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- The RE-aluminizing technique and coating structure of gas turbine blade made of alloy M38G are studied. 研究了渦輪葉片材料M38G合金滲稀土-鋁塗層的工藝過程和組織結構。
- By comparing data form the controllable calculating program and results of blowing tests,it offers a method to simulate the aerodynamic property of gas turbine blade. 介紹了採用可控擴壓計算程序計算的壓氣機葉片數據與吹風試驗結果的對照結論,提出採用可控擴壓方法設計的燃氣透平葉片的氣動性能可以通過程序計算模擬。
- The tool design and tool motion can take care of reaching surfaces such as blind cavities and pockets in walls.ECM is used for machining of gas turbine blades. 另外，電解加工與切削加工相結合（例如電解磨削，電解珩磨，電解研磨等），往往可以取得很好的加工效果。
- The no machining directional solidification hollow turbine blades, hollow guide vans and complex structure parts used in aero engine and gas turbine made by vacuum precision investment casting. 航空發動機、燃機等精鑄真空無餘量空心渦輪、導向葉片及複雜結構件。多種熱處理爐上用料盤,夾具等耐熱合金鋼精鑄件。
- The gas turbine feeds on the fuel it pumps. 燃氣輪機以它所抽入的燃料為能源。
- Local Heat Transfer Characteristics in "Impingement-Film" Cooling Style About Inner Side of Gas Turbine Blade 渦輪葉片內"衝擊-氣膜出流"局部換熱特性數值模擬
- First Chinese Instance Base for CAD System of Investment Casting Mould Used in Gas Turbine Blade Manufacture 渦輪葉片精鑄模具CAD系統實例庫的設計與研究
- The Interior Heat Transfer Characteristics of Gas Turbine Blade Due to Dense Film Cooling Holes 密集型氣膜出流內部冷氣側換熱特性實驗研究
- The Interior Heat Transfer Characteristics of Gas Turbine Blade Due to Sparse Film Cooling Holes 稀疏型氣膜出流內部冷氣側換熱特性實驗研究
- Wuxi Turbine Blade Works Co., Ltd. 無錫透平葉片有限公司。
- Research on Modeling Technologies of Aviation Gas Turbine Blades 航空燃氣渦輪葉片造型技術研究
- porous gas turbine blade 多孔燃氣渦輪葉片
- The blade of a gas turbine fractured and the unit stopped unnaturally in a refinery. 某煉化廠煙氣輪機一動葉片斷裂引起停機事故。
- Kawasima T,Iinuma H,Minagawa N.Optical Semiconductor Blade Vibration Monitoring System for Gas Turbine Engine[J]. 胡廣書.;數字信號處理之理論、演算法與實現[M]
- An Analysis of the Vibration Characteristics of a Gas Turbine Bladed Disc 燃氣輪機葉片輪盤振動特性分析
- KEY WORDS Anisotropic, Constitutive model, Viscoplastic, Turbine blade. 關鍵詞：正交異性，本構模型，粘塑性，渦輪葉片
- Effects of Platform Friction Damper on Resonant Stresses in Gas Turbine Blades 緣板摩擦阻尼器的減振實驗研究
- The process of blade root profile in gas turbine and revising calculation of profile of turning tool is discussed in detail in the paper. 就燃氣輪機葉片葉根齒形加工及所用車刀刀齒型線的修正計算做了詳細論述。
- Check no damage for fan blades and turbine blades. 檢查風扇葉片和渦輪葉片無損壞跡象。
- Using 3-D rigid-viscoplastic finite element method, the multi-stage forging process of a gas turbine compressor blade was simulated. 利用剛粘塑性有限元法,對某重型燃機壓氣機葉片的多工步鍛造過程進行了三維有限元模擬。
