SU367678A1 - SYSTEM OF SUPPORTING TANK FUEL OF AIRCRAFT - Google Patents

SYSTEM OF SUPPORTING TANK FUEL OF AIRCRAFT

Info

Publication number
SU367678A1
SU367678A1 SU1651140/23A SU1651140A SU367678A1 SU 367678 A1 SU367678 A1 SU 367678A1 SU 1651140/23 A SU1651140/23 A SU 1651140/23A SU 1651140 A SU1651140 A SU 1651140A SU 367678 A1 SU367678 A1 SU 367678A1
Authority
SU
USSR - Soviet Union
Prior art keywords
aircraft
pressurization
tank fuel
fuel tanks
safety valve
Prior art date
Application number
SU1651140/23A
Other languages
Russian (ru)
Inventor
И.В. Емельянов
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 SU1651140/23A priority Critical patent/SU367678A1/en
Application granted granted Critical
Publication of SU367678A1 publication Critical patent/SU367678A1/en

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  • Fuel-Injection Apparatus (AREA)

Abstract

Система наддува топливных баков летательного аппарата, содержащая трубопроводы наддува, соединенные с заборником скоростного напора и бортовым источником сжатого газа, с установленными на них обратными клапанами, предохранительным клапаном и дросселем, отличающаяся тем, что, с целью исключения забросов давления в топливных баках при наборе высоты, на трубопроводе подачи воздуха перед предохранительным клапаном смонтировано перекрывное устройство, выполненное в виде запорного клапана, снабженного подпружиненным весовым механизмом.The system of pressurization of fuel tanks of an aircraft, containing pipelines of pressurization, connected to an intake of a high-speed head and an onboard source of compressed gas, with non-return valves installed on them, a safety valve and a throttle, characterized in that, in order to avoid pressure surges in fuel tanks during ascent , on the air supply pipe in front of the safety valve, a shut-off device is installed, made in the form of a check valve equipped with a spring-loaded weight mechanism.

SU1651140/23A 1971-04-28 1971-04-28 SYSTEM OF SUPPORTING TANK FUEL OF AIRCRAFT SU367678A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU1651140/23A SU367678A1 (en) 1971-04-28 1971-04-28 SYSTEM OF SUPPORTING TANK FUEL OF AIRCRAFT

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU1651140/23A SU367678A1 (en) 1971-04-28 1971-04-28 SYSTEM OF SUPPORTING TANK FUEL OF AIRCRAFT

Publications (1)

Publication Number Publication Date
SU367678A1 true SU367678A1 (en) 2005-02-27

Family

ID=60514259

Family Applications (1)

Application Number Title Priority Date Filing Date
SU1651140/23A SU367678A1 (en) 1971-04-28 1971-04-28 SYSTEM OF SUPPORTING TANK FUEL OF AIRCRAFT

Country Status (1)

Country Link
SU (1) SU367678A1 (en)

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