鱼雷涡轮机减速系统设计新方法

朱允进; 钱志博; 武 雷

doi:10.11993/j.issn.1673-1948.2009.06.015

鱼雷涡轮机减速系统设计新方法

doi: 10.11993/j.issn.1673-1948.2009.06.015

西北工业大学航海学院, 陕西西安, 710072

详细信息

作者简介:
朱允进(1982-)，男，在读硕士，主要研究方向为水下动力推进技术

中图分类号: TJ630.32
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- 被引次数: 0
出版历程
- 收稿日期: 2008-05-31
- 修回日期: 2009-08-17
- 刊出日期: 2009-12-30

A New Design Method of Deceleration System for Torpedo Turbines

College of Marine Engineering, Northwestern Polytechnical University, Xi′an 710072, China

摘要

摘要: 针对以往鱼雷涡轮机减速系统设计中的不足，根据鱼雷涡轮发动机的工作特性，确定减速系统传动类型和传动级数，推导出齿轮体积与传动比之间的数学模型，运用结构参数与空间布局耦合的新方法，建立了多级齿轮传动系统的空间布局优化数学模型，采用非支配排序遗传算法-II(NSGA-II)完成了空间布局方案的优化设计，在满足约束条件的情况下，得到了齿轮系统结构参数和空间布局坐标。计算结果表明，该方法在减速系统设计中具有很好的工程应用价值。
- 鱼雷 /
- 减速系统 /
- 非支配排序遗传算法-II(NSGA-II) /
- 齿轮优化 /
- 结构设计 /
- 布局设计
Abstract: In order to overcome the shortcomings in conventional design of deceleration system of torpedo turbine, the drive type and drive series of deceleration system are determined, and a mathematical model is deducted to describe the relation between gear volume and speed ratio according to the operational characteristic of a certain type of torpedo turbine engine. By using a new method of coupling structural parameters and space layout, a space layout optimization model of a multi-gear drive system is established, and optimization design of space layout is completed by using the non-dominated sorted genetic algorithm-II(NSGA-II). Structural parameters and space layout coordinates of a gear system are obtained under the restrictive conditions. Calculation results show that the proposed method applicable for deceleration system design of torpedo turbines.
- torpedo /
- deceleration system /
- non-dominated sorted genetic algorithm-II(NSGA-II) /
- gear optimization /
- structure design /
- layout design

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参考文献(6)

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