V22 机械配件、构件 标准查询与下载

DIN EN 2585:2006 航空航天系列.室温条件下高负荷、宽系列、带自润滑衬套的耐蚀钢关节轴承.尺寸和负载

This standard specifies the characteristics of spherical plain bearings in corrosion resisting steel, with self- lubricating liner, narrow series, for elevated load at ambient temperature, with or without swaging groove, intended for use in the 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 - Bearings, spherical plain in corrosion resisting steel with self-lubricating liner - Wide series - Elevated load at ambient temperature - Dimensions and loads; German and English version EN 2585:2001

DIN EN 3048:2006 航空航天系列.室温条件下高负荷、轻系列、带自润滑衬套的耐蚀钢关节轴承.尺寸和负载

This standard specifies the characteristics of spherical plain bearings in corrosion resisting steel, with self-lubricating liner, light series, for elevated load at ambient temperature, with or without swaging groove, intended for use in the fixed or moving parts of the aircraft structure and control mechanisms. They shall be used in the temperature range - 55 ?to + 163 ?#,,#

Aerospace series - Bearings, spherical plain in corrosion resisting steel with self-lubricating liner - Light series - Elevated load at ambient temperature - Dimensions and loads; German and English version EN 3048:2001

SAE AMS2310F-2006 钢横截抗拉性能抽样和试验资格

This specification covers procedures for sampling and testing aircraft-quality, special aircraft-quality, and premium aircraft-quality requiring transverse tensile property testing.

Qualification Sampling and Testing of Steels for Transverse Tensile Properties

SAE AIR4012B-2006 USAF飞行器轮

This SAE Aerospace Information Report is intended to provide comprehensive reference and background information pertaining to military aircraft wheel service experience. The document contains extensive technical performance information for a variety of active military aircraft as well as field and depot service experience and lessons learned. This SAE Aerospace Information Report (AIR) documents general technical data associated with many of the wheels used in the Air Force. This document is intended to be used as a general reference for the aerospace community.

(R) USAF Aircraft Wheels

SAE AS21443A-2006 滑轮、减少摩擦、机架、滚珠轴承

(R) Bearing, Ball, Airframe, Anti-Friction, PulleyTABLE 1 IS ABOUT RADIAL LIMIT LOAD RATING LB AND WEIGHT POUNDS (APPROX) ETC..

(R) Bearing, Ball, Airframe, Anti-Friction, Pulley

SAE AS5355A-2006 夹紧带槽V形带联结器

This SAE Aerospace Standard (AS) establishes the requirements for a V-band grooved clamp couplings that are intended for use on fluid-line tubing joints, tailpipe joints, and accessory mount joints, on flight vehicles or other attachments. The semi-rigid coupling joint assemblies, hereafter referred to as the joint, shall operate within the temperature ranges specified in their applicable part standards.

Couplings, Clamp, Grooved, V-Band

BS EN 2336:2005 航空航天系列.带装配槽的钢制球面滑动轴承.尺寸和负载

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 °C to 150 °C. 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 °C to 121 °C or,  synthetic hydrocarbon 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 grease code letter A is limited to 121 °C.

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

DLA MS27595 REV E-2006 聚四氟乙烯连续环形支持包装固定器

1. SURFACES MUST BE SMOOTH AND FREE FROM IRREGULARITIES. EDGES MUST BE CLEAN AND SHARP. 2. DIMENSIONS IN INCHES. 3. FOR USE IN PACKING GROOVES CONFORMING TO SPECIFICATION MIL-G-5514,

RETAINER, PACKING BACKUP, CONTINUOUS RING, POLYTETRAFLUOROETHYLENE

DLA MS28782 REV E-2006 聚四氟乙烯裱包装固定器

This specification sheet is approved for use by all epartments and Agencies of the Department of Defense.

RETAINER, PACKING, BACK-UP, TEFLON

DLA MS17815 REV B NOTICE 1-2006 飞机场灯的索卡

MS17815B is inactive for new design and is no longer used, except for replacement purposes.

CLAMP, CABLE, AVIATION GROUND LIGHTS

ASTM F2563-06(2010) 娱乐用飞机工具箱装配说明书

1.1 This practice covers the instructions a kit producer must provide to a consumer in order to assemble and safely flight-test a recreational aircraft to ensure compliance with applicable ASTM standards. 1.2 The instructions prescribe the necessary mechanical skills or training, or both, required for successful completion of the kit, as well as necessary tooling, fixtures, inspections, measurements, and other pertinent items required for successful completion of the kit. Proof of compliance with these instructions may be vital for obtaining flight authorizations from the applicable CAA. 1.3 This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety and health practices and determine the applicability of regulatory limitations prior to use.

Standard Practice for Kit Assembly Instructions of Aircraft Intended Primarily for Recreation

AGMA 06FTM10-2006 直升机设施用双螺旋混合行星齿轮传动高接触比超安全高传动比的制造、装配和试验

An ultra-safe, high ratio planetary transmission, for application as a helicopter main rotor drive, has been designed, fabricated and tested under the sponsorship of NRTC-RITA. The anticipated improvements offered by this new planetary transmission are reduced weight, reduced transmitted noise and improved fail-safety. This paper discusses the fabrication assembly and test results for the subject planetary transmission. The design and analysis of this transmission system have been discussed in a previous paper presented at the AGMA FTM in 2004. The ultra-safe, high ratio planetary transmission design utilizes a compound planetary configuration with a 17.5:1 reduction ratio which would replace a conventional two stage simple planetary transmission. The new design uses ultra-safe principles such as split-torque paths and high combined contact ratio gearing. Double helical gears in the planet/ ring meshes balance axial tooth forces so that axial bearing reactions are not required. The spur gear sun/planet meshes are staggered to achieve a compact spatial arrangement. Fabrication and assembly of the components for this transmission are complicated by their configuration. The grinding process for the helical gears must use small diameter wheels due to the proximity of the adjacent helix, since most the gears in this configuration are integrated designs. Assembly procedures also require special consideration because of the integrated design and helical gears. Test results are presented to support the goals of this project, including, concept verification, weight reduction, noise reduction and determination of the operating characteristics of the test transmission.

Fabrication, Assembly and Test of a High Ratio, Ultra Safe, High Contact Ratio, Double Helical Planetary Transmission for Helicopter Applications

SAE AMS4800E-2006 91Sn 4.5Sb 4.5Cu巴比特轴承

This specification covers bearings cast on one or both faces of a steel or bronze backing. Primarily for bearings, bushings, and sleeves.

Bearings, Babbitt 91Sn - 4.5Sb - 4.5Cu

ASTM F2563-06 娱乐用主要预期飞行器工具组件用法说明的标准实施规程

1.1 This practice covers the instructions a kit producer must provide to a consumer in order to assemble and safely flight-test a recreational aircraft to ensure compliance with applicable ASTM standards.1.2 The instructions prescribe the necessary mechanical skills or training, or both, required for successful completion of the kit, as well as necessary tooling, fixtures, inspections, measurements, and other pertinent items required for successful completion of the kit. Proof of compliance with these instructions may be vital for obtaining flight authorizations from the applicable CAA.This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety and health practices and determine the applicability of regulatory limitations prior to use.

Standard Practice for Kit Assembly Instructions of Aircraft Intended Primarily for Recreation

SAE AS9552A-2005 CRES UNS S32100 扁平钢托架

(R) BRACKET, FLAT, CRES UNS S32100 FSC 5340TABLE2 - PART NUMBERS AND LENGTH (L) DIMENSIONS

Bracket, Flat, Cres UNS S32100

HB 7782-2005 定向凝固叶片中再结晶的检测与评定方法

本标准规定了航空发动机定向凝固涡轮工作叶片中再结晶的检测方法与评定标准。 本标准适用于航空发动机定向凝固涡轮工作叶片生产制造过程中再结晶的检测与评定。

Testing and evaluation method for recrystallization on directionally solidified blades

HB 7780-2005 镁合金铸件规范

本规范规定了镁合金及铸件的要求、质量保证规定和交货准备等。 本规范适用于镁合金砂型和金属型铸件的生产和验收。

Specification for magnesium alloy castings

HB/Z 358-2005 航空钢弹簧制件热处理

本指导性技术文件规定了航空钢弹簧制件热处理的常用材料牌号及技术标准、设备、工艺材料、工艺、质量控制和检验等。 本指导性技术文件适用于航空钢弹簧制件的热处理。

Heat treatment for spring parts of steel for aviation

HB 963-2005 铝合金铸件规范

本规范规定了铝合金铸件的要求、质量保证规定和交货准备等。 本规范适用于砂型、金属型、熔模、石膏型、壳型等铝合金铸件。 本规范不适用于铝合金铸件。

Specification for aluminium alloy castings

HB 0-83-2005 航空附件产品型号命名

本标准规定了航空附件产品的型号命名方法。 本标准适用于具有独立功用、可单独出厂并需编写产品标准（技术条件或技术规范）的航空附件产品（包括飞机、发动机在起动、起飞和着陆等工作状态中所用的各系统附件及军械、救生和空投传输等装置，以下简称产品）的型号命名。

Type designation of accessory for aviation