The 9ni 4co Steels
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Author | : T. P. Groeneveld |
Publisher | : |
Total Pages | : 22 |
Release | : 1966 |
Genre | : Steel, High strength |
ISBN | : |
This memorandum briefly discusses the physical metallurgy, heat treatment, mechanical properties, stress-corrosion properties, and fabrication of the 9Ni-4Co-XC steels. This family of steels was developed specifically to meet the requirements of the aircraft and aerospace industries for materials possessing high strength and high toughness. By varying the composition and heat treatment, the 9Ni-4Co-xC steels can develop strengths in the 200 to 300 ksi tensile-strength range and reportedly possess high toughness. The lower carbon grades have excellent weldability, developing strength in the 180 to 200 ksi range with high toughness without the need for preheat or postweld-heat treatment. (Author).
Author | : A. J. Hiller |
Publisher | : |
Total Pages | : 20 |
Release | : 1967 |
Genre | : |
ISBN | : |
Author | : |
Publisher | : |
Total Pages | : 94 |
Release | : 1967 |
Genre | : Nickel steel |
ISBN | : |
The DMIC Handbook on 9Ni-4Co steels presents available information and data covering the metallurgy, manufacturing, and mechanical properties of these steels. The metallurgical portion summarizes melting, primary working, and compositional aspects. The manufacturing portion covers forming, heat treating, and welding, each of which is a concern of the users of these steels. Mechanical properties presented include room and elevated-temperature tensile, fatigue, and limited compressive and shear data for the 0.25 and 0.45 carbon grades. Twenty-nine references are included. (Author).
Author | : M. D. McAninch |
Publisher | : |
Total Pages | : 462 |
Release | : 1991 |
Genre | : Steel |
ISBN | : |
Author | : S. J. Matas |
Publisher | : |
Total Pages | : 17 |
Release | : 1965 |
Genre | : Chromium |
ISBN | : |
The effects of alloy content and heat treatment on the strength and toughness of 9Ni-4Co alloy steels are discussed in detail. The strength was determined with standard tension specimens, while toughness was evaluated with various accepted, sharply notched specimen types. Of the alloying elements used, carbon acted as the strongest embrittler but was necessary as a strengthener. Silicon and the carbide-forming elements decreased toughness, particularly at higher carbon contents. Hence, the use of silicon at other than residual levels was undesirable. The addition of carbide-forming elements in appreciable amounts needed careful consideration. Nickel was used in substantial amounts to improve toughness, while cobalt was added to inhibit retained austenite formation consequent upon the high nickel content. Cobalt enhanced self-tempering effects, particularly for the lower carbon varieties. Heat treatment strongly influenced the properties as a result of the attendant changes in the microstructure. Isothermal transformation to lower bainite enhanced toughness in the 0.45%C, 9%Ni-4% Co high performance (HP) 9-4-45 steel. The toughness was superior to that of tempered martensite at equivalent strengths. The properties of upper bainite were not as attractive as those of lower bainite. Mixed structures composed of bainite and martensite lowered toughness. The two commercial grades of the 9Ni-4Co alloy system, HP 9-4-25 and HP 9-4-45, had a better combination of strength and toughness than other carbon-strengthened steels. The self-tempering characteristics of the HP 9-4-25 grade and its inherent toughness contributed to high joint efficiences and formability in the as-welded condition. No post-heat treatment of the welded joint was required.
Author | : D. F. Bulloch |
Publisher | : |
Total Pages | : 179 |
Release | : 1968 |
Genre | : Cobalt alloys |
ISBN | : |
Material characterization data and design allowables were determined for two grades of the 9Ni-4Co steel group: 9Ni-4Co-0.30C quenched and tempered to 220-240 ksi tensile ultimate strength, and 9Ni-4Co-0.45C quenched to a bainitic structure with 260 to 280 ksi tensile ultimate strength. The effects of chemistry and processing variations on mechanical properties were evaluated by testing three heats of 9Ni-4Co-0.30C and four heats of 9Ni-4Co-0.45C. Both alloys were vacuum-arc-remelted with carbon deoxidation. Tension, compression, shear, and bearing allowables were developed per MIL-HDBK-5 guidelines in three grain directions at temperatures from -110F to 500F. The 9Ni-4Co-0.30C and 9Ni-4Co-0.45C were found suitable for aircraft structural forgings with minimum tensile ultimate strengths of 220 ksi and 260 ksi respectively. Material characterization data showed that both alloys have good stress corrosion resistance, competitive derived mechanical properties and fatigue properties, and satisfactory metallurgical stability. Grain direction did not significantly influence their mechanical properties. The 9Ni-4Co-0.30C showed superior plane-strain fracture toughness, whereas the 9Ni-4Co-0.45C compared favorably with other steels in the same strength range. Both showed excellent resistance when tested for delayed fracture in salt water. On the basis of the data obtained in this program, a proposed Military Material Specification was drafted for both alloys. (Author).
Author | : |
Publisher | : |
Total Pages | : 238 |
Release | : 1965 |
Genre | : Technology & Engineering |
ISBN | : |
Author | : Batelle Memorial Institute, Columbus, Ohio. Defense Metals Information Center |
Publisher | : |
Total Pages | : |
Release | : 1966 |
Genre | : Nickel steel |
ISBN | : |
Author | : H. Lee Craig |
Publisher | : ASTM International |
Total Pages | : 440 |
Release | : 1976 |
Genre | : |
ISBN | : |
Author | : American Society for Testing and Materials |
Publisher | : ASTM International |
Total Pages | : 336 |
Release | : 1970 |
Genre | : Corrosion and anti-corrosives |
ISBN | : |