Integral Engine Inlet Particle Separator. Volume 1. Technology Program

Abstract

Volume I of this report describes the results of a 30-month program to design and evaluate integral engine inlet separators in 2, 5, and 15 lb/sec sizes. The separators are designed to remove sand, dust, and single foreign objects from the air entering a turboshaft engine. Program effort included: (1) Definition of turboshaft engine environment in terms of amounts and types of ingested materials. (2) Mechanical and aerodynamic design trade-off studies of integral engine separators followed by full-scale model performance tests of 2 and 15 lb/sec separators. (3) Detailed design and procurement of 2, 5, and 15 lb/sec separators, and design and procurement of improved components. (4) Model tests of the separators to obtain detailed aerodynamic and off-design performance data. (5) Preparation of a separator design guide for integral engine separators in the 2 to 15 lb/sec size range. The design guide (including environment definition) is presented in Volume II of this report. Volume I documents all other aspects of the program.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1975
Accession Number
ADA013834

Entities

People

  • Bernard F. Shattuck
  • Robert J. Duffy

Organizations

  • General Electric

Tags

Communities of Interest

  • Air Platforms
  • Human Systems

DTIC Thesaurus Topics

  • Aircrafts
  • Boundary Layer
  • Diffusion
  • Gas Turbines
  • Geometry
  • Leading Edges
  • Mach Number
  • Measurement
  • Plastic Explosives
  • Pressure Distribution
  • Pressure Gradients
  • Secondary Flow
  • Static Pressure
  • Test And Evaluation
  • Test Facilities
  • Turbines
  • Turboshaft Engines

Readers

  • Aerodynamics.
  • Internal Combustion Engine (ICE) Technology.
  • Systems Analysis and Design