民用涡轴发动机进气系统结冰试验

宋建宇; 吴晶峰; 邱长波

doi:10.13224/j.cnki.jasp.2020.05.020

民用涡轴发动机进气系统结冰试验

doi: 10.13224/j.cnki.jasp.2020.05.020

基金项目: 国家留学基金委（201901750002）

计量
- 文章访问数: 424
- HTML浏览量: 6
- PDF量: 403
- 被引次数: 0
出版历程
- 收稿日期: 2019-11-09
- 刊出日期: 2020-05-28

Civil turboshaft engine induction system icing test

1.
Airworthiness Certification Center,Civil Aviation Ad ministration of China,Beijing 100102,China
2.
Hunan Powerplant Research Institute,Aero Engine Corporation of China,Zhuzhou Hunan 412002,China

摘要

摘要: 围绕中国民航规章CCAR-33部R2版中第33.68条款适航要求,针对涡轴发动机提出了一种满足适航要求的试验方法,包括结冰关键点分析、结冰取证试验点选定、整机结冰取证试验三部分。结合涡轴发动机工作包线,开展结冰关键点分析以选定结冰取证试验点。在结冰包线内选择了若干结冰计算点,并计算每个点的结冰位置与结冰量。计算结果显示:温度接近0 ℃且海拔高度较低的区域是涡轴发动机结冰量显著的区域。结冰试验时在-4~-1 ℃的温度区间寻找刚出现结冰的温度点与结冰量最大的温度点。试验结果显示:结冰量最大的温度点是最严酷的结冰试验点。
- 适航 /
- 涡轴发动机 /
- 进气系统结冰 /
- 结冰关键点分析 /
- 取证试验
Abstract: Focusing on the content of China Civil Aviation Regulations CCAR-33R2 article 33.68, a test method for turboshaft engine complying with airworthiness regulation requirement was provided, including icing critical point analysis, icing certification test points determination, engine icing certification test. In combination with the turboshaft engine operating envelope, critical point analysis was conducted to determine the icing certification test points. Several icing calculation points were selected in the icing envelope, and icing positions and amounts were calculated for each point. The calculation results show that the area where the temperature is close to 0 ℃ and the altitude is low is the zone where the turboshaft engine has a significant ice amount. During the icing test, the temperature points at which ice formation just occurred and the amount of icing was the largest were found in the temperature range of -4 ℃ to -1 ℃. The test results show that the temperature point with the largest amount of icing is the most severe icing test point.
- airworthiness /
- turboshaft engine /
- induction system icing /
- icing critical point analysis /
- certification test

HTML

参考文献(27)

[1]	Federal Aviation Administration.Capital airlines flight 20,vickers-armstrongs viscount,N7462［EB/OL］.［2019-09-08］.https:∥lessonslearned.faa.gov/ll_main.cfm?TabID=3&CategoryID=3&LLID=74
[2]	Federal Aviation Administration.Air florida flight 90,boeing model 737-200,N62AF［EB/OL］.［2019-09-08］.https:∥lessonslearned.faa.gov/ll_main.cfm?TabID=3&CategoryID=3&LLID=2.
[3]	WINTERSHOVEN D.Final report on the accident to the Eurocopter AS355F1 registered OO-HSB in Zuienkerke on 23-NOV-2008［R］.Brussels:Air accident investigation unit,AAIU-2008-19-Zuienkerke-HSB,2009.
[4]	BAPTIST P H,BHARATH K N.Nacelle inlet lip anti-icing with engine oil:US 7,131,612 B2［P/OL］.2006-11-07［2019-09-08］.https:∥patentimages.storage.googleapis.com/ce/e5/ea/b053df1beb51b6/US7131612.pdf.
[5]	中华人民共和国交通运输部.民用航空产品和零部件合格审定规定:CCAR-21R4［S］.北京:中国民用航空局,2017:25-26.
[6]	中华人民共和国交通运输部.运输类飞机适航标准:CCAR-25R5［S］.北京:中国民用航空局,2016:130-189.
[7]	中华人民共和国交通运输部.运输类旋翼航空器适航规定:CCAR-29R2［S］.北京:中国民用航空局,2017:199-288.
[8]	中国民用航空局.航空发动机适航规:CCAR-33R2［S］.北京:中国民用航空局,2012:33-34.
[9]	PELLISSIER M P C,HABASHI W G.Optimization via FENSAP-ICE of aircraft hot-air anti-icing systems［J］.Journal of Aircraft,2011,48(1):256-276.
[10]	杨倩,董威,郭之强,等.涡扇发动机短舱结冰试验相似方法［J］.航空动力学报,2019,34(9):1988-2000. YANG Qian,DONG Wei,GUO Zhiqiang,et al.Scaling method of turbofan engine nacelle under icing test［J］.Journal of Aerospace Power,2019,34(9):1988-2000.(in Chinese)
[11]	CAO Yihua,LI Guozhi.Helicopter flight characteristics in icing conditions［J］.The Aeronautical Journal,2012,116(1183):963-979.
[12]	DONG W,ZHU J,ZHENG M,et al.Thermal analysis and testing of nonrotating cone with hot-air anti-icing system［J］.Journal of Propulsion and Power,2015,31(3):896-903.
[13]	DONG W,ZHU J,ZHENG M,et al.Experimental study on icing and anti-icing characteristics of engine inlet guide vanes［J］.Journal of Propulsion and Power,2015,31(5):1330-1337.
[14]	LIAN Wenlei,XUAN Yimin.Experimental investigation on a novel aero-engine nose cone anti-icing system［J］.Applied Thermal Engineering,2017,121:1011-1021.
[15]	王健,胡娅萍,吉洪湖,等.旋转整流罩积冰生长与脱落过程的实验［J］.航空动力学报,2014,29(6):1352-1357. WANG Jian,HU Yaping,JI Honghu,et al.Experiment of ice accretion and shedding on rotating spinner［J］.Journal of Aerospace Power,2014,29(6):1352-1357.(in Chinese)
[16]	杨军,张靖周,郭文,等.航空发动机进口支板结冰和防冰试验［J］.航空动力学报,2014,29(2):277-283. YANG Jun,ZHANG Jingzhou,GUO Wen,et al,Experiment of anti-icing and icing on inlet strut of aero-engine［J］.Journal of Aerospace Power,2014,29(2):277-283.(in Chinese)
[17]	Federal Aviation Administration.Turbojet,turboprop,turboshaft,and turbofan engine induction system icing and ice ingestion:AC20-147A［S］.Washington DC:Federal aviation administration,2014:4-24.
[18]	YANG Bin,ZHOU Yanpei.Icing certification of civil aircraft engines［J］.Procedia Engineering,2011,17:603-615.
[19]	COBER S G,ISAAC G A,STRAPP J W.Characterizations of aircraft icing environments that include supercooled large drops［J］.Journal of Applied Meteorology,2001,40:1991-1992.
[20]	Federal Aviation Administration.Aircraft icing handbook volume 1 of 3［R］.Federal Aviation Agency,DOT/FAA/CT-88/8-1,1991.
[21]	BOWDEN D T,GENSEMER A E,SKEEN C A.Engineering summary of airframe icing technical data［R］.Washington DC:Federal Aviation Agency,ADS-4,1964.
[22]	Federal Aviation Administration.Turbojet,turboprop,and turbofan engine induction system icing and ice ingestion:AC20-147［S］.Washington DC:Federal Aviation Administration,2004:10-11.
[23]	Federal Aviation Administration.33.68Amdt33-34 Induction system icing［S］.Washington DC:Federal Aviation Administration,2015:1-2.
[24]	BARTLETT C S.Icing simulation in the aeropropulsion systems test facility propulsion development test cell c-2［R］.Arnold Engineering Development Center,AEDC-TR-91-12,1995.
[25]	熊荆江,袁先圣,刘祥平,等.某涡轴发动机环境结冰试验设备调试［J］.科学技术与工程,2017,17(32):258-259. XIONG Jingjiang,YUAN Xiansheng,LIU Xiangping,et al.Commissioning of environment icing simulation test facility for a turboshaft engine［J］.Science Technology and Engineering,2017,17(32):258-259.(in Chinese)
[26]	Society of Automotive Engineers.Calibration and acceptance of icing wind tunnels:SAE ARP 5905［S］.Warrendale,US:Society of Automotive Engineers,2009:16-17.
[27]	林森什,胡路平,叶宇琛.直升机发动机进气系统结冰试验及试验结果分析［J］.直升机技术,2019,200(2):57-58. LIN Senshi,HU Luping,YE Yuchen.The icing test and analysis of the helicopter’s engine air intake system［J］.Helicopter Technique,2019,200(2):57-58.(in Chinese)