Volume 35 Issue 8
Aug.  2020
Turn off MathJax
Article Contents
Article Navigation >  Journal of Aerospace Power  > 2020  >  35(8): 1735-1743
ZHANG Gong, HE Xin, FENG Jianwen. Risk model in conceptual design phase of civil aero-engine type certification[J]. Journal of Aerospace Power, 2020, 35(8): 1735-1743. doi: 10.13224/j.cnki.jasp.2020.08.018
Citation: ZHANG Gong, HE Xin, FENG Jianwen. Risk model in conceptual design phase of civil aero-engine type certification[J]. Journal of Aerospace Power, 2020, 35(8): 1735-1743. doi: 10.13224/j.cnki.jasp.2020.08.018
shu

Risk model in conceptual design phase of civil aero-engine type certification

doi: 10.13224/j.cnki.jasp.2020.08.018

  • Structure Certification Division,Airworthiness Certification Center,Civil Aviation Administration of China,Beijing 100102,China

  • Received Date: 2020-02-11
  • Publish Date: 2020-08-28
    Abstract
  • A systematic working mechanism for risk identification in conceptual design phase of civil aero-engine was established to promote efficient type certification with corrective actions. The mechanism comprehensively categorized the risks of regulations, means of compliance, implementations and critical technical points, by which the regulation terms information table was developed. 278 potential risks were identified by regulation terms information table utilization in specific civil aero-engine model. In addition, the potential risk of typical rotor integrity regulation in process from requirement definition to design implementation was analyzed in detail, which verified the mechanism and regulation terms information table.

     

    • FullText(HTML)
  • loading
    • References(20)
  • [1]
    中国民用航空局航空器适航审定司.航空器型号合格审定程序［R］.北京:中国民用航空局,2011.
    [2]
    Federal Aviation Administration.ORDER 8110.4C:type certification［R］.Washington DC:Federal Aviation Administration,2011.
    [3]
    European Aviation Safety Agency.UG.CERT.00002-005:certification handbook［R］.Cologne,Germany:European Aviation Safety Agency,2016.
    [4]
    HAN Bingbing,GAO Yanlei,LI Xin.The study of relationship between transport category aircraft and aircraft engine type certification［J］.Procedia Engineering,2014,80:26-33.
    [5]
    科兹纳.项目管理-计划、进度和控制的系统方法［M］.杨爱华,王丽珍,洪宇,等，译.北京:电子工业出版社,2014.
    [6]
    Project Management Institute.项目管理知识体系指南［M］.北京:电子工业出版社,2013.
    [7]
    National Transportation Safety Board.Aircraft accident report:United Airlines Flight 232 McDonnell Douglas DC-10-10 Sioux gateway airport,Sioux City,Iowa,July 19,1989［R］.Washington DC:National Transportation Safety Board,1989.
    [8]
    National Transportation Safety Board.Aircraft accident report:uncontained engine failure,Delta Airlines Flight 1288,McDonnell Douglas MD-88,N927DA,Pensacola,Florida,July 6,1996［R］.Washington DC:National Transportation Safety Board,1996.
    [9]
    National Transportation Safety Board.Aircraft accident report:Overseas National Airways,Inc.,Douglas DC-10-30,N1032F,John F.Kennedy International Airport,Jmaica,New York,November 12,1975［R］.Washington DC:National Transportation Safety Board,1976.
    [10]
    Air Accidents Investigation Branch.Report on the accident to Boeing 777-236ER,G-YMMM,at London Heathrow Airport on 17 January 2008［R］.Aldershot,UK:Air Accidents Investigation Branch,2010.
    [11]
    Radio Technical Commission for Aeronautics,Inc.Software consideration in airborne systems and equipment certification［R］.Washington DC:Radio Technical Commission for Aeronautics,2011.
    [12]
    Radio Technical Commission for Aeronautics.Design assurance guidance for airborne electronic hardware［R］.Washington DC:Radio Technical Commission for Aeronautics,2000.
    [13]
    Australian Transport Safety Bureau.In-flight uncontained engine failure overhead Batam Island,Indonesia 4 November 2010 VH-OQA Airbus A380-842［R］.Australian Capital Territory，Australia:Australian Transport Safety Bureau,2013.
    [14]
    Federal Aviation Administration.Advisory circular 33.27-1:turbine rotor strength requirement of 14 CFR 33.27［R］.Washington DC：Federal Aviation Administration,2004.
    [15]
    Federal Aviation Administration.Advisory circular 33.27-1A:engine and turbosupercharger rotor overspeed requirement of 14 CFR §［R］.Washington DC：Federal Aviation Administration,2011.
    [16]
    Federal Aviation Administration.Advisory circular 33-2B:aircraft engine type certification handbook［R］.Washington DC：Federal Aviation Administration,1993.
    [17]
    Federal Aviation Administration.Advisory circular 33-3:turbine and compressor rotors type certification substantiation procedures［R］.Washington DC：Federal Aviation Administration,1968.
    [18]
    Federal Aviation Administration.Advisory circular 33-7:certification of 30-second and 2-minute one-engine-inoperative (OEI) ratings for rotrocraft turbine engines［R］.Washington DC：Federal Aviation Administration,2006.
    [19]
    Federal Aviation Administration.Advisory circular 33-7A:guidance for 30-second and 2-minute one-engine-inoperative (OEI) ratings for rotrocraft turbine engines［R］.Washington DC：Federal Aviation Administration,2009.
    [20]
    Federal Aviation Administration.Policy statement PS-ANE-33.27-01:guidance for turbine,compressor,fan,and turbosupercharger rotor overspeed,loss of load requirement in 14 CFR,§ 33.27［R］.Washington DC：Federal Aviation Administration,2017.
    • Relative Articles
    • Supplements(0)
    • Cited By
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索
    Get Citation
    PDF(1544.0KB)
    XML

    Article Metrics

    Article views (459) PDF downloads(283) Cited by()
    Proportional views
    Related

    Copyright © 《Journal of Aerospace Power》 All Rights Reserved.

    Supported by: Beijing Renhe Information Technology Co., Ltd.  

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return