V22 机械配件、构件 标准查询与下载

DIN EN 4535-2:2010 航空航天系列.高负荷自润滑衬板铝合金法兰连接的衬套.第2部分:尺寸和载荷.英寸系列

This standard specifies the characteristics of bushes flanged in aluminium alloy with self-lubricating liner elevated load for aerospace applications. The bushes are intended for use in fixed or moving parts of the aircraft structure and control mechanisms. They shall be used in the temperature range - 55 ФC to 121 ФC.

Aerospace series - Bushes, flanged in aluminium alloy with self-lubricating liner, elevated load - Part 2: Dimensions and loads - Inch series; German and English version EN 4535-2:2009

DIN EN 4534-2:2010 航空航天系列.高负载带有自润滑衬垫的铝合金平纹衬套.第2部分:尺寸和负载.英制系列.德文和英文版本EN 4534-2-2009

This standard specifies the characteristics of plain bushes in aluminium alloy with self-lubricating liner, elevated load for aerospace applications.The bushes are intended for use in fixed or moving parts of the aircraft structure and control mechanisms.They shall be used in the temperature range - 55 ФC to 121 ФC.

Aerospace series - Bushes, plain in aluminium alloy with self-lubricating liner, elevated load - Part 2: Dimensions and loads - Inch series; German and English version EN 4534-2:2009

SAE AS15002C-2010 II类钢直螺纹表面裂纹液压润滑配件

Fitting, Lubricating, Hydraulic, Surface Check, Straight Threads, Steel, Type II

SAE AS18280E-2010 3000 psi流体连接24°锥形非扩口配件

This SAE Aerospace Standard (AS) establishes the requirements for 24 degree cone flareless fluid connection fittings and nuts, internally or externally swaged, preset, or welded sleeves for use in aircraft fluid systems at nominal operating pressures up to and including 3000 psi. Fittings shall be furnished in the types and styles designated by the applicable AS, MS, NAS standard drawings. This specification includes the requirements for flareless fittings used with externally preset bite type sleeves and also for machined acorn fitting ends such as NAS1760, AS4458, and AS4703. It is intended to serve as a procurement specification for the fittings described herein and in Section 6. The requirements for externally preset bite type sleeves are given in AS18280/1. The requirements for swaged or welded sleeves and tube ends are given in AS18280/2.

Fittings, 24° Cone Flareless, Fluid Connection, 3000 psi

SAE AS21151E-2009 -65至300°F温度的II型自调整机身双排精密度外螺纹、有杆端滚珠轴承

Bearing, Ball, Rod End, Double Row, Precision, External Thread, Self-Aligning, Airframe, Type II, -65 to 300°F

NF L31-524:2009 航空航天系列.带自润滑衬瓦的耐腐蚀钢制精密滚珠轴承.尺寸规格及载荷量.英制系列

Aerospace series - Spherical plain bearings in corrosion resisting steel with self-lubricating liner, narrow series - Dimensions and loads - Inch series.

NF L31-525:2009 航空航天系列.带自润滑班轮的宽系耐腐蚀钢关节轴承.尺寸规格和负载.英制系列

Aerospace series - Spherical plain bearings in corrosion resisting steel with self-lubricating liner, wide series - Dimensions and loads - Inch series.

NF L31-607-2:2009 航空航天系列.带自润滑式班轮的高架承载铝合金法兰轴衬.第2部分:尺寸规格和负载.英制系列

Aerospace series - Bushes, flanged in aluminium alloy with self-lubricating liner, elevated load - Part 2 : dimensions and loads - Inch series.

DIN EN 2755:2009 航空航天系列.具有自润滑轴套的球面耐蚀钢轴承.环境温度下的提升的负荷.技术规范,德文和英文版本 EN 2755:2009

This standard specifies the required characteristics, inspection and test methods, qualification and acceptance conditions for spherical plain bearings in corrosion resisting steel, with self-lubricating liner, for elevated loads at ambient temperature intended for use in fixed or moving parts of the aircraft structure and control mechanisms, This standard applies whenever referenced.

Aerospace series - Bearings, spherical plain in corrosion resisting steel with self-lubricating liner - Elevated load at ambient temperature - Technical specification; German and English version EN 2755:2009

BS EN 2755:2009 航空航天系列.具有自润滑轴套的球面防腐钢轴承.室温环境下高负荷.技术规范

Aerospace series - Bearings, spherical plain in corrosion resisting steel with self-lubricating liner - Elevated load at ambient temperature - Technical specification

BS EN 4537-2:2009 航空航天系列.高负荷带自润滑衬料耐蚀钢制有法兰的套筒.第2部分:尺寸规格和负载.英制系列

This standard specifies the characteristics of flanged bushes in corrosion resisting steel with self-lubricating liner elevated load for aerospace applications. The bushes are intended for use in fixed or moving parts of the aircraft structure and control mechanisms. They shall be used in the temperature range – 55 °C to 163 °C.

Aerospace series - Bushes, flanged in corrosion-resisting steel with self-lubricating liner, elevated load - Part 2:Dimensions and loads - Inch series

SAE ARP5862-2009 航运帽盖,罩盖和孔塞

The primary purpose of the shipping closure is to protect the aircraft parts or system from storage caps, covers, plugs and related shipping hardware. These items are commonly used on aircraft engines and associated hardware but may be used elsewhere. Military and commercial customer requirements for the prevention of damage or contamination to stored parts are generally limited to the generic instructions "all openings should be sufficiently covered to prevent the entrance of dust, dirt, moisture or other foreign contaminants". This recommended practice outlines basic minimum parameters for suggested item construction and usage. Additionally this recommended practice provides instruction on how to apply these closures to various openings.

Shipping Caps, Covers and Plugs

BS EN 4534-2:2009 航空航天系列.高负载带有自润滑衬垫的铝合金圆环平纹衬套.第2部分:尺寸规格和负载.英制系列

This standard specifies the characteristics of plain bushes in aluminium alloy with self-lubricating liner, elevated load for aerospace applications. The bushes are intended for use in fixed or moving parts of the aircraft structure and control mechanisms. They shall be used in the temperature range − 55 °C to 121 °C.

Aerospace series - Bushes, plain in aluminium alloy with self-lubricating liner, elevated load - Part 2:Dimensions and loads - Inch series

BS EN 4535-2:2009 航空航天系列.带有高负荷自润滑轴套的防铝合金中的法兰衬套.尺寸规格和负荷.英制系列

This standard specifies the characteristics of bushes flanged in aluminium alloy with self-lubricating liner elevated load for aerospace applications. The bushes are intended for use in fixed or moving parts of the aircraft structure and control mechanisms. They shall be used in the temperature range – 55 °C to 121 °C.

Aerospace series - Bushes, flanged in aluminium alloy with self-lubricating liner, elevated load - Part 2:Dimensions and loads - Inch series

BS EN 4613:2009 航空航天系列.带自润滑衬套的窄系列耐蚀钢制关节轴承.尺寸规格和负荷.英制尺寸系列

This standard specifies the characteristics of bearings, spherical plain in corrosion resisting steel with selflubricating liner, narrow series for aerospace applications. They are intended for use in fixed or moving parts of the aircraft structure and control mechanisms. They shall be used in the temperature range – 55 °C to 163 °C.

Aerospace series - Spherical plain bearings in corrosion resisting steel with self-lubricating liner, narrow series - Dimensions and loads - Inch series

SAE AS21151D-2008 -65～300℉、II型机身自调外螺纹精密双排杆端滚珠轴承

Bearing, Ball, Rod End, Double Row, Precision, External Thread, Self-Aligning, Airframe, Type II, -65 to 300°F

QJ 3296.11-2008 蜂窝夹层结构用镶嵌件 第11部分：盲孔自锁镶嵌件

Inserts for honeycomb sandwich structures - Part 11: Blind hole self-locking inserts

QJ 3296.5-2008 蜂窝夹层结构用镶嵌件 第5部分：通孔螺纹B型镶嵌件

Inserts for honeycomb sandwich structures - Part 5: Through-hole threaded Type B inserts

QJ 3294-2008 蜂窝夹层结构用镶嵌件安装要求

Installation requirements for inserts for honeycomb sandwich structures

QJ 3296.7-2008 蜂窝夹层结构用镶嵌件 第7部分：盲孔螺纹B型镶嵌件

Inserts for honeycomb sandwich structures - Part 7: Blind hole threaded inserts, Type B