Volume 36 Issue 2
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WANG Xiaoming. Development history of civil turbine engine endurance test requirements[J]. Journal of Aerospace Power, 2021, 36(2): 431-439. doi: 10.13224/j.cnki.jasp.2021.02.022
Citation: WANG Xiaoming. Development history of civil turbine engine endurance test requirements[J]. Journal of Aerospace Power, 2021, 36(2): 431-439. doi: 10.13224/j.cnki.jasp.2021.02.022

Development history of civil turbine engine endurance test requirements

doi: 10.13224/j.cnki.jasp.2021.02.022
  • Received Date: 2020-10-21
  • Publish Date: 2021-02-28
  • The development history of 33.87 endurance test in aero-engine airworthiness standards CCAR-33R2 was comprehensively reviewed. Based on the interpretation of airworthiness regulation requirements, the current research of 33.87 endurance test in the world was deeply tracked. It showed the endurance test requirement remained essentially unchanged since 1 957 when the current 6 hour×25 cycles formats were implemented, but turbine engine designs had evolved significantly. The progress of engine design technology brought incompatibility with airworthiness regulations, so exploratory research and application on alternative test of 150 hour endurance test was carried out in the world. Despite of some existing issues for clarifications, the relevant research can provide reference for the accepted compliance method research and the airworthiness standard formulation and revision in China. It is of great significance for improving the compilation and revision ability about China's airworthiness technical regulations to track domestic and international airworthiness technology trends continuously and deeply, and then take positive response strategies timely and carry out targeted research on relevant provisions.

     

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  • [1]
    綦蕾,李红琳,陈智强.浅谈民用航空发动机适航技术新要求[J].航空动力,2020(1):45-48.
    QI Lei,LI Honglin,CHEN Zhiqiang.New airworthiness technical requirements for civil aero engines[J].Aerospace Power,2020(1):45-48.(in Chinese)
    [2]
    Civil Aeronautics Board.Aircraft engine airworthiness:CAR Part 13[S].Washington DC:Civil Aeronautics Board,1937:1-8.
    [3]
    Civil Aeronautics Board.Aircraft engine airworthiness:CAR Part 13[S].Washington DC:Civil Aeronautics Board,1952:4.
    [4]
    Civil Aeronautics Board.Aircraft engine airworthiness:CAR Part 13[S].Washington DC:Civil Aeronautics Board,1956:5.
    [5]
    Civil Aeronautics Board.Aircraft engine airworthiness:CAR Part 13 amendment 13-1[S].Washington DC:Civil Aeronautics Board,1957:3.
    [6]
    Civil Aeronautics Board.Aircraft engine airworthiness:CAR Part 13 amendment 13-2[S].Washington DC:Civil Aeronautics Board,1958:1.
    [7]
    Civil Aeronautics Board.Aircraft engine airworthiness:CAR Part 13 amendment 13-5[S].Washington DC:Civil Aeronautics Board,1963:2.
    [8]
    Civil Aeronautics Board.Aircraft engine airworthiness:CAR Part 13 amendment 13-6[S].Washington DC:Civil Aeronautics Board,1964:2.
    [9]
    Federal Aviation Administration.Airworthiness Standards:aircraft engines FAR Part 33[S].Washington DC:Federal Aviation Administration,1965.
    [10]
    Federal Aviation Administration.Airworthiness Standards:aircraft engines FAR Part 33 amendment 33-3[S].Washington DC:Federal Aviation Administration,1967.
    [11]
    Federal Aviation Administration.Airworthiness Standards:aircraft engines FAR Part 33 amendment 33-6[S].Washington DC:Federal Aviation Administration,1974.
    [12]
    Federal Aviation Administration.Airworthiness Standards:aircraft engines FAR Part 33 amendment 33-10[S].Washington DC:Federal Aviation Administration,1984.
    [13]
    Federal Aviation Administration.Airworthiness Standards:aircraft engines FAR Part 33 amendment 33-12[S].Washington DC:Federal Aviation Administration,1988.
    [14]
    Federal Aviation Administration.Airworthiness Standards:aircraft engines FAR Part 33 amendment 33-18[S].Washington DC:Federal Aviation Administration,1996.
    [15]
    Federal Aviation Administration.Airworthiness standards:aircraft engines FAR Part 33 amendment 33-25[S].Washington DC:Federal Aviation Administration,2008.
    [16]
    Federal Aviation Administration.Airworthiness standards:aircraft engines FAR Part 33 amendment 33-30[S].Washington DC:Federal Aviation Administration,2009.
    [17]
    Federal Aviation Administration.Airworthiness standards:aircraft engines FAR Part 33 amendment 33-32[S].Washington DC:Federal Aviation Administration,2012.
    [18]
    Joint Aviation Authorities.Joint aviation requirements:engines JAR-E change 5[S].Hoofddorp,Netherlands:Joint Aviation Authorities,1980.
    [19]
    Joint Aviation Authorities.Joint aviation requirements:engines JAR-E change 6[S].Hoofddorp,Netherlands:Joint Aviation Authorities,1981.
    [20]
    Joint Aviation Authorities.Joint aviation requirements:engines JAR-E change 9 orange paper E/97/1[S].Hoofddorp,Netherlands:Joint Aviation Authorities,1997.
    [21]
    Joint Aviation Authorities.Joint aviation requirements:engines JAR-E change 10[S].Hoofddorp,Netherlands:Joint Aviation Authorities,1999.
    [22]
    Joint Aviation Authorities.Joint aviation requirements:engines JAR-E amendment 12[S].Hoofddorp,Netherlands:Joint Aviation Authorities,2003.
    [23]
    European Aviation Safety Agency.Certification specifications for engines:CS-E[S].Cologne,Germany:European Aviation Safety Agency,2003.
    [24]
    European Aviation Safety Agency.Certification specifications for engines:CS-E amendment 1[S].Cologne,Germany:European Aviation Safety Agency,2007.
    [25]
    European Aviation Safety Agency.Certification specifications and acceptable means of compliance for engines:CS-E amendment 4[S].Cologne,Germany:European Aviation Safety Agency,2015.
    [26]
    European Aviation Safety Agency.Certification specifications and acceptable means of compliance for engines:CS-E amendment 5[S].Cologne,Germany:European Aviation Safety Agency,2018.
    [27]
    Federal Aviation Administration.FAA validation of EASA state of design turbine aircraft engines FAA significant standards difference summary list per FAA-EASA technical validation procedures (TIP) revision:14 CFR Part 33 amendment 34 compared to CS-E amendment 514 CFR Part 33 amendment 34 compared to CS-E amendment 5[R].Washington DC:Federal Aviation Administration,2019.
    [28]
    中国民用航空局.航空发动机适航规定:CCAR-33R2[S].北京:中国民用航空局,2011.
    [29]
    Federal Aviation Administration.Engine overtorque test,calibration test,endurance test,and teardown inspection for turbine engine certification (§§33.84,33.85,33.87,33.93):AC 33.87-1A[R].Washington DC:Federal Aviation Administration,2015.
    [30]
    Aviation Rule Making Advisory Committee.Alternate test to 14CFR33.87 endurance test[R].Washington DC:Federal Aviation Administration,2017.
    [31]
    BRANDON R.Letter from FAA office of rulemaking to ARAC[R].Washington DC:Federal Aviation Administration,2020.
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