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Turbine Blade Investment Casting Die Technology pp 1–20Cite as

Introduction

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Abstract

Aero-engine, as the component of the propulsion system for an aircraft that generates mechanical power, is regarded as the heart of an aircraft [1]. With the development of aircraft power technology and the demands for national defense, the aero-engine has to meet the requirements of the new generation of aircraft, such as high speed, high altitude, long flight time, long distance, and high thrust-to-weight ratio.

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References

  1. Liu DX, Chen G et al (2003) Aero-engine: the heart of airplane. Aviation Industry Press, Beijing (in Chinese)

    Google Scholar 

  2. Fang CD (2004) Prospective development of aeroengines. Aeroengine 30(1):1–5 (in Chinese)

    Google Scholar 

  3. “Handbook of Aviation Manufacturing Engineering” editorial board (1998) Handbook of aviation manufacturing engineering. Aviation Industry Press, Beijing (in Chinese)

    Google Scholar 

  4. Anders JM, Haarmeyer J, Heukenkamp H (1999) A parametric blade design system (Part I + II). In: Von Karman Institute for fluid dynamics: lecture series 1999–2002 turbomachinery blade design systems

    Google Scholar 

  5. Burman J, Gebart BR, Mårtensson H (2000) Development of a blade geometry definition with implicit design variables. In: 38th AIAA Aerospace Sciences Meeting and Exhibit, Reno, N.Y, 0671

    Google Scholar 

  6. Miller PL, Oliver JH, Miller DP, Tweedt DL (1996) BladeCAD: An interactive geometric design tool for turbomachinery blades. In: NASA Technical Memorandum 107262, 41st gas turbine and aeroengine congress, Birmingham, United Kingdom; June 10–13

    Google Scholar 

  7. Miller PL, Oliver JH, Miller DP, Tweedt DL (1997) Using stream surfaces for blade design. Mech Eng 119(4):66

    Google Scholar 

  8. Corral R, Pastor G (1999) A parametric design tool for cascades of airfoils. ASME, International Gas Turbine and Aeroengine Congress and Exhibition, Indianapolis, IN, June 7–10

    Google Scholar 

  9. Cairns DS, Mandell JF, McKittrick LR, Rabern DA, et al (1999) Design/manufacturing synthesis of a composite blade for the AOC 15/50 wind turbine. In: 1999 ASME Wind Energy Symposium, USA, pp. 58–65

    Google Scholar 

  10. Yang SY (1998) Study on mathematical molding and NC manufacturing technique in CAD/CAM turbocharger blade molding. Intern-combust Engine Eng 19(3):38–39 (in Chinese)

    Google Scholar 

  11. Cui YM, Han QY, Zhang XM (2001) Research on the surface modeling technology based on ARX. Inf Electric Power 1:45–47 (in Chinese)

    Google Scholar 

  12. Wang WH, Mo R, Wang ZQ et al (1999) The development and application of a CAD/CAM prototyping system for turbine blade modeling. Aeronaut Comput Tech 29(4):14–15 (in Chinese)

    Google Scholar 

  13. Tian Q, Mo R, Xia Y et al (2007) CAD modeling method for aeroengine blade. Aeronaut Manufact Technol 2:78–81 (in Chinese)

    Google Scholar 

  14. Yang YC, Wang WH, Jun YC et al (2007) The system of cathode designing for turbine blade modeling. Mod Manufact Eng 2:108–110 (in Chinese)

    Google Scholar 

  15. Fuh JYH, Zhang YF, Nee AYC, Fu MW (2004) Computer-aided injection mold design and manufacture. Marcel Dekker Inc, New York

    Google Scholar 

  16. Ong SK, Prombanpong S, Lee KS (1995) An object-oriented approach to computer-aided design of a plastic injection mould. J Intell Manufact 6(1):1–10

    Article  Google Scholar 

  17. Chin KS, Wong TN (1996) Knowledge-based evaluation for the conceptual design development of injection molding parts. Eng Appl Artif Intell 9(4):359–376

    Article  Google Scholar 

  18. Chin KS, Wong TN (1996) Developing a knowledge-based injection mould cost estimation system by decision tables. Int J Adv Manufact Technol 11(5):353–365

    Article  Google Scholar 

  19. Mok CK, Chin KS, Ho JKL (2001) An interactive knowledge based CAD system for mould design in injection moulding processes. Int J Adv Manufact Technol 17(1):27–38

    Article  Google Scholar 

  20. Moka CK, Chin KS, Lan HB (2008) An Internet-based intelligent design system for injection moulds. Robot Comput-Integr Manufact 24(1):1–15

    Article  Google Scholar 

  21. Bozdana TA, Eyercioglu O (2002) Development of an expert system for the determination of injection moulding parameters of thermoplastic materials: EX-PIMN. J Mater Process Technol 128(1–3):113–122

    Article  Google Scholar 

  22. Chan WM, Yan L, Xiang W et al (2003) A 3D CAD knowledge-based assisted injection mould design system. Int J Adv Manufact Technol 22(5–6):387–395

    Article  Google Scholar 

  23. Lin BT, Chan CK, Wang JC (2008) A knowledge-based parametric design system for drawing dies. Int J Adv Manufact Technol 36(7–8):671–680

    Article  Google Scholar 

  24. Cai Y, Lou ZL, Zhang YQ (2002) System of intelligent injection molding design by model-based reasoning. J Shanghai Jiaotong Univ 36(4):474–477 (in Chinese)

    Google Scholar 

  25. Lou ZL, Liu LY, Jiang HF et al (2002) Knowledge-based engineering in mold base design and its key technology. J Shanghai Jiaotong Univ 36(4):487–490 (in Chinese)

    Google Scholar 

  26. Zhu LP (2001) Research and development for injection mold design system based on CBR. Shanghai Jiaotong Univ, Shanghai (in Chinese)

    Google Scholar 

  27. Li CY, Li JJ, Wen JY et al (2001) Management and control of concurrent design process for progressive dies based on multi-intelligent agents. Forg Stamp Technol 26(1):60–62 (in Chinese)

    Google Scholar 

  28. Zhou L, Xia JK (2006) Interactive intelligent optimization design system for extrusiondie. Die Mould Indus 32(8):19–23 (in Chinese)

    Google Scholar 

  29. Shen JX, Gu ZC (1996) Injection mold base design based on UG. Machinery 12:12–14 (in Chinese)

    Google Scholar 

  30. Wang WH, Zhang XT, Yang LN et al (2005) Review on the investment casting die on aero-engine turbine blade and its research treads. Aeronaut Manufact Technol 6:26–29 (in Chinese)

    Google Scholar 

  31. Wang ZY, Wu SF, Qin HB (2004) Transformation technology from part design model to blank model. Comput Integr Manufact Syst 10(6):620–624 (in Chinese)

    Google Scholar 

  32. Qin HB, Wu SF, Hou ZL et al (2005) The manufacturing process planning based on blank model. Mie China 34(7):120–122 (in Chinese)

    Google Scholar 

  33. Zhu CK, Quan YT (2005) Automatic forming of the 3D solid molding draft of rough casting. Foundry 34(7):120–122 (in Chinese)

    Google Scholar 

  34. Xu YB, Fan Z, Ding JN et al (2005) Research on the MEMS CAD technology based on ACIS platform. Mach Des Manuf 10:79–81 (in Chinese)

    Google Scholar 

  35. Ma S, Wang YG (1994) Research on information modeling based on features and feature mapping. Comput Aided Eng 4:20–26 (in Chinese)

    Google Scholar 

  36. Liu W, Chen J (2006) Injection process information system based on UG NX 3.0. Die Mould Technol 4:51–52 (in Chinese)

    Google Scholar 

  37. Yang YC (2008) Research and application of model conversion for turbine blade. Northwestern Polytechnical University, Xi’an (in Chinese)

    Google Scholar 

  38. Liu XH (2008) Application and research of model -conversion for turbine guide vanes. Northwestern Polytechnical University, Xi’an (in Chinese)

    Google Scholar 

  39. Tan ST, Sze WS, Yuen MF et al (1990) Parting lines and parting surfaces of injection moulded parts. J Eng Manuf 204(4):211–221

    Article  Google Scholar 

  40. Ravi B, Srinivasan MN (1990) Design criteria for computer-aided parting surface design. Comput Aided Des 22(1):11–18

    Article  Google Scholar 

  41. Tu XW, Suo QD, Lou ZL (2003) On automatic searching of the parting line in injection mold design. Mech Sci Technol 22(6):865–868 (in Chinese)

    Google Scholar 

  42. Zhu XL, He FJ, Gao CP (1999) Computer-aided parting surface design. J Jilin Univ Technol (Nat Sci Ed) 29(3):30–34 (in Chinese)

    Google Scholar 

  43. Zhang P, Mo R, Wang ZQ et al (2000) Automatic parting surface design for turbine blade die based on rule. J Northwest Polytech Univ 18(2):310–315 (in Chinese)

    Google Scholar 

  44. Meng ZQ (2003) Research for parting design of turbo blade precise casting mould on the case-based reasoning (CBR). Northwestern Polytechnical University, Xi’an (in Chinese)

    Google Scholar 

  45. Srivastava MB, Brodersen RW (1991) Rapid-prototyping of hardware and software in an unified framework. In: IEEE International Conference on Computer-Aided Design, Piscataway, IEEE Service Center, NJ 152–155

    Google Scholar 

  46. Su Y (2003) Template design method for die structure of auto panel. Harbin Institute Technology, Harbin (in Chinese)

    Google Scholar 

  47. Hunter R, Vizan A, Perez J et al (2005) Knowledge model as an integral way to reuse the knowledge for fixture design process. J Mater Process Technol 164–165:1510–1518

    Article  Google Scholar 

  48. Shi L (2004) Research on the key technologies of computer integration design for auto panel die. Harbin Institute of Technology, Harbin (in Chinese)

    Google Scholar 

  49. Yang YY, Shi L, Su Y (2004) Template design of die structure of auto panel. China Mech Eng 15(10):902–904 (in Chinese)

    Google Scholar 

  50. Xin M (2005) Standard part intelligent selection method for investment casting die. Northwestern Polytechnical University, Xi’an (in Chinese)

    Google Scholar 

  51. Lim EM, Menq CH, Yen DW (1997) Integrated planning for precision machining of complex surfaces-III. Compensation of dimensional errors. Int J Mach Tools Manuf 9(37):1313–1326

    Google Scholar 

  52. Li Q, Wang SJ, Shen CY et al (2002) Predication of shrinkage in mold design. Electromach Mould 5:53–54 (in Chinese)

    Google Scholar 

  53. Jones S, Yuan C (2003) Advances in shell moulding for investment casting. J Mater Process Technol 135(2–3):258–265

    Article  Google Scholar 

  54. Ito M, Yamagishi T, Oshida Y (1996) Effect of selected physical properties of waxes on investments and casting shrinkage. J Prosthet Dent 75(2):211–216

    Article  Google Scholar 

  55. Ferreira JC, Mateus A (2003) A numerical and experimental study of fracture in RP stereolithography patterns and ceramic shells for investment casting. J Mater Process Technol 134(1):135–144

    Article  Google Scholar 

  56. Qi H, Yang Y, Jiang YM (2002) Numerical simulation of fluid flow and heat transfer during mold filling of casting. Foundry Technol 4(23):216–218 (in Chinese)

    Google Scholar 

  57. Song YH, Yan YN, Zhang RJ, Lu QP, Xu D (2001) Three dimensional non-linear coupled thermo-mechanical FEM analysis of the dimensional accuracy for casting dies in rapid tooling. Finite Elem Anal Des 38(1):79–91

    Article  MATH  Google Scholar 

  58. Modukuru SC, Ramakrishnan N, Sriramamurthy AM (1996) Determination of the die profile for the investment casting of aerofoil-shaped turbine blades using the finite-element method. J Mater Process Technol 58(2–3):223–226

    Article  Google Scholar 

  59. Zhang D, Zhang WH, Wan M et al (2006) Reversing design methodology of the die profile in investment casting based on the Simulation of displacement field and identification of featured parameters. Acta Aeronautica Et Astronautica Sinica 3:509–514 (in Chinese)

    Google Scholar 

  60. Bu K, Zhao J, Wang JF et al (2006) Exploring reliability and precision in mould optimization design of aero-Engine turbine blade. J Northwest Polytech Univ 1:80–83 (in Chinese)

    Google Scholar 

  61. Zhang JM (1998) Blade machining technology of SNECMA company in France. Aviat process Technol 2:21–23 (in Chinese)

    Google Scholar 

  62. Jiang YH (1993) Structural design and experiment on the composite shell mold for investment casting of turbine blade. Foundry 3:35–47 (in Chinese)

    Google Scholar 

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Author information

Authors and Affiliations

  1. Northwestern Polytechnical University, Xi’an, China

    Dinghua Zhang, Yunyong Cheng, Ruisong Jiang & Neng Wan

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  1. Dinghua Zhang
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  2. Yunyong Cheng
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  3. Ruisong Jiang
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  4. Neng Wan
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Correspondence to Dinghua Zhang .

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© 2018 National Defense Industry Press and Springer-Verlag GmbH Germany

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Zhang, D., Cheng, Y., Jiang, R., Wan, N. (2018). Introduction. In: Turbine Blade Investment Casting Die Technology. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-662-54188-3_1

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  • DOI: https://doi.org/10.1007/978-3-662-54188-3_1

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  • Publisher Name: Springer, Berlin, Heidelberg

  • Print ISBN: 978-3-662-54186-9

  • Online ISBN: 978-3-662-54188-3

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