Gas Turbine Compressor Development Program for 1.5/3 KW Generator Set.

reportActive / Technical Report | Accession Number: ADA033577 | Open PDF

Abstract:

This report summarizes a study that performed the preliminary design of a small gas turbine engine, capable of providing 6-hp for driving a 1.53 Kw generator set, and presents the results of performance testing the resultant compressor design. Author

Author(s):
Lee, Jessie B. ; Zanelli, Eugene A.
Author Organization(s):
AIRESEARCH MFG CO OF ARIZONA PHOENIX
Descriptive Note:
Final rept. 28 Feb 74-31 Oct 75,
Pagination:
0052

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
75-311130
Contract/Grant Number(s):
DAAK02-74-C-0167
Task Number(s):
01
Project Number(s):
1G763702DG11
 Subject Terms
Joint Capability Areas:
JCA_5_Command and Control; JCA_5.3_Planning; JCA_5.3.4_Develop Courses of Action; JCA_5.3.5_Analyze Courses of Action; JCA_5.3.3_Develop Strategy; JCA_1.2_Force Preparation; JCA_1_Force Support; JCA_3.2_Engagement; JCA_3_Force Application; JCA_1.2.6_Concepts; JCA_3.2.1_Kinetic Means; JCA_4.6_Engineering
Modernization Areas:
Microelectronics; Fully Networked C3
Communities of Interest:
Energy and Power Technologies
Descriptor(s):
*GAS TURBINES, *COMPRESSORS, *AUXILIARY POWER PLANTS, *TURBOGENERATORS, ARMY RESEARCH
Field(s)/Group(s):
Electric Power Production and Distribution, Hydraulic and Pneumatic Equipment, Jet and Gas Turbine Engines
Keyword(s):
ASG11, WU013, PE63702A
Report Date:
1975 Dec 01