Real-time Blade Tip Timing (BTT) in rotating machinery enables condition-based maintenance and blade failure prevention. In this paper, we propose a new 6 GHz microwave sensing system suitable for BTT in gas and steam turbines. The system working principle is similar to the short range radar technique, using probes mounted in the turbine wall, in direct view of the passing blades. The front end of the system consists of a miniature open-ended coaxial resonator sealed by a ceramic cap. Its principle of operation is simple and robust, thus well-suited for the turbine harsh environment, while the radiated TEM mode allows for insensitivity to mounting orientation. The probe was validated through simulation and prototypes were successfully teste...
Turbine blades suffer vibrations when they rotate inside a turbo machine. The measurement of those v...
Deterioration of rotor blades due to foreign object damage (FOD), erosion by sand/water, low cycle f...
Key Technology Features: a) First stage turbine environment (1300 C+ gas path using bleed air coolin...
Blade tip timing is an effective method for blade vibration measurements in turbomachinery. This met...
Real time tip clearance measurement in gas turbines and other rotating machinery is an interesting w...
The development of new active tip clearance control and structural health monitoring schemes in turb...
One of the crucial issues regarding turbine maintenance is registering blade vibrations. These vibra...
The ability to monitor the structural health of the rotating components, especially in the hot secti...
The paper describes in detail a Tip-Timing measurement on a combined cycle power plant with a steam ...
Due to its non-intrusive manner, blade tip timing (BTT) is considered a potential tool for the condi...
In order to increase efficiency and reliability of steam turbines, last stage blades are equipped wi...
To effectively monitor the vibration of blades in a rotating machine, a non-contacting method cal...
The advent of tip-timing systems makes it possible to assess turbomachinery blade vibration using no...
The accurate control of running gaps between static and rotating components is vital to preserve mec...
Gas turbine efficiency can be improved with tighter turbine tip clearances. An approach being develo...
Turbine blades suffer vibrations when they rotate inside a turbo machine. The measurement of those v...
Deterioration of rotor blades due to foreign object damage (FOD), erosion by sand/water, low cycle f...
Key Technology Features: a) First stage turbine environment (1300 C+ gas path using bleed air coolin...
Blade tip timing is an effective method for blade vibration measurements in turbomachinery. This met...
Real time tip clearance measurement in gas turbines and other rotating machinery is an interesting w...
The development of new active tip clearance control and structural health monitoring schemes in turb...
One of the crucial issues regarding turbine maintenance is registering blade vibrations. These vibra...
The ability to monitor the structural health of the rotating components, especially in the hot secti...
The paper describes in detail a Tip-Timing measurement on a combined cycle power plant with a steam ...
Due to its non-intrusive manner, blade tip timing (BTT) is considered a potential tool for the condi...
In order to increase efficiency and reliability of steam turbines, last stage blades are equipped wi...
To effectively monitor the vibration of blades in a rotating machine, a non-contacting method cal...
The advent of tip-timing systems makes it possible to assess turbomachinery blade vibration using no...
The accurate control of running gaps between static and rotating components is vital to preserve mec...
Gas turbine efficiency can be improved with tighter turbine tip clearances. An approach being develo...
Turbine blades suffer vibrations when they rotate inside a turbo machine. The measurement of those v...
Deterioration of rotor blades due to foreign object damage (FOD), erosion by sand/water, low cycle f...
Key Technology Features: a) First stage turbine environment (1300 C+ gas path using bleed air coolin...