{"id":332981,"date":"2024-10-19T23:12:11","date_gmt":"2024-10-19T23:12:11","guid":{"rendered":"https:\/\/pdfstandards.shop\/product\/uncategorized\/bs-s-1501975\/"},"modified":"2024-10-25T22:06:48","modified_gmt":"2024-10-25T22:06:48","slug":"bs-s-1501975","status":"publish","type":"product","link":"https:\/\/pdfstandards.shop\/product\/publishers\/bsi\/bs-s-1501975\/","title":{"rendered":"BS S 150:1975"},"content":{"rendered":"
PDF Pages<\/th>\n | PDF Title<\/th>\n<\/tr>\n | ||||||
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1<\/td>\n | BRITISH STANDARD AEROSPACE SERIES <\/td>\n<\/tr>\n | ||||||
2<\/td>\n | Committees responsible for this British\ufffdStandard <\/td>\n<\/tr>\n | ||||||
3<\/td>\n | Contents <\/td>\n<\/tr>\n | ||||||
5<\/td>\n | NOTE\ufffdThe specified heat treatment and tensile and stress rupture properties comply with AECMA Rec… 1 Inspection and testing procedure 1.1 General 1.2 Sulfur printing or deep etching tests 1.3 Ultrasonic examination 2 Manufacture 3 Chemical composition 4 Surface dressing <\/td>\n<\/tr>\n | ||||||
6<\/td>\n | 5 Condition 5.1 The material shall be supplied in the appropriate condition stated below: 5.2 Parts shall be supplied finally heat treated. 6 Heat treatment 6.1 Softening treatment 6.2 Final heat treatment 7 Mechanical properties 7.1 Tensile test at room temperature 7.2 Hardness test <\/td>\n<\/tr>\n<\/table>\n","protected":false},"excerpt":{"rendered":" Specification for chromium-molybdenum-vanadium-niobium heat-resisting steel billets, bars, forgings and parts (930-1080 MPa) (Cr 10.5, Mo 0.6, V 0.2, Nb 0.3)<\/b><\/p>\n |