?u= Tue, 05 Nov 2024 16:34:39 +0000 en-US hourly 1 https://wordpress.org/?v=6.7.1 ?u=/wp-content/uploads/2024/11/cropped-icon-150x150.png ?u= 32 32 ?u=/product/publishers/din/din-en-4866/ Tue, 05 Nov 2024 16:34:39 +0000 Aerospace series - Definitions of imperfections and defects in organic matrix composite materials

Published By	Publication Date	Number of Pages
DIN	2022-07	108

]]> This document provides a list of terms with their definitions illustrated by typical photographs, in order to define a common vocabulary on the imperfections and damage that may occur during manufacture on organic matrix composite materials (which will be called "resin" along this document). Some types of damage may also be encountered in use. This document is restricted to their definitions and does not give any acceptance criteria. The word "imperfection" will be preferred to the word "defect", although the word "defect" might be usually used. Defect acceptance criteria to be discussed between the user and customer and documented appropriately between the two parties.

]]> ?u=/product/publishers/din/din-en-4385/ Tue, 05 Nov 2024 16:29:41 +0000 Aerospace series - Non-metallic materials - General organization of standardization - Links between types of standards

Published By	Publication Date	Number of Pages
DIN	2022-07	20

]]> This document specifies the general organization of the EN standards for non-metallic materials and their links with other types of standards for aerospace applications. It corresponds to level 0 (see 4.1).

]]> ?u=/product/publishers/din/din-en-4387/ Tue, 05 Nov 2024 16:29:41 +0000 Aerospace series - Non-metallic materials - Rules for drafting and presentation of technical specifications

Published By	Publication Date	Number of Pages
DIN	2022-07	47

]]> This document specifies the general rules for drafting and presentation of EN aerospace series non-metallic material technical specifications.

]]> ?u=/product/publishers/din/din-en-4382/ Tue, 05 Nov 2024 16:29:41 +0000 Aerospace series - Heat resisting alloy NI-PH3601 (NiCr22Mo9Nb) - Solution treated - Seamless tubes - For hydraulic application - D =50 mm, a =3 mm

Published By	Publication Date	Number of Pages
DIN	2007-04	14

]]> This standard specifies the requirements relating to: Heat resisting alloy NI-PH3601 (NiCr22Mo9Nb) – Solution treated – Seamless tubes – For hydraulic application D =50 mm, a =3 mm for aerospace applications.

]]> ?u=/product/publishers/din/din-en-4379/ Tue, 05 Nov 2024 16:29:34 +0000 Aerospace series - Heat resisting alloy NI-PH3601 (NiCr22Mo9Nb) - Solution treated, forging De = 200 mm

Published By	Publication Date	Number of Pages
DIN	2008-09	17

]]> This standard specifies the requirements relating to: Heat resisting alloy NI-PH3601 (NiCr22Mo9Nb) – Solution treated, forging De = 200 mm for aerospace applications.

]]> ?u=/product/publishers/din/din-en-4373/ Tue, 05 Nov 2024 16:29:31 +0000 Aerospace series - Heat resisting alloy NI-PD9001 (NiCu31) - Annealed, seamless tube D = 75 mm, a = 3 mm

Published By	Publication Date	Number of Pages
DIN	2008-03	17

]]> This standard specifies the requirements relating to: Heat resisting alloy NI-PD9001 (NiCu31) Annealed – Seamless tube, D 75 mm, a 3 mm for aerospace applications.

]]> ?u=/product/publishers/din/din-en-4245/ Tue, 05 Nov 2024 16:29:06 +0000 Aerospace series - Heat resisting alloy FE-PM1708 - Vacuum arc remelted - As forged - Forging stock - De = 300 mm

Published By	Publication Date	Number of Pages
DIN	2020-05	20

]]> This document specifies the requirements relating to: Heat resisting alloy FE-PM1708, vacuum arc remelted, as forged, forging stock, De = 300 mm, for aerospace applications.

]]> ?u=/product/publishers/din/din-en-4244/ Tue, 05 Nov 2024 16:29:04 +0000 Luft- und Raumfahrt - Hochwarmfeste Legierung FE-PM1708 - Lichtbogenvakuumerschmolzen - Gehärtet und angelassen - Stangen - a oder D = 200 mm - 1 000 MPa = Rm = 1 140 MPa

Published By	Publication Date	Number of Pages
DIN	2020-05	20

]]> Dieses Dokument legt die Anforderungen an hochwarmfeste Legierung FE-PM1708, lichtbogenvakuumerschmolzen, gehärtet und angelassen, Stangen, a oder D = 200 mm, 1000 MPa = Rm = 1140 MPa für Anwendungen in der Luft und Raumfahrt fest.*Inhaltsverzeichnis

]]> ?u=/product/publishers/din/din-en-3864/ Tue, 05 Nov 2024 16:26:42 +0000 Luft- und Raumfahrt - Nichtmetallische Werkstoffe - Transparente Glaswerkstoffe - Prüfverfahren - Bestimmung des Bruchmoduls

Published By	Publication Date	Number of Pages
DIN	2013-08	18

]]> Diese Norm legt die Anforderungen für die Bestimmung des Bruchmoduls von transparenten Glaswerkstoffen für Luftfahrzeuganwendungen fest, entweder im entspannten oder im chemisch oder thermisch gespannten Zustand.*Inhaltsverzeichnis

]]> ?u=/product/publishers/din/din-en-3863/ Tue, 05 Nov 2024 16:26:42 +0000 Aerospace series - Non-metallic materials - Glass tranparencies - Test methods - Determination of flatness

Published By	Publication Date	Number of Pages
DIN	2013-05	18

]]> This standard defines the requirements for the determination of the flatness of monolithic glass transparencies for aircraft applications. The method is designed to eliminate the effect of the glass deflecting under its own weight, thus eliminating false results.

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