V11 航空与航天用金属铸锻材料 标准查询与下载



共找到 5950 条与 航空与航天用金属铸锻材料 相关的标准,共 397

This European Standard specifies a method of determining the attenuation variation of an optical cable when clamped to a mandrel with cable ties, simulating the condition in an installed harness.

Aerospace series - Fibres and cables@ optical@ aircraft use - Test methods - Part 517: Cable tie clamping test

ICS
49.090
CCS
V11
发布
2017-03
实施

This European Standard specifies the characteristics of laminated washers, in corrosion resisting steel, for maximum operating temperature 120 °C, for aerospace applications.

Aerospace series - Washers@ laminated@ in corrosion resisting steel

ICS
49.030.50
CCS
V11
发布
2017-03
实施

This European Standard specifies the dimensions and tolerances of: Strips, cold rolled in steel Thickness 0,1 mm a 2,5 mm for aerospace applications.

Aerospace series - Strips@ cold rolled in steel@ Thickness 0@1 mm ��a ��2@5 mm - Dimensions

ICS
49.025.10
CCS
V11
发布
2017-03
实施

This European Standard specifies a method for the high temperature exposure of protection sleeve for electrical cable and cable bundles for aerospace application. It shall be used together with EN 6059-100.

Aerospace series - Electrical cables@ installation - Protection sleeves - Test methods - Part 302: High temperature exposure

ICS
49.060
CCS
V11
发布
2017-03
实施

This European Standard specifies the general characteristics, qualification and acceptance requirements for self-wrapping shielding (EMI) protective sleeve designed for EMI shielding of cable and cable bundles for aerospace applications.

Aerospace series - Electrical cables@ installation - Selfwrapping shielding (EMI) protective sleeve - Part 001: Technical specification

ICS
49.060
CCS
V11
发布
2017-03
实施

This European Standard specifies a method for the sun light exposure of protection sleeve for electrical cable and cable bundles for aerospace application. It shall be used together with EN 6059-100.

Aerospace series - Electrical cables, installation - Protection sleeves - Test methods - Part 301: Sun light exposure

ICS
49.060
CCS
V11
发布
2017-03
实施

This European Standard specifies the method for determining the effect of exposure to a humid atmosphere on the physical and mechanical characteristics of fibre reinforced plastics. This standard applies to all laminates, whatever the nature of the reinforcement and organic matrix used, unless otherwise indicated in the material standard and/or technical specification.

Aerospace series - Fibre reinforced plastics - Determination of the effect of exposure to humid atmosphere on physical and mechanical characteristics

ICS
49.025.40
CCS
V11
发布
2017-03
实施

This European Standard specifies a method of checking the break resistance and attenuation variation recovery of an optical cable subjected to severe bending under load.

Aerospace series - Fibres and cables, optical, aircraft use - Test methods - Part 516: Severe cable bend test

ICS
49.090
CCS
V11
发布
2017-03
实施

This European Standard specifies the technical requirements to minimize the hazards listed in Clause 4 which can arise during the commissioning, the operation and the maintenance of deicers and equipment designed exclusively for de-icing and washing of aircraft with de-icing/anti-icing/washing liquids when used as intended, including misuse reasonably foreseeable by the manufacturer, when carried out in accordance with the specifications given by the manufacturer or his authorized representative. It also takes into account some requirements recognized as essential by authorities, aircraft and ground support equipment (GSE) manufacturers as well as airlines and handling agencies. NOTE 1 Safety of aircraft in connection with de-icing/anti-icing operations is not dealt with in this European Standard. Any, even minor, aircraft de-icing or anti-icing operation directly affects flight safety on take-off. Prevention of aeronautical accidents resulting from in-flight icing principally concerns the fluids and methods used, but it may in certain cases also concern de-icing or anti-icing equipment design or operation. These aeronautical aspects are controlled by the applicable Civil Aviation regulations ICAO 9640-AN/940, Manual of aircraft ground de-icing/anti-icing operations and EASA EU-OPS Subpart D 45 and its Acceptable Means of Compliance (AMC) and covered in ISO 11076:2012 (AEA Recommendations). They are not covered in this European Standard. This European Standard applies to: a) self-propelled deicers with fixed or mobile platform or hinged boom; b) towable deicers with fixed or mobile platform or hinged boom; c) stationary de-icing/anti-icing equipment (e. g. fixed boom, gantry or tower cranes equipped with aircraft de-icing/anti-icing fluid systems). This European Standard does not apply to: d) fixed installations, such as separate storage tanks or heating and filling stations, which are not an integrated part of the stationary de-icing equipment; e) hydraulic control systems; f) pneumatic systems; g) flow generating systems as such. No extra requirements on noise and vibration are provided other than those in EN 1915-3 and EN 1915-4. NOTE 2 EN 1915-3 and EN 1915-4 provide the general GSE vibration and noise requirements. This European Standard is not dealing with hazards in respect to a standard automotive chassis and the traffic on the apron. This part of EN 12312 is not applicable to deicers and de-icing/anti-icing equipment which are manufactured before the date of publication of this standard by CEN. This part of EN 12312 when used in conjunction with EN 1915-1, EN 1915-2, EN 1915-3 and EN 1915-4 provides the requirements for deicers and de-icing/anti-icing equipment.

Aircraft ground support equipment - Specific requirements - Part 6: Deicers and de-icing/anti-icing equipment

ICS
49.100
CCS
V11
发布
2017-03
实施

This European Standard specifies the characteristics for the positioner used with the M22520/2-01 crimping tool to crimp electrical contacts according to EN 4008-002.

Aerospace series - Elements of electrical and optical connection - Crimping tools and associated accessories - Part 003: Positioner for crimping tool M22520/2-01 - Product standard

ICS
49.060
CCS
V11
发布
2017-03
实施

This European Standard specifies a method of determining the attenuation variation of an optical cable during mechanical bending under load at the maximum and minimum operating temperatures.

Aerospace series - Fibres and cables@ optical@ aircraft use - Test methods - Part 510: Bending test

ICS
49.090
CCS
V11
发布
2017-03
实施

This document specifies the required characteristics, inspections and tests, quality assurance and qualification, acceptance and delivery conditions for bushes, designed to be subjected under load, to slow sliding movements, rotations and small oscillations only for aerospace applications. This standard applies to all bushes when referred to in the respective product standards or in a design documentation. The liner is designed to be used in the temperature range of -50 °C to 163 °C. Aluminium bushes are limited to -55 °C to 121 °C.

Aerospace series - Bushes with self-lubricating liner - Technical specification

ICS
49.035
CCS
V11
发布
2017-03
实施

This European Standard defines the characteristics of hermetic square flange receptacles in the family of bayonet coupling circular connectors, intended for use in an operating temperature range of - 65 °C to 175 °C or 200 °C continuous. It applies to models defined in Table 3. For plugs and protective covers see EN 3646-008 and EN 3646-009 respectively.

Aerospace series - Connectors@ electrical@ circular@ bayonet coupling@ operating temperature 175 ��or 200 ��continuous - Part 005: Receptacle@ hermetic@ square flange mounting - Product standard

ICS
49.060
CCS
V11
发布
2017-03
实施

This European Standard specifies the required characteristics for four types of heat-shrinkable polyolefin sleevings for use in aircraft electrical systems at operating temperatures between - 55 °C and 135 °C. Type A: Very flexible, flame retarded, shrink ratio 2:1 This sleeving has very good flexibility, is flame retarded and will shrink at low temperatures. It is suitable where sensitive components and delicate wiring need protection from excessive heat during shrinking. Type B: Flexible, flame retarded, shrink ratio 2:1, 3:1 and 4:1 This sleeving is flexible and flame retarded. It is suitable for general purposes and is available with high shrink ratios. Type C: Flexible, not flame retarded, shrink ratio 2:1 and 3:1 This sleeving is flexible and not flame retarded and is available in two shrink ratios. Type D: Semi-rigid, flame retarded, shrink ratio 2:1 This sleeving is semi-rigid and flame retarded. It is suitable where strain relief and mechanical support are required These sleevings are normally supplied with internal diameters up to 102 mm for shrink ratios of 2:1 and 4:1 and up to 39 mm for shrink ratios of 3:1 and in the following colours for type B, black, brown, red, yellow, green, blue, orange, violet, grey, white and green/yellow. Types A and D are black only. Type C is transparent, is not flame retarded and does not meet the flammability requirements of EN 4708-001. Sizes or colours other than those specifically listed in this standard may be available. These items shall be considered to comply with this standard if they comply with the property requirements listed in Tables 5, 6 and 7 except for dimensions and mass.

Aerospace series - Sleeving@ heat-shrinkable@ for binding@ insulation and identification - Part 101: Polyolefin sleeving - Operating temperatures -55 ��to 135 ��- Product standard

ICS
49.060
CCS
V11
发布
2017-03
实施

This European Standard specifies methods for determining the flammability characteristics of protective sleeves, including heat shrink dual wall sleeves, for electric cable and cable bundles. It shall be used together with EN 6059-100. These tests are designed to satisfy the requirements in JAR-25 Section 1, Part 1, Appendix F. There are two methods included in this standard: Method 1 - Applicable for textile fabric sleeves. Method 2 - Applicable non-textile sleeves for use on electrical/optical cables and harness components.

Aerospace series - Electrical cables@ installation - Protection sleeves - Test methods - Part 304: Flammability

ICS
13.220.40;49.060
CCS
V11
发布
2017-03
实施

This European Standard specifies the characteristics of UV laser printable, single and multicore silver plated copper screened (spiral) and jacketed electrical cables for use in the on-board electrical systems of aircraft, at operating temperatures between - 55 °C and 200 °C. It shall also be possible to mark these cables by qualified compatible marking. These markings shall be in accordance with EN 3838.

Aerospace series - Cables@ electrical@ single and multicore for general purpose - Operating temperatures between - 55 ��and 200 ��- Part 012: MNA (1 core)@ MNB (pair)@ MNC (3 cores)@ MND (4 cores)@ cables family - Silver plated copper screened (spiral) an

ICS
49.060
CCS
V11
发布
2017-03
实施

This European Standard defines the single module plug used in the family of rectangular electrical connectors. The receptacle corresponding to this plug is defined in EN 4165-025. Accessories and protective cover corresponding to those plugs are defined in EN 4165-026. The cavity of this connector is uncoded, so it can accept polarized modules N, A, B, C and D as defined in EN 4165-002.

Aerospace series - Connectors, electrical, rectangular, modular - Operating temperature 175 °C continuous - Part 024: Single module plug - Product standard

ICS
49.060
CCS
V11
发布
2017-03
实施

Aerospace series. Steel. Sheets and plates, hot rolled. Dimensions

ICS
49.025.10
CCS
V11
发布
2017-02-28
实施
2017-02-28

Aerospace series. Hexavalent chromium free anodizing of aluminium and aluminium alloys

ICS
49.025.20;49.040
CCS
V11
发布
2017-02-28
实施
2017-02-28

Aerospace series. Steel. Sheet and strip, cold rolled. Thickness 0,1 mm a 3 mm. Dimensions

ICS
49.025.10
CCS
V11
发布
2017-02-28
实施
2017-02-28



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