Airworthiness certification technology of normal aircraft natural icing flight test

被引:0
|
作者
Gao G. [1 ]
Zhang B. [2 ]
Quan J. [1 ]
Yin C. [1 ]
Ding L. [1 ]
Jiang Y. [3 ]
机构
[1] Shenyang Aircraft Airworthiness Certification Center of CAAC, Shenyang
[2] Aircraft Design and Research Institute, Harbin Aircraft Industry Group, Harbin
[3] China Aerodynamics Research and Development Center, Mianyang
关键词
airworthiness certification; de-ice and anti-ice system; flight test procedures; ice detection; natural icing flight test;
D O I
10.7527/S1000-6893.2023.28531
中图分类号
学科分类号
摘要
When applying for Flight in Known Icing(FIKI),civil aircraft should demonstrate compliance with the requirements of de-ice and anti-ice related airworthiness regulations. Thereinto,natural icing flight test is a critical item which must be completed. Taking natural icing flight test of Y12F aircraft as an example,based on guidance documents issued by Civil Aviation Administration of China(CAAC)and Federal Aviation Administration(FAA)for FIKI and combined with the airworthiness certification process of natural icing flight test of Y12F aircraft,this paper analyzes and summarizes the airworthiness certification requirements and critical techniques of the de-ice and anti-ice system,the test instrument and installation,flight test airspace,icing atmospheric conditions,flight test items,flight test status,flight test procedures,flight test results and analysis,ice detection,icing atmospheric detection,icing accumulation state monitoring,etc. This paper also elaborates the classification of problems discovered during the flight test,the corresponding solutions,design improvement proposals,and completed supplementary certification work. Concurrently certificated by CAAC and FAA,Y12F aircraft obtained approval for FIKI from both authorities. The constructed airworthiness certification method for natural icing flight test has become an important practical guidance material for FIKI airworthiness certification. © 2024 Chinese Society of Astronautics. All rights reserved.
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共 88 条
  • [11] Pilot guide flight in icing conditions:AC91-74B[S], (2015)
  • [12] HICKMAN G A, FENG Y X,, Et al., Icing sensor and ice protection system,Revision 3:NASA CR-194245[S], (1990)
  • [13] HEINRICH A, ZUMWALT G,, Et al., Aircraft icing handbook, 2, (2000)
  • [14] LEWIS W., Recommended values of meteorological factors to be considered in the design of aircraft ice-prevention equipment, (1949)
  • [15] BRAGG M B., Effect of residual and in-tercycle ice accretions on airfoil performance, (2002)
  • [16] PELLICANO P., Guidance for new airplane icing certification projects[C]∥ SAE 2007 Aircraft & Engine Icing International Conference, (2007)
  • [17] PELLICANO P., Supercooled large droplet(SLD)icing and certification of Part 23 airplanes[C]∥ FAA 2009 Small Airplane Directorate Program Managers Meeting, (2009)
  • [18] SHIN J, BOND T H., Results of an icing test on a NACA 0012 airfoil in the NASA Lewis icing research tunnel, 30th Aerospace Sciences Meeting and Exhibit, (1992)
  • [19] DE MATTEIS P., An overview of the CIRA icing wind tunnel[C]∥ 41st Aerospace Sciences Meeting and Exhibit, (2003)
  • [20] ARRINGTON E., Aerodynamic calibration of the NASA Lewis icing research tunnel(1997 tests, 36th AIAA Aerospace Sciences Meeting and Exhibit, (1998)