B.S. S 114 Structural and constructional steels
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B.S. S 114 Chemical Composition
BS 2S 114: 1964 / Specification for aircraft material. Manganese-molybdenum steel (55/65 tonf/sq in: limiting ruling section 2½ inches)
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B.S. S 114 Physical Properties
Temperature
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B.S. S 114 Heat Treatments
- The final heat treatment shall be:
a) Hardening in oil from a temperature between 840-870°C
b)Temper at a suitable temperature between 550-680°C.
Hardened and tempered bars which have been subjected to a cold straightening or cold rolling operation shall be given a stress relieving treatment which shall be sufficient to restore proof stress.
B.S. S 114 Mechanical Properties
Temperature
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- 5Cross References
- 6Composition
- 5Mechanical Properties
- 3Physical Properties
- 1Heat Treatment
- -Metallography
- -Machinability
- -Stress-Strain
- -Formability
- -Fatigue
- -Fracture
- -Creep
- -Joints
- -Coatings
- -Dimensions
- -Tribology
- -Corrosion
- -Ageing
- -Weatherability
- -Irradiation
- -Total Suppliers