49.035 航空航天制造用零部件 标准查询与下载
共找到 2327 条与 航空航天制造用零部件 相关的标准，共 156 页
The purpose of this report is to provide design, application and maintenance engineers with basic information on the use of metallic Spring Energized sealing devices when used as piston (OD) and rod (ID) seals in aircraft fluid power components such as actuators, valves, and swivel glands. The Spring Energized seal is defined and the basic types in current use are described. Guidelines for selecting the type of Spring Energized seal for a given design requirement are covered in terms of friction, leakage, service life, installation characteristics, and interchangeability. Spring Energized seals can also be made in various forms and types, including face seals (internal and external pressure sealing types), and rotary variants too. These further types will not be discussed in this document, but many of the same principles apply for them as well.
Selection of Metallic Spring Energized Seals for Aerospace
- ICS
- 49.035
- CCS
- V21
- 发布
- 2010-12-02
- 实施
This standard specifies the characteristics of bearings, spherical plain in corrosion resisting steel with self-lubricating liner, elevated load under low oscillations, with low friction coefficient, narrow series, inch series. They shall be used in the temperature range – 54 °C to 120 °C.
Aerospace series. Bearings, spherical plain, in corrosion resisting steel with self-lubricating liner elevated load under low oscillations. Narrow series. Dimensions and loads. Inch series with low friction coefficient
- ICS
- 49.035
- CCS
- V22
- 发布
- 2010-11-30
- 实施
- 2010-11-30
This standard specifies the characteristics of bearings, spherical plain in corrosion resisting steel with self-lubricating liner, elevated load under low oscillations, with low friction coefficient, wide series, inch series. They shall be used in the temperature range – 54 °C to 120 °C.
Aerospace series. Bearings, spherical plain, in corrosion resisting steel with self-lubricating liner elevated load under low oscillations. Wide series. Dimensions and loads. Inch series with low friction coefficient
- ICS
- 49.035
- CCS
- V22
- 发布
- 2010-11-30
- 实施
- 2010-11-30
This standard specifies the characteristics of bearings, spherical plain in corrosion resisting steel with self lubricating liner, elevated load under low oscillations, with low friction coefficient, narrow series, inch series.They shall be used in the temperature range - 54 °C to 120 °C.
Aerospace series - Bearings, spherical plain, in corrosion resisting steel with self-lubricating liner elevated load under low oscillations - Narrow series - Dimensions and loads - Part 003: Inch series with low friction coefficient
- ICS
- 49.035
- CCS
- 发布
- 2010-11-21
- 实施
- 2010-11-21
This standard specifies the characteristics of bearings, spherical plain in corrosion resisting steel with self lubricating liner, elevated load under low oscillations, with low friction coefficient, wide series, inch series.They shall be used in the temperature range - 54 °C to 120 °C.
Aerospace series - Bearings, spherical plain, in corrosion resisting steel with self-lubricating liner elevated load under low oscillations - Wide series - Dimensions and loads - Part 003: Inch series with low friction coefficient
- ICS
- 49.035
- CCS
- 发布
- 2010-11-21
- 实施
- 2010-11-21
Aerospace series - Test specification for vibration control components; German and English version EN 4662:2010
- ICS
- 49.035
- CCS
- V22
- 发布
- 2010-10-01
- 实施
This standard covers the requirements for spherical, sel-aligning, self-lubricating bearings which are for use in the ambient temperature range -65 to +160°F (-54 to +71 \MD) at high cyclic speeds. The scope of the standard is to provide a liner system qualification procedure for helicopter sliding bearings defined and controlled by source control drawings. Once a liner system is qualified the source-controlled bearings are further tested under application conditions.
Bearing, Plain, Self-Aligning, Self- Lubricating, High Speed Oscillation -65 to +160 °F General Specification for
- ICS
- 49.035
- CCS
- V22
- 发布
- 2010-09-21
- 实施
Aerospace series - Bushes, plain in corrosion resisting steel with self-lubricating liner, elevated load - Part 2: Dimensions and loads - Inch series; German and English version EN 4536-2:2009
- ICS
- 49.035
- CCS
- V21
- 发布
- 2010-09-01
- 实施
This standard covers plain and flanged sleeve bearings which are self-lubricating by incorporating polytetrafluoroethylene (PTFE) in a liner in the bore for use in a temperature range of -65 to +250 °F (-54 to +121 °C). This procurement document and it's corresponding parts sheets are being updated and re-formatted from MIL-B-8942 to the SAE standard.
Bearings, Sleeve, Plain and Flanged, Self Lubricating -65 to +250 °F
- ICS
- 49.035
- CCS
- V22
- 发布
- 2010-08-13
- 实施
PLUG, MACHINE THREAD DRILLED, PREFORMED PACKING, AS8879 THREAD (UNS S34700)
- ICS
- 49.035
- CCS
- V20
- 发布
- 2010-07-19
- 实施
This document is intended to give advisory information for the selection of plain bearings and bearing materials most suitable for aircraft landing gear applications. Information included herein was derived from bearing tests and service experience/reports. Airframe/landing gear manufactureres, commerical airlines, U.S. Air Force and Naval Air Systems Command provided input for the document. Information is given on bearing installation methods and fits that have given satisfactory performance and service life Bast metal corrosion is a major cause of problems in bearing installations for landing gear. Therefore, methods of corrosion prevention are discussed. Effort is directed toward minimizing maintenance and maximizing life expectancy of landing gear bearings. Lubricated and self-lubricating bearings are also discussed. There are wide ranges of bearing load and motion requirements for applications in aircraft landing gears. For this reason, it is the responsibility of the designer to select that information which pertains to the particular application. Anti-friction bearings, defined as rolling element bearings generally used in wheel and live axle applications, will not be discussed in this document. Landing gear shock strut bearing design and selection criteria are covered in SAE AIR 5883 and, therefore, are not discussed in detail in this document.
Plain Bearing Selection for Landing Gear Applications
- ICS
- 49.035
- CCS
- V22
- 发布
- 2010-07-15
- 实施
No scope available.
Bearing, Plain, Self-Lubricating, Self-Aligning, Low Speed, Narrow, Grooved Race, -65 to +325°F
- ICS
- 49.035
- CCS
- V22
- 发布
- 2010-06-14
- 实施
No scope available.
Bearing, Plain, Self-Lubricating, Self-Aligning, Low Speed, Wide, Chamfered Race, -65 to +325°F
- ICS
- 49.035
- CCS
- V22
- 发布
- 2010-06-14
- 实施
This standard specifies the procedure and the parameter for testing static and dynamic stiffness of vibration control components (e.g. shock mounts with bushes).This standard applies to vibration control components all installed for aircraft applications. It may be applied when referred to in the product standard or in a design specification.
Aerospace series - Test specification for vibration control components
- ICS
- 49.035
- CCS
- 发布
- 2010-04-09
- 实施
- 2010-04-09
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
- ICS
- 49.035
- CCS
- V22
- 发布
- 2010-04
- 实施
This standard specifies the characteristics of bearings, spherical plain in corrosion resisting steel with self-lubricating 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 ФC to 163 ФC.
Aerospace series - Spherical plain bearings in corrosion resisting steel with self-lubricating liner, narrow series - Dimensions and loads - Inch series; German and English version EN 4613:2009
- ICS
- 49.035
- CCS
- V22
- 发布
- 2010-04
- 实施
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
- ICS
- 49.035
- CCS
- V22
- 发布
- 2010-04
- 实施
This standard specifies the characteristics of bearings, spherical plain with self lubricating liner in corrosion resisting steel with self-lubricating liner, wide 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 ФC to 163 ФC.
Aerospace series - Spherical plain bearings in corrosion resisting steel with self-lubricating liner, wide series - Dimensions and loads - Inch series; German and English version EN 4614:2009
- ICS
- 49.035
- CCS
- V21
- 发布
- 2010-04
- 实施
This British Standard specifies procedures for the inspection, testing and acceptance of seamless steel tube and tubestock for aerospace use. The standard is applicable to material specifications in the British Standard Aerospace T series and also to other British Standard material specifications for seamless steel tubes and tubestock which are suitable for aerospace use.
Aerospace series - Procedure for inspection, testing and acceptance of seamless steel tubes and tubestock
- ICS
- 49.035
- CCS
- V21
- 发布
- 2010-03-31
- 实施
- 2010-03-31
This document covers recommendations for the application of existing qualified and approved in-service fixed wing aircraft tires, wheels and brakes to military and commercial rotorcraft. NOTE: This document does not address the use of radial tires due to insufficient data to support their approved use on rotorcraft, see paragraph 4.3.14 for specific impact on ground resonance. This document provides recommended parameters and data to enable evaluation of existing aircraft tires, wheels and brakes for rotorcraft applications. It is intended for use by commercial and military personnel in formulating detail design and performance specifications. It is not intended to be used as a procurement document.
Rotorcraft: Application of Existing Aircraft Designed Tires, Wheels and Brakes
- ICS
- 49.035
- CCS
- V42
- 发布
- 2010-01-06
- 实施
