| 1. | The non - design condition parameters of torpedo turbine engine were also analyzed
对鱼雷处于非设计工况时的参数进行了分析。 |
| 2. | In the paper , the structure type of torpedo turbine engine and the three - speed system states of work gas were researched . the work process of torpedo turbine engine was analyzed
本文对鱼雷涡轮机结构类型、鱼雷涡轮机的三速制工况进行了计算研究，对涡轮发动机的工作过程进行了分析。 |
| 3. | In simulation theory terms , torpedo turbine engine system is a complicated system . especially at non - design condition , the works of matching and controlling inner parameters of system is more difficult
鱼雷涡轮发动机属于复杂系统，特别是变工况条件下，系统各参数的匹配与控制则更为复杂。 |
| 4. | This paper is based on the theory of engineering thermodynamics . the research object is unclosed - cycle - form partial - flow two - stage impulse torpedo turbine . first we study the design condition of torpedo turbine
本文以工程热力学为理论基础，以鱼雷开式循环部分进气纯冲动式复速级涡轮发动机为研究对象。 |
| 5. | Simulator curves and programs will work well in the design of torpedo turbine propulsion system and have important reference value in the design and simulation of whole torpedo
相信得到的仿真曲线和仿真程序在鱼雷涡轮动力装置的设计过程中发挥良好的作用，并在未来鱼雷总体设计、仿真中同样具有重要的参考价值。 |
| 6. | Based on the theory of engineering thermodynamics , inner parameter and thermodynamic calculation mathematic model of turbine engine were established . the thermodynamic calculation and the structure design of torpedo turbine engine were completed at the same time
以工程热力学为基础，建立了涡轮机内部参数和热力计算的数学模型，并对鱼雷涡轮机的各个部分进行了热力计算和结构设计计算。 |
| 7. | The precondition of establishing mathematics model of torpedo turbine system in design condition is to fulfill the external conditions ( such as torpedo sailing speed and depth etc . ) and inner conditions ( such as turbine power and efficiency etc . ) . after establishing mathematics model of torpedo turbine system in design condition , we compiled simulation program to compute all kinds of inner parameters of turbine engine include engine type , principal layout of turbine , inner structure of turbine and state parameters of gases
首先分析设计工况时涡轮机动力系统，在满足鱼雷动力系统的各项外部条件(如鱼雷航深、航速等)和内部条件(如涡轮机功率、效率，燃烧室压力、温度，转子机械强度等)的前提下，建立起设计工况涡轮发动机的数学模型，编程计算并确定涡轮机内部机械结构和燃气热力学状态各参数。 |
