Toimialayhteisöt

 

This document specifies the application method and quality assurance for aluminium pigmented coatings as per EN 4473 for fasteners or other parts in titanium, titanium alloys, nickel or cobalt based alloys and corrosion resisting steels.

 

1 Scope 1.1 In scope This document describes: - the fundamentals and concepts for Long Term Archiving and Retrieval of CAD 3D mechanical composite information and associated composite specific PMI; - the document structure of the EN 9300-3XX family, and the links between all these parts; - the qualification methods for long term preservation of archived composite information; more specially, principles for the validation properties and for verification of the quality of the composite information archived; - specifications for the preservation planning of archived composite information; - specific functions for administration and monitoring of CAD composite archived models; - the definition of Archive Information Packages for composite CAD data. This document establishes long term archiving requirements applicable to, but not limited to, most laminated type composite items made with composite manufacturing processes such as: - hand lay-up; - tape laying; - fibre placement; - stitched resin film infusion (SRFI); - resin transfer moulding (RTM); - vacuum-assisted resin transfer moulding (VARTM); - controlled Atmospheric Pressure Resin Infusion (CAPRI); - co-cured or co-bonded composite items; - sandwich panel composite construction; - braided layers. 1.2 Out of scope The following is outside the scope of this part of EN 9300: - multi-function advanced composite structure; - composite items made with composite manufacturing processes such as filament winding, 3D braiding, or 3D weaving; NOTE Braided parts that can be represented as layered braided sleeve material can be in scope. - injection moulded fibre reinforced thermoplastics; - other Additive Manufacturing processes such as those covered by ISO/ASTM 52900; - PMI described in EN 9300-1xx series.

 

ISO 13164-1:2013 gives general guidelines for sampling, packaging, and transporting of all kinds of water samples, for the measurement of the activity concentration of radon-222. The test methods fall into two categories: a) direct measurement of the water sample without any transfer of phase (see ISO 13164-2); b) indirect measurement involving the transfer of the radon-222 from the aqueous phase to another phase (see ISO 13164-3). The test methods can be applied either in the laboratory or on site. The laboratory is responsible for ensuring the suitability of the test method for the water samples tested.

 

ISO 13164-3:2013 specifies a test method for the determination of radon-222 activity concentration in a sample of water following its transfer from the aqueous phase to the air phase by degassing and its detection. It gives recommendations for rapid measurements performed within less than 1 h. The radon-222 activity concentrations, which can be measured by this test method utilizing currently available instruments, range from 0,1 Bq l-1 to several hundred thousand becquerels per litre for a 100 ml test sample. This test method is used successfully with drinking water samples. The laboratory is responsible for ensuring the validity of this test method for water samples of untested matrices. This test method can be applied on field sites or in the laboratory. Annexes A and B give indications on the necessary counting conditions to meet the required sensitivity for drinking water monitoring

 

 

This document specifies requirements for testing of products manufactured from vitrified clay and other materials specified in the following standards: - pipes, fittings and joints according to EN 295-1; - adaptors, connectors and flexible couplings according to EN 295-4; - perforated pipes and fittings according to EN 295-5; - components of manholes and inspection chambers according to EN 295 6; - pipes and joints for pipe jacking according to EN 295-7.

 

This document specifies the requirements for the validation of the structural integrity for the following running gear structural components: - Components in the load path between the track and the car body (e.g. bogie frame, axlebox, or other equivalent components) and - Components that are in the traction and braking load paths without secondary retention. The following components are excluded from the scope of this document: - Structural components that are rigidly attached to the car body (e.g. bolsters directly attached to the car body or connected via slewing rings, centre pivots, etc.); - Equipment structures (e.g. traction motor housings, gearbox housings, and brake units), including components that are rigidly attached to them, that are not in the load path between the track and the car body; - Components for which the structural integrity validation requirements are regulated by other specific EN standards (e.g. wheels, axles, brake discs, bearings, coil springs etc.); - Suspension components including springs, dampers, elastic elements and their connecting elements; - Revolving components (e.g. drive train components etc.).

 

This document supports and complements the implementation of the risk management process defined in ISO 17666 in situations when the application of a quantitative risk assessment is deemed necessary. This document defines the principles, process, implementation and requirements for conducting a quantitative risk assessment and explains the details of probabilistic risk assessment (PRA) as applied to space system safety, reliability, and quality assurance (SR&QA). While PRA can be applied to project risk management involving cost and schedule, this application is outside the scope of this document. This document provides the basic requirements and procedures for the use of PRA techniques to assess safety risk and mission success risk in space programmes and projects. This document is applicable to all international space projects involving: 1. the design of space vehicles for the transportation of personnel in space; 2. the design of space and non-terrestrial planetary stations inhabited by human beings; 3. the design of space and launch vehicles powered by, or carrying, nuclear materials; 4. the design of autonomous space and launch vehicles controlled smart software programs/systems or artificial intelligence software programs/systems; 5. other projects as directed by the authorities or clients. These types of projects generally involve scenarios, chains of events or activities that could result in the death of, or serious injury to, members of the public, astronauts or pilots, or the workforce, or the loss of critical or high-value equipment and property. For other types of projects, it is intended that PRA be performed at the discretion of the project management.

 

Tämä standardi on laadittu eurooppalaisia yhdenmukaistettuja tuotestandardeja SFS-EN 771-1:2012 + A1:2015, SFS-EN 771-2:2012 + A1:2015, SFS-EN 771-3:2012 + A1:2015, SFS-EN 771-4:2012 + A1:2015, SFS-EN 771-6:2012 + A1:2015, SFS-EN 845-1:2013 + A1:2016, SFS-EN 845 2:2013 + A1:2016 sekä SFS-EN 998 2:2016 täydentäväksi kansalliseksi soveltamisstandardiksi. Tässä soveltamisstandardissa esitetään suositus, mitkä ominaisuudet on ilmoitettava ko. tuotestandardien mukaan CE-merkityille muuratuille tuotteille (poltetut tiilet, kalkkihiekkatiilet ja -harkot, kevytsorabetoniharkot, höyrykarkaistut kevytbetoniharkot, luonnonkivimuurauskappaleet, muurauslaastit mukaan lukien yleislaastit, ohutsaumalaastit ja kevytlaastit, rakoseinän muuraussiteet, konsolit sekä ylityspalkit) eri käyttökohteissa sekä ominaisuuksille asetetut vähimmäisvaatimustasot tai luokat.

 

This document specifies requirements for flat products for pressure purposes made of stainless steels, including austenitic creep-resisting steels, in thicknesses as specified in Tables 7 to 10. The requirements and definitions of ISO 9328-1 also apply to this document.

 

 

1.1 This document specifies the technical delivery conditions for forgings and for rolled or forged bars for construction of pressure equipment manufactured from the following steels: — non-alloy and alloy ferritic or martensitic steels with specified room temperature properties and supplementary requirements for elevated temperature properties, — nickel steels with specified low temperature properties, — weldable fine grain steels with high proof strength, — stainless steels. NOTE The term forgings covers open die forgings including ring rolled products as well as closed die forgings. 1.2 In addition to the requirements of this document, the general technical delivery requirements in ISO 404 apply, unless otherwise indicated.

 

This document specifies the technical delivery requirements for Non-alloy and alloy (Mo, Cr and CrMo) steels with specified elevated temperature properties for pressure equipment,which comply with the chemical composition of steels given in Table 1. This document applies to forgings and rolled or forged bars in thicknesses up to 250 mm (partly up to 500 mm) manufactured from the steels listed in Table 1 and to be delivered according to the specifications given in ISO 9327-1.

 

This document applies to forgings and rolled or forged bars in thicknesses up to 50 mm manufactured from the steels which comply to the chemical composition of steels given in Table 1 and to be delivered according to the specifications given in ISO 9327-1.

 

This document applies to forgings and rolled or forged bars in thicknesses up to 250 mm manufactured from fine grain steels (see NOTE 1) which comply with the chemical composition of steels given in Table 1 and to be delivered according to the specifications given in ISO 9327-1. NOTE 1 Fine grain steels are here understood as steels with grain size 6 or finer according to the grain size charts in ISO 643.

 

This document applies to forgings and rolled or forged bars manufactured from the stainless steels given in Table 1 and delivered according to the specifications given in ISO 9327-1.

 

This document specifies the general technical delivery conditions for steel flat products (plate/sheet and strip) used principally for the construction of pressure equipment. The general technical delivery requirements of ISO 404 also apply to products supplied in accordance with this document.

 

This document specifies the technical delivery conditions for plates and strip for pressure equipment made of non-alloy and alloy steels as specified in Tables A.1 and B.1. The requirements and definitions of ISO 9328-1 also apply to this document.

 

This document specifies the technical delivery conditions for plates and strip for pressure equipment made of nickel-alloy steels as specified in Tables A.1 and B.1. The requirements and definitions of ISO 9328-1 also apply to this document. NOTE This document offers the possibility of specifying products in accordance with European design codes and ASME-type design codes.

 

This International Standard establishes technical requirements and guidelines for the quality assurance of COTS EEE components, ensuring that performance, quality, schedule, cost and other critical requirements are met throughout the entire life cycle of space mission. The family includes electro-optical components. This standard does not cover specific test items for different types of components.