SU786203A1 - FUEL FILLING SYSTEM FOR AIRCRAFT - Google Patents

FUEL FILLING SYSTEM FOR AIRCRAFT

Info

Publication number
SU786203A1
SU786203A1 SU2704034/23A SU2704034A SU786203A1 SU 786203 A1 SU786203 A1 SU 786203A1 SU 2704034/23 A SU2704034/23 A SU 2704034/23A SU 2704034 A SU2704034 A SU 2704034A SU 786203 A1 SU786203 A1 SU 786203A1
Authority
SU
USSR - Soviet Union
Prior art keywords
fuel
aircraft
flow control
filling system
fuel filling
Prior art date
Application number
SU2704034/23A
Other languages
Russian (ru)
Inventor
Ю.В. Козлов
В.М. Цыганов
В.К. Носокин
Л.И. Заславский
Original Assignee
Ю.В. Козлов
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 Ю.В. Козлов filed Critical Ю.В. Козлов
Priority to SU2704034/23A priority Critical patent/SU786203A1/en
Application granted granted Critical
Publication of SU786203A1 publication Critical patent/SU786203A1/en

Links

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  • Loading And Unloading Of Fuel Tanks Or Ships (AREA)

Abstract

Система заправки топливом летательного аппарата, содержащая топливные баки с насосами для перекачки топлива, расходную магистраль подачи топлива на двигатель, магистраль отдачи топлива в заправляемый самолет, связанную с гибким шлангом, заканчивающимся стыковочным конусом, магистраль дозаправки топлива со стыковочным узлом и средство регулирования расхода топлива, при этом все магистрали снабжены расходомерами, подключенными к блоку контроля расхода топлива, отличающаяся тем, что, с целью обеспечения взрывобезопасности и повышения надежности в систему введен блок контроля степени электризации топлива, содержащий датчик электромагнитного излучения искровых разрядов, подключенный к последовательно соединенным преобразователю сигнала и приводу, управляющему средством регулирования расхода топлива.An aircraft refueling system containing fuel tanks with pumps for pumping fuel, a consumable fuel supply line to the engine, a fuel return line to the aircraft being fueled connected to a flexible hose ending with a docking cone at the same time, all the lines are equipped with flow meters connected to the fuel consumption control unit, characterized in that, in order to ensure explosion safety and increase In adezhnosti introduced fuel flow control degree electrification comprising electromagnetic radiation sensor spark discharges connected to the series-connected inverter drive signal and that controls the fuel flow control means.

SU2704034/23A 1978-12-28 1978-12-28 FUEL FILLING SYSTEM FOR AIRCRAFT SU786203A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU2704034/23A SU786203A1 (en) 1978-12-28 1978-12-28 FUEL FILLING SYSTEM FOR AIRCRAFT

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU2704034/23A SU786203A1 (en) 1978-12-28 1978-12-28 FUEL FILLING SYSTEM FOR AIRCRAFT

Publications (1)

Publication Number Publication Date
SU786203A1 true SU786203A1 (en) 2005-03-20

Family

ID=60524619

Family Applications (1)

Application Number Title Priority Date Filing Date
SU2704034/23A SU786203A1 (en) 1978-12-28 1978-12-28 FUEL FILLING SYSTEM FOR AIRCRAFT

Country Status (1)

Country Link
SU (1) SU786203A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2537191C2 (en) * 2013-04-18 2014-12-27 Открытое акционерное общество "Лётно-исследовательский институт имени М.М. Громова" Spark-safe filling of aircraft fuel tanks at pressure

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2537191C2 (en) * 2013-04-18 2014-12-27 Открытое акционерное общество "Лётно-исследовательский институт имени М.М. Громова" Spark-safe filling of aircraft fuel tanks at pressure

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