B.S. S 117 Structural and constructional steels
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B.S. S 117 Chemical Composition
BS 2S 117: 1964 / Specification for aircraft material. 1 per cent chromium steel (55/65 tonf/sq in: limiting ruling section 1⅛ inch)
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B.S. S 117 Physical Properties
Temperature
This material has 19 properties — only a subset is shown here.
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B.S. S 117 Heat Treatments
- The final heat treatment shall be:
a) Hardening in oil from a temperature between 860-890°C
b)Temper at a suitable temperature between 550-700°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 117 Mechanical Properties
Temperature
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B.S. S 117 International Equivalent Materials
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Equivalence categories reflect chemical-composition and mechanical-property comparison — always verify suitability against the governing specification for your application.
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- 3Cross References
- 6Composition
- 6Mechanical Properties
- 3Physical Properties
- 1Heat Treatment
- -Metallography
- -Machinability
- -Stress-Strain
- -Formability
- -Fatigue
- -Fracture
- -Creep
- -Joints
- -Coatings
- -Dimensions
- -Tribology
- -Corrosion
- -Ageing
- -Weatherability
- -Irradiation
- -Total Suppliers