Accession Number:

ADA002483

Title:

Evaluation Program on Using Compressor Bleed Air as a Source of Pneumatic Power for Fluidic Circuits.

Descriptive Note:

Final rept. Oct 72-Oct 73,

Corporate Author:

AIRESEARCH MFG CO OF ARIZONA PHOENIX

Personal Author(s):

• McCarty,R. S.

Report Date:

1973-10-05

Pagination or Media Count:

76.0

Abstract:

The program activities encompassed study and analysis of the characteristics of compressor bleed air as it is affected by engine power settings, engine age, location of the extraction point, inlet ingestion, and how the contamination of all of these affect fluidic components.

Descriptors:

• *AIRCRAFT ENGINES
• *FLUIDIC CONTROL
• *BLEED SYSTEMS
• PARTICLE SIZE
• TURBOPROP ENGINES
• NAVAL AIRCRAFT
• CONTAMINANTS
• PNEUMATIC ACTUATORS
• ROTARY COMPRESSORS

Subject Categories:

• Fluidics and Fluerics
• Jet and Gas Turbine Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE