A gas turbine engine includes a frame, a plurality of fan blades configured to rotate about a longitudinal centerline axis of the gas turbine engine, and a mounting assembly coupling the frame to a structure. The gas turbine engine includes a sensor assembly coupled to the mounting assembly and having at least one sensor configured to detect a load on the mounting assembly and to take a corrective action when detecting propeller swirl above a predetermined limit, the feature is configured to take a corrective action when a propeller swirl is detected above a predetermined limit.
一种燃气涡轮发动机,包括框架、被构造为绕燃气涡轮发动机的纵向中心线轴线旋转的多个风扇叶片、以及将框架联接到结构的安装组件。燃气涡轮发动机包括传感器组件和特征,传感器组件联接到安装组件并且具有至少一个传感器,该至少一个传感器被构造为检测安装组件上的负载并且当检测到螺旋桨旋流高于预定极限时采取校正动作,该特征被构造为当检测到螺旋桨旋流高于预定极限时采取校正动作。
Gas turbine engine with sensor assembly for monitoring propeller swirl
具有用于监测螺旋桨旋流的传感器组件的燃气涡轮发动机
2025-02-14
Patent
Electronic Resource
Chinese
IPC: | F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G01M TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES , Prüfen der statischen oder dynamischen Massenverteilung rotierender Teile von Maschinen oder Konstruktionen |
Sensor assembly for detecting propeller swirl in turbine engine
European Patent Office | 2025
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