IGTC-96 EVALUATION OF ABRADABLE TURBINE SEAL BY FRICTION-WEAR TEST AND ENGINE PERFORMANCE TEST(Session C-4 Material and Manufacturing I)
スポンサーリンク
概要
- 論文の詳細を見る
Friction-wear test at room temperature under simulated rub conditions and engine performance test have been done on candidate materials considered for use as abradable turbine seals in a small gas turbine engine. Wear ratio, radial load curve and rub debris size obtained from the friction-wear test have been the important factors to select the seal material. Selected seal materials have been confirmed to improve the turbine efficiency due to the minimized blade tip wear and tip clearance.
- 公益社団法人日本ガスタービン学会の論文
著者
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Nishiyama Y.
Material Research Laboratory Technical Institute Kawasaki Heavy Industries Ltd.
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Nakamura T.
Material Research Laboratory, Technical Institute, Kawasaki Heavy Industries, LTD.
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Hirakawa H.
Jet Engine Division, Kawasaki Heavy Industries, LTD.
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Wasada N.
Jet Engine Division, Kawasaki Heavy Industries, LTD.
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Wasada N.
Jet Engine Division Kawasaki Heavy Industries Ltd.
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Hirakawa H.
Jet Engine Division Kawasaki Heavy Industries Ltd.
関連論文
- IGTC-96 EVALUATION OF ABRADABLE TURBINE SEAL BY FRICTION-WEAR TEST AND ENGINE PERFORMANCE TEST
- IGTC-96 EVALUATION OF ABRADABLE TURBINE SEAL BY FRICTION-WEAR TEST AND ENGINE PERFORMANCE TEST(Session C-4 Material and Manufacturing I)