CONTROL APPROACHES TO SOLUTION OF COMPRESSOR STALL

560286

01/01/1956

Event
Pre-1964 SAE Technical Papers
Authors Abstract
Content
The control of compressor stall and surge is one of the most difficult problems confronting the control engineer today. Three modes of stall control are presented: (1) the scheduling, or open loop, control now in use on most gas turbine engines, (2) the closed loop control using compressor parameters which synthesize the stall boundary, and (3) the closed loop control using an incipient stall ‘sensor’. The use of a closed loop control which uses synthesizing stall parameters may partially solve some of the present problems, such as variations in physical properties of fuel. However, there is a great incentive to develop a means for detecting incipient stall and surge in order to aid in reducing the development time for future supersonic, high altitude gas turbine engines.
Meta TagsDetails
DOI
https://doi.org/10.4271/560286
Pages
8
Citation
GEBHARDT, W., and BODEMULLER, R., "CONTROL APPROACHES TO SOLUTION OF COMPRESSOR STALL," SAE Technical Paper 560286, 1956, https://doi.org/10.4271/560286.
Additional Details
Publisher
Published
Jan 1, 1956
Product Code
560286
Content Type
Technical Paper
Language
English