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jet engine exhaust stacks

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Journal Articles
Alloy Digest (1966) 15 (11): SA-204.
Published: 01 November 1966
... HECLA EM, 20 is an iron-nickel-cobalt-chromium austenitic alloy steel having high oxidation and scaling resistance. It is recommended for high temperature service and medium loads up to 2000 F, such as turbine blading, jet engine exhaust stacks and combustion chambers. This datasheet provides...
Journal Articles
Alloy Digest (2002) 51 (5): SS-853.
Published: 01 May 2002
... improves weldability. Typical uses include furnace parts, heating elements, aircraft and jet engine parts, heat exchangers, carburizing-annealing boxes, sulfite liquor handling equipment, kiln liners, boiler baffles, refinery and chemical processing equipment, and auto exhaust parts. This datasheet...
Journal Articles
Alloy Digest (1968) 17 (8): SS-212.
Published: 01 August 1968
... and toughness. Forms Available: Bars, plates and sheet. Applications: .4pplicable for high-temperature service and medium loads up to 2OOO F. Rotors, turbine blad- ing, bolts for high-temperature applications, air- craft cabin heaters,exhaust stacks for jet engines, tail cones, afterburner rings...
Journal Articles
Alloy Digest (2004) 53 (1): SS-898.
Published: 01 January 2004
... 24 60 in. Applications: Typical applications for Type 347 are aircraft exhaust manifolds, collector rings, expansion joints, furnace stacks and dampers, high-temperature applications to 900 °C (1650 °F), jet engine parts, and tubing in heat exchangers. Type 348 is often used in handling primary water...