SU1140510A1 - METHOD OF STABILIZATION OF PRESSURE IN THE SYSTEM OF FEEDING OF AVIATION ENGINE FUEL - Google Patents

METHOD OF STABILIZATION OF PRESSURE IN THE SYSTEM OF FEEDING OF AVIATION ENGINE FUEL

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Publication number
SU1140510A1
SU1140510A1 SU3627654/06A SU3627654A SU1140510A1 SU 1140510 A1 SU1140510 A1 SU 1140510A1 SU 3627654/06 A SU3627654/06 A SU 3627654/06A SU 3627654 A SU3627654 A SU 3627654A SU 1140510 A1 SU1140510 A1 SU 1140510A1
Authority
SU
USSR - Soviet Union
Prior art keywords
fuel
pressure
stabilization
pump
feeding
Prior art date
Application number
SU3627654/06A
Other languages
Russian (ru)
Inventor
В.А. Калугин
Ю.М. Кузин
Original Assignee
В.А. Калугин
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 В.А. Калугин filed Critical В.А. Калугин
Priority to SU3627654/06A priority Critical patent/SU1140510A1/en
Application granted granted Critical
Publication of SU1140510A1 publication Critical patent/SU1140510A1/en

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  • Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)

Abstract

Способ стабилизации давления в системе подачи топлива авиационного двигателя, включающий забор топлива из бака насосом, непрерывное измерение параметров топлива за насосом и перепуск топлива из-за насоса в бак с расходом, пропорциональным величине измеряемых параметров, отличающийся тем, что, с целью повышения точности стабилизации давления, в качестве параметров топлива используют модуль амплитуды и период колебаний давления, а перепуск топлива осуществляют пропорционально отношению этих величин.The method of stabilizing the pressure in the fuel supply system of an aircraft engine, including the fuel intake from the tank by a pump, continuous measurement of fuel parameters behind the pump and fuel bypass due to the pump into the tank with a flow rate proportional to the value of the measured parameters, characterized in that in order to improve the accuracy of stabilization pressure, as the parameters of the fuel, the amplitude modulus and the period of pressure fluctuations are used, and the fuel bypass is carried out in proportion to the ratio of these values.

SU3627654/06A 1983-07-27 1983-07-27 METHOD OF STABILIZATION OF PRESSURE IN THE SYSTEM OF FEEDING OF AVIATION ENGINE FUEL SU1140510A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU3627654/06A SU1140510A1 (en) 1983-07-27 1983-07-27 METHOD OF STABILIZATION OF PRESSURE IN THE SYSTEM OF FEEDING OF AVIATION ENGINE FUEL

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU3627654/06A SU1140510A1 (en) 1983-07-27 1983-07-27 METHOD OF STABILIZATION OF PRESSURE IN THE SYSTEM OF FEEDING OF AVIATION ENGINE FUEL

Publications (1)

Publication Number Publication Date
SU1140510A1 true SU1140510A1 (en) 2004-08-10

Family

ID=60540384

Family Applications (1)

Application Number Title Priority Date Filing Date
SU3627654/06A SU1140510A1 (en) 1983-07-27 1983-07-27 METHOD OF STABILIZATION OF PRESSURE IN THE SYSTEM OF FEEDING OF AVIATION ENGINE FUEL

Country Status (1)

Country Link
SU (1) SU1140510A1 (en)

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