Engine/Transmission/Airframe Advanced Integration Techniques

Abstract

Innovative engine/transmission/airframe integrated design concepts were developed to provide total airflow and power management for a utility transport helicopter which meets projected requirements of future Army aircraft. These requirements include engine compartment cooling, drive train and transmission oil cooling, engine oil cooling, exhaust plume and hot metal infrared (IR) signature suppression, and engine inlet foreign particle protection.

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Document Details

Document Type
Technical Report
Publication Date
May 01, 1975
Accession Number
ADA012236

Entities

People

  • Richard D. Semple
  • Theodore Himka

Organizations

  • Boeing Rotorcraft Systems

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aerodynamic Configurations
  • Aircraft Equipment
  • Aircrafts
  • Airframes
  • Army Aircraft
  • Composite Materials
  • Exhaust Gases
  • Exhaust Plumes
  • Flight Speeds
  • Heat Transfer
  • Helicopters
  • Horizontal Stabilizers
  • Nose Wheels
  • Rotary Wing Aircraft
  • Spars
  • Turbines
  • Utility Aircraft

Readers

  • Aerospace Engineering
  • Electrical Engineering