A method to introduce context-awareness into gas turbine engines was briefly presented in which linkage among components is replaced by coherent consistency under integrated management. Such configuration allows free access to components individually toward adaptation to environmental elements and user demands.
Based on this method an alternative to HPC of GE90-94B high by pass ratio turbofan engine was designed and modeled by computer in average-fidelity level. In this way, suitable methods to design and draw characteristic map of intended type were introduced. In addition, new dimensionless parameters were defined, which satisfy requirements of individual rotational speed for each stage in multi-stages axial flow compressors.
Summary of results indicates that this mechanism allows collecting optimum performance of compressor and advances its operation. Free access to each component allows adaptation of each stage to environmental elements and user demands whose outcome is such an adaptation for compressor entirely.