Turbine Blade of Gas Turbine Engine Additional Unloading by Changing the Layout of the Gravity Centre of the Shroud Shelf

Ozoliņš, Ēriks; Ozoliņš, Ilmārs; Ramana, L

doi:10.2478/tae-2019-0002

Cited by 1 publication

(1 citation statement)

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“…When compressor stator blades with attached structures are subjected to an excitation force, the adjacent working faces will slide relatively, and the resulting friction will consume vibration energy and thus affect vibration characteristics [5]. Therefore, the nonlinear characteristics of the contact surface will significantly affect the vibration response behavior of the stator blade, and tests show that this dry friction damping is related to a variety of factors [6].…”

Section: Introductionmentioning

confidence: 99%

Numerical Study on Vibration Response of Compressor Stator Blade Considering Contact Friction of Holding Ring

Liu

Zhang

et al. 2023

Applied Sciences

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There are many kinds of assembly structures in heavy-duty gas turbine compressor stator blades which have significant influence on the complex damping vibration characteristics. At present, compressor design is becoming more and more compact, so it is very meaningful to accurately obtain stator blade vibration characteristics of structures with contact damping. Firstly, a fretting slip friction dynamic model was introduced, and then a vibration analysis model of the compressor stator blade with outer ring structure was established based on the slip friction theory. Then, the vibration response of the compressor stator blade was obtained according to various working conditions, and the main factors affecting the vibration characteristics of the stator blade were revealed. Finally, the vibration response of the blade under a particular exciting force condition was simulated. The results show that the damping vibration characteristics of the compressor stator blades were affected by the excitation force and the normal load of the contact surface. The vibration response curve of the stator blade and the equivalent stiffness coefficient of the contact surface were analyzed, and the friction motion of the contact surface changed with the change of the working condition. The model can simulate the nonlinear vibration characteristics of stator blades. This method provides a reference for the vibration safety analysis of compressor stator blades.

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Section: Introductionmentioning

confidence: 99%