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
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
Aerospace series. Cadmium plating of steels with specified tensile strength = 1 450 MPa, copper, copper alloys and nickel alloys
航空用合金钢热轧钢板规范
Specification for hot-rolled steel plate of alloy structural steel for aviation
Steel rod, bars and wire for cold heading and cold extrusion. Technical delivery conditions for steels for quenching and tempering
Steel rod, bars and wire for cold heading and cold extrusion. General technical delivery conditions
Steel rod, bars and wire for cold heading and cold extrusion. Technical delivery conditions for case hardening steels
Steel rod, bars and wire for cold heading and cold extrusion. Technical delivery conditions for steels not intended for heat treatment after cold working
Aerospace series. Hexagonal steel bars drawn. Dimensions. Tolerances h 11 and h 12
Aerospace series - Steel and heat resisting alloys - Wrought products - Technical specification - Part 002 : bar and section
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
Aerospace series - Hexavalent chromium free anodizing of aluminium and aluminium alloys; German and English version EN 4827:2017
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
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
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
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
Aerospace series. Strips, cold rolled in steel, Thickness 0,1 mm
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
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
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
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