摘要
回顾并展望了燃气涡轮机在鱼雷动力推进系统中的应用与发展,分析了燃气涡轮机在鱼雷动力推进系统中的发展需要,基于对鱼雷燃气涡轮机动力系统的组成、原理和特点的认识,指出满足鱼雷要求的涡轮机类型一般是轴流式或重入式部分进气单级或复级冲动涡轮机,与航空燃气涡轮机作比较,其在结构、驱动目的、能源、冷却介质以及废气排放等方面有较大区别,与液体火箭发动机燃气涡轮泵比较,其在使用燃料、使用环境和工作方式等方面也有很大区别,最后对开展鱼雷燃气涡轮机的研究提出了几点建议。
The current development and application of gas turbine to torpedo power are reviewed and the developmental requirement is discussed. Analyzing the structure, princlple and feature of gas turbine, it is pointed out that the general type of gas turbine which meets torpedo＇s requirements are axial flow type or reentry type, single staged or muhiple velocity staged, impulse turbine with partial axial gas flow. There exists evident difference between aircraft and torpedo gas turbines with respect to struture, driving purpose, energy source, cooling medium and exhaust discharge, and there also exists apparent difference between gas turbines for liquid rocket and torpedo in regard to fuel, operational envirnment and mechanism. Some suggestions are proposed about torpedo gas turbine research.
出处
《鱼雷技术》
2006年第4期11-15,共5页
Torpedo Technology
