REDUCING COST, TIME AND RISK IN AEROENGINE COMPRESSOR TESTING

Citation
R. Backhouse et P. Ivey, REDUCING COST, TIME AND RISK IN AEROENGINE COMPRESSOR TESTING, Proceedings of the Institution of Mechanical Engineers. Part G, Journal of aerospace engineering, 211(G6), 1997, pp. 395-402
Citations number
5
ISSN journal
09544100
Volume
211
Issue
G6
Year of publication
1997
Pages
395 - 402
Database
ISI
SICI code
0954-4100(1997)211:G6<395:RCTARI>2.0.ZU;2-G
Abstract
There is constant pressure to reduce engine development cycles to mini mize costs and bring forward the revenue earning part of the engine's life. As cost and time are designed out, the risk of performance short fall must be minimized by bidding efficiencies from demonstrated techn ology. This requires a large-scale ongoing advanced development progra m. In compressor development, high-speed tests are unavoidable but are expensive; low-speed rigs are easier to instrument and provide a cost -effective filter for the high-speed designs. The large-scale, low-spe ed compressor at Cranfield is one of only four worldwide. Recent inves tment in data reduction software has greatly reduced the test/analysis cycle time.