SU753005A1 - FUEL FLUID SYSTEM - Google Patents
FUEL FLUID SYSTEMInfo
- Publication number
- SU753005A1 SU753005A1 SU2703473/23A SU2703473A SU753005A1 SU 753005 A1 SU753005 A1 SU 753005A1 SU 2703473/23 A SU2703473/23 A SU 2703473/23A SU 2703473 A SU2703473 A SU 2703473A SU 753005 A1 SU753005 A1 SU 753005A1
- Authority
- SU
- USSR - Soviet Union
- Prior art keywords
- line
- filling
- diameter
- supply tank
- purge
- Prior art date
Links
Landscapes
- Loading And Unloading Of Fuel Tanks Or Ships (AREA)
Abstract
1. Система заправки самолета топливом, содержащая последовательно соединенные штангу с приемником топлива, редуктор и магистраль заправки и отсечными кранами, с подключенными через блок управления и сигнализаторы давления к сигнализаторам уровня заправки и распределителем, выходы которого соединены с оборудованным насосом подкачки расходным баком, а также сливную и продувочную линии магистрали заправки, отличающаяся тем, что, с целью повышения безопасности и надежности заправки, продувочная линия подключена к верхней зоне надтопливного пространства расходного бака, а магистраль заправки соединена со сливной линией посредством конфузорного устройства, перед которым установлено сопло, подключенное к выходу подкачивающего насоса через обратный клапан и отсечной кран.2. Система по п.1, отличающаяся тем, что диаметр сливной линии равен 0,25-0,3 диаметра магистрали заправки.1. Aircraft refueling system, containing successively connected boom with fuel receiver, reducer and refueling line and shut-off cranes, connected to the fuel level level alarms and distributor through the control unit and pressure alarms, the outputs of which are connected to a supply tank equipped with a booster pump drain and purge lines of the filling line, characterized in that, in order to increase the safety and reliability of the filling, the purge line is connected to the upper zone of the overfuel second supply tank space, and filling line connected to the return line by a confuser device, to which a nozzle connected to the output of the feed pump via a check valve and shutoff kran.2. A system according to claim 1, characterized in that the diameter of the discharge line is 0.25-0.3 the diameter of the filling line.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU2703473/23A SU753005A1 (en) | 1978-12-28 | 1978-12-28 | FUEL FLUID SYSTEM |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU2703473/23A SU753005A1 (en) | 1978-12-28 | 1978-12-28 | FUEL FLUID SYSTEM |
Publications (1)
Publication Number | Publication Date |
---|---|
SU753005A1 true SU753005A1 (en) | 2005-05-10 |
Family
ID=60524552
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SU2703473/23A SU753005A1 (en) | 1978-12-28 | 1978-12-28 | FUEL FLUID SYSTEM |
Country Status (1)
Country | Link |
---|---|
SU (1) | SU753005A1 (en) |
-
1978
- 1978-12-28 SU SU2703473/23A patent/SU753005A1/en active
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