Research on Cryogenic Pneumatic Mist Jet Impinging Cooling and Lubricating of Grinding Processes

Article Preview

Abstract:

Grinding, characterized by its high specific energy consumption, may generate high grinding zone temperature. These can cause thermal damage to the ground surface and poor surface integrity, especially in the grinding of difficult-to-machine materials. Conventional cooling methods based on large amounts of water-oil emulsions can be both ineffective and environmentally unacceptable. Here a new high efficiency cooling technology—cryogenic pneumatic mist jet impinging cooling technology is offered. It utilizes the high penetrative power of fast cryogenic air jet combined with a little quantity of 0°C water to greatly improve heat transfer effects in the machining zone. The experimental results indicated that CPMJI could offer better machining effects compared to cold air jet and traditional flood cooling method in the grinding of titanium alloy.

You might also be interested in these eBooks

Info:

Periodical:

Key Engineering Materials (Volumes 359-360)

Pages:

460-464

Citation:

Online since:

November 2007

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2008 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

[1] X. Li: Proceedings of 34th National Heat Transfer Conference (Pittsburgh, USA, 2000) pp.595-601.

Google Scholar

[2] H.J. Xu, Y.C. Fu and et al: Science in China Series E, Vol. 45 (2002), pp.261-272.

Google Scholar

[3] S. Paul and A. B. Chattopadhyay: Cryogenics, Vol. 35 (1995), pp.515-523.

Google Scholar

[4] H. Z. Choi and S.W. Lee: 1st International Euspen Conference (Bremen, Germany, 1999) Vol. 1, pp.416-419.

Google Scholar

[5] Q.L. An, Y.C. Fu and et al: Key Eng. Mat., Vol. 315-316 (2006), pp.244-248.

Google Scholar

[6] M.R. Schumack, J.B. Chung and et al: Transactions of the ASME, Vol. 113 (1991), pp.190-197.

Google Scholar

[7] Q.L. An: Cryogenic Mist Jet Impinging Cooling and Its Application in Machining of Titanium Alloy (Ph.D. Dissertation, Nanjing University of Aeronautics & Astronautics, China 2006), pp.89-90.

Google Scholar