Experimental measurements of out-of-plane vibrations of a simple blisk design using Blade Tip Timing and Scanning LDV measurement methods

• Published in: Mechanical systems and signal processing Vol. 28; pp. 517 - 527
• Main Authors: Di Maio, D., Ewins, D.J.
• Format: Journal Article
• Language: English
• Published: Kidlington Elsevier Ltd 01.04.2012; Elsevier
• Subjects: Applied sciences; Blade Tip Timing; Blades; Continuous cycle engines: steam and gas turbines, jet engines; Design engineering; Discs; Disks; Dynamics; Engines and turbines; Exact sciences and technology; Forced response; Fundamental areas of phenomenology (including applications); Industrial metrology. Testing; Measurement and testing methods; Mechanical engineering. Machine design; Physics; Rotating; Scanning; Solid mechanics; Structural and continuum mechanics; Tacking Scanning LDV; Vibration; Vibration, mechanical wave, dynamic stability (aeroelasticity, vibration control...); Forced response; Tacking Scanning LDV; Blade Tip Timing; Blades; Forced vibration; Turbojet; Laser Doppler velocimeters; Vibration measurement; Vibration test; Experimental study; Modeling; Vibrometer; Aerospace industry; Operating conditions; Laser dopplerometry; Rotating disk; Turbine blade; Aircraft
• ISSN: 0888-3270; 1096-1216
• DOI: 10.1016/j.ymssp.2011.09.018

The study of dynamic properties of rotating structures, such as bladed discs, can be conveniently done using simple bladed discs where the blades do not have staggering angles. Simplified design, although not truly representative of real structures, can be easy and economic to manufacture and, still, very helpful for studying specific dynamic properties. An example of this can be called as mass mistune blisk study. Experimental measurements of vibrations of bladed discs under rotating conditions can be performed using Scanning Laser Doppler Vibrometer (SLDV) systems. However, in the aerospace industry, the vibrations of complex bladed discs must be measured under operating conditions which are more hostile than laboratory simulations. The Blade Tip Timing (BTT) measurement method is a measurement technique, which can be used to measure vibrations of bladed discs of an engine aircraft under operating conditions. However, the BTT technique is ineffective when used with a flat bladed disc whose blade vibrations cannot be measured. This can be detrimental when the use of controlled dynamic parameters, such as those obtained from a simple bladed disc design, can improve the confidence for the validation of post-processing software. This paper presents a work about experimental measurements of a simple bladed disc design whose vibrations were measured synchronously by Scanning LDV and BTT measurement systems. A rotating test rig and its mechanical modifications for the installation of the BTT probes are introduced. Implications of rotating a specimen inconsistently are presented so as solutions to obtained constant revolving speed. The experimental comparisons of forced response vibrations measured synchronously at one blade are presented and explained. ► Rotating test rig design for BTT measurements. ► Problems of rotational speed oscillations in BTT measurements. ► Modification of a bladed disc design for BTT measurements. ► Comparison of measurement results using BTT and SLDV systems.