Characterization of an Aircraft Auxiliary Power Unit Test Rig for Cycle Optimization Studies

Abstract

Detailed information of the thermodynamic parameters, system performance, and operating behavior of aircraft auxiliary power units (APU) cycles is rarely available in literature. In order to set up numeric models and study cycle modifications, validation data with well-defined boundary conditions is needed. Thus, the paper introduces an APU test rig based on a Garrett GTCP36-28 with detailed instrumentation, which will be used in a further step as a demonstration platform for cycle modifications. The system is characterized in the complete feasible operating range by alternating bleed air load and electric power output. Furthermore, simulations of a validated numerical cycle model are utilized to predict the load points in the operating region which were unstable during measurements. The paper reports and discusses turbine shaft speed, compressor air mass flow, fuel mass flow, efficiencies, compressor outlet pressure and temperature, turbine inlet and outlet temperature as well as exhaust gas emissions. Furthermore, the results are discussed with respect to the difference compared to a Hamilton Sundstrand APS3200. Though the efficiencies of the GTCP36-28 are lower compared to the APS3200, the general behavior is in good agreement. In particular, the effects of separate compressors for load and power section are discussed in contrast to the GTCP36-28 system design comprising a single compressor. In general, it was shown that the GTCP36-28 is still appropriate for the utilization as a demonstration platform for cycle modification studies.

A fault detection method for Auxiliary Power Unit based on monitoring parameters selection

“…However, detailed information of the thermodynamic parameters, system performance, and operating behavior of aircraft APU cycles is rarely available in literature. Zanger et al 7 introduced an APU test rig based on a Garrett GTCP36-28 with detailed instrumentation, which would be used in a further step as a demonstration platform for cycle modifications.…”

Development of a Far-Field Noise Estimation Model for an Aircraft Auxiliary Power Unit

“…Generally, a diagnostic capability is embedded into the system during the design phase depending on the technologies (hardware, sensors, processing techniques) available at that time. Performance-based monitoring (also called gas-path analysis) is an example of the prevalent approach for a gas turbine's health monitoring or fault detection [1][2][3][4][5][6][7]. However, these methods require the installation of thermodynamic sensors which could be intrusive and may not be feasible if they were not considered during the product's design phase.…”