V22 机械配件、构件 标准查询与下载

DIN EN 2546:2006 航空航天系列.飞机控制杆用钝化耐蚀钢制带径向齿的锁紧垫圈.尺寸

The standard specifies the characteristics of lock washers in corrosion resisting steel, with radial serrations primarily intended for flight control rods. These lock washers are intended to immobilise the rod end in relation to the rod body, whilst allowing a precise positional adjustment.

Aerospace series - Washers, lock with radial serrations in corrosion resisting steel passivated for flight control rods - Dimensions; German and English version EN 2546:2006

DIN EN 2588:2006 航空航天系列.带组装导槽的耐蚀钢制球面滑动轴承.尺寸和承载

The standardspecifies the characteristics of spherical plain bearing sin corrosion resisting steel, with assembly slots, with or without lubrication holes and groove, intended for use in fixed or moving parts of aircraft structure and control mechanisms. They may be used in the temperature range from -54 ?to 150 ?#,,#

Aerospace series - Bearings, spherical plain in corrosion resisting steel with assembly slots - Dimensions and loads; German and English version EN 2588:2006

DIN EN 14607-7:2006 航天工程. 机械. 第7部分: 机械构件; 英文版本 EN 14607-7: 2004

This part 7 of space engineering - Mechanical defines the mechanical engineering requirements for mechanical part.

Space engineering - Mechanical - Part 7: Mechanical parts; English version EN 14607-7:2004

DIN EN 4168:2006 航空航天系列.三部分弹簧张力夹具.耐热钢FE-PA2601(A286)制外夹具

Aerospace series - Clips, spring tension, three parts - Outer clips in heat resisting steel FE-PA2601 (A286); German and English version EN 4168:2004

DIN EN 4167:2006 航空航天系列.三部分弹簧张力夹具.耐热钢FE-PA2601(A286)制内夹具

This standard specifies the characteristics of inner clips, three part clips, spring tension, in FE-PA2601 for applications at a maximum temperature of 260 ? for aerospace applications. They shall be assembled with parts from EN 4166 and EN 4168.#,,#

Aerospace series - Clips, spring tension, three parts - Inner clips in heat resisting steel FE-PA2601 (A286); German and English version EN 4167:2004

DIN EN 2335:2006 航空航天.耐蚀钢制不带组装导槽的关节轴承.尺寸和负荷

This standard specifies the characteristics of spherical plain bearings in corrosion resisting steel, without assembly slot, with or without swaging groove, with or without lubrication holes and grooves, intended for use in fixed or moving parts of aircraft structure and control mechanisms. They may be used in the temperature range from - 54 ?to 150 ? However, as they are lubricated with the following greases (see EN 2337): ester type very high pressure grease (code letter A), operating range from - 73 ?to 121 ?or, synthetic hydrocarbon type very high pressure grease general purpose (code letter B), operating range from - 54 ?to 177 ? Their field of application when lubricated with grease code letter A is limited to 121 ?

Aerospace series - Bearings, spherical plain in corrosion resisting steel without assembly slot - Dimensions and loads; German and English version EN 2335:2005

DIN EN 4166:2006 航空航天系列.三部分弹簧张力夹具.聚四氟乙烯轴衬

Aerospace series - Clips, spring tension, three parts - PTFE bushes; German and English version EN 4166:2004

DIN EN 4040:2006 航空航天.宽内环的带自润滑内衬的耐蚀钢制关节轴承.室温高负荷.尺寸和负荷

This standard specifies the characteristics of spherical plain bearings in corrosion resisting steel with self lubricating liner, with wide inner ring, for elevated loads at ambient temperature. They are intended for use between fixed or moving parts of the aircraft structure and their control mechanisms. The spherical plain bearings defined the temperature from -54 ?to +163 ?

Aerospace series - Bearings, spherical plain in corrosion resisting steel with self-lubricating liner with wide inner ring - Elevated loads at ambient temperature - Dimensions and loads; German and English version EN 4040:2006

DIN EN 2336:2006 航空航天.耐蚀钢制带组装导槽的关节轴承.尺寸和负荷

This standard specifies the characteristics of spherical plain bearings in steel, with assembly slots, with or without lubrication holes and grooves, intended for use in fixed or moving parts of aircraft structure and control mechanisms. They may be used in the temperature range from - 54 ?to 150 ? However, as they are lubricated with the following greases (see EN 2337): ester type very high pressure grease (code letter A), operating range from - 73 ?to 121 ?or, synthetic hydrocarbon type very high pressure grease general purpose (code letter B), operating range from - 54 ?to 177 ? Their field of application when lubricated with grease code letter A is limited to 121 ?#,,#

Aerospace series - Bearings, spherical plain in steel with assembly slots - Dimensions and loads; German and English version EN 2336:2005

NF L31-520*NF EN 2337:2006 航空航天.关节轴承.交货技术条件

Aerospace series - Spherical plain bearings - Technical specification.

NF L31-523*NF EN 2588:2006 航空航天系列.有装配槽的耐蚀钢制 向心关节轴承.尺寸和负载

Aerospace series - Bearings, spherical plain in corrosion resisting steel with assembly slots - Dimensions and loads.

SAE AS81935/7-2006 -65至+325°F耐腐蚀钢制宽内螺口连接的自润滑、自准杆端平面轴承

BEARING, PLAIN ROD END, SELF-ALIGNING, SELFLUBRICATING, WIDE, INTERNALLY THREADED, STEEL, CORROSION RESISTANT (CRES) -65 TO +325 °F;TABLE 1 - DIMENSIONS;TABLE 2 - LOAD VALUES;

BEARING, PLAIN ROD END, SELF-ALIGNING, SELFLUBRICATING, WIDE, INTERNALLY THREADED, STEEL, CORROSION RESISTANT (CRES) -65 TO +325 °F

DLA A-A-50213 A VALID NOTICE 2-2006 法国铁路和轮船机械工程师用规则和不规则绘图曲线板装置规则和不规则绘图曲线板

A-A-50213A, dated 25 September 2001, has been reviewed and determined to be valid for use in acquisition.

CURVES, DRAFTING, REGULAR AND IRREGULAR: CURVE SETS, DRAFTING, REGULAR AND IRREGULAR; FRENCH, MECHANICAL ENGINEERS, RAILROAD, AND SHIPS

DIN EN 4035:2006 航空航天系列.减小内部径向间隙和带螺纹钛合金杆耐腐蚀钢可调自动对心双列球轴承的杆端.尺寸和载荷

This standard specifies the characteristics of adjustable rod ends with self-aligning double row ball bearing in corrosion resisting steel with reduced internal radial clearance and threaded shank in titanium alloy, designed to withstand only slow rotations and oscillations under load. They consist of: a rod end comprising: circumferential groove to identify location; either seals or shields; an optional longitudinal groove for locking purpose; an inner ring with balls. These rod ends are intended for use with flight control rods or rods for aerospace structures. They are intended to be used in the temperature range: 54 ?to 150 ? However, being lubricated with the following greases: very high pressure grease, ester type (code A), operational range 73 ?to 121 ?or very high pressure grease, synthetic hydrocarbons, general purpose (code B), operational range 54 ?to 177 ?(see EN 2067), their field of application when lubricated with code A grease is limited to 121 ?

Aerospace series - Rod ends, adjustable with self-aligning double row ball bearing in corrosion resisting steel, reduced internal radial clearance and threaded shank in titanium alloy - Dimensions and loads; German and English version EN 4035:2006

DLA MS51998 VALID NOTICE 3-2006 设计及使用限制锯齿环形锁定螺纹螺杆嵌块

MS51998, dated 14 September 2001, has been reviewed and determined to be valid for use in acquisition.

INSERT, SCREW THREAD-LOCKED IN, RING LOCKED, SERRATED, DESIGN AND USAGE LIMITATIONS FOR

DLA MS51837 VALID NOTICE 3-2006 牙形孔尺寸安装螺纹嵌件

MS51837, dated 14 September 2001, has been reviewed and determined to be valid for use in acquisition.

INSERT, SCREW THREAD - THREAD FORMING HOLE DIMENSIONS FOR AND INSTALLATION OF

SAE AS81935/6-2006 -65至+325°F耐腐蚀钢制宽外螺口连接的自润滑、自准杆端平面轴承

BEARING, PLAIN ROD END, SELF-ALIGNING, SELFLUBRICATING, WIDE, EXTERNALLY THREADED, STEEL, CORROSION RESISTANT (CRES) -65 TO +325 °F;TABLE 1 - DIMENSIONS;TABLE 2 - LOAD VALUES;

BEARING, PLAIN ROD END, SELF-ALIGNING, SELFLUBRICATING, WIDE, EXTERNALLY THREADED, STEEL, CORROSION RESISTANT (CRES) -65 TO +325 °F

NF L31-285:2006 航空航天系列.减小内部径向间隙和带螺纹钛合金杆耐腐蚀钢可调自动对心双列球轴承的杆端.尺寸和载荷

Aerospace series - Rod ends, adjustable with self-aligning double row ball bearing in corrosion resisting steel, reduced internal radial clearance and threaded shank in titanium alloy - Dimensions and loads.

BS EN 4036:2006 航空航天系列.减小内部径向间隙耐腐蚀钢可调自动对心双列球轴承和螺纹柄的杆端.尺寸和载荷

This standard specifies the characteristics of adjustable rod ends with self-aligning double row ball bearing with reduced internal radial clearance and threaded shank in corrosion resisting steel, designed to withstand only slow rotations and oscillations under load. They consist of: - a rod end comprising: - circumferential groove to identify location; - either seals or shields; - an optional longitudinal groove for locking purpose; - an inner ring with balls. These rod ends are intended for use with flight control rods or rods for aerospace structures. They are intended to be used in the temperature range: − 54 °C to 150 °C. However, being lubricated with the following greases: - very high pressure grease, ester type (code A), operational range − 73 °C to 121 °C or - very high pressure grease, synthetic hydrocarbons, general purpose (code B), operational range − 54 °C to 177 °C (see EN 2067), their field of application when lubricated with code A grease is limited to 121 °C.

Rod ends, adjustable with self-aligning double row ball bearing and threaded shank in corrosion resisting steel, reduced internal radial clearance - Dimensions and loads

BS EN 2337:2006 航空航天系列.球面关节轴承.技术规范

This standard specifies the required characteristics, inspection and test methods, qualification and acceptance conditions for spherical plain bearings designed to withstand static loads and loads with slight swivelling. It is applicable whenever referenced.

Spherical plain bearings - Technical specification