航改燃气轮机总体性能与排气装置的一体化设计  

Integrated Design of Aero-Derivative Gas Turbine and Exhaust System

作　　者：周亚峰[1] 谢业平[1] 李泳凡[1] 

机构地区：[1]沈阳发动机设计研究所,沈阳110015

出　　处：《航空发动机》2008年第1期7-9,45,共4页Aeroengine

摘　　要：分析了舰用航改燃气轮机的设计特点,提出了在总体性能设计中采用排气装置一体化设计技术的合理性;对某型舰用燃气轮机排气装置的一体化设计进行的理论分析表明:排气装置达到了一体化的设计目的,燃气轮机整体性能得到了最佳的性能匹配。The design features of the aero - derived marine gas turbine were analyzed and the rationality of integrated design technology of exhaust system adopted in the overall performance design was presented. The theoretical analysis of integrated design of a marine gas turbine exhaust system shows that the purpose of the integrated design of the exhaust system is achieved and the optimum performance matching is obtained in the gas turbine overall performance.

关 键 词：航改燃气轮机 性能计算 排气装置 引射器 

分 类 号：U664.131[交通运输工程—船舶及航道工程] TQ051.84[交通运输工程—船舶与海洋工程]