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
Specification of the rotating component in space science experiments—Part 9：Delivery
- ICS
- 49.035
- CCS
- V22
- 发布
- 2019-06-04
- 实施
- 2019-10-01 00:00:00.0
Specification of the rotating component in space science experiments—Part 10：Storage and reinspection
- ICS
- 49.035
- CCS
- V22
- 发布
- 2019-06-04
- 实施
- 2019-10-01 00:00:00.0
本标准规定了主要用于航空电机的标准轻型深沟球轴承的结构、尺寸和要求。 本标准适用于航空电机用标准轻型深沟球轴承的选用。
Standard light annular ball bearings primarily for aircraft generators and motor-generators
- ICS
- 49.035
- CCS
- V22
- 发布
- 2018-06-07
- 实施
- 2019-01-01
General specification for deep groove bearings of aircraft generators and motor generators
- ICS
- 49.035
- CCS
- V22
- 发布
- 2018-05-14
- 实施
- 2018-12-01 00:00:00.0
本标准规定了主要用于航空电机的宽型深沟球轴承的结构、尺寸和要求。 本标准适用于航空电机用宽型深沟球轴承的选用。
Wide cartridge annular ball bearings primarily for aircraft generators and motor-generators
- ICS
- 49.035
- CCS
- V22
- 发布
- 2018-05-14
- 实施
- 2018-12-01
本标准规定了主要用于航空电机的薄超轻型深沟球轴承的结构、尺寸和要求。 本标准适用于航空电机用薄超轻型深沟球轴承的选用。
Thin extra light annular ball bearings primarily for aircraft generators and motor-generators
- ICS
- 49.035
- CCS
- V22
- 发布
- 2018-05-14
- 实施
- 2018-12-01
Interface design specification for standard modules of science experiment rack in space station
- ICS
- 49.045
- CCS
- V22
- 发布
- 2017-12-29
- 实施
- 2018-04-01 00:00:00.0
GB/T 28878的本部分规定了空间科学实验装置转动部件的测试条件、项目和顺序、方法以及测试结果的数据处理。 本部分适用于空间科学实验装置转动部件的性能测试。其他有效载荷及空间飞行器平台的转动部件性能测试可参照使用。
Specification of the rotating component in space science experiments—Part 6：Property testing
- ICS
- 49.035
- CCS
- V22
- 发布
- 2016-12-13
- 实施
- 2017-03-01 00:00:00.0
GB/T 28878的本部分规定了空间科学实验装置转动部件的滚动轴承润滑设计及验证的要求。 本部分适用于空间科学实验装置转动部件滚动轴承的润滑设计。其他有效载荷和空间飞行器平台转动部件的润滑设计可参照使用。
Specification of the rotating component in space science experiments.Part 2:Requirements of lubrication design
- ICS
- 49.035
- CCS
- V22
- 发布
- 2016-08-29
- 实施
- 2016-11-01
GB/T 28878的本部分规定了空间科学实验装置转动部件的可靠性试验项目、方法和程序，以及试验条件制定、试验周期确定的方法和可靠性试验的实施程序。 本部分适用于空间科学实验装置转动部件地面进行的可靠性试验。其他有效载荷和空间飞行器平台转动部件的可靠性试验可参照使用。
Specification of the rotating component in space science experiments.Part 7:Reliability test
- ICS
- 49.035
- CCS
- V22
- 发布
- 2016-08-29
- 实施
- 2016-11-01
This standard specifies the required characteristics, inspection and test methods, qualification and acceptance conditions for rod assemblies with two adjustable ends with integrated bolts, designed to withstand static and dynamic loads possible for interior and substructure in the temperature range from -55 °C to 85 °C. It is applicable whenever referenced. For a complete overview see EN 4691-2.
Aerospace series - Tie rod with integrated bolts - Part 1: Technical specification; German and English version EN 4691-1:2017
- ICS
- 49.035
- CCS
- V22
- 发布
- 2018-04-00
- 实施
This standard specifies the dimensions and tolerances of rod assemblies for aerospace applications with two adjustable ends with integrated bolts for interior and sub structure in the temperature range -55 °C to 85 °C. The rod ends should not be screwed completely apart.
Aerospace series - Tie rod with integrated bolts - Assembly code A, B and C; German and English version EN 4693:2017
- ICS
- 49.035
- CCS
- V22
- 发布
- 2018-04-00
- 实施
This standard specifies the dimensions and tolerances of rod assemblies for aerospace applications with two adjustable ends with integrated bolts for interior and sub structure in the temperature range -55 °C to 85 °C. The rod ends should not be screwed completely apart.
Aerospace series - Tie rod with integrated bolts - Assembly code D, E and F; German and English version EN 4694:2017
- ICS
- 49.035
- CCS
- V22
- 发布
- 2018-04-00
- 实施
This standard specifies the dimensions and tolerances of rod assemblies for aerospace applications with two adjustable ends with integrated bolts for interior and sub structure in the temperature range -55 °C to 85 °C. The rod ends should not be screwed completely apart.
Aerospace series - Tie Rod with integrated bolts - Assembly Code G, H and K; German and English version EN 4695:2017
- ICS
- 49.035
- CCS
- V22
- 发布
- 2018-04-00
- 实施
This standard shows the locking clips for the construction kit of rod assemblies for aerospace applications with two adjustable ends with integrated bolts for interior and sub structure in the temperature range -55 °C to 85 °C (EN 4691-2).
Aerospace series - Tie Rod with integrated bolts - Locking clip; German and English version EN 4692:2017
- ICS
- 49.035
- CCS
- V22
- 发布
- 2018-04-00
- 实施
Aerospace series. Tie rod with integrated bolts. Overview construction kit
- ICS
- 49.035
- CCS
- V22
- 发布
- 2018-01-26
- 实施
- 2018-01-26
This European Standard specifies the characteristics of plain bushes in corrosion resisting steel with self-lubricating liner and the design recommendation of shafts and housings. The bushes are intended for operation within the temperature range of 55 °C to 163 °C and assembly with an interference fit into fixed and moving aerospace parts.
Aerospace series - Bush, plain, in corrosion resisting steel with self-lubricating liner - Dimensions and loads; German and English version EN 2287:2017
- ICS
- 49.030.99
- CCS
- V22
- 发布
- 2017-12-01
- 实施
Aerospace series. Static seal elements O-Ring for straight thread tube fitting boss, ethylene-propylene, moulded, phosphate ester resistant (-55
- ICS
- 49.035
- CCS
- V22
- 发布
- 2017-07-10
- 实施
- 2017-07-10
Aerospace series - Hydraulic tubing joints and fittings - Planar flexure test
- ICS
- 49.080
- CCS
- V22
- 发布
- 2017-04
- 实施
Aerospace series. Rod-ends, adjustable, single fork with UNJ threaded shank min. engagement: 1,5 x thread diameter in corrosion resisting steel. Dimensions and loads. Inch series
- ICS
- 49.035
- CCS
- V22
- 发布
- 2017-01-31
- 实施
- 2017-01-31
