TROUBLESHOOT KERUSAKAN BLADE HIGH PRESSURE COMPRESSOR ENGINE CFM56-7B

FAUNJI, AHMAD (2019) TROUBLESHOOT KERUSAKAN BLADE HIGH PRESSURE COMPRESSOR ENGINE CFM56-7B. Tugas Akhir thesis, Institut Teknologi Dirgantara Adisutjipto.

[img] Text (ABSTRAK)
16060023_ABSTRAK.pdf

Download (184kB)
[img] Text (BAB I)
16060023_BAB I.pdf

Download (100kB)
[img] Text (DAFTAR PUSTAKA)
16060023_DAFTAR PUSTAKA.pdf

Download (50kB)
[img] Text (FULL SKRIPSI)
16060023.pdf
Restricted to Repository staff only

Download (2MB)

Abstract

High Pressure Compressor (HPC) is an important component of the engine, because to increase the air pressure that will go into the combustion. However, this component has a problem, that is damage in the blade. The purpose of this study is to know what damage in the blade high pressure compressor along with the causes and how to resolve them. The way to find out the damage that is on the HPC blade by means of borescope inspection. Then the process of measuring the damage found and obtained a nick of 0.03 inch (0.76 mm) and missing material of 0.03 inch (0.94 mm). Based on the engine shop manual (ESM) Task 72-31-03-300-001, blades that are damaged can still be repaired by the blending method. The final nick result after blending is 0.03 inch (1 mm) and missing material is 0.05 inch (1.3 mm) and still within its limits. The next process is balancing to balance the high pressure compressor rotor blade and after the balancing process is complete it is declared serviceable

Item Type: Thesis (Tugas Akhir)
Subjects: T Technology > T Technology (General)
Divisions: Institut Teknologi Dirgantara Adisujtipto > D3 Aeronaitika
Depositing User: Mr AHMAD FAUNJI
Date Deposited: 04 Jul 2024 07:17
Last Modified: 04 Jul 2024 07:17
URI: http://eprints.stta.ac.id/id/eprint/2177

Actions (login required)

View Item View Item

Downloads

Downloads per month over past year