SU753005A1 - FUEL FLUID SYSTEM - Google Patents

FUEL FLUID SYSTEM

Info

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
Application number
SU2703473/23A
Other languages
Russian (ru)
Inventor
Н.Е. Чудаков
В.М. Цыганов
Original Assignee
Н.Е. Чудаков
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Н.Е. Чудаков filed Critical Н.Е. Чудаков
Priority to SU2703473/23A priority Critical patent/SU753005A1/en
Application granted granted Critical
Publication of SU753005A1 publication Critical patent/SU753005A1/en

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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.

SU2703473/23A 1978-12-28 1978-12-28 FUEL FLUID SYSTEM SU753005A1 (en)

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)

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