Design and Verification of Multi-Step Blade Tip Clearance Control System for Large Gas Turbine Using Hydraulic Pressure
In the gas turbine, the clearance between the blade tip of the rotor and the inside of the stationary casing varies depending on the rotation of the rotor and the heat output of the combustor. Accordingly, the assembly clearance is determined, and the leakage of the gas occurs because of the gap dur...
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| Principais autores: | , , , |
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| Formato: | Artigo |
| Idioma: | Inglês |
| Publicado: |
Korean Society for Precision Engineering
2020-05-01
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| Series: | 한국정밀공학회지 |
| Assuntos: | |
| Acceso en liña: | http://www.jkspe.or.kr/upload/pdf/NODE09331199.pdf |
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