X376 PITCH FAN FLIGHTWORTHINESS RATING TEST

Abstract

This specification defines the flightworthiness rating test requirements for the X376, ducted, pitch trim control fan. The General Electric X376 pitch fan is designed for supplying augmented control and trim force in V/ STOL systems. It is comprised of a single stage, tip-turbine driven fan supplied with turbojet exhaust gas bleed through two separated nozzle scrolls. The double scroll arrangement provides single-engine operating capability in a two-engine, cross-ducted lift propulsion system.

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Document Details

Document Type
Technical Report
Publication Date
Apr 19, 1962
Accession Number
AD0634946

Entities

Organizations

  • General Electric

Tags

Communities of Interest

  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Army Aviation
  • Contracts
  • Engines
  • Exhaust Gases
  • Frequency
  • Gases
  • Generators
  • Government Procurement
  • Governments
  • Propulsion System Components
  • Propulsion Systems
  • Sea Level
  • Steady State
  • Test Equipment
  • Thrust Reversal
  • Turbojet Engines
  • Vibration

Fields of Study

  • Engineering
  • Physics

Readers

  • Aerospace Engineering