CERTAIN PROBLEMS OF THE JET DRIVE OF A HELICOPTER ROTOR BY MEANS OF A TURBOJET ENGINE ATTACHED TO THE BLADES,

Abstract

The creation of a turbojet engine suitable for work on rotor blades requires the effectuation of various experimental and design investigations. The following are the main problems: Ensuring efficiency of bearings and heat dissipation from oil under the conditions of large radial loads; and balancing the gyroscopic moment created by the engine rotor revolving together with the rotor blade. (Author)

Document Details

Document Type
Technical Report
Publication Date
Mar 30, 1964
Accession Number
AD0602565

Entities

People

  • B. P. Kaganovich

Organizations

  • National Air and Space Intelligence Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircrafts
  • Airframes
  • Dissipation
  • Efficiency
  • Engines
  • Helicopter Rotors
  • Helicopters
  • Jet Aircraft
  • Turbojet Engines
  • Vehicles

Fields of Study

  • Physics

Readers

  • Aerospace Engineering
  • Combustion and Flow Dynamics.
  • Theoretical Analysis.