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局部内冷空气系统流体网络分析与数字化计算方法

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燃气轮机内冷空气系统结构、气路流动与运行工况极为复杂,造成了内冷空气系统流体计算难度很大,传统一维流体网络法的计算精度已经不能满足当代发动机分析与设计的需求,急需开发一种面向燃气轮机内冷空气系统的高精度、快速的系统级别的流体计算方法.本文面向某船用燃气轮机高压转子内冷空气系统的卸荷腔,创新性地利用一维-三维联合仿真计算方法,实现了快速求解流体网络节点信息的同时解析关键区域流动传热细节.研究结果表明,与传统一维流体网络法相比,一维-三维耦合计算可以通过边界数据传递与耦合计算提高整体计算精度,与传统CFD计算方法相比,一维-三维耦合计算可以加快计算收敛速度,以卸荷腔高压涡轮腔室为例,一维-三维联合仿真计算方法可以节约计算收敛时间约83%,同时三维流体计算域可以获得关键区域的流场细节,对系统级别计算下掌握关键区域流动特性具有重要意义.
Fluid Network Analysis and Digital Calculation Method for Local Internal Cold Air System
The structure,air path flow and operation conditions of the cold air system in the gas turbine are extremely complex,which makes it very difficult for fluid calculation of the cold air system in the gas turbine.The calculation accuracy of the traditional one-dimensional fluid network method can no longer meet the needs of contemporary engine analysis and design.It is urgent to develop a high precision and fast system level fluid calculation method for the cold air system in the gas turbine.Aiming at the unloading chamber of the cold air system in the high-pressure rotor of a Marine gas turbine,the one-dimensional and three-dimensional co-simulation method is innovatively adopted in this paper to quickly solve the node information of the fluid network and analyze the heat transfer details of the flow in key areas.The results show that compared with the traditional one-dimensional fluid network method,the one-dimensional-three-dimensional coupling calculation can improve the overall calculation accuracy through boundary data transfer and coupling calculation,and compared with the traditional CFD calculation method,the one-dimensional-three-dimensional coupling calculation can accelerate the convergence rate of the calculation.Taking the unloading chamber of high pressure turbine chamber as an example,the one-dimensional and three-dimensional co-simulation calculation method can save about 83%of the convergence time,and the three-dimensional fluid calculation domain can obtain the details of the flow field in the key region,which is of great significance for mastering the flow characteristics of the key region under the system level calculation.

Gas TurbineInternal Cold Air SystemUnloading ChamberFluid NetworkJoint Simulation

于柠宁、徐倩楠、张海

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哈尔滨工程大学

中国航发四川燃气涡轮研究院

燃气轮机 内冷空气系统 卸荷腔 流体网络 联合仿真

航空发动机及燃气轮机重大专项哈尔滨工程大学高水平科研引导专项

J2019-Ⅰ-0007-00073072022QBZ0302

2024

风机技术
沈阳豉风机研究所(有限公司)

风机技术

影响因子:0.643
ISSN:1006-8155
年,卷(期):2024.66(1)
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