DIN 65169:2017-07
Aerospace - Brazed and high-temperature brazed components - Directions for design
| Fecha edición: |
2017-07-01
En Vigor
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| Idiomas disponibles: | Alemán |
| Resumen: | This standard applies to the design of brazed and high-temperature brazed metallic components for aerospace use. To achieve brazings of high quality and high component safety, a number of factors has to be considered: base material, solder and auxiliary material, joint configuration, surface preparation, procedures such as furnace brazing, flame brazing, induction brazing, utilization of jigs or fixtures, mechanical stresses, tightness, corrosion resistance, operating temperature of the component, suitability for repair and inspection. |
| Keywords: | Aeronautical equipment|Aerospace transport|Air transport|Aircraft components|Auxiliary materials|Brazing|Components|Design|High-temperature brazing|Inspection|Joining processes|Materials|Pre-treatment of surfaces|Repair|Repairs|Soldered joints|Solderings|Sounding heads|Space transport|Specification (approval)|Strength of materials|Testing|Torch brazing|Welding |
| ICS: | 49.035 - Componentes para la construcción aeroespacial |
| CTN: | |
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Reemplazo Normas |
Reemplaza a DIN 65169:1986-10 Reemplaza a DIN 65169:2016-08 |
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