System and method for turbomachinery blade diagnostics via discrete markings

Systems and methods include a blade monitoring system. The blade monitoring system includes a processor. The processor is configured to receive a sensor signal from a sensor configured to observe a blade of the turbomachinery. The processor is also configured to derive a measurement based on a marki...

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Bibliographic Details
Main Authors Ball, Michael Allen, Schleif, Kurt Kramer
Format Patent
LanguageEnglish
Published 22.02.2022
Subjects
AIR INTAKES FOR JET-PROPULSION PLANTS
ARRANGEMENTS, SYSTEMS OR APPARATUS FOR CHECKING NOT PROVIDEDFOR ELSEWHERE
BLASTING
CHECKING-DEVICES
COMBUSTION ENGINES
CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
ENGINE PLANTS IN GENERAL
GAS-TURBINE PLANTS
GENERATING RANDOM NUMBERS
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
LIGHTING
MACHINES OR ENGINES IN GENERAL
MECHANICAL ENGINEERING
NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES
PHYSICS
REGISTERING OR INDICATING THE WORKING OF MACHINES
STEAM ENGINES
TIME OR ATTENDANCE REGISTERS
VOTING OR LOTTERY APPARATUS
WEAPONS
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Summary:Systems and methods include a blade monitoring system. The blade monitoring system includes a processor. The processor is configured to receive a sensor signal from a sensor configured to observe a blade of the turbomachinery. The processor is also configured to derive a measurement based on a marking disposed on the blade of the turbomachinery, wherein the marking comprises a discrete feature; and to display the measurement to an operator of the turbomachinery
Bibliography:Application Number: US201816005588