised by the type of circuit or by the means used for producing pulses by the use of an energy-accumulating element discharged through the load by a switching device controlled by an external signal and not incorporating positive feedback
- H03K3/55—Generators characterised by the type of circuit or by the means used for producing pulses by the use of an energy-accumulating element discharged through the load by a switching device controlled by an external signal and not incorporating positive feedback the switching device being a gas-filled tube having a control electrode
Landscapes
- Generation Of Surge Voltage And Current (AREA)
Abstract
661,410. Condenser arrangements. MINISTER OF SUPPLY. Jan. 16, 1950 [Jan. 31, 1949]. No. 2675/49. Class 38 (iv). [Also in Group XL (c)] A high voltage pulse generator comprises a capacitor which is charged from a power source and discharged into an inductive load by means of an ionizable switching path, a first rectifier being connected in parallel with the switch and a second rectifier connected in series with the load and an auxiliary inductor connected in parallel with the series circuit of the second rectifier and load, the time constant of the circuit formed by the auxiliary inductor, the capacitor and the second rectifier being long compared with the de-ionization time of the switch. The Figure shows a capacitor C2 which is charged from the D.C. source of voltage V via the resistor R and is periodically discharged into the inductive load L1 and the auxiliary inductor L2 when the ignitron V1 is fired. The pulse of current which flows during the discharge is approximately a half sinusoid and has a duration t determined by the resonant frequency of capacitor C2 and the inductance of the load L1. At the end of time t the voltage across capacitor C2 has reversed but reversal of current through the load L1 is prevented by rectifier D1. Rectifier D2 presents a low resistance path for reverse current flow and thus effectively shorts ignitron V1 when the direction of current flow through capacitor C2 reverses. At the end of interval t therefore current flows through the circuit D2, C2, L2 for a time T which is determined by the resonant frequency of C2 and L2 and which may be made approximately equal to the interval between successive current pulses. The impulse voltage across the ignitron VI can be made such that a voltage which would otherwise result in back-firing is not reached within its de-ionization time.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB267549A GB661410A (en) | 1949-01-31 | 1949-01-31 | Improvements in and relating to current pulse generating circuit arrangements |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB267549A GB661410A (en) | 1949-01-31 | 1949-01-31 | Improvements in and relating to current pulse generating circuit arrangements |
Publications (1)
Publication Number | Publication Date |
---|---|
GB661410A true GB661410A (en) | 1951-11-21 |
Family
ID=9743784
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB267549A Expired GB661410A (en) | 1949-01-31 | 1949-01-31 | Improvements in and relating to current pulse generating circuit arrangements |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB661410A (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2166928A (en) * | 1984-11-09 | 1986-05-14 | David Michael Hine | Extra low frequency long range wireless signalling/paging pulse sending apparatus |
US5561350A (en) | 1988-11-15 | 1996-10-01 | Unison Industries | Ignition System for a turbine engine |
US5754011A (en) | 1995-07-14 | 1998-05-19 | Unison Industries Limited Partnership | Method and apparatus for controllably generating sparks in an ignition system or the like |
US6670777B1 (en) | 2002-06-28 | 2003-12-30 | Woodward Governor Company | Ignition system and method |
US7355300B2 (en) | 2004-06-15 | 2008-04-08 | Woodward Governor Company | Solid state turbine engine ignition exciter having elevated temperature operational capability |
-
1949
- 1949-01-31 GB GB267549A patent/GB661410A/en not_active Expired
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2166928A (en) * | 1984-11-09 | 1986-05-14 | David Michael Hine | Extra low frequency long range wireless signalling/paging pulse sending apparatus |
US5561350A (en) | 1988-11-15 | 1996-10-01 | Unison Industries | Ignition System for a turbine engine |
US5754011A (en) | 1995-07-14 | 1998-05-19 | Unison Industries Limited Partnership | Method and apparatus for controllably generating sparks in an ignition system or the like |
US6034483A (en) | 1995-07-14 | 2000-03-07 | Unison Industries, Inc. | Method for generating and controlling spark plume characteristics |
US6353293B1 (en) | 1995-07-14 | 2002-03-05 | Unison Industries | Method and apparatus for controllably generating sparks in an ignition system or the like |
US6670777B1 (en) | 2002-06-28 | 2003-12-30 | Woodward Governor Company | Ignition system and method |
US7355300B2 (en) | 2004-06-15 | 2008-04-08 | Woodward Governor Company | Solid state turbine engine ignition exciter having elevated temperature operational capability |
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