V22 机械配件、构件 标准查询与下载
共找到 2047 条与 机械配件、构件 相关的标准，共 137 页
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BRACKET, MOUNTING, PLASTIC FOR USE WITH MS3367 PLASTIC TIEDOWN STRAPS
- ICS
- 49.060
- CCS
- V22
- 发布
- 2014-06-13
- 实施
Scope is unavailable.
BEARING, PLAIN, ROD END, SELF-ALIGNING, SELF-LUBRICATING, NARROW, EXTERNALLY THREADED, -65 TO +325 °F
- ICS
- 49.035
- CCS
- V22
- 发布
- 2014-06-03
- 实施
Scope is unavailable.
ADAPTER, AIRCRAFT, JACKING POINT, DESIGN AND INSTALLATION OF
- ICS
- 49.100
- CCS
- V22
- 发布
- 2014-05-29
- 实施
Scope is unavailable.
BEARING, BALL, AIRFRAME, ANTI-FRICTION, EXTERNAL SELF ALIGNING, EXTRA LIGHT DUTY
- ICS
- 49.045
- CCS
- V22
- 发布
- 2014-04-08
- 实施
Scope is unavailable.
BRACKET, ANGLE, 90°, CADMIUM PLATED, STEEL, UNS G41300, .190 BOLT
- ICS
- 49.035
- CCS
- V22
- 发布
- 2014-03-23
- 实施
La présente Norme Européenne définit les caractéristiques des anneaux d'arrêt, à montage radial, en acier, phosphatés pour applications aérospatiales.Ces anneaux d'arrêt sont seulement utilisés lorsque l'EN 3384 ne peut être employée pour des problèmes de montage.La phosphatation limite l'utilisation à des températures ne dépassant pas 200 oC.
Aerospace series - Rings retaining, radial mounting, steel, phosphated
- ICS
- 49.030.50
- CCS
- V22
- 发布
- 2014-03-12
- 实施
- 2014-03-12
Aerospace series - Weldability and brazeability of materials in aerospace constructions - Part 004: Welding and brazing of homogeneous assemblies of high alloyed steels; German version EN 4632-004:2012, Corrigendum to DIN EN 4632-004:2013-11
- ICS
- 49.025.01
- CCS
- V22
- 发布
- 2014-03
- 实施
This specification covers a nitriding grade of aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock. These products have been used typically for nitrided parts such as bearings, operating under heavy loads and high speeds at moderate temperatures, and subject to rigid inspection standards, and requiring highest surface hardness, high core toughness, and less distortion than parts made from steel requiring quenching to case harden, but usage is not limited to such applications.
Steel Bars, Forgings, and Tubing, Nitriding, 1.4Cr - 1.2Mo - 0.3V (0.29 - 0.36C) Aircraft-Quality for Bearing Applications
- ICS
- 49.025.10
- CCS
- V22
- 发布
- 2013-11-07
- 实施
Aerospace series - Weldability and brazeability of materials in aerospace constructions - Part 004: Welding and brazing of homogeneous assemblies of high alloyed steels; German version EN 4632-004:2012
- ICS
- 49.025.01
- CCS
- V22
- 发布
- 2013-11-01
- 实施
The focus of this SAE Aerospace Standard (AS) is the integration of thermally actuated pressure release devices, hereafter referred to as fuse plugs, with the wheel and brake assembly. It does not address the manufacturing, quality or acceptance test requirements pertaining to the production of these fuse plugs. It establishes minimum design, installation, qualification, and operational requirements for fuse plugs which are used only in tubeless tire type aircraft braked wheels. Fuse plugs are designed to completely release the contained inflation pressure from a tubeless tire and wheel assembly when brake generated heat causes the tire or wheel to exceed a
Thermal Sensitive Inflation Pressure Release Devices for Tubeless Aircraft Wheels
- ICS
- 83.160.20
- CCS
- V22
- 发布
- 2013-11-01
- 实施
Aerospace series - Weldability and brazeability of materials in aerospace constructions - Part 006: Homogeneous assemblies of titanium alloys; German version EN 4632-006:2013
- ICS
- 49.025.01
- CCS
- V22
- 发布
- 2013-11-01
- 实施
Aerospace series. Connectors, plug and receptacle, electrical, rectangular, interchangeable insert type, rack to panel, operating temperature 150°C continuous. Specification of performance and contact arrangements
- ICS
- 49.060
- CCS
- V22
- 发布
- 2013-09-30
- 实施
- 2013-09-30
Aerospace series - Steel X2NiCoMo18-8-5 (1.6359) - Vacuum induction melted and vacuum arc remelted - Solution treated and precipitation treated - Bar - a or D < ou = 150 mm - 1 750 MPa < or = Rm < or = 2 000 MPa
- ICS
- 49.025.10
- CCS
- V22
- 发布
- 2013-08-17
- 实施
- 2013-08-17
AMS-T-6845B stabilizes this document because equivalent technical requirements are contained in AMS5566. AMS-T-6845B has been declared ""STABILIZED"" by AMS Committee F and will no longer be subjected to periodic reviews for currency. Users are responsible for verifying references and continued suitability of technical requirements. Newer technology may exist. AMS Committee F has never performed a technical update of this document. Users of this document should refer any certification issues (e.g. exceptions listed on the certification report) to the cognizant engineering organization for their disposition. CAUTION: In many cases the purchaser is not the co
Tubing, Steel, Corrosion-Resistant (S30400), Aerospace Vehicle Hydraulic System 1/8 Hard Condition
- ICS
- 49.080
- CCS
- V22
- 发布
- 2013-07-31
- 实施
Aerospace series - Bearing spherical plain, metal to metal, in corrosion resisting steel, cadmium plated - Wide series - Dimensions and loads - Inch series; German and English version EN 4266:2013
- ICS
- 49.035
- CCS
- V22
- 发布
- 2013-06
- 实施
Aerospace series - Connectors, electrical, circular, scoop-proof, triple start threaded coupling, operating temperature 175 °C or 200 °C continuous - Part 001: Technical specification; German and English version EN 3645-001:2013
- ICS
- 49.060
- CCS
- V22
- 发布
- 2013-06
- 实施
This standard covers the requirements for spherical, self-aligning, self-lubricating, bearings which are for use in the ambient temperature range of -65 to +160 degree F (-54 to 71 degree C) at high cyclic speeds 300 cpm (13 fpm) for liners with a thickness less than 0.015 inch. The scope of this 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. Under Department of Defense (DoD) Policies and Procedures, any qualification requirements and associated Qua
Bearings, Plain, Self-Aligning, Self-Lubricating, 300 cpm (13 fpm) -65 to +160 degree F (-54 to +71 degree C), Liners Less than 0.015 Inches
- ICS
- 49.035
- CCS
- V22
- 发布
- 2013-05-08
- 实施
The reason for creating this standard is to quality bearings for use in tail rotor bearing applications. The standard also incorporates an ""A"" part number designation for a new liner system that has 2-1/2 times the life of the standard liner system.
Bearings, Plain, Self-Aligning, Self-Lubricating, 1400 cpm (15 fpm), Oscillation, -65 to +160 degree F (-54 to +71 degree C)
- ICS
- 49.035
- CCS
- V22
- 发布
- 2013-05-06
- 实施
The reason for creating this standard is to quality bearings with a liner thickness less than .015 inches for use in main rotor bearing applications. The standard also incorporates an ""A"" part number designation for a new liner system that has 2-1/2 times the life of the standard liner system.
Bearings, Plain, Self-Aligning, Self-Lubricating, 300 cpm (13 fpm), Oscillation, -65 to +160 degree F, Liners Less than .015 Inch Thick
- ICS
- 49.035
- CCS
- V22
- 发布
- 2013-05-06
- 实施
Aerospace series. Bearing spherical plain, metal to metal, in corrosion resisting steel, cadmium plated. Wide series. Dimensions and loads. Inch series
- ICS
- 49.035
- CCS
- V22
- 发布
- 2013-04-30
- 实施
- 2013-04-30
