{"id":334290,"date":"2024-10-19T23:18:28","date_gmt":"2024-10-19T23:18:28","guid":{"rendered":"https:\/\/pdfstandards.shop\/product\/uncategorized\/bs-en-30012019\/"},"modified":"2024-10-25T22:16:31","modified_gmt":"2024-10-25T22:16:31","slug":"bs-en-30012019","status":"publish","type":"product","link":"https:\/\/pdfstandards.shop\/product\/publishers\/bsi\/bs-en-30012019\/","title":{"rendered":"BS EN 3001:2019"},"content":{"rendered":"
This document specifies the requirements for tempered soda-lime float glass plies which are made from annealed glass either of the universally available type or of high light transmission type. The annealed glass is manufactured by a continuous process for general use. The plies are tempered by either a thermal or chemical process. The tempered glass is used mainly for cockpit glazing.<\/p>\n
PDF Pages<\/th>\n | PDF Title<\/th>\n<\/tr>\n | ||||||
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2<\/td>\n | National foreword <\/td>\n<\/tr>\n | ||||||
6<\/td>\n | 1 Scope 2 Normative references <\/td>\n<\/tr>\n | ||||||
7<\/td>\n | 3 Terms and definitions 4 Required characteristics 4.1 Composition 4.2 Material <\/td>\n<\/tr>\n | ||||||
8<\/td>\n | 4.3 Standard thickness ) 4.4 Dimensions 4.5 Density 4.6 Linear expansion 4.7 Flatness 4.8 Refractive index 4.9 Light transmission 4.10 Haze 4.11 Optical distortion <\/td>\n<\/tr>\n | ||||||
9<\/td>\n | 4.12 Optical defects 4.13 Bending and thermal tempering optical defects 4.13.1 Bending marks 4.13.2 Checker pattern 4.13.3 Tong impressions 4.14 Strength 4.14.1 Modulus of rupture <\/td>\n<\/tr>\n | ||||||
10<\/td>\n | 4.14.2 Stress profile 5 Quality assurance 5.1 Qualification 5.2 Batch acceptance tests 6 Storage and packing 7 Marking 8 Ordering <\/td>\n<\/tr>\n<\/table>\n","protected":false},"excerpt":{"rendered":" Aerospace series. Tempered float glass plies for aircraft applications. Technical specification<\/b><\/p>\n |