SU372893A1 - SYSTEM OF SUPPORTING TANK FUEL OF AIRCRAFT - Google Patents

SYSTEM OF SUPPORTING TANK FUEL OF AIRCRAFT

Info

Publication number
SU372893A1
SU372893A1 SU1655606/23A SU1655606A SU372893A1 SU 372893 A1 SU372893 A1 SU 372893A1 SU 1655606/23 A SU1655606/23 A SU 1655606/23A SU 1655606 A SU1655606 A SU 1655606A SU 372893 A1 SU372893 A1 SU 372893A1
Authority
SU
USSR - Soviet Union
Prior art keywords
aircraft
tank fuel
supporting tank
pressure stabilizer
air
Prior art date
Application number
SU1655606/23A
Other languages
Russian (ru)
Inventor
И.В. Емельянов
А.А. Крылов
В.А. Ярыгин
Original Assignee
И.В. Емельянов
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 И.В. Емельянов filed Critical И.В. Емельянов
Priority to SU1655606/23A priority Critical patent/SU372893A1/en
Application granted granted Critical
Publication of SU372893A1 publication Critical patent/SU372893A1/en

Links

Landscapes

  • Separation Using Semi-Permeable Membranes (AREA)

Abstract

Система наддува топливных баков летательного аппарата, содержащая трубопроводы подачи нейтрального газа и воздуха с установленными на них перед точкой соединения регуляторами расхода и стабилизатором давления, отличающаяся тем, что, с целью повышения экономичности и надежности работы системы, в магистрали подачи воздуха перед регулятором расхода смонтирован дроссельный клапан, исполнительный орган которого соединен с мембраной, разделяющей полости стабилизатора давления.The system of pressurization of the fuel tanks of the aircraft, containing pipelines for supplying neutral gas and air with flow regulators and a pressure stabilizer installed in front of the connection point, characterized in that, in order to improve the efficiency and reliability of the system, a throttle valve is mounted in front of the air flow regulator the valve, the executive body of which is connected to the membrane separating the cavity of the pressure stabilizer.

SU1655606/23A 1971-05-13 1971-05-13 SYSTEM OF SUPPORTING TANK FUEL OF AIRCRAFT SU372893A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU1655606/23A SU372893A1 (en) 1971-05-13 1971-05-13 SYSTEM OF SUPPORTING TANK FUEL OF AIRCRAFT

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU1655606/23A SU372893A1 (en) 1971-05-13 1971-05-13 SYSTEM OF SUPPORTING TANK FUEL OF AIRCRAFT

Publications (1)

Publication Number Publication Date
SU372893A1 true SU372893A1 (en) 2005-02-27

Family

ID=60514410

Family Applications (1)

Application Number Title Priority Date Filing Date
SU1655606/23A SU372893A1 (en) 1971-05-13 1971-05-13 SYSTEM OF SUPPORTING TANK FUEL OF AIRCRAFT

Country Status (1)

Country Link
SU (1) SU372893A1 (en)

Similar Documents

Publication Publication Date Title
GB1056477A (en) Liquid or gas supply system for a gas turbine engine
ES464686A1 (en) Safety device for venting a fuel tank
SU372893A1 (en) SYSTEM OF SUPPORTING TANK FUEL OF AIRCRAFT
SU526130A1 (en) System of pressurization of neutral gas of fuel tanks of the aircraft
ES8406104A1 (en) Fuel supply system
SU359926A1 (en) SYSTEM FOR SUPPORTING THE TANK OF AIRPLANE
SU372892A1 (en) SYSTEM OF SUPPORTING TANK FUEL OF AIRCRAFT
SU438237A1 (en) The system of pressurization of the fuel tanks of the aircraft by neutral gas
SU491259A1 (en) System of pressurization of neutral gas of fuel tanks of aircraft
ES396983A1 (en) Fuel supply systems for gas turbine engines
FR2312062A1 (en) Device for injecting antifreeze into aircraft fuel - has fuel container divided by membrane connected to Venturi in supply line
SU720934A1 (en) Fuel gas pressurization system
SU225639A1 (en) Pressure control system in aircraft fuel tanks
FR2276468A1 (en) Engine fuel control system using pressure injection - compensates for variable fuel tank pressure and high air pressure drop
SU464168A1 (en) The system of pressurization of the fuel tanks of the aircraft by neutral gas
SU345760A1 (en) SYSTEM OF SUPPORTING THE TANK FUEL OF AIRCRAFT
GB1234945A (en) Auxiliary cold-starting carburettors and recharging feeder tanks therefor for internal combustion engines
ES431854A1 (en) Improvements introduced in a pressure regulator valve. (Machine-translation by Google Translate, not legally binding)
SU828613A1 (en) SYSTEM FOR SUPPORTING THE TANK OF AIRPLANE
SU658850A1 (en) DRAINAGE SYSTEM - PRESSING THE FUEL TANKS OF THE PLANE
SU213594A1 (en) SYSTEM FOR SUPPORTING GAS OF FUEL TANK OF PLANES
SU238973A1 (en) SAFETY VALVE FOR SUPPLEMENT SYSTEM AIRCRAFT FUEL TANKS
GB842177A (en) Improvements in or relating to fuel supply systems for aircraft
SU342441A1 (en) System of pressurization of neutral gas of fuel tanks of aircraft
SU367678A1 (en) SYSTEM OF SUPPORTING TANK FUEL OF AIRCRAFT