HEAVY-LIFT TIP TURBOJET ROTOR SYSTEM. VOLUME 11. ENGINE DESIGN

Abstract

The report discusses the design of the Model 357-1 engine for rotor tip operational environment. The detail design meets requirements of MIL-E-5007B except for items peculiar to rotor tip operation. These items include operational attitudes, effect of continuous gyroscopic couples and high g field environment. The report includes an analytical design analysis of the static structure, rotating elements, bearings, accessory drives, lubrication system, and miscellaneous engine parts.

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Document Details

Document Type
Technical Report
Publication Date
Oct 01, 1965
Accession Number
AD0624716

Tags

DTIC Thesaurus Topics

  • Aircrafts
  • Airframes
  • Calorific Value
  • Centrifugal Compressors
  • Centrifugal Fields
  • Combustion
  • Engines
  • Exhaust Gases
  • Fuel Systems
  • Gas Turbines
  • Jet Engines
  • Mechanical Structure
  • Pressure Distribution
  • Systems Engineering
  • Turbines
  • Turbojet Engines
  • Yield Strength

Fields of Study

  • Physics

Readers

  • Aerodynamics.
  • Software Engineering
  • Tribology (the study of the boundary interaction between sliding surfaces, lubrication, wear and friction).