First measurements on BEARCAT, the SAFRAN’s heavily instrumented turboshaft
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Bibliographic record
Abstract
View Video Presentation: https://doi.org/10.2514/6.2023-1936.vid In this paper, we will present examples of first experimental results obtained on a brand new turboshaft test rig called BEARCAT. BEARCAT is based on a Makila engine, a turboshaft developed by Safran Helicopter Engines and powering the H215 and the H225 Helicopter of Airbus Helicopters. BEARCAT has been developed by SAFRAN-Tech, the Research and Technology Center of the SAFRAN Group. This test engine is devoted to the fine characterization of aero-thermal phenomena occurring within the combustion chamber and the High Pressure Turbine as well as their interactions. Therefore, BEARCAT differs from a standard test engine by the implementation of moving probes inside the combustion chamber and the 2-stage High Pressure Turbine, in order to perform both steady and non-steady flow measurements. These data will be used to validate CFD codes and models
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Codex and Gemma teacher scores by category
| Category | Codex | Gemma |
|---|---|---|
| Metaresearch | 0.000 | 0.000 |
| Meta-epidemiology (narrow) | 0.000 | 0.000 |
| Meta-epidemiology (broad) | 0.000 | 0.000 |
| Bibliometrics | 0.000 | 0.001 |
| Science and technology studies | 0.000 | 0.000 |
| Scholarly communication | 0.000 | 0.000 |
| Open science | 0.000 | 0.000 |
| Research integrity | 0.000 | 0.000 |
| Insufficient payload (model declined to judge) | 0.000 | 0.002 |
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