SU133353A1 - Aircraft flashing pulse ma - Google Patents
Aircraft flashing pulse maInfo
- Publication number
- SU133353A1 SU133353A1 SU648256A SU648256A SU133353A1 SU 133353 A1 SU133353 A1 SU 133353A1 SU 648256 A SU648256 A SU 648256A SU 648256 A SU648256 A SU 648256A SU 133353 A1 SU133353 A1 SU 133353A1
- Authority
- SU
- USSR - Soviet Union
- Prior art keywords
- aircraft
- pulse
- flash
- flashing pulse
- flashing
- Prior art date
Links
Landscapes
- Audible And Visible Signals (AREA)
Description
Известные самолетные проблесковые импульсные ма ки с зоной действи в 180°, вклЕочающие в себ импульсные ламны, батареи конденсаторов и устройство поджига.Known aircraft flash pulse beacons with an operating area of 180 °, including pulsed luminaires, capacitor banks and an ignition device.
Описываемый проблесковый импульсный ма к, име меньший вес и гибариты, обеспечивает зону действи в 360°.The flashing pulsed light, described as having a smaller weight and gibarites, provides a 360 ° range.
Это достигаетс тем, что схема поджига автоматически бесконтакторным способом осуществл ет зажигание двух импульсных ламп с заданной частотой в противофазе, а блок питающих конденсаторов находитс в импульсном режиме с частотой разр дки, равной удвоенной частоте вспрлшки импульсной лампы при сохранении энергии вспышки каждой из ламп.This is achieved by the fact that the ignition circuit automatically, in a non-contact manner, ignites two flash lamps with a given frequency in antiphase, and the power supply capacitor unit is in a pulse mode with a discharge frequency equal to twice the flash frequency of each of the lamps.
На черт, изображена принципиальна электрическа схема самолетного проблескового импульсного ма ка.On the features depicted is the electrical circuit diagram of an aircraft flashing flash beacon.
Импульсные лампы 1 с трансформатором 2 поджига взаимосв заны с блоком 3 питающих конденсаторов и блоком 4 поджига.Pulse lamps 1 with an ignition transformer 2 are interconnected with a block of 3 supply capacitors and a block 4 of ignition.
Блок 5 питающих конденсаторов состоит из двух последовательных групп питающих конденсаторов 5 по восемь штук в каждой. Зар дка конденсаторов 5 осуществл етс через селеновые выпр мители 6 по схеме удвоени через конденсатор 7 зар дки от бортсети переменного тока . Блок 3 конденсаторов 5 рассчитан на обеспечение посто нным током двух импульсных ламп У и работает в импульсном режиме с частотой разр дки, равной удвоенной частоте вспышки каждой импульсной лампыБлок 4 поджига, предназначенный дл бесконтакторного поджига импульсных ламп / через трансформатор 2 поджига, состоит из симметричного мультивибратора 8, собранного на лампе 6Н 1п. Положительный импульс, снимаемый с сетки левой половины лампы 6Н 1п, зажигает тиратрон Я при этом конденсатор/О разр жаетс через открытый тиратрон 9 на первичную обмотку трансформатора 2 поджига. Со вторич,ной обмотки трансформатора 2 снимаетс напр жение высокой частоты,Unit 5 supply capacitors consists of two consecutive groups of supply capacitors 5 of eight each. The capacitors 5 are charged through selenium rectifiers 6 according to a doubling scheme through a charging capacitor 7 from an AC power supply network. The block 3 of the capacitors 5 is designed to provide two pulsed lamps U with direct current and operates in a pulsed mode with a discharge frequency equal to twice the flash frequency of each flash lamp. 8, assembled on the lamp 6N 1P. A positive pulse taken from the grid of the left half of the 6H 1p lamp ignites the thyratron. At the same time, the capacitor / O is discharged through the open thyratron 9 to the primary winding of the ignition transformer 2. From the secondary winding of the transformer 2, the high-frequency voltage is removed,
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| SU648256A SU133353A1 (en) | 1959-12-23 | 1959-12-23 | Aircraft flashing pulse ma |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| SU648256A SU133353A1 (en) | 1959-12-23 | 1959-12-23 | Aircraft flashing pulse ma |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| SU133353A1 true SU133353A1 (en) | 1960-11-30 |
Family
ID=48404357
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| SU648256A SU133353A1 (en) | 1959-12-23 | 1959-12-23 | Aircraft flashing pulse ma |
Country Status (1)
| Country | Link |
|---|---|
| SU (1) | SU133353A1 (en) |
-
1959
- 1959-12-23 SU SU648256A patent/SU133353A1/en active
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