ANALISIS PENGARUH ROTOR CLEARANCE PADA HIGH PRESSURE COMPRESSOR DAN HIGH PRESSURE TURBINE TERHADAP PENURUNAN EXHAUST GAS TEMPERATURE MARGIN PADA MESIN CFM56-3C1
DOI:
https://doi.org/10.22441/jtm.v12i2.16716Keywords:
Rotor clearence, Exhaust Gas Temperatur Margin, CFM56-3C1Abstract
The aircraft engine shall always be checked for performance by paying attention to engine parameters and performes maintenance to maintain the condition of the aircraft. The most important parameter of the engine is Exhaust Gas Temperature Margin (EGTM) which is the difference between the maximum temperature limit on the mesin and the actual temperature read at the time of take-off. On the CFM56-3C1 engine with serial number 856745, a test was carried out to determine the condition of the engine's performance, the results showed that the engine has an EGT Margin -10.9 °C and has decreased by 26.2 °C from the last engine repair. From the results, it is necessary to improve the performance of the EGT Margin engine by carrying out improvements to the workscope performance level, namely improvements to the clearance or distance between the rotor on the High pressure Compressor and the compressor case and the distance of the rotor on the High Pressure Turbine with the turbine shroud/stator which can cause a decrease in the value EGT Margin or called EGT Effect. EGT Effect calculation needs to be done to find out how big the contribution of the rotor clearance mismatch on HPC and HPT to the decrease in EGT value. The Margin affected by rotor clearance can be calculated from the actual clearance measurement minus the maximum clearance size that the factory has set and multiplied by the EGT Effect value per mils/microinch of each stage. From these calculations, we can identify the correlation of how much clearance Effect has on the EGT Margin deterioration. From the calculation, the decrease in EGT Margin value on HPT is 7.4332 °C and the decrease in EGT Margin value on HPC is 7.792785 °C with a total decrease in EGT Margin value due to clearance on HPC and HPT is 15.225985 °C or contributes 58.1 % of the decrease in the value of EGT Margin since the last mesin repair.Downloads
References
Darga, W. S. (2021, August 2). Analisis Pengaruh High pressure Compressor Rotor Clearance. Jurnal Teknologi Kedirgantaraan. Dipetik April 12, 2022
David Aubuchon, J. C. (2016). CFM56-3 Turbofan Mesin. Seneca College.
Mainil, A. K. (2011). Analisa Kinerja Mesin Turbofan Cfm56-3. Universitas Bengkulu. Dipetik April 12, 2022.
Muhammad Takdir, M. J. (2013). Analisis Pengaruh Compressor Wash Terhadap Egt. STT Adisutjipto Yogyakarta.
Pramono, A. (2010). Analisis Fatique Life Cycle Pada High Pressure Turbine Nozzle Terhadap Exhaust Gas Temperature Mesin CFM56-3. Transmisi, 6(1), 539-548.
Hadi, S., Bakar, A., & Virdhawati, D. M. Evaluasi Validitas Rumus Performa Kompresor Mesin CFM56-3C PT. G Berdasarkan Data Test Cell. Jurnal Industri Elektro dan Penerbangan, 5(3).
Peng, H. B., Dan, M., & Qu, H. C. (2011). Research of Aero-Mesin Life Prediction Based on Take-Off EGTM. In Applied Mechanics and Materials (Vol. 99, pp. 286-292). Trans Tech Publications Ltd.
Pandu Darmadi, S. (2010, Oktober 15). Pengembangan Metode Optimasi Interval Perawatan Mesin CFM56-3.
Darmansah, D. (2022, Februari). Analisis Pengaruh Hpc Clearance, Hpt Clearance, Dan Hpt Nozzle Throat Area.
Nur, F. M. (2017, September 27). Analisis Degradasi EGT Margin, Mesin CFM56-3, Boeing 737-300, Boeing 737-400, Boeing 737-500.
H. Balaghi Enalou. (2018). Performance Improvement Of The CFM56-3 Aircraft Engine By Electric Power Transfer.
A., A. S. (t.thn). Pengujian Vibrasi Pada Test Cell Turbofan Engine Type Cfm 56-7b. Politeknik Negeri Semarang.
Anggoro, P. Y. (2016). Studi Perhitungan Efektivitas Derate Thrust Engine CFM56-5B Pada Pesawat Airbus A320-200.
Effiom, S. O. (2018). Off-wing fleet maintenance study of a CFM56-3B turbofan engine: the propulsive engine of Boeing 737-300 civil aircraft. Vol. 13 No. 1 (2018).
Pereira, B. C. (2015). Numerical analysis of Flow around a fan blade of a CFM56-3. Engenharia Aeronautica.
Yafid Effendi, J. (2020). Analisis Aliran Udara Fan Blade Pada Mesin CFM56-7B Boeing 737-800NG Dengan Computational Fluid Dynamic (Cfd). Vol 4, No 1 (2020).
Ridaura, J. A. R. (2014). Correlation analysis between HPC blade chord and
compressor efficiency for the CFM56-3. Tecnico Lisboa.
CFMI. (2021, December). Mesin Shop Manual CFM56-3. Mycfmportal.com. Dipetik April 12, 2022.
CFMI. (2018). Workscope Planning Guide.
CFMI. (1993). CFM56-3 Basic Mesin Training Manual. Cincinati, Ohio: CFMI. Dipetik April 12, 2022.
Rolls-Royce. (1996). The Jet Mesin. Derby: Rolls-Royce. Dipetik April 12, 2022
Downloads
Published
How to Cite
Issue
Section
License
The copyright to this article is transferred to Universitas Mercu Buana (UMB) if and when the article is accepted for publication. The undersigned hereby transfers any and all rights in and to the paper including without limitation all copyrights to UMB. The undersigned hereby represents and warrants that the paper is original and that he/she is the author of the paper, except for material that is clearly identified as to its original source, with permission notices from the copyright owners where required. The undersigned represents that he/she has the power and authority to make and execute this assignment.
We declare that:
1. This paper has not been published in the same form elsewhere.
2. It will not be submitted anywhere else for publication prior to acceptance/rejection by this Journal.
3. A copyright permission is obtained for materials published elsewhere and which require this permission for reproduction.
Furthermore, I/We hereby transfer the unlimited rights of publication of the above mentioned paper in whole to UMB. The copyright transfer covers the exclusive right to reproduce and distribute the article, including reprints, translations, photographic reproductions, microform, electronic form (offline, online) or any other reproductions of similar nature.
The corresponding author signs for and accepts responsibility for releasing this material on behalf of any and all co-authors. This agreement is to be signed by at least one of the authors who have obtained the assent of the co-author(s) where applicable. After submission of this agreement signed by the corresponding author, changes of authorship or in the order of the authors listed will not be accepted.
Retained Rights/Terms and Conditions
1. Authors retain all proprietary rights in any process, procedure, or article of manufacture described in the Work.
2. Authors may reproduce or authorize others to reproduce the Work or derivative works for the authors personal use or for company use, provided that the source and the UMB copyright notice are indicated, the copies are not used in any way that implies UMB endorsement of a product or service of any employer, and the copies themselves are not offered for sale.
3. Although authors are permitted to re-use all or portions of the Work in other works, this does not include granting third-party requests for reprinting, republishing, or other types of re-use.
This work is also licensed under a Creative Commons Attribution-NonCommercial 4.0 International License.









