49.030.99 其他紧固件 标准查询与下载

DIN EN 3819:2008 航空航天系列.扳手和和套管的间隙

This standard defines the minimum clearance area required around nuts and bolt heads when using either double hexagon box or socket wrenches defined in AECMA standard,

Aerospace series - Clearance for wrenches and sockets; German and English version EN 3819:2008

DIN EN 3710:2008 航空航天系列.双六角套筒.技术规范

This standard specifies the properties of double-hex sockets for aerospace use.

Aerospace series - Sockets, bi-hexagonal - Technical specification; German and English version EN 3710:2008

LST EN 3916-2008 航空航天系列 插入件，薄壁 部件的回收程序

Aerospace series - Insert, thin wall - Salvage procedure for components

DS/EN 3916:2008 航空航天系列 插入件，薄壁 部件的回收程序

1.1 This specification covers the accepted methods for the reclamation of installation holes for standard thin wall inserts, within assemblies.1.2 To enable rectification when defects or damage occur to the standard insert tapped installation hole, or to rectify any out of position of the hole within the specified parameters of use.1.3 To control the machining of the existing insert hole and the installation requirements of the replacement oversize thin wall insert.

Aerospace series - Insert, thin wall - Salvage procedure for components

BS EN 3916:2008 航空航天系列.薄壁插入件.部件用修复程序

1.1 This specification covers the accepted methods for the reclamation of installation holes for standard thin wall inserts, within assemblies. 1.2 To enable rectification when defects or damage occur to the standard insert tapped installation hole, or to rectify any out of position of the hole within the specified parameters of use. 1.3 To control the machining of the existing insert hole and the installation requirements of the replacement oversize thin wall insert.

Aerospace series - Insert, thin wall - Salvage procedure for components

SAE AS3509B-2008 UNS N06600型镍合金成套电缆安全性

Scope unavailable.

Cable, Safety, Kit, Nickel Alloy, UNS N06600

SAE AS3121A-2008 2024-T4和2024-T351长型、标准和.010特大直径的铝制膨胀插头

Scope is unavailable.

Plug, Expansion - Aluminum, 2024-T4 and 2024-T351, Long, Std and .010 Oversize Diameters (UNS A92024)

SAE AS3122A-2008 2024-T4和2024-T351长型铝制膨胀销(UNS A92024)

Scope is unavailable.

Pin, Expansion - Aluminum, 2024-T4 and 2024-T351, Long (UNS A92024)

NF L24-967*NF EN 3915:2008 航空航天系列.部件修复用NI-PH2601(NI-P100HT、Inconel 718)型耐热镍基合金制MJ螺纹、自锁紧、薄壁插件.等级:1275MPa(室温)/550℃.技术规范

Aerospace series - Insert, thin wall, self-locking, MJ threads, in heat resisting nickel base alloy NI-PH2601 (NI-P100HT, Inconel 718), for salvage of components - Classification : 1 275 MPa (at ambient temperature) / 550 oC - Technical specification.

LST EN 4302-2008 航天系列-开口环插入工具，四方驱动

Aerospace series - Open ring insert tool, square drive

LST EN 3729-2008 航空航天系列 环，螺纹，自锁，左旋螺纹，耐热钢 FE-PA92HT（A286），镀银

Aerospace series - Rings, threaded, self-locking, left-hand thread, in heat resisting steel FE-PA92HT (A286), silver plated

LST EN 3819-2008 航空航天系列 扳手和套筒的间隙

Aerospace series - Clearance for wrenches and sockets

LST EN 3781-2008 航空航天系列 螺旋缠绕式挡圈用槽 设计标准

Aerospace series - Grooves for spiral wound retaining rings - Design standard

LST EN 4355-2008 航空航天系列 六叶槽 驱动器，插座

Aerospace series - Six lobe recess - Drivers, socket

LST EN 3915-2008 航空航天系列 插入件，薄壁，自锁，MJ 螺纹，耐热镍基合金 NI-PH2601（NI-P100HT，Inconel 718），用于部件修复 分类：1275 MPa（在环境温度下）/ 550掳C 技术规范

Aerospace series - Insert, thin wall, self-locking, MJ threads, in heat resisting nickel base alloy NI-PH2601 (NI-P100HT, Inconel 718), for salvage of components - Classification: 1 275 MPa (at ambient temperature) / 550 °C - Technical specification

SAE AS85052/3A-2008 500℉17-7 PH心管环形夹具

THIS CLAMP STANDARD IS REVISED TO INCORPORATE THE LATEST SAE MATERIAL SPECIFICATION ANDSTANDARDS.

Clamp, Loop, Tube 17-7 PH Cres, 500°F

SAE AS3510B-2008 电缆安全成套工具.UNS S32100型耐腐蚀和耐热钢

Cable, Safety, Kit - Corrosion and Heat Resistant Steel, UNS S32100

Cable, Safety, Kit - Corrosion and Heat Resistant Steel, UNS S32100

SAE AS3220A-2008 非扩口式铝制套管配件

Fitting, Sleeve, Flared, Aluminum

Fitting, Sleeve, Flared, Aluminum

EN 3916:2008 航空航天系列.薄壁插入件.部件用修复程序

This specification covers the accepted methods for the reclamation of installation holes for standard thin wall inserts, within assemblies. To enable rectification when defects or damage occur to the standard insert tapped installation hole, or to rectify any out of position of the hole within the specified parameters of use. To control the machining of the existing insert hole and the installation requirements of the replacement oversize thin wall insert.

Aerospace series - Insert, thin wall - Salvage procedure for components

BS EN 3819:2008 航空航天系列.扳手和套管的间隙

Aerospace series - Clearance for wrenches and sockets