49.035 航空航天制造用零部件 标准查询与下载

BS EN 4034:2007 航空航天系列.飞机机架转动轴承.耐腐蚀钢制带法兰外圈内径递减的自准双列自调滚珠轴承.尺寸和负荷

This standard specifies the characteristics of self-aligning double row ball bearings with flanged outer ring in corrosion resisting steel, reduced internal clearance, designed to withstand only slow rotations and oscillations under load. They are intended for use between fixed and moving parts of the aircraft structure and their control mechanisms. 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 3280), their field of application when lubricated with code A grease is limited to 121 °C.

Aerospace series - Bearings, airframe rolling - Double row self-aligning ball bearings with flanged outer ring in corrosion resisting steel, reduced internal radial clearance - Dimensions and loads

BS EN 3061:2007 航空航天系列.飞机机架转动轴承.耐腐蚀钢制带法兰定位盖的刚性单列滚珠轴承.尺寸和负荷

This standard specifies the characteristics of rigid single row ball bearings in corrosion resisting steel with a solid or lightweight flanged alignment housing, designed to withstand only slow rotations and slight oscillations under load. They are intended for use in the hubs of torsion lever and in separated supports for airframe/aerospace applications. The airframe rolling bearings defined in this standard may be used in the temperature range from – 54 °C to 150 °C. However, being lubricated with the following greases (see EN 3727): - ester type very high pressure grease (code letter A), operating range from – 73 °C to 121 °C or, - synthetic hydrocarbons type very high pressure grease general purpose (code letter B) operating range from – 54 °C to 177 °C. Their field of application when lubricated with code letter A grease is limited to 121 °C.

Aerospace series - Bearings, airframe rolling - Rigid single row ball bearings in corrosion resisting steel, with flanged alignment housing - Dimensions and loads

SAE AS9592B-2007 190螺栓、CRES UNS S32100、90°角撑架

BRACKET, ANGLE, 90? CRES UNS S32100, .190 BOLTFIGURE 1 - ANGLE BRACKETTable1 part numbers and dimensions

BRACKET, ANGLE, 90? CRES UNS S32100, .190 BOLT

EN 3060:2007 航空航天系列.飞机机架转动轴承.镉板钢中带镉板法兰定位盖的机架用刚性单列滚珠轴承.尺寸和负载

This standard specifies the characteristics of rigid single row ball bearings in steel, cadmium-plated with cadmium plated flanged alignment housing designed to withstand only slow rotations and oscillations under load.They are intended for use inThe hubs of torsion lever and in separated supports for airframe/aerospace applications.The airframe rolling bearings defined inThis standard may be used inThe temperature range from-54 ℃ to 150 ℃. However, being lubricated withThe following greases (see EN 3727): ester type very high pressure grease (code letter A), operating range from-73 ℃ to 121 ℃ or, synthetic hydrocarbons type very high pressure grease general purpose (code letter B) operating range from-54 ℃ to 177 ℃.Their field of application when lubricated with code letter A grease is limited to 121 ℃.

Aerospace series - Bearings, airframe rolling - Rigid single row ball bearings in steel, cadmium plated, with flanged alignment housing, cadmium plated - Dimensions and loads

EN 3059:2007 航空航天系列.飞机机架滚动轴承.钢制带法兰定位盖的镀镉刚性单列滚珠轴承.尺寸和负荷

This standard specifies the characteristics of rigid single row ball bearings in steel, with cadmium-plated flanged alignment housing designed to withstand only slow rotations and oscillations under load. They are intended for use in the hubs of torsion lever and in separated supports for airframe/aerospace applications. The airframe rolling bearings defined inThis standard may be used in the temperature range from-54 ℃ to 150 ℃. However, being lubricated with the following greases (see EN 3727): ester type very high pressure grease (code letter A), operating range from-73 ℃ to 121 ℃ or, synthetic hydrocarbons type very high pressure grease general purpose (code letter B) operating range from-54 ℃ to 177 ℃. Their field of application when lubricated with code letter A grease is limited to 121 ℃.

Aerospace series - Bearings, airframe rolling - Rigid single row ball bearings in steel with flanged alignment housing, cadmium plated - Dimensions and loads

EN 3061:2007 航空航天系列.飞机机架转动轴承.耐腐蚀钢制带法兰定位盖的刚性单列滚珠轴承.尺寸和负荷

This standard specifies the characteristics of rigid single row ball bearings in corrosion resisting steel with a solid or lightweight flanged alignment housing, designed to withstand only slow rotations and slight oscillations under load. They are intended for use in the hubs of torsion lever and in separated supports for airframe/aerospace applications. The airframe rolling bearings defined inThis standard may be used in the temperature range from-54 ℃ to 150 ℃. However, being lubricated with the following greases (see EN 3727): ester type very high pressure grease (code letter A), operating range from-73 ℃ to 121 ℃ or, synthetic hydrocarbons type very high pressure grease general purpose (code letter B) operating range from-54 ℃ to 177 ℃. Their field of application when lubricated with code letter A grease is limited to 121 ℃.

Aerospace series - Bearings, airframe rolling - Rigid single row ball bearings in corrosion resisting steel, with flanged alignment housing - Dimensions and loads

EN 4033:2007 航空航天系列.飞机机架滚动轴承.耐腐蚀钢性单排滚珠轴承.内半径公差递减的直径级别8和9.尺寸和荷载

This standard specifies the characteristics of rigid single row ball bearings, in corrosion resisting steel, reduced internal radial clearance, diameter series 8 and 91), designed to withstand only slow rotations and oscillations under load. They are intended for use between fixed and moving parts of the aircraft structure and their control mechanisms. 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 3280), their field of application when lubricated with code A grease is limited to 121 ℃.

Aerospace series - Bearings, airframe rolling - Rigid single row ball bearings in corrosion resisting steel - Diameter series 8 and 9, reduced internal radial clearance - Dimensions and loads

EN 4034:2007 航空航天系列.飞机机架转动轴承.耐腐蚀钢制带法兰外圈内径递减的自准双列自调滚珠轴承.尺寸和负荷

This standard specifies the characteristics of self-aligning double row ball bearings with flanged outer ring in corrosion resisting steel, reduced internal clearance, designed to withstand only slow rotations and oscillations under load.They are intended for use between fixed and moving parts of the aircraft structure andTheir control mechanisms.They are intended to be used inThe temperature range:-54 ℃ to 150 ℃. However, being lubricated withThe 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 3280),Their field of application when lubricated with code A grease is limited to 121 ℃.

Aerospace series - Bearings, airframe rolling - Double row self- aligning ball bearings with flanged outer ring in corrosion resisting steel, reduced internal radial clearance - Dimensions and loads

DIN EN 4198:2007 航空航天系列.耐腐蚀钢带自润滑衬垫和螺纹柄的可调自动对心滑动轴承的杆端.尺寸和载荷

This standard specifies the characteristics of adjustable rod-ends consisting of: - a self-aligning ball bearing with self-lubricating liner,EN 2501, - a rod-end with threaded shank consisting of: - a circumferential groove to identity location, - an opational longitudinal groove for locking purposes. These rod-ends are intended for use with flying control rods or rods for aerospace structures.They shall be used within the temperature range from:-55°C to 163°C.

Aerospace series - Rod-ends, adjustable self-aligning plain bearing with self-lubricating liner and threaded shank in corrosion resisting steel - Dimensions and loads; German and English version EN 4198:2006

DIN EN 4036:2007 航空航天系列.减小内部径向间隙的耐腐蚀钢中可调自动对心双列滚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 rages -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.

Aerospace series - Rod ends, adjustable with self-aligning double row ball bearing and threaded shank in corrosion resisting steel, reduced internal radial clearance - Dimensions and loads; German and English version EN 4036:2006

DIN EN 4041:2007 航空航天系列.机架滚动轴承.带扩展内圈和法兰直排轴套的防腐蚀钢中刚性单列滚珠轴承.尺寸和负荷

This standard specifies the characteristics of rigid single row ball bearings in corrosion resisting steel with an extended inner ring and a solid or lightweight flanged alignment bush,designed to withstand only slow rotations and slight oscillations under load. They are intended for used in airframe fixed and moving elements and in flight control linkages. The bearings defined in this standard shall be used in the temperature range from -54°C to 150°C. However,as they are lubricated with the following greases(see EN 3727): - ester type very hihgh pressure grease(code letter A),operating range from -73°C to 121°C or, - synthetic hydrocarbons type very high pressure grease general purpose(code letter B) operating range from -54°C to 177°C. Their field of application when lubricated with code letter A grease is limited to 121°C.

Aerospace series - Bearings, airframe rolling - Rigid single row ball bearings in corrosion resisting steel, with extended inner ring and flanged alignment bush - Dimensions and loads; German and English version EN 4041:2006

DLA A-A-59701 B-2007 静电放电机械腕绳子捆扎 常规

This commercial item description (CID) covers the general requirements for electrical discharging wrist straps.

WRIST STRAP, ELECTROSTATIC DISCHARGE, GENERAL REQUIREMENTS FOR

DS/EN 2011:2007 轴承，机身滚动，刚性，单列耐腐蚀钢球轴承，直径系列 8 和 9 尺寸和载荷 航空航天系列

This standard specifies the characteristics, of rigid single row ball bearings of diameter 8 and 9 designed to withstand only slow rotations and oscillations under load. They are intended for use between fixed and moving parts of the aircraft structure and their control mechanisms.

Bearings, airframe rolling, rigid, single row ball bearings in corrosion resisting steel, diameter series 8 and 9 - Dimensions and loads - Aerospace series

DS/EN 2014:2007 轴承，机身滚动，刚性，单列耐腐蚀钢球轴承，直径系列 0 和 2 尺寸和载荷 航空航天系列

This standard specifies the characteristics, of rigid single row ball bearings of diameter 0 and 2 designed to withstand only slow rotations and oscillations under load. They are intended for use between fixed and moving parts of the aircraft structure and their control mechanisms.

Bearings, airframe rolling, rigid, single row ball bearings in corrosion resisting steel, diameter series 0 and 2 - Dimensions and loads - Aerospace series

DS/EN 2017:2007 轴承，机身滚动，双列，自动调心球轴承，耐腐蚀钢，直径系列 2 尺寸和载荷 航空航天系列

This standard specifies the characteristics, of double row self aligning ball bearings of diameter series 2 designed to withstand only slow rotations and oscillations under load. They are intended for use between fixed and moving parts of the aircraft structure and their control mechanisms.

Bearings, airframe rolling, double row, self aligning ball bearings, in corrosion resisting steel, diameter series 2 - Dimensions and loads - Aerospace series

DS/EN 2020:2007 轴承，机身滚动，单列，耐腐蚀钢调心滚子轴承，直径系列 3 和 4 尺寸和载荷 航空航天系列

This standard specifies the characteristics, of rigid single row ball bearings of diameter series 3 and 4 designed to withstand only slow rotations and oscillations under load. They are intended for use between fixed and moving parts of the aircraft structure and their control mechanisms.

Bearings, airframe rolling, single row, self aligning roller bearings in corrosion resisting steel, diameter series 3 and 4 - Dimensions and loads - Aerospace series

SAE AMS4805E-2007 油浸渍的89Cu - 10Sn烧结金属粉末的轴承

This specification covers one type of sintered metal powder in the form of oil-impregnated bearings.

Bearings, Sintered Metal Powder, 89Cu - 10Sn, Oil Impregnated

DIN EN 3727:2007 航空航天系列.有法兰定位盖的飞机机架用滚动轴承.技术规范

Aerospace series - Bearings, airframe rolling rigid with flanged alignment housing - Technical specification; German and English version EN 3727:2006

DLA A-A-50201 A VALID NOTICE 2-2007 带盒笔和铅笔支点弹簧绘图圆规

A-A-50201A, dated 25 September 2001, has been reviewed and determined to be valid for use in acquisition.

COMPASS, DRAFTING, PIVOT, DROP SPRING BOW, PEN& PENCIL, WITH CASE

SAE AIR5937-2007 电力制动器信息

This SAE Aerospace Information Report (AIR) describes the design, operation, and attributes of electrical braking systems for both military and commercial aircraft. At this time, the document focuses only on brakes utilizing electromechanical actuators (EMAs), as that is the present state of the art. As such, the discussions herein assume that EMAs can simply replace the hydraulic actuation portion of typical brake system leaving things such as the wheel and heat sink unchanged. Furthermore, the document provides detail information from the perspective of brake system design and operation. The document also addresses failure modes, certification issues, and past development efforts. Details on the design and control of electric motors, gear train design, ball or roller screw selection are available in the reference documents and elsewhere, but are outside the scope of this document. Other all-electric technologies such as piezoelectric actuation or more exotic methods of applying drag to a rotating wheel may be included at a later time. Important: Electric braking systems for aircraft are at the early stages of production implementation. There are also a variety of control schemes that may be used to provide acceptable EMA performance. As a result, many of the details involved in the design of electric brake systems are proprietary or competition sensitive to the brake system OEMs. This AIR attempts to provide a basic technical overview of electric brakes without compromising any particular manufacturers intellectual property concerns.

Information on Electric Brakes