Fuel Pressure Increase Limiter,

Abstract

The invention belongs to the field of the automatic control of turbojet engines, in particular, to fuel pressure increase limiters. Known are fuel pressure increase limiters, predominantly for a turbojet engine, which contain a spring-opposed servopistion with a rod, the cavities of which are connected by channels with a constant pressure valve, and a control slid valve. The purpose of the invention is to provide the optimal rate of pressure increase. To do this, made in the rod are additional channels connected to both cavities of the servodrive by means of holes which are provided in its body.

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Document Details

Document Type
Technical Report
Publication Date
Jul 26, 1977
Accession Number
ADA049393

Entities

People

  • A. A. Ryzhov
  • M. A. Medvedeva
  • V. I. Bolshagin
  • V. S. Dyakonov
  • Yu. M. Akhmetov

Organizations

  • National Air and Space Intelligence Center

Tags

DTIC Thesaurus Topics

  • Air Force
  • Automatic
  • Energy Generators
  • Energy Systems
  • Engines
  • Flow Rate
  • Foreign Technology
  • Gas Turbines
  • Generators
  • Heat Engines
  • Heat Transfer Devices
  • Inventions
  • Jet Aircraft
  • Jet Engines
  • Patents
  • Translations
  • Turbojet Engines

Readers

  • Electrical Engineering
  • Internal Combustion Engine (ICE) Technology.
  • Microwave Engineering.