| Citation: | GONG Lifeng, XIONG Qingyong, LUO Mingzhi, FU Qiuju. Speed prediction for power turbine rotors of turboshaft engine on loss-of-load[J]. Journal of Aerospace Power, 2021, 36(2): 352-357. doi: 10.13224/j.cnki.jasp.2021.02.013
|
| [1] |
Australian Transport Safety Bureau.In-flight uncontained engine failure-overhead Batam Island,Indonesia-4 November 2010 VH-OQA,Airbus A380-842［R］.Australian Transport Safety Bureau,AO-2010-089,2010.
|
| [2] |
陈光.航空发动机结构设计分析［M］.北京:北京航空航天大学出版社,2006.
|
| [3] |
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,2011:11-12.
|
| [4] |
刘传凯,李艳茹,邱天,等.涡轮轴断裂条件下的涡扇发动机性能建模［J］.航空动力学报,2017,32(12):2855-2861. LIU Chuankai,LI Yanru,QIU Tian,et al.Performance modeling of turbofan engine in event of shaft failure［J］.Journal of Aerospace Power,2017,32(12):2855-2861.(in Chinese)
|
| [5] |
刘传凯,李圆圆,李艳茹,等.涡轮轴断裂条件下空气系统强瞬变过程分析［J］.北京航空航天大学学报,2016,42(1):47-53. LIU Chuankai,LI Yuanyuan,LI Yanru,et al.Dynamic analysis of air system with fast transients in shaft failure event［J］.Journal of Beijing University of Aeronautics and Astronautics,2016,42(1):47-53.(in Chinese)
|
| [6] |
PSARRA A.Gas turbine shaft failure modelling friction and wear modelling of turbines in contact［D］.Bedfordshire,UK:Cranfield University,2010.
|
| [7] |
GALLAR L.Gas turbine shaft over-speed/failure performance modelling［D］.Bedfordshire,UK:Cranfield University,2010.
|
| [8] |
SORIA C.Gas turbine shaft over-speed/failure performance modelling:aero/thermodynamics modelling and overall engine system response［D］.Bedfordshire,UK:Cranfield University,2014.
|
| [9] |
CALCAGNI C.Secondary air system dynamics modelling during shaft failure［D］.Bedfordshire,UK:Cranfield University,2008.
|
| [10] |
Federal Aviation Administration.Turbine,compressor,fan,and turbosupercharger rotors［EB/OL］.［2020-04-28］.https://www.ecfr.gov/cgi-bin/text-idx?SID=6ffffc64f8329f68636e14d6a6cf16d1&mc=true&node=se14.1.33_127&rgn=div8.
|
| [11] |
Federal Aviation Administration.Engine and turbosupercharger rotor overspeed requirements of 14 CFR § 33.27:AC No.33.27-1A［S］.Washington DC:Government Publishing Office,2011:7-8.
|
| [12] |
European Union Aviation Safety Agency.Certification specifications and acceptable means of compliance for engines:CS-E［S］.Cologne:European Union Aviation Safety Agency,2018:1-E-27-1-E-28.
|
| [13] |
Federal Aviation Administration.Guidance for 30-second and 2-minute one-engine-inoperative (OEI) ratings for rotorcraft turbine engines:AC No.33-7A［S］.Washington DC:Government Publishing Office,2009:2.
|
| [14] |
ANDERSON J D.Computational fluid dynamics:the basics with applications［R］.New York:McGraw-Hill,1995.
|
| [15] |
AIAA.Guide for the verification and validation of computational fluid dynamics simulations［R］.AIAA-98-077,1998.
|
| [16] |
SARAVANAMUTTOO H I H,ROGERS G F C,COHEN H.Gas turbine theory［M］.Edinburgh,Scotland:Longman Imprint,2009.
|
| [17] |
艾自胜,张长青,单连成,等.Excel在曲线拟合中的应用［J］.苏州大学学报(医学版),2008,28(5):759-762. AI Zisheng,ZHANG Changqing,SHAN Liancheng,et al.The application of excel in curve fitting［J］.Suzhou University Journal of Medical Science,2008,28(5):759-762.(in Chinese)
|
| [18] |
哈尔滨工业大学理论力学考研室.理论力学［M］.北京:高等教育出版社,2016.
|
| [19] |
European Union Aviation Safety Agency.Certification memorandum-turbine over-speed resulting from shaft failure［R］.Brussels:European Union Aviation Safety Agency EASA CM-PIFS-003,2012.
|
| [20] |
张塘卫.某型涡轴发动机动力涡轮超转保护响应时间测试［J］.电子测试,2016(15):41-43. ZHANG Tangwei.Response time test for overspeed protection in the power turbine of a turbo shaft engin［J］.Electronic Test,2016(15):41-43.(in Chinese)
|
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