pressure turbine
英 [ˈpreʃə(r) ˈtɜːbaɪn]
美 [ˈpreʃər ˈtɜːrbaɪn]
网络 反唤水轮机; 反动轮机; 高压涡轮机
双语例句
- The blade tip crack of the high pressure turbine is repaired by using the laser welding, which can reduce effectively the repair cost and increase the economic effectiveness of the engine repair.
采用激光熔焊方法，修复了高压涡轮工作叶片叶尖裂纹，有效降低了发动机修理成本，提高了发动机修理的经济效益。 - Dynamic performance analysis of low pressure turbine ( LPT) component with damping-sleeves
带阻尼套筒的某型发动机低压涡轮部件的动力特性分析 - The high pressure turbine tip clearance variation versus time under different operating conditions were analyzed by the finite element method.
利用有限元分析软件分析了某型高压涡轮叶顶间隙在不同工况下随时间的变化。 - Low pressure turbine oil electrohydraulic control system;
低压透平油电液控制系统； - The forming technology of skin-cooling high pressure turbine was analyzed, introduced polyurethane bulging die structure design and the working process and die debugging improvement.
分析了高压涡轮冷却外壳的成形工艺，并介绍了聚氨酯胀形模的结构设计和模具工作过程以及模具调试改进。 - At present heat rate calculate of the double back pressure turbine is according to single back pressure turbine, which brings deviation of heat rate calculate.
目前双背压汽轮机是按单背压汽轮机来进行热耗率计算的，由此带来热耗率计算的偏差。 - Large eddy simulation of separated flow transition on a highly-loaded low pressure turbine profile Mechanism of the Interaction between Plateau Vortex and Southwest Vortex During a Heavy Rain Event
大负荷低压涡轮叶型分离转捩流动的大涡模拟一次大暴雨过程中高原低涡与西南低涡相互作用机制探讨 - In turbofan engine's design, the structure with a large meridional expansion was used between HP and LP turbine, and this structure has brought the difficulty for the low pressure turbine design.
在涡扇发动机的设计中，高低压涡轮过渡段处多采用较大子午扩张的结构，此结构给低压涡轮设计带来了难度。 - The flow field in low pressure turbine guide vane was simulated by third order accuracy Godunov scheme with TVD property.
求解了某型航空发动机的低压涡轮导向器内流场。 - The characteristics of turbulent flow in a high pressure turbine cascade were investigated experimentally.
本文对一种高压涡轮导向叶栅中的紊流特性进行了实验研究。 - Casting Process Design and Manufacture for Nozzle Chest Casting of Super-critical Pressure Turbine
超超临界汽轮机喷嘴室铸造工艺设计及其生产 - Turbine driven centrifugal compressor Large eddy simulation of separated flow transition on a highly-loaded low pressure turbine profile
涡轮机驱动离心压缩机大负荷低压涡轮叶型分离转捩流动的大涡模拟 - The secondary flow loss plays a main part in the total loss of high pressure turbine's ( HPT).
叶顶间隙二次流在高压涡轮总损失中占据了较大比重。 - The thermal-elastic stress analysis of high pressure turbine plate
高压涡轮盘的热弹性应力分析 - Experimental Investigation on the Sector Cascade of High Pressure Turbine Guide
高压涡轮导向器扇形叶栅试验研究 - A piece of the first class high pressure turbine guide-vane fractured in exhaust edge after the engine test.
某发动机试车后，检查发现一片高压涡轮导向叶片排气边掉块。 - Repairing Technology of High Pressure Turbine Blade Tip Crack for an Aero-Engine
某型发动机高压涡轮叶片叶尖裂纹修复工艺研究 - Here an example is: heating the feedwater of condensing turbine by exhaust steam of a back pressure turbine ( through tubular steam cooler) to raise the set's heat economy.
介绍一例：利用管式蒸汽冷却器将背压机排汽加热凝汽机给水，从而提高机组热经济性。 - Application of recovery of low temperature potential energy capacity and ultra-low pressure turbine in oxidation progress are described.
详述氧化工序低温位能量回收和超低压透平应用。 - The over-limit and visual cracks occurred in an aero-engine high pressure turbine blade tip were repaired using laser welding.
采用激光熔焊法，排除了某型发动机高压涡轮工作叶片叶尖裂纹超标及开口型叶尖裂纹故障。 - 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。 - Experimental Study of High Pressure Turbine Cascade Trailing Edge Loss
高压涡轮叶栅尾缘损失的试验研究 - Investigation of aerodynamic design of low pressure turbine at low reynolds number conditions
低雷诺数环境中低压涡轮部件的气动设计探索 - Taking the low pressure turbine outlet temperature T4 smart sensor as the object, simulations have been done.
以涡轮后燃气温度T4智能传感器为研究对象，进行了分布式统计判决仿真，并与最优中心决策以及最优似然比决策作了对比分析。 - Flow Field Analysis of High Pressure Turbine Stage with Cooling Flows
带冷气影响的某高压涡轮级流场分析 - In addition, the paper also analyzes the performance on the change of exhaust steam pressure of the back pressure turbine and the different heat supply temperature in the integrated system.
此外，论文还分析了背压汽机排汽压力及供暖温度变化时，一体化系统的性能情况。 - Finally, two difficult problems in optimization design are analyzed in this paper. The two problems are the optimization design of high load low pressure turbine and the optimization design under multiple work conditions.
最后，本文分析了优化设计中的两个难点问题，它们分别是高负荷低压涡轮的优化设计和多工况优化设计。 - Low pressure turbine is an important component of the aero-engine, and the multi-stage low pressure turbine integrates advanced aerodynamics and mechanical features.
低压涡轮是航空发动机的重要组成部分，多级的低压涡轮融汇了先进的空气动力学和机械设计特性。 - The results show that reheat cycle has much higher specific work than new cycle without reheat. Thermal efficiency of new cycle with reheat can be improved when total pressure ratio is big and low pressure turbine inlet temperature is high.
结果显示：与无再热新循环相比，再热使循环比功得到大幅提高；而再热循环热效率在低压透平入口温度较高，总压比较大时可得到较大幅度地提高。