Author: Charles A. HoffmanPublisher:
ISBN:
Category : Carbides
Languages : en
Pages : 56
Book Description
The investigation indicated promise for this material used in gas-turbine-blade applications.
Initial Investigation of Carbide-type Ceramal of 80-percent Titanium Carbide Plus 20-percent Cobalt for Use as Gas-turbine-blade Material
Author: Charles A. HoffmanPublisher:
ISBN:
Category : Carbides
Languages : en
Pages : 56
Book Description
The investigation indicated promise for this material used in gas-turbine-blade applications.
Catalog of Technical Reports
Author: Business and Defense Services AdministrationPublisher:
ISBN:
Category :
Languages : en
Pages : 920
Book Description
High-temperature Protection of a Titanium-carbide Ceramal with a Ceramic-metal Coating Having a High Chromium Content
Author: Dwight G. MoorePublisher:
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.
Technical Information Pilot
Author: Catalog of Technical Reports
Author: United States. Dept. of Commerce. Office of Technical ServicesPublisher:
ISBN:
Category :
Languages : en
Pages : 742
Book Description
Investigation of Bonding Between Metals and Ceramics
Author: H. J. HamjianPublisher:
ISBN:
Category : Boron compounds
Languages : en
Pages : 30
Book Description
The experiments conducted with boron carbide and each of four metals showed that nickel, cobalt, and iron formed a bonding zone between the metal and the ceramic and that chromium showed satisfactory physical wetting characteristics on the ceramic.
Mechanical Properties at Room Temperature of Four Cermets of Titanium Carbide with Nickel Binder
Author: Aldie E. JohnsonPublisher:
ISBN:
Category : Binders (Materials)
Languages : en
Pages : 670
Book Description
Room-temperature stress-strain curves are presented for compression, tension, and shear loadings of four compositions of titanium carbide with nickel binder. Values of ultimate strength, modulus of elasticity, modulus of rigidity, Poisson's ratio in the elastic region, density, and hardness for the four materials are tabulated.
Bibliography of Technical Reports
Author: Technical Note - National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for AeronauticsPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 526
Book Description
Investigation of Fretting Corrosion by Microscopic Observation
Author: Douglas GodfreyPublisher:
ISBN:
Category : Fretting corrosion
Languages : en
Pages : 690
Book Description
Fretting corrosion was concluded to be caused by the removal of finely divided and apparently virgin material due to inherent forces and that its primary reaction is independent of of vibratory motion or high sliding speeds. Fretting corrosion occurred to clean nonmetals and metals readily and glass microscope slides and steel balls provided an excellent method for visual studies.