Analysis of Rotating Cooling Effects with Oil for Turbine Blade

Jiang Qin; Hong Chuang Sun; Xin Yang Bai; Gong Nan Xie; Jie Cai Han

doi:10.13675/j.cnki.tjjs.2017.02.019

Analysis of Rotating Cooling Effects with Oil for Turbine Blade

Jiang Qin, Hong Chuang Sun, Xin Yang Bai, Gong Nan Xie, Jie Cai Han

School of Marine Science and Technology

Harbin Institute of Technology

Research output: Contribution to journal › Article › peer-review

Abstract

The air turbine can be used to solve the problems of fuel and power supply for Scramjet. The main obstacle is the cooling measure of turbine blades under limited cooling source. In this article, a new scheme was proposed to cool the blades with fuel used as coolant. Based on this oil cooling scheme, a three dimensional model was established to evaluate the feasibility and study heat transfer under rotation by numerical simulation. The results show that oil cooling scheme can efficiently reduce the temperature of blade with few negative effects on the performance of turbine. The temperature of blade can decrease greatly with the fuel mass flow rate of 1g/s. The maximum pressure of the coolant in the cooling channel can reach 114.5MPa in the rotating condition. Rotation effect enhances the turbulence intensity in the cooling channel and strengthens heat convection between the blade and fuel.

Original language	English
Pages (from-to)	399-407
Number of pages	9
Journal	Tuijin Jishu/Journal of Propulsion Technology
Volume	38
Issue number	2
DOIs	https://doi.org/10.13675/j.cnki.tjjs.2017.02.019
State	Published - 1 Feb 2017

Keywords

Fuel cooling
Numerical simulation
Rotating cooling
Turbine blade

Access to Document

10.13675/j.cnki.tjjs.2017.02.019

Cite this

@article{5a33497ea5f34b1e9e8b378aa6b15dbb,

title = "Analysis of Rotating Cooling Effects with Oil for Turbine Blade",

abstract = "The air turbine can be used to solve the problems of fuel and power supply for Scramjet. The main obstacle is the cooling measure of turbine blades under limited cooling source. In this article, a new scheme was proposed to cool the blades with fuel used as coolant. Based on this oil cooling scheme, a three dimensional model was established to evaluate the feasibility and study heat transfer under rotation by numerical simulation. The results show that oil cooling scheme can efficiently reduce the temperature of blade with few negative effects on the performance of turbine. The temperature of blade can decrease greatly with the fuel mass flow rate of 1g/s. The maximum pressure of the coolant in the cooling channel can reach 114.5MPa in the rotating condition. Rotation effect enhances the turbulence intensity in the cooling channel and strengthens heat convection between the blade and fuel.",

keywords = "Fuel cooling, Numerical simulation, Rotating cooling, Turbine blade",

author = "Jiang Qin and Sun, {Hong Chuang} and Bai, {Xin Yang} and Xie, {Gong Nan} and Han, {Jie Cai}",

year = "2017",

month = feb,

day = "1",

doi = "10.13675/j.cnki.tjjs.2017.02.019",

language = "英语",

volume = "38",

pages = "399--407",

journal = "Tuijin Jishu/Journal of Propulsion Technology",

issn = "1001-4055",

publisher = "Journal of Propulsion Technology",

number = "2",

}

TY - JOUR

T1 - Analysis of Rotating Cooling Effects with Oil for Turbine Blade

AU - Qin, Jiang

AU - Sun, Hong Chuang

AU - Bai, Xin Yang

AU - Xie, Gong Nan

AU - Han, Jie Cai

PY - 2017/2/1

Y1 - 2017/2/1

N2 - The air turbine can be used to solve the problems of fuel and power supply for Scramjet. The main obstacle is the cooling measure of turbine blades under limited cooling source. In this article, a new scheme was proposed to cool the blades with fuel used as coolant. Based on this oil cooling scheme, a three dimensional model was established to evaluate the feasibility and study heat transfer under rotation by numerical simulation. The results show that oil cooling scheme can efficiently reduce the temperature of blade with few negative effects on the performance of turbine. The temperature of blade can decrease greatly with the fuel mass flow rate of 1g/s. The maximum pressure of the coolant in the cooling channel can reach 114.5MPa in the rotating condition. Rotation effect enhances the turbulence intensity in the cooling channel and strengthens heat convection between the blade and fuel.

AB - The air turbine can be used to solve the problems of fuel and power supply for Scramjet. The main obstacle is the cooling measure of turbine blades under limited cooling source. In this article, a new scheme was proposed to cool the blades with fuel used as coolant. Based on this oil cooling scheme, a three dimensional model was established to evaluate the feasibility and study heat transfer under rotation by numerical simulation. The results show that oil cooling scheme can efficiently reduce the temperature of blade with few negative effects on the performance of turbine. The temperature of blade can decrease greatly with the fuel mass flow rate of 1g/s. The maximum pressure of the coolant in the cooling channel can reach 114.5MPa in the rotating condition. Rotation effect enhances the turbulence intensity in the cooling channel and strengthens heat convection between the blade and fuel.

KW - Fuel cooling

KW - Numerical simulation

KW - Rotating cooling

KW - Turbine blade

UR - http://www.scopus.com/inward/record.url?scp=85019386685&partnerID=8YFLogxK

U2 - 10.13675/j.cnki.tjjs.2017.02.019

DO - 10.13675/j.cnki.tjjs.2017.02.019

M3 - 文章

AN - SCOPUS:85019386685

SN - 1001-4055

VL - 38

SP - 399

EP - 407

JO - Tuijin Jishu/Journal of Propulsion Technology

JF - Tuijin Jishu/Journal of Propulsion Technology

IS - 2

ER -

Analysis of Rotating Cooling Effects with Oil for Turbine Blade

Abstract

Keywords

Access to Document

Other files and links

Fingerprint

Cite this