Mach Controller,

Abstract

Devices which regulate the flight Mach number of aircraft contain a static pressure chamber, a chamber at the pressure of the oncoming flow, an air reduction valve, a diaphragm, and a lever which acts upon the fuel supply regulator. The proposed invention provides the elastic diaphragm with a lever connected to the nozzle flap of the air reduction valve, changing the pressure gradient of the turbine, while the dynamic head reduction valve is designed with a jet ejector. This makes it possible to increase the response and stability of the regulator.

Document Details

Document Type
Technical Report
Publication Date
Jan 03, 1975
Accession Number
ADA006830

Entities

People

  • A. Kh. Makarov
  • V. I. Konstantinov

Organizations

  • National Air and Space Intelligence Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircrafts
  • Barometric Pressure
  • Biological Phenomena
  • Dynamic Pressure
  • Ecological And Environmental Phenomena
  • Ecological And Environmental Processes
  • Intellectual Property
  • Inventions
  • Law
  • Mach Number
  • Patents
  • Pressure Gradients
  • Regulators
  • Skeletal Muscle
  • Static Pressure

Fields of Study

  • Physics

Readers

  • Combustion and Flow Dynamics.
  • Electrical Engineering
  • Internal Combustion Engine (ICE) Technology.