SU378076A1 - DEVICE FOR DEVELOPING FUEL FROM SUSPENDED TANK OF AIRCRAFT - Google Patents

DEVICE FOR DEVELOPING FUEL FROM SUSPENDED TANK OF AIRCRAFT

Info

Publication number
SU378076A1
SU378076A1 SU1694222/23A SU1694222A SU378076A1 SU 378076 A1 SU378076 A1 SU 378076A1 SU 1694222/23 A SU1694222/23 A SU 1694222/23A SU 1694222 A SU1694222 A SU 1694222A SU 378076 A1 SU378076 A1 SU 378076A1
Authority
SU
USSR - Soviet Union
Prior art keywords
fuel
aircraft
tank
outboard
developing fuel
Prior art date
Application number
SU1694222/23A
Other languages
Russian (ru)
Inventor
Л.И. Заславский
С.С. Жарков
Original Assignee
Л.И. Заславский
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 Л.И. Заславский filed Critical Л.И. Заславский
Priority to SU1694222/23A priority Critical patent/SU378076A1/en
Application granted granted Critical
Publication of SU378076A1 publication Critical patent/SU378076A1/en

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Landscapes

  • Jet Pumps And Other Pumps (AREA)
  • Loading And Unloading Of Fuel Tanks Or Ships (AREA)
  • Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)

Abstract

Устройство для выработки топлива из подвесного бака летательного аппарата, содержащее двухсекционный трубопровод перекачки, снабженный запорным клапаном, отличающееся тем, что, с целью упрощения топливной системы и снижения веса подвесного бака, на выходном конце трубопровода перекачки смонтирован струйный насос, соединенный с источником топлива высокого давления, а расходный бак соединен с подвесным баком посредством двухсекционного сливного трубопровода, верхний конец которого установлен на допустимом уровне топлива в расходном баке.A device for generating fuel from an aircraft outboard tank containing a two-section transfer pipeline, equipped with a shut-off valve, characterized in that, in order to simplify the fuel system and reduce the weight of the outboard tank, a jet pump is connected to the high-pressure fuel source at the output end of the transfer pipeline , and the supply tank is connected to the outboard tank by means of a two-section drain pipe, the upper end of which is set at the permissible level of fuel in the supply ake.

SU1694222/23A 1971-08-30 1971-08-30 DEVICE FOR DEVELOPING FUEL FROM SUSPENDED TANK OF AIRCRAFT SU378076A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU1694222/23A SU378076A1 (en) 1971-08-30 1971-08-30 DEVICE FOR DEVELOPING FUEL FROM SUSPENDED TANK OF AIRCRAFT

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU1694222/23A SU378076A1 (en) 1971-08-30 1971-08-30 DEVICE FOR DEVELOPING FUEL FROM SUSPENDED TANK OF AIRCRAFT

Publications (1)

Publication Number Publication Date
SU378076A1 true SU378076A1 (en) 2005-02-27

Family

ID=60514783

Family Applications (1)

Application Number Title Priority Date Filing Date
SU1694222/23A SU378076A1 (en) 1971-08-30 1971-08-30 DEVICE FOR DEVELOPING FUEL FROM SUSPENDED TANK OF AIRCRAFT

Country Status (1)

Country Link
SU (1) SU378076A1 (en)

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