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 页
Aerospace series - Steel and heat resisting alloys - Wrought products - Technical specification - Part 002 : bars and sections
- ICS
- 49.025.10
- CCS
- V11
- 发布
- 2021-05-12
- 实施
- 2021-08-28
This document specifies the electrolytic cadmium plating of parts and fasteners in steel of tensile strength UTS ≤ 1450 MPa, copper, copper alloys and nickel alloys, whose temperature in service does not exceed 235 °C.
Aerospace series - Cadmium plating of steels with specified tensile strength ≤ 1450 MPa, copper, copper alloys and nickel alloys; German and English version EN 2133:2020
- ICS
- CCS
- V11
- 发布
- 2021-03-00
- 实施
Aerospace series. Cadmium plating of steels with specified tensile strength = 1 450 MPa, copper, copper alloys and nickel alloys
- ICS
- CCS
- V11
- 发布
- 2020-12-23
- 实施
- 2020-12-23
航空用合金钢热轧钢板规范
Specification for hot-rolled steel plate of alloy structural steel for aviation
- ICS
- CCS
- V11
- 发布
- 2018-3-27
- 实施
- 2018-8-1
Steel rod, bars and wire for cold heading and cold extrusion. Technical delivery conditions for steels for quenching and tempering
- ICS
- 77.140.60;77.140.65
- CCS
- V11
- 发布
- 2017-12-08
- 实施
- 2017-12-08
Steel rod, bars and wire for cold heading and cold extrusion. General technical delivery conditions
- ICS
- 77.140.60;77.140.65
- CCS
- V11
- 发布
- 2017-11-24
- 实施
- 2017-11-24
Steel rod, bars and wire for cold heading and cold extrusion. Technical delivery conditions for case hardening steels
- ICS
- 77.140.60;77.140.65
- CCS
- V11
- 发布
- 2017-11-20
- 实施
- 2017-11-20
Steel rod, bars and wire for cold heading and cold extrusion. Technical delivery conditions for steels not intended for heat treatment after cold working
- ICS
- 77.140.60;77.140.65
- CCS
- V11
- 发布
- 2017-11-17
- 实施
- 2017-11-17
Aerospace series. Hexagonal steel bars drawn. Dimensions. Tolerances h 11 and h 12
- ICS
- 49.025.10
- CCS
- V11
- 发布
- 2017-11-03
- 实施
Aerospace series - Steel and heat resisting alloys - Wrought products - Technical specification - Part 002 : bar and section
- ICS
- 49.025.10
- CCS
- V11
- 发布
- 2017-05-05
- 实施
- 2017-05-05
This document specifies the characteristics of flanged bushes in aluminium alloy with self-lubricating liner and the design recommendation of shafts and housings. The bushes are intended for operation within the temperature range of -55 °C to 121 °C and assembly with an interference fit into fixed and moving aerospace parts.
Aerospace series - Bushes@ flanged aluminium alloy@ with self-lubricating liner - Dimensions and loads
- ICS
- 49.030.99
- CCS
- V11
- 发布
- 2017-05
- 实施
Aerospace series - Hexavalent chromium free anodizing of aluminium and aluminium alloys; German and English version EN 4827:2017
- ICS
- 49.025.20;49.040
- CCS
- V11
- 发布
- 2017-05
- 实施
This document specifies the characteristics of plain bushes in aluminium alloy with self-lubricating liner and the design recommendation of shafts and housings. The bushes are intended for operation within the temperature range of -55 °C to 121 °C and assembly with an interference fit into fixed and moving aerospace parts.
Aerospace series - Bushes@ plain@ aluminium alloy@ with self-lubricating liner - Dimensions and loads
- ICS
- 49.030.99
- CCS
- V11
- 发布
- 2017-05
- 实施
This European Standard specifies the characteristics of configuration, dimensions, tolerances and mass for moulded O-Ring seal elements, phosphate ester fluid resistant, for straight thread tube fitting boss for use as static seals in hydraulic systems for aerospace application. Application temperature range: -55 °C to 107 °C of continuous operation.
Aerospace series - Static seal elements O-Ring for straight thread tube fitting boss@ ethylene-propylene@ moulded@ phosphate ester resistant (-55 ��to 107 �� - Inch series
- ICS
- 49.035
- CCS
- V11
- 发布
- 2017-05
- 实施
This European Standard specifies the characteristics of configuration, dimensions, tolerances and mass for moulded O-Ring seal elements, phosphate ester fluid resistant, for use as static seals in hydraulic systems for aerospace application. Application temperature range: -55 °C to 107 °C of continuous operation.
Aerospace series - Static seal elements O-Ring ethylene - propylene, moulded, phosphate ester resistant (-55 °C to 107 °C) - Inch series
- ICS
- 49.035
- CCS
- V11
- 发布
- 2017-05
- 实施
This standard specifies the characteristics of gasket seal with nickel alloy C seal on heat resisting steel, 3 holes, for pipe couplings for inch series aerospace applications. Nominal pressure: up to 21000 kPa; depends on the associated tube material and tube wall thickness in the assembly (see EN 4814). Temperature range: -55 °C to 600 °C. NOTE Assembly in accordance with TR 4815. This part should not be reused after disassembling.
Aerospace series - Flange couplings - Gasket seal with nickel alloy C seal on heat resisting steel plate with 3 fastening holes - Inch series
- ICS
- 49.080
- CCS
- V11
- 发布
- 2017-04
- 实施
Aerospace series. Strips, cold rolled in steel, Thickness 0,1 mm
- ICS
- 49.025.10
- CCS
- V11
- 发布
- 2017-03-31
- 实施
- 2017-03-31
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 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 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
