V38 液压、冷气系统及其附件 标准查询与下载
共找到 272 条与 液压、冷气系统及其附件 相关的标准，共 19 页
Pollution des circuits hydrauliques par particules solides - Généralités. .
- ICS
- 49.080;75.120
- CCS
- V38
- 发布
- 1982-09-01
- 实施
- 1982-09-18
この規格は，航空機油圧系統(6.1参照)に用いる大部分の油圧構成部品(6.2参照)に共通の一般要求事項について規定する。
Hydraulic system components, aircraft, general specification for
- ICS
- 49.080
- CCS
- V38
- 发布
- 1982-03-01
- 实施
この規格は，MIL-H-5440(JIS W 2914)及びMIL-H-8891の要求事項に従って設計された航空機油圧系統，並ぴにMIL-P--5518(JIS W 0604)の要求事項に従って設計された航空機空気圧系統の試験に関する要求事項及び試駿方法について規定する。
Test for aircraft hydraulic and emergency pneumatic systems
- ICS
- 49.080
- CCS
- V38
- 发布
- 1982-03-01
- 实施
Hydraulic systems, aircraft, type I and II, design and installation requirements for
- ICS
- 49.080
- CCS
- V38
- 发布
- 1982-03-01
- 实施
Aerospace fluid systems; Thermal shock testing of piping and fittings
- ICS
- 3010;1150
- CCS
- V38
- 发布
- 1982-03
- 实施
General technical requirements for aviation hydraulic steering gear
- ICS
- CCS
- V38
- 发布
- 1982-01-01
- 实施
- 1982-01-01
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Fitting end, attachable, hydraulic, high-pressure hose
- ICS
- 83.140
- CCS
- V38
- 发布
- 1981-12-16
- 实施
- 1981-12-16
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Hose, rubber, hydraulic, fuel and oil resistant
- ICS
- 83.140
- CCS
- V38
- 发布
- 1981-12-16
- 实施
- 1981-12-16
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Hose assemblies, rubber, hydraulic, fuel and oil resistant
- ICS
- 83.140
- CCS
- V38
- 发布
- 1981-10-06
- 实施
- 1981-10-06
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Adapter, hose to tube, pipe and flange,reusable : Hydraulic, fuel and oil lines
- ICS
- 83.14
- CCS
- V38
- 发布
- 1981-10-06
- 实施
- 1981-10-06
Aircraft; Connections for checking hydraulic systems by ground appliances
- ICS
- 5190;1150
- CCS
- V38
- 发布
- 1981-10
- 实施
Replenishment connection for liquid nitrogen.
- ICS
- 49.100;49.080
- CCS
- V38
- 发布
- 1978-04-01
- 实施
- 1978-04-01
This amendment forms a part of Military Specification MIL-P-26191B(USAF), dated 29 October 1970, and is approved for use by a l l Departments and Agencies of the Department of Defense.
PUMPING UNIT, HYDRAULIC AF/M27M-1 AND AF/M27M-2
- ICS
- 49.080
- CCS
- V38
- 发布
- 1978
- 实施
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Tube fitting’s assembly function inspection for aircraft hydraulic system
- ICS
- 49.08
- CCS
- V38
- 发布
- 1977-12-13
- 实施
- 1977-12-13
SPECIFICATION 1. Inspection and testing procedure 2. Process of manufacture 3. Chemical composition 4. Surface dressing 5. Condition 6. Final heat treatment 7. Mechanical properties 8. Special tests 9. Susceptibility to intercrystalline corrosion 10. Non-destructive testing 11. Final marking APPENDICES A. Notes on table 1 B. Notes on table 2 TABLES 1. Tolerances on outside diameters and thicknesses, and test conditions. Metric unit sizes 2. Tolerances on outside diameters and thicknesses, and test conditions. Imperial unit sizes
Specifications for 18/10 chromium-nickel corrosion-resisting steel tube for hydraulic purposes (niobium/titanium stabilized: 550 MPa)
- ICS
- 49.080
- CCS
- V38
- 发布
- 1977-05-31
- 实施
- 1977-05-31
이 규격은 내고온 석유계 윤활유가 사용되며, -55℃(-67℉)정도의 저온에서 사용되는 항
Rings, sealing, synthetic rubber oil resistant
- ICS
- 21.14
- CCS
- V38
- 发布
- 1976-12-17
- 实施
- 1976-12-17
This British Standard specifies the dimensions for three basic external profiles (types 1, 2 and 3 respectively) for flanges for V-flange couplings used in aircraft for the purpose of coupling components to piping/ducting or effecting joints in piping/ducting. It also specifies a standard range of flange outside diameters for each profile type as follows. Type 1. Solid profile 44.45 mm to 222.25 mm diameter Type 2. Solid profile; large 239.47 mm to 379.17 mm diameter diameter/low pressure Type 3. Rolled flange profile 39.42 mm to 219.48 mm diameter In addition, the basic requirements for the associated couplings clamps are included.
Specification for V-flange couplings for aircraft piping and ducting - metric series
- ICS
- 49.080
- CCS
- V38
- 发布
- 1976-08-31
- 实施
- 1976-08-31
JOINTS, HYDRAULIC SWIVEL
JOINTS, HYDRAULIC SWIVEL
- ICS
- 49.080
- CCS
- V38
- 发布
- 1976-04-16
- 实施
This document is a compendium of recommended practices for the design of tubing systems for the transmission of liquid and gasses in fluid power systems for aerospace vehicles such as aircraft, missiles and boosters, and is considered applicable to the design of future space vehicles and other applications using aircraft technology. Primary emphasis is given to recommended practices for line sizing, tube routing, supports and clamping, stress considerations and permissible defects, and provisions for flexure through the use of flexible hoses, coiled tubes, swivel joints, and expansion glands. Fluid power systems are differentiated from the normal aircraft fuel and oil systems and the various fluid systems used for environmental control and air conditioning systems; however, the practices cited herein will in many cases be applicable to these other systems. A section (3) regarding tubing materials and fitting types currently in use in included for reference, but particular recommendations are purposely avoided since their selection is dependent upon the specific requirements of each particular vehicle system and many other factors.
Recommended Practice for the Design of Tubing Installations for Aerospace Fluid Power Systems
- ICS
- 49.080
- CCS
- V38
- 发布
- 1976-04-01
- 实施
Provides a design for quick-release couplings with involute spline drive, intended primarily for aircraft engine/gearbox accessories which require to be removed whilst the engine/gearbox is in service. Comprises design notes and recommendations, accessory flanges up to and above spigot reference 25O, engine/gearbox pads up to and above spigot reference 250, coupling clamps, selected involute splines.
Aircraft; Accessory drives and mounting pads
- ICS
- 49.050
- CCS
- V38
- 发布
- 1975-03
- 实施
