| 1. | Intermediate pressure turbine
中压涡轮机 |
| 2. | Multi - pressure turbine
多压涡轮机 |
| 3. | Mixed pressure turbine
混压涡轮机 |
| 4. | Back pressure turbine
背压涡轮机 |
| 5. | Retrofit of 25 mw intermediate - pressure turbine and economic analysis of high - intermediate - pressure associate turbine
机组改造和与高压机组联合运行的经济性分析 |
| 6. | New and improved nickle - base , iron - nickle - cobalt - base superalloys were available for use in high - pressure turbine airfoils in aircraft gas turbines
新改进的镍基、铁镍钴基超耐热合金可用在飞机燃气轮中的高压透平机翼上。 |
| 7. | The long - term life and low cycle fatigue life of low pressure turbine blade for an aeroengine under real loading spectrum is analyzed by using this method
用该方法对某型发动机低压涡轮工作叶片在实际飞行载荷谱作用下的持久寿命和低循环疲劳寿命进行了分析。 |
| 8. | To investigate the aerodynamic design ideas and concrete methods of high performance low pressure turbine ( lpt ) at low reynolds number condition , a new lpt of high load , large chord and proper velocity distribution was designed
摘要为了探索高空低雷诺数情况下高性能低压涡轮部件的气动设计思路和设计方法，通过采用高负荷、大弦长的叶片设计和选择恰当的叶片表面速度分布形式设计了一台新低压涡轮。 |
| 9. | These variable geometry components include high pressure - compressor , high - pressure turbine , low - pressure turbine , inlet area ratio of mixer and main nozzle throat area . the results of calculation show that the adjusting of low - pressure turbine and mixer has a remarkable effect on the performance of engine and bypass ratio
计算结果表明，低压涡轮和混合器的调节对发动机的性能和涵道比的影响尤为显著；在其它部件几何结构不同时，单个部件几何调节后，发动机性能的变化趋势是不同的。 |
| 10. | A simplify high pressure turbine ( hpt ) tip clearance model is analyzed with the cyclic symmetry method . research on the flow , heat and structure integration analyses is achieved in this paper . flow / heat analysis is done by fluent software , and heat / structure analysis is done by ansys software
针对涡轮部件的结构特点,进行了适当的简化,利用参数化设计思想建立了涡轮叶尖间隙计算模型,用循环对称的方法分析了某型发动机高压涡轮叶尖间隙在工作过程中变化的情况。 |
