共找到 6455 条与 紧固件 相关的标准,共 431 页
The document specifies the characteristics of screws, pan head, offset cruciform recess, coarse tolerance normal shank, long thread, in alloy steel, cadmium plated. Classification: 1100 MPa/235 ФC.
Aerospace series - Screws, pan head, offset cruciform recess, coarse tolerance normal shank, long thread, in alloy steel, cadmium plated - Classification: 1100 MPa (at ambient temperature)/235 °C; German and English version EN 4161:2009 + AC:2010
Aerospace series - Nuts, anchor, self-locking, fixed, 60 o corner, with counterbore, in alloy steel, cadmium plated, MoS2 lubricated - Classification : 1 100 MPa (at ambient temperature) / 235 oC.
Aerospace series - Nuts, anchor, self-locking, fixed, 90 o corner, with counterbore, in heat resisting steel, MoS2 lubricated - Classification 1 100 MPa (at ambient temperature) / 315 oC.
Aerospace - Sleeves, wall thickness 0,5 mm, for fasteners with countersunk head; Text in German and English
Aerospace series - Bolts, normal hexagonal head, coarse tolerance normal shank, medium length thread, in heat resisting nickel base alloy, aluminium IVD coated - Classification: 1250 MPa (at ambient temperature)/425 °C; German and English version EN 4131:
Aerospace - Self-locking nuts with reduced locking torque with maximum operating temperature less than or equal to 425 °C - Technical Specification
Aerospace series - Bolts, normal hexagonal head, coarse tolerance normal shank, medium length thread, in alloy steel, cadmium plated - Classification: 1100 MPa (at ambient temperature)/235 °C; German and English version EN 4129:2009 + AC:2010
Aerospace series - Bolts, normal hexagonal head, coarse tolerance normal shank, medium length thread, in titanium alloy, aluminium IVD coated - Classification: 1100 MPa (at ambient temperature)/425 °C; German and English version EN 4130:2009 + AC:2010
This European Standard specifies the characteristics of thrust wire nuts for pipe couplings 8°30', in titanium alloy, for aerospace applications. Nominal pressure: up to 28 000 kPa Temperature range:–55°C to 135°C
Aerospace series - Pipe coupling 8 °30' in titanium alloy - Thrust wire nuts
PLUG, MACHINE THREAD DRILLED, PREFORMED PACKING, AS8879 THREAD (UNS S34700)
Nut, Self-Locking, Double Hexagon, Solid Film Lubricated, Counterbored 160 ksi, 800 °F, UNS S66286
NUT, SELF-LOCKING, EXTENDED DOUBLE HEXAGON, REDUCED FLANGE, DRY FILM LUBE, UNS S66286, CLASS: 160 KSI/800 DEGREES F
This SAE Aerospace Standard (AS) establishes the requirements for port preparation, installation and removal procedure for AS5550 fitting assembly and AS5865 fitting reducer assembly, and is applicable when specified on engineering drawings, or in procurement documents.
Fitting Assembly - 24Degree Cone Flareless per AS5827, 5080 psi, Port Connection Port Preparation, Installation and Removal of AS5550 and AS5865
Aerospace series - Nuts, hexagonal, self-locking, ball seat, in heat resisting steel, MoS2 lubricated - Classification : 900 MPa (at ambient temperature)/315 oC.
Aerospace series - Nuts, hexagonal, plain, reduced height, normal across flats, in steel, cadmium plated - Classification : 900 MPa (at ambient temperature)/235 oC.
Aerospace series - 60° interface for adaptors, threaded, with lockring - Geometric configuration; German and English version EN 2606:2009
This European Standard specifies the characteristics of self-locking, floating, self-aligning, two lugs anchor nuts, in heat resisting steel, MoS2-lubricated. Classification: 900 MPa/ 315 °C.
Aerospace series - Nuts, anchor, self-locking, floating, self-aligning, two lugs, in heat resisting steel, MoS2 lubricated - Classification: 900 MPa (at ambient temperature)/315 °C
This European Standard specifies the characteristics of one lug, floating anchor nuts, with counterbore and self-locking feature achieved by forming the upper portion out-of-round, in steel, cadmium plated, MoS2 lubricated. Classification: 1 100 MPa/ 315 °C.
Aerospace series - Nuts, anchor, self-locking, floating, one lug, with counterbore, in steel, cadmium plated, MoS2 lubricated - Classification: 1110 MPa (at ambient temperature)/235 °C
This procurement specification covers aircraft quality studs made from a low alloy steel of the type identified under the Unified Numbering System as UNS G87400, and of a series of room temperature tensile strengths ranging from 125 000 psi to 185 000 psi. Primarily for aerospace propulsion system applications in light alloys where good strength is required and the part is protected against corrosion.
Studs, Steel, Low Alloy Heat Treated, Roll Threaded
This procurement specification covers aircraft quality bolts and screws made from a corrosion resistant austenitic iron base alloy of the type identified as SAE 20302 and of 125 000 psi tensile strength at room temperature. Primarily for aerospace propulsion system applications where a good corrosion resistance and moderate strength is required.
Bolts and Screws, Steel, Corrosion Resistant 125 000 psi Tensile Strength Roll Threaded
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