High-temperature Protection of a Titanium-carbide Ceramal with a Ceramic-metal Coating Having a High Chromium Content PDF Download
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Author: Dwight G. Moore Publisher: ISBN: Category : Ceramic metals Languages : en Pages : 40
Book Description
At a blade temperature of 1800 degrees F, this coating would probably greatly prolong the life of a K-138 turbine blade under operating conditions sufficiently severe to accelerate failure of the uncoated blade by oxidation.
Author: Dwight G. Moore Publisher: ISBN: Category : Ceramic metals Languages : en Pages : 40
Book Description
At a blade temperature of 1800 degrees F, this coating would probably greatly prolong the life of a K-138 turbine blade under operating conditions sufficiently severe to accelerate failure of the uncoated blade by oxidation.
Author: Dwight G. Moore Publisher: ISBN: Category : Titanium carbide Languages : en Pages : 26
Book Description
Four ceramic-metal coatings of varying frit content were prepared and applied to ceramals containing 80 percent chromium and 20 percent cobalt. Oxidation penetration, transverse breaking load, and thermal shock resistance of the various specimens were determined after prolonged heating in air at temperatures of 1650, 1800, 2000, and 2200 degrees F. The effects of varying firing time, firing temperature, and number of coats applied were studied for one coating.
Author: United States. Business and Defense Services Administration. Iron and Steel Division Publisher: ISBN: Category : Chromium Languages : en Pages : 116
Author: Dwight G. Moore
Author: Dwight G. Moore
Author: Dwight G. Moore
Author: 
Author: United States. National Advisory Committee for Aeronautics
Author: Business and Defense Services Administration
Author: 
Author: United States. National Advisory Committee for Aeronautics
Author: 
Author: United States. Business and Defense Services Administration
Author: United States. Business and Defense Services Administration. Iron and Steel Division