SU1316182A1 - EMERGENCY DRAIN SYSTEM OF FUEL FROM AIRPLANE TANK - Google Patents
EMERGENCY DRAIN SYSTEM OF FUEL FROM AIRPLANE TANKInfo
- Publication number
- SU1316182A1 SU1316182A1 SU3921286/23A SU3921286A SU1316182A1 SU 1316182 A1 SU1316182 A1 SU 1316182A1 SU 3921286/23 A SU3921286/23 A SU 3921286/23A SU 3921286 A SU3921286 A SU 3921286A SU 1316182 A1 SU1316182 A1 SU 1316182A1
- Authority
- SU
- USSR - Soviet Union
- Prior art keywords
- fuel
- emergency
- tank
- guaranteed
- emergency drain
- Prior art date
Links
Landscapes
- Loading And Unloading Of Fuel Tanks Or Ships (AREA)
Abstract
Система аварийного слива топлива из балки самолета, содержащая насосы подкачки, размещенные в расходном отсеке бака, стакан отрицательных перегрузок, в котором установлен один из насосов подкачки, трубопровод подачи топлива к двигателю с обратными клапанами, трубопровод аварийного слива с перекрывным краном, насос перекачки топлива в расходный отсек и датчик-сигнализатор уровня гарантированного остатка топлива, электрически связанный с перекрывным краном, отличающаяся тем, что, с целью упрощения эксплуатации системы и повышения безопасности полета путем автоматического прекращения аварийного слива по достижении гарантированного остатка топлива, трубопровод аварийного слива подсоединен к насосу подкачки, установленному в стакане отрицательных перегрузок, верхний срез которого выполнен на уровне гарантированного остатка топлива.An emergency fuel discharge system from an aircraft beam containing booster pumps located in the tank's supply compartment, a negative overload tank in which one of the booster pumps is installed, a fuel supply pipeline to the engine with non-return valves, an emergency drain pipeline with a shut-off valve, a fuel transfer pump the expendable compartment and the sensor-signaling device of the level of guaranteed residual fuel electrically connected with the shut-off valve, characterized in that, in order to simplify the operation of the system and increase safety Flight quality by automatically terminating the emergency drain upon reaching the guaranteed remaining fuel, the emergency emptying pipe is connected to the booster pump installed in the negative overload glass, the upper section of which is made at the level of the guaranteed remaining fuel.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU3921286/23A SU1316182A1 (en) | 1985-07-04 | 1985-07-04 | EMERGENCY DRAIN SYSTEM OF FUEL FROM AIRPLANE TANK |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU3921286/23A SU1316182A1 (en) | 1985-07-04 | 1985-07-04 | EMERGENCY DRAIN SYSTEM OF FUEL FROM AIRPLANE TANK |
Publications (1)
Publication Number | Publication Date |
---|---|
SU1316182A1 true SU1316182A1 (en) | 2004-12-20 |
Family
ID=60543138
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SU3921286/23A SU1316182A1 (en) | 1985-07-04 | 1985-07-04 | EMERGENCY DRAIN SYSTEM OF FUEL FROM AIRPLANE TANK |
Country Status (1)
Country | Link |
---|---|
SU (1) | SU1316182A1 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2669906C2 (en) * | 2016-08-03 | 2018-10-16 | Александр Александрович Панфилов | Aircraft plug-plane aircraft |
-
1985
- 1985-07-04 SU SU3921286/23A patent/SU1316182A1/en active
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2669906C2 (en) * | 2016-08-03 | 2018-10-16 | Александр Александрович Панфилов | Aircraft plug-plane aircraft |
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