Real-time turbomachinery blade breakage monitoring unit and turbo-apparatus
AssigneeKorea Aerospace Research Institute
InventorsJeong S. Kang, Bong J. Cha, Lee K. Ahn
Life of this patent
Estimating the term…
Loading patent…
AssigneeKorea Aerospace Research Institute
InventorsJeong S. Kang, Bong J. Cha, Lee K. Ahn
Estimating the term…
Disclosed herein are a turbo-machinery blade breakage monitoring unit and a turbo-apparatus having the same. The blade breakage monitoring unit includes a pressure sensor disposed near a rotor having a plurality of blades to be rotated at a predetermined speed, the pressure sensor functioning to measure total pressures of the respective blades. The blade breakage monitoring unit further includes a controller electrically connected to the pressure sensor and functioning to judge whether or not each measured total pressure value, transmitted from the pressure sensor, is within a preset criterion total pressure range. With the use of the blade breakage monitoring unit, total pressures of the respective blades are monitored in real time at a position downstream of the blades when the blades are rotated at a high speed within the turbo-apparatus, such as a turbine, compressor and fan, enabling real-time monitoring of breakage of the blades.
A turbo-machinery blade breakage monitoring system comprising:
Dependencies are inferred from the claim text.