New model-based method for aero-engine turbine blade tip clearance measurement
Chinese Journal of Aeronautics
Chinese Journal of Aeronautics ; 36 , 8 ; 128-147
01.08.2023
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Astigmatic turbine blade tip clearance sensor for gas turbine aero engines
| Tema Archiv | 1987
Gas Turbine Aero-Engine First Stage Turbine Blade Failure Investigation
| Online Contents | 2009
| British Library Conference Proceedings | 2007
Gas turbine engine turbine blade tip active clearance control system and method
| Europäisches Patentamt | 2016
Rotor Blade Vibration Measurement on Aero Gas Turbine Engines
| Springer Verlag | 2020