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Volumn 39, Issue 1, 2009, Pages 33-37

Numerical analysis of high pressure turbine tip clearance variation

Author keywords

Finite element method; High pressure turbine (HPT); Machine tool; Segmental application of boundary conditions; Tip clearance

Indexed keywords

APPLICATIONS; BOUNDARY CONDITIONS; BOUNDARY ELEMENT METHOD; DEFORMATION; ENGINES; MACHINE TOOLS; MACHINERY; MACHINING; TORSIONAL STRESS; TURBINES;

EID: 59949084760     PISSN: 16715497     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article
Times cited : (7)

References (12)
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    • Hennecke, D.K.1    Trappmann, K.2
  • 2
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    • A technique for the measurement of blade tip clearance in a gas turbine
    • AIAA Paper 89-2916
    • Chivers J. A technique for the measurement of blade tip clearance in a gas turbine[C]//AIAA Paper 89-2916, 1989.
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  • 3
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    • A reduced model for prediction of thermal and rotational effects on turbine tip clearance
    • NASA-2003-212226
    • Kypuros J A, Melcher K J. A reduced model for prediction of thermal and rotational effects on turbine tip clearance[R]. NASA-2003-212226, 2003.
    • (2003)
    • Kypuros, J.A.1    Melcher, K.J.2
  • 4
    • 59949084341 scopus 로고
    • Models for predicting tip clearance changes in gas turbines
    • NASA, N83-29258
    • Pilidis P, Maccallum N R L. Models for predicting tip clearance changes in gas turbines[R]. NASA, N83-29258, 1983.
    • (1983)
    • Pilidis, P.1    Maccallum, N.R.L.2
  • 6
    • 45449107845 scopus 로고    scopus 로고
    • Calculation program for turbine tip clearance and result analysis
    • Niu Dong-sheng, Chen Wei, Qi Wen-kai. Calculation program for turbine tip clearance and result analysis[J]. Gas Turbine Experiment and Research, 2004, 17(4): 31-34.
    • (2004) Gas Turbine Experiment and Research , vol.17 , Issue.4 , pp. 31-34
    • Niu, D.-S.1    Chen, W.2    Qi, W.-K.3
  • 7
    • 59949091190 scopus 로고
    • Optimization of CFM56 HPT tip clearance
    • Liu Yu-guo. Optimization of CFM56 HPT tip clearance[J]. International Astronautics, 1994(4): 53-55.
    • (1994) International Astronautics , Issue.4 , pp. 53-55
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  • 8
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    • Experimental study of the cooling effectiveness of a rotating disc with a central cooling air feed
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    • (2000) Journal of Aerospace Power , vol.87 , Issue.15 , pp. 260-263
    • Xu, G.-Q.1    Ding, S.-T.2    Tao, Z.3
  • 9
    • 84896693619 scopus 로고    scopus 로고
    • Turbine engine clearance control systems: Current practices and future directions
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    • Lattime S, Steinetz B. Turbine engine clearance control systems: current practices and future directions[C]//AIAA Paper 2002-3790, 2002.
    • (2002)
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  • 10
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    • Test rig for evaluating active turbine blade tip clearance control concepts
    • AIAA Paper 2003-4700
    • Lattime S, Stemetz B, Robbie M. Test rig for evaluating active turbine blade tip clearance control concepts[C]//AIAA Paper 2003-4700, 2003.
    • (2003)
    • Lattime, S.1    Stemetz, B.2    Robbie, M.3
  • 11
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    • Chinese source
  • 12
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    • Experiment study of convective heat transfer and discharge coefficient of jet impingement inside semi-confined channel
    • Nanjing: Nanjing University of Aeronautics and Astronautics
    • Zhang Ze-yuan. Experiment study of convective heat transfer and discharge coefficient of jet impingement inside semi-confined channel[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2006.
    • (2006)
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.