Frame plate and flame holder integration design and capability analysis

Feng Li; Ming Cheng; Rui Qing Guo; Shou Tang Shang; Zheng Fu Tang; Long Xian Li

Frame plate and flame holder integration design and capability analysis

Feng Li^*
, Ming Cheng
, Rui Qing Guo
, Shou Tang Shang
, Zheng Fu Tang
, Long Xian Li

^*Corresponding author for this work

School of Energy and Power Engineering

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

4 Scopus citations

Abstract

Based on the increasing demand for high thrust weight ratio and high stealthy aero-engine, the design method of integration design frame plate and flame holder afterburner was given and some model afterburner simulations and experiments were conducted. The results show that the length and can flow resistance could be reduced greatly, and the capability and thrust weight ratio of aero-engine can be increased apparently. This work would help to provide a new research direction and method for high thrust weight ratio and high stealthy aero-engine technology.

Original language	English
Pages (from-to)	2169-2174
Number of pages	6
Journal	Hangkong Dongli Xuebao/Journal of Aerospace Power
Volume	27
Issue number	10
State	Published - Oct 2012

Keywords

Afterburner
Flame holder
Frame plate design
Integration frame plate
Ramjet burner

Cite this

@article{f8b012f28ef24c5bbcd582192fcbb466,

title = "Frame plate and flame holder integration design and capability analysis",

abstract = "Based on the increasing demand for high thrust weight ratio and high stealthy aero-engine, the design method of integration design frame plate and flame holder afterburner was given and some model afterburner simulations and experiments were conducted. The results show that the length and can flow resistance could be reduced greatly, and the capability and thrust weight ratio of aero-engine can be increased apparently. This work would help to provide a new research direction and method for high thrust weight ratio and high stealthy aero-engine technology.",

keywords = "Afterburner, Flame holder, Frame plate design, Integration frame plate, Ramjet burner",

author = "Feng Li and Ming Cheng and Guo, \{Rui Qing\} and Shang, \{Shou Tang\} and Tang, \{Zheng Fu\} and Li, \{Long Xian\}",

year = "2012",

month = oct,

language = "英语",

volume = "27",

pages = "2169--2174",

journal = "Hangkong Dongli Xuebao/Journal of Aerospace Power",

issn = "1000-8055",

publisher = "BUAA Press",

number = "10",

}

TY - JOUR

T1 - Frame plate and flame holder integration design and capability analysis

AU - Li, Feng

AU - Cheng, Ming

AU - Guo, Rui Qing

AU - Shang, Shou Tang

AU - Tang, Zheng Fu

AU - Li, Long Xian

PY - 2012/10

Y1 - 2012/10

N2 - Based on the increasing demand for high thrust weight ratio and high stealthy aero-engine, the design method of integration design frame plate and flame holder afterburner was given and some model afterburner simulations and experiments were conducted. The results show that the length and can flow resistance could be reduced greatly, and the capability and thrust weight ratio of aero-engine can be increased apparently. This work would help to provide a new research direction and method for high thrust weight ratio and high stealthy aero-engine technology.

AB - Based on the increasing demand for high thrust weight ratio and high stealthy aero-engine, the design method of integration design frame plate and flame holder afterburner was given and some model afterburner simulations and experiments were conducted. The results show that the length and can flow resistance could be reduced greatly, and the capability and thrust weight ratio of aero-engine can be increased apparently. This work would help to provide a new research direction and method for high thrust weight ratio and high stealthy aero-engine technology.

KW - Afterburner

KW - Flame holder

KW - Frame plate design

KW - Integration frame plate

KW - Ramjet burner

UR - https://www.scopus.com/pages/publications/84869841234

M3 - 文章

AN - SCOPUS:84869841234

SN - 1000-8055

VL - 27

SP - 2169

EP - 2174

JO - Hangkong Dongli Xuebao/Journal of Aerospace Power

JF - Hangkong Dongli Xuebao/Journal of Aerospace Power

IS - 10

ER -

Frame plate and flame holder integration design and capability analysis

Abstract

Keywords

Other files and links

Fingerprint

Cite this