Title of article :
Thermal Stresses and Cracks During the Growth of Large-sized Sapphire with SAPMAC Method
Author/Authors :
Chenghai، نويسنده , , Xu and Songhe، نويسنده , , Meng and Mingfu، نويسنده , , Zhang and Hongbo، نويسنده , , Zuo and Guigen، نويسنده , , Wang، نويسنده ,
Issue Information :
روزنامه با شماره پیاپی سال 2007
Pages :
6
From page :
475
To page :
480
Abstract :
The finite-element method has been used to study the thermal stress distribution in large-sized sapphire crystals grown with the sapphire growth technique with micro-pulling and shoulder-expanding at cooled center (SAPMAC) method. A critical defect model has been established to explain the growth and propagation of cracks during the sapphire growing process. It is demonstrated that the stress field depends on the growth rate, the ambient temperature and the crystallizing direction. High stresses always exist near the growth interfaces, at the shoulder-expanding locations, the tailing locations and the sites where the diameters undergo sharp changes. The maximum stresses always occur at the interface of seeds and crystals. Cracks often form in the critical defect region and spread in the m-planes and a-planes under applied tensile stresses during crystal growth. The experimental results have verified that with the improved system of crystal growth and well-controlled techniques, the large-sized sapphire crystals of high quality can be grown due to absence of cracks.
Keywords :
Thermal Stress , Sapphire , Crack , SAPMAC method
Journal title :
Chinese Journal of Aeronautics
Serial Year :
2007
Journal title :
Chinese Journal of Aeronautics
Record number :
2264676
Link To Document :
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