Full Text:   <4057>

CLC number: V232.3

On-line Access: 2012-08-30

Received: 2012-02-22

Revision Accepted: 2012-07-30

Crosschecked: 2012-08-15

Cited: 2

Clicked: 5540

Citations:  Bibtex RefMan EndNote GB/T7714

-   Go to

Article info.
1. Reference List
Open peer comments

Journal of Zhejiang University SCIENCE A 2012 Vol.13 No.9 P.665-673

http://doi.org/10.1631/jzus.A1200047


Containment of high-speed rotating disk fragments


Author(s):  Hai-jun Xuan, Lu-lu Liu, Yi-ming Feng, Qing He, Juan-juan Li

Affiliation(s):  High-Speed Rotating Machinery Laboratory, Institute of Chemical Machinery, Faculty of Engineering, Zhejiang University, Hangzhou 310027, China

Corresponding email(s):   marine@zju.edu.cn, fymlx163@gmail.com

Key Words:  Aeroengine, Disk fragments, Engine casing, Containment capability, Numerical simulation


Hai-jun Xuan, Lu-lu Liu, Yi-ming Feng, Qing He, Juan-juan Li. Containment of high-speed rotating disk fragments[J]. Journal of Zhejiang University Science A, 2012, 13(9): 665-673.

@article{title="Containment of high-speed rotating disk fragments",
author="Hai-jun Xuan, Lu-lu Liu, Yi-ming Feng, Qing He, Juan-juan Li",
journal="Journal of Zhejiang University Science A",
volume="13",
number="9",
pages="665-673",
year="2012",
publisher="Zhejiang University Press & Springer",
doi="10.1631/jzus.A1200047"
}

%0 Journal Article
%T Containment of high-speed rotating disk fragments
%A Hai-jun Xuan
%A Lu-lu Liu
%A Yi-ming Feng
%A Qing He
%A Juan-juan Li
%J Journal of Zhejiang University SCIENCE A
%V 13
%N 9
%P 665-673
%@ 1673-565X
%D 2012
%I Zhejiang University Press & Springer
%DOI 10.1631/jzus.A1200047

TY - JOUR
T1 - Containment of high-speed rotating disk fragments
A1 - Hai-jun Xuan
A1 - Lu-lu Liu
A1 - Yi-ming Feng
A1 - Qing He
A1 - Juan-juan Li
J0 - Journal of Zhejiang University Science A
VL - 13
IS - 9
SP - 665
EP - 673
%@ 1673-565X
Y1 - 2012
PB - Zhejiang University Press & Springer
ER -
DOI - 10.1631/jzus.A1200047


Abstract: 
Disk burst accidents sometimes happen in aeroengines. To avoid tragic consequences, aeroengine casings must have sufficient containment capability. Experiments and simulations need to be conducted to study the impact, distortion, and perforation caused by disk burst and which may give important clues to potential failure mechanisms. This paper presents some containment tests of high-speed rotating disk fragments, in which the original disks were burst into three equal fragments within a predetermined rotating speed range. The failure modes of the containment casing varied significantly with the thickness of the containment casing. Shearing, tearing, tensile fracture, and large plastic stretching deformation occurred in a thin-walled containment casing, while a thick-walled casing could contain disk fragments and withstand large plastic deformation. numerical simulations were carried out to study the impact process and failure modes further. Good agreement was found between the results of the simulations and the tests.

Darkslateblue:Affiliate; Royal Blue:Author; Turquoise:Article

Reference

[1]Aviation Safety Network, 2006. Aircraft Accident Boeing 767-223 ER N330AA Los Angeles International Airport. Available from: http://aviation-safety.net/database/record. php?id=20060602-0 [Accessed on Feb. 17, 2008]

[2]Carney, K.S., Pereira, J.M., Revilock, D.M., Matheny, P., 2009. Jet engine fan blade containment using an alternate geometry. International Journal of Impact Engineering, 36(5):720-728.

[3]Chen, G., Chen, X., Chen, Z.F., Qu, M., 2007. Simulation of A3 steel blunt projectile impacting 45 steel plates. Explosion and Shock Waves, 27(5):390-397 (in Chinese).

[4]Frankenberger, C.E., 1998. FAA T53-L-13L Turbine Fragment Containment Test. Report No. DOT/FAA/AR-98/22, Federal Aviation Administration, Washington.

[5]Gerstle, J.H., 1975. Analysis of rotor fragment impact on ballistic fabric engine burst containment shields. Journal of Aircraft, 12(4):388-393.

[6]Hagg, A.C., Sankey, G.O., 1974. The containment of disk burst fragments by cylindrical shells. Journal of Engineering for Power, Transaction of the ASME, 96:114-123.

[7]Hradecky, S., 2010. Accident: Qantas A388 near Singapore on Nov 4th 2010, Uncontained Engine Failure. The Aviation Herald. Available from: http://avherald.com/h?article= 43309c6d&opt=0 [Accessed on Feb. 11, 2012]

[8]Johnson, G.R., Cook, W.H., 1983. A Constitutive Model and Data for Metals Subjected to Large Strains, High Strain Rates and High Temperatures. Proceedings of the Seventh International Symposium on Ballistics, Hague, the Netherlands.

[9]Johnson, G.R., Cook, W.H., 1985. Fracture characteristics of three metals subjected to various strains, strain rates, temperatures and pressures. Engineering Fracture Mechanics, 21(1):31-48.

[10]Naik, D., Sankaran, S., Mobasher, B., Rajan, S.D., Pereira, J.M., 2009. Development of reliable modeling methodologies for fan blade out containment analysis-Part I: Experimental studies. International Journal of Impact Engineering, 36(1):1-11.

[11]Roberts, G.D., Revilock, D.M., Binienda, W.K., Nie, W.Z., Mackenzie, S.B., Todd, K.B., 2002. Impact testing and analysis of composites for aircraft engine fan cases. Journal of Aerospace Engineering, 15(3):104-110.

[12]Sarkar, S., Atluri, S.N., 1996. Effects of multiple blade interaction on the containment of blade fragments during a rotor failure. Finite Elements in Analysis and Design, 23(2-4):211-223.

[13]Sharda, J., Deenadayalu, C., Mobasher, B., Rajan, S.D., 2006. Modeling of multilayer composite fabrics for gas turbine engine containment systems. Journal of Aerospace Engineering, 19(1):38-45.

[14]Stahlecker, Z., Mobasher, B., Rajan, S.D., Pereira, J.M., 2009. Development of reliable modeling methodologies for engine fan blade out containment analysis. Part II: Finite element analysis. International Journal of Impact Engineering, 36(3):447-459.

[15]Stamper, E., Hale, S., 2008. The Use of LS-DYNA Model to Predict Containment of Disk Burst Fragments. 10th International LS-DYNA Users Conference, Dearborn, Michigan.

[16]Teng, X., Wierzbicki, T., 2008. Gouging and fracture of engine containment structure under fragment impact. Journal of Aerospace Engineering, 21(3):174-186.

[17]Xuan, H.J., Wu, R.R., 2006. Aeroengine turbine blade containment tests using high-speed rotor spin testing facility. Aerospace Science and Technology, 10(6):501-508.

[18]Yuriy, N.S., Dmitriy, V.G., 2006. Numerical Analysis of Aircraft Engine Fan Blade-Out. 42nd AIAA/ASME/SAE/ ASEE Joint Propulsion Conference & Exhibit, Sacramento, California.

Open peer comments: Debate/Discuss/Question/Opinion

<1>

Please provide your name, email address and a comment





Journal of Zhejiang University-SCIENCE, 38 Zheda Road, Hangzhou 310027, China
Tel: +86-571-87952783; E-mail: cjzhang@zju.edu.cn
Copyright © 2000 - 2022 Journal of Zhejiang University-SCIENCE