A method includes receiving image data from a camera 162 coupled to an air intake system of a gas turbine engine. The image data corresponds to an air passage of the air intake system. The method also includes comparing the received image data to reference image data of the air intake system 164. The method also includes generating an icing notification 168 based at least in part on the comparison when a difference between the received image data and reference image data is greater than an icing threshold.
IMAGING ASSISTED GAS TURBINE ANTI-ICING SYSTEM
BILDGESTÜTZTES GASTURBINENENTEISUNGSSYSTEM
SYSTÈME ANTIGIVRAGE DE TURBINE À GAZ ASSISTÉE PAR IMAGERIE
04.11.2020
Patent
Elektronische Ressource
Englisch