Response of SiC/SiC to Transient Thermal Conditions [electronic resource] : A Review.

The database on thermal shock behavior of SiC/SiC composites is very limited. The existing data suggests continuous fiber ceramic matrix composites, such as SiC/SiC, exhibit very good thermal shock characteristics but most data was obtained for -Delta T conditions as a result of quenching from an el...

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Bibliographic Details
Online Access: Online Access
Corporate Author: Pacific Northwest National Laboratory (U.S.) (Researcher)
Format: Government Document Electronic eBook
Language:English
Published: Washington, D.C : Oak Ridge, Tenn. : United States. Dept. of Energy ; distributed by the Office of Scientific and Technical Information, U.S. Dept. of Energy, 2001.
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MARC

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245 0 0 |a Response of SiC/SiC to Transient Thermal Conditions  |h [electronic resource] :  |b A Review. 
260 |a Washington, D.C :  |b United States. Dept. of Energy ;  |a Oak Ridge, Tenn. :  |b distributed by the Office of Scientific and Technical Information, U.S. Dept. of Energy,  |c 2001. 
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500 |a Published through the Information Bridge: DOE Scientific and Technical Information. 
500 |a 06/30/2001. 
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500 |a Fusion Materials: Semi-Annual Progress Report for Period Ending June 30, 2001, 30:45-54. 
500 |a Jones, Russell H. 
520 3 |a The database on thermal shock behavior of SiC/SiC composites is very limited. The existing data suggests continuous fiber ceramic matrix composites, such as SiC/SiC, exhibit very good thermal shock characteristics but most data was obtained for -Delta T conditions as a result of quenching from an elevated temperature. Thermal shock in a fusion energy system will result from plasma discharge and will result in a +Delta T. One study was reported for SiC/SiC composites given a +Delta T with no loss in strength following 25 cycles at a heating rate of 1700 degrees C/s. Monolithic SiC failed in 1.5 cycles at a heating rate of 1400 degrees C/s. Thermal fatigue test results also suggest that SiC/SiC composites will exhibit little or no degradation for 100's of cycles. It was estimated that radiation could, in an extreme case, cause a reduction in the thermal shock performance from a calculated Delta Tc of 957K to about 300K if the fiber strength is reduced by 50%. Newer composites with greater radiation resistance should have a much smaller change in the Delta Tc. 
536 |b AC05-76RL01830. 
650 7 |a Ceramics.  |2 local. 
650 7 |a Radiations.  |2 local. 
650 7 |a Heating Rate.  |2 local. 
650 7 |a Transients.  |2 local. 
650 7 |a Plasma.  |2 local. 
650 7 |a Thermal Shock.  |2 local. 
650 7 |a Thermal Fatigue.  |2 local. 
650 7 |a Quenching.  |2 local. 
650 7 |a Performance.  |2 local. 
650 7 |a Fibers.  |2 local. 
650 7 |a Silicon Carbides.  |2 local. 
650 7 |a Thermonuclear Reactors.  |2 local. 
650 7 |a Plasma Physics And Fusion Technology.  |2 edbsc. 
710 2 |a Pacific Northwest National Laboratory (U.S.).  |4 res. 
710 1 |a United States.  |b Department of Energy.  |4 spn. 
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