An Optimum Application of Austenitic Nodular Iron for Gas Turbine Components
Keyword(s):
A new modification of an economical casting material is presented for use in the intermediate temperature range, which is considered to be 800 to 1300 F. An illustration is given of two large castings actually produced for the 1500-hp ATAC regenerative gas turbines engine. Comparisons are made with other materials, giving information stress-rupture at various temperature levels and some cost information. Also included are design suggestions for better utilization of foundry techniques.
Relaxation of Dielectric Loss Peak over Intermediate Temperature Range in Bi 5 TiNbWO 15 Intergrowth
2009 ◽
Vol 26
(4)
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pp. 047701
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Keyword(s):
2017 ◽
Vol 5
(42)
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pp. 22224-22233
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1991 ◽
Vol 23
(1)
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pp. 171-177
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Keyword(s):
2011 ◽
Vol 509
(24)
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pp. 6889-6892
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2017 ◽
Vol 35
(7)
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pp. 641-646
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1993 ◽
Vol 32
(Part 1, No. 5B)
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pp. 2230-2233