Some Fundamental Experiences of Design and Development of the "Kunlun" Aero-Engine

YAN Cheng-zhong

Chinese

您当前的位置：

首页 >

文章列表页 >

Some Fundamental Experiences of Design and Development of the "Kunlun" Aero-Engine

更新时间：2026-07-07

- Some Fundamental Experiences of Design and Development of the "Kunlun" Aero-Engine
- Vol. 20, Issue 2, (2005)
- 作者机构：
  
  中国航空工业第一集团公司沈阳发动机设计研究所,辽宁,沈阳,110015
- 作者简介：
- 基金信息：
- DOI：
  CLC：
- Published：2005
- 稿件说明：
移动端阅览
YAN Cheng-zhong. Some Fundamental Experiences of Design and Development of the "Kunlun" Aero-Engine[J]. 2005, 20(2).
DOI：

YAN Cheng-zhong. Some Fundamental Experiences of Design and Development of the "Kunlun" Aero-Engine[J]. 2005, 20(2). DOI：

摘要

介绍了我国首次按GJB241-87"航空涡轮喷气和涡轮风扇发动机通用规范"的要求

自行设计研制成功的"昆仑"加力式双转子涡轮喷气发动机的设计研制基本经验:认真贯彻"航空涡轮喷气和涡轮风扇发动机通用规范"

严格按规范的要求进行设计和试验;合理控制创新与继承的比例

既要保持先进性

又要降低风险性;把作战适用性、可靠性、耐久性、维修性与性能并重;设计中留有较大的温度裕度和喘振裕度;进行苛刻的、充分的试验是发动机可靠性的基础。

Abstract

Briefly introduces some fundamental experiences of design and development of the "Kunlun" two-spool afterburning turbojet engine

which was successfully self-designed and developed in China.The design

development and test were strictly followed out the "General Specification of Turbojet and Turbofan Aero-Engines".The adequate proportion between creativeness and inheritance was controlled to reduce risk without sacrificing the engine’s advanced status.The design regarded the operability

reliability

durability and maintainability as important as performance.Large exhaust temperature margin and surge margin were ensured.Strict and sufficient ground and flight tests were the base of the engine reliability.

关键词

Keywords

references

Views

488

下载量

CSCD

Alert me when the article has been cited

提交

Tools

Publicity Resources

Prediction method on equivalent thermal conductivity coefficient of plain braided C/SiC composites material based on finite element method

Aerodynamic characteristics of design Mach number of 5 two-dimensional inlet with mixed-compression under typical condition

Computation of effect of different nozzle parameters on internal performance of convergent-divergent axisymmetric nozzle

Study of novel flow control concept for fix-geometry two-dimensional mix-compression supersonic inlet

Nonlinear dynamic response analysis of unbalance-rubbing coupling faults of rotor-ball bearing-stator coupling system

Related Author

LU Si-da

GAO Xi-guang

SONG Ying-dong

WENG Xiao-chai

GUO Rong-wei

ZHU Dan-dan

SHAO Wan-ren

WENG Xiao-chai

Related Institution

Jiangsu Province Key Laboratory of Aerospace Power System, College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics

Department of Power and Propulsion, School of Engineering, Cranfield University, Bedfordshire MK4

State Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing University of Aeronautics and Astronautics

Unit 94710, the Chinese People's Liberation Army

Innovation Center for Advanced Aero-Engine

AI问答

Postal code：100079
Tel：（010）53879206 Email：tmw@bjxintong.com.cn
Technical support is provided by Beijing Founder electronics co., LTD 京ICP备09082226号-64 京公网安备11010602201714号
It is recommended to read the content of this site in Chrome&IE9+. Please switch to extreme mode in browser 360.
Cookies We use cookies to help provide and enhance our service and tailor content. By continuing, you agree to the use of cookies.

⁰