ROUGHNESS INVESTIGATIONS ON IN-SERVICE HIGH-PRESSURE COMPRESSOR BLADES - PART I: AN AUTOMATED PROCESS FOR HIGH-FIDELITY ROUGHNESS MEASUREMENTS

被引:0
作者
Vasilopoulos, Ilias [1 ]
Rostamian, Mirco [2 ]
Voigt, Matthias [1 ]
Meyer, Marcus [2 ]
Mailach, Ronald [1 ]
机构
[1] Tech Univ Dresden, Chair Turbomachinery & Flight Prop, D-01062 Dresden, Germany
[2] Rolls Royce Deutschland Ltd & Co KG, D-15827 Blankenfelde Mahlow, Germany
来源
PROCEEDINGS OF ASME TURBO EXPO 2023: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, GT2023, VOL 13C | 2023年
关键词
Surface roughness; optical metrology; compressor blades; SURFACE-ROUGHNESS;
D O I
暂无
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The two-part publication deals with roughness investigations on in-service high-pressure compressor (HPC) blades, both in terms of measurements and simulations. In this paper (Part I), an automated process for performing detailed surface roughness measurements of the blades has been developed. Specifically, a highly accurate Alicona sensor (20x lens; capable of capturing roughness values down to 0.1 mu m) was combined with a pick-and-place robotic arm, and the system was trained to conduct roughness measurements on all the different rotor blades of a 10-stage HPC. First, the Alicona measuring device is validated against a NanoFocus device of similar accuracy. Then, a detailed measurement of the roughness on the suction and pressure side of Rotor 2 is demonstrated, using a 100-point grid. This process is further accelerated by using a reduced number of measuring points. The location of those points has been determined by numerical optimization that aims at minimizing the error between an RBF-based approximation model and the detailed measured roughness distribution. Finally, a summary of the roughness measurements through the entire HPC is given (rotors only; before and after cleaning of the blades at an ultrasonic bath) and the paper ends with a discussion of the results.
引用
收藏
页数:11
相关论文
共 23 条
  • [11] Influence of combined compressor and turbine deterioration on the overall performance of a jet engine using RANS simulation and Pseudo Bond Graph approach
    Goeing, Jan
    Seehausen, Hendrik
    Pak, Vladislav
    Lueck, Sebastian
    Seume, Joerg R.
    Friedrichs, Jens
    [J]. JOURNAL OF THE GLOBAL POWER AND PROPULSION SOCIETY, 2020, 4
  • [12] Turbine blade surface deterioration by erosion
    Hamed, AA
    Tabakoff, W
    Rivir, RB
    Das, K
    Arora, P
    [J]. JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2005, 127 (03): : 445 - 452
  • [13] Klein M., GT2022-82113
  • [14] Leach RK, 2010, FUNDAMENTAL PRINCIPLES OF ENGINEERING NANOMETROLOGY, P1
  • [15] Millsaps K.T., ASME TURBO EXPO 2004
  • [16] nanofocus, NanoFocus surf custom
  • [17] Schluter L., ASME TURBO EXPO
  • [18] Sun H., GT2019-90784
  • [19] Syverud E, 2006, PROCEEDINGS OF THE ASME TURBO EXPO 2006, VOL 5, PTS A AND B, P491
  • [20] SURFACE-ROUGHNESS MEASUREMENTS ON GAS-TURBINE BLADES
    TAYLOR, RP
    [J]. JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 1990, 112 (02): : 175 - 180