V29 航天用液压元件与附件 标准查询与下载

SAE AS4623C-2000 聚四氟乙烯对芳族增强3000psi、275°F重载飞行器液压系统软管组件

This document defines the requirements for heavy-duty polytetrafluoroethylene (PTFE) lined, para-aramid reinforced, hose assembly suitable for use in 275 °F, 3000 psi aircraft systems where rapid rate pulsing and torsional/longitudinal flexing may occur in addition to normal hydraulic system loading. Size -16 and -20 are limited to +225 °F service.

Hose Assembly, Polytetrafluoroethylene, Para-Aramid Reinforced, 3000 psi, 275 °F, Heavy-Duty, Aircraft Hydraulic Systems

SAE AS614B-2000 聚四氟乙烯金属增强3000psi、400°F重载型液压和气动软管组件

This SAE Aerospace Standards (AS) defines the requirements for heavy duty polytetrafluoroethylene (PTFE) lined, metallic reinforced, hose assemblies suitable for use in high temperature, high pressure, 4000 psi, aircraft and missile hydraulic fluid systems.

Hose Assembly, Polytetrafluoroethylene, Metallic Reinforced, 4000 psi, 400 Degrees F, Heavy Duty, Hydraulic and Pneumatic [Superseded: SAE ARP 614B]

SAE AIR860A-2000 飞行器电气加热系统

It is intended that the scope of this information report be limited to electrical heating of passenger, crew, and cargo compartments only. No attempt has been made to develop the complete electrical circuitry associated with the electrical heating components; however, the electrical circuitry required for heating component operation, safety, and monitoring will be included as available. Specific design information is given for various modern aircraft utilizing electrical heating. Each aircraft discussed will be identified by alphabetical letter designation and included in the appropriate appendix.

Aircraft Electrical Heating Systems

SAE AIR4543A-2000 航空液压和驱动课程的学习

This Aerospace Information Report (AIR) contains technical information on aerospace hydraulic and actuation technologies lessons learned. The lessons learned were prepared by system designers and hydraulic engineers from the aerospace industry and government services as part of SAE Committee A-6, Aerospace Fluid Power, Actuation, and Control Technologies, and were presented at three Lessons Learned Symposia in 1989 and 1990 held during A-6 Committee meetings. The technical topics represent many years of design experience in hydraulics and actuation, which it is felt is a resource for learning that should be documented and made available to current and future aerospace hydraulic engineers and designers. The document is organized into two sections; systems and components, with further categories within the components section. The information topics are presented in a concise format of problem, issue, and solution, with accompanying descriptive diagrams and illustrations for clarity and understanding.

Aerospace Hydraulics and Actuation Lessons Learned

BS ISO 12333:2000 航空航天.定量液压马达.35000KPa系统的一般规范

This International Standard establishes the general specifications for constant displacement hydraulic motors to be installed in aircraft, which transform hydraulic power into mechanical energy in the form of a rotational torque to 35 000 kPa systems. Primary and secondary function motors (see clause 3) are covered in this International Standard; actuators with internal rotation angle limits and low-speed motors are not covered in this International Standard. This International Standard shall be used in conjunction with the detail specification particular to each application.

Aerospace - Constant displacement hydraulic motors - General specifications for 35000 kPa systems

BS ISO 12334:2000 航空航天.液压的压力补偿的变量输送泵.35000KPa系统的一般要求

This International Standard specifies the general requirements for pressure-compensated, variable delivery hydraulic pumps, suitable for use in aircraft hydraulic systems at 35 000 kPa. This International Standard shall be used in conjunction with detail specifications concerning each pump model.

Aerospace - Hydraulic, pressure-compensated, variable delivery pumps - General requirements for 35000 kPa systems

SAE AS1553A-2000 有管支承且带有环衬的压板性能标准

This standard covers heat and corrosion resistant steel loop clamps with a woven steel wire cushion that is attached to the clamp by spot welding and is intended for use in applications up to 1200 degrees F (649 degrees C). To establish the performance requirements for loop clamps with a woven steel wire cushion.

Performance Standard for Tube Support Loop-Cushioned Clamp

SAE AS28889-1999 FSC 4820 5000 psi高增压空气阀门

Valve, Air, High Pressure Charging, 5000 psi FSC 4820

Valve, Air, High Pressure Charging, 5000 psi FSC 4820

SAE AS6399-1999 合成绕线橡胶软管的冰消除系统.代替1999年7月1日作废的MIL-H-6399B标准

This document establishes the requirements for a lightweight, nonkink, flexible elastomeric hose. This hose is typically used with air-operated aircraft ice-preventive systems.

Hose, Rubber, Wire-Wound, Synthetic, Ice Eliminating System Should Be Used Instead of MIL-H-6399B, Which Was Cancelled on 1 July 1999

SAE ARP4296A-1999 联轴器接头,软管端和流体系统的(R)绘图释义及标准的加工惯例

This SAE Aerospace Recommended Practice (ARP) is intended to interpret and clarify engineering drawing requirements relating to the manufacture and inspection of fluid system couplings, tube fittings, and hose ends. Because it is impractical to define every minute detail of the part on the face of the drawing, this document describes interpretations of dimensioning of general machining features and otherwise undefined tolerances that fall under the heading of good shop practice. This document services as a supplement to engineering drawings when referenced on applicable documents.

(R) Drawing Interpretation and Standard Machining Practices, Couplings, Fittings and Hose Ends, Fluid Systems

SAE AIR560C-1999 导弹液压泵

Missile pumps are categorized by a moderate testing life and a relatively short operational service life. Generally, the pumps are operated at higher speeds, temperatures, and pressures than those used in manned aircraft systems, yet reliability must be extremely high, since there rarely is a redundant system aboard the missile. Due to the short but critical life and performance requirements, development, reliability and acceptance testing should be focused on eliminating infant mortality failures. Missile pumps must be compatible with very severe environmental conditions during the service life. In general, the temperature, vibration, shock, and acceleration encountered are more severe than those met in manned aircraft. This SAE Aerospace Information Report (AIR) will be confined to describing missile environments and pump usage that differ significantly from those normally encountered in manned aircraft. Since missile pumps are usually driven by a secondary power source, and since this AIR is intended for use by systems designers, as well as pump designers, a brief description of some of these sources and some potential problem areas associated with each are included for reference. A more detailed treatment of auxiliary power sources can be found in AIR744. Detailed test requirements are not included in this AIR since a wide variation exists between those operating conditions and environments that might be encountered on an air-to-air missile, hung beneath the wing of a fighter aircraft, and that of an ICBM (Intercontinental Ballistic Missile), launched from an environmentally controlled silo. Missile pumps frequently have their genesis in standard aircraft pumps, however, what distinguishes them from manned aircraft pumps is that they are usually operated outside of, or at the extreme of their long-life design parameters. Therefore, if a new design pump is being proposed for a missile application, environmental conditions referenced in this AIR should be considered, as opposed to long-life operation and environmental requirements of a manned aircraft, engine-driven pump.

Missile Hydraulic Pumps

DIN ISO 8575:1998 航空航天.流体系统.液压系统管道

The document specifies the requirements relating to the sizes and material of tubing for use in aerospace hydraulic pressure and return systems. For pressure lines, the requirements apply to the pressure and temperature ranges covered by pressure classes D and E and temperature types II and III as specified in ISO 6771.#,,#

Aerospace - Fluid systems - Hydraulic system tubing (ISO 8575:1990)

SAE AS8775-1998 飞机和导弹液压系统部件通用规范;应代替1998年9月28日作废的MIL-H-8775D

This specification covers the general requirements that are common to most hydraulic components, used in aeronautical hydraulic systems.

Hydraulic System Components, Aircraft and Missiles, General Specification for Should Be Used Instead of MIL-H-8775D, which Was Cancelled on 28 September, 1998

NAVY MIL-V-23219 NOTICE 1-1998 高压空气减少阀组

MIL-V-23219, dated 26 March 1962, is inactive for new design and is no longer used, except for replacement purposes.

VALVE MANIFOLDS, HIGH PRESSURE AIR REDUCING

SAE AS8712-1997 低压泄气阀

This specification covers the requirements for one type of low-pressure relief valve for use in pressurized shipping containers.

Valve; Air Relief, Low Pressure

SAE AIR888B-1997 过滤器元件的细孔丝网

This SAE Aerospace Information Report (AIR) discusses the terminology, types, method of manufacture and chemistry of fine wire meshes used for filtration of hydraulic, lubrication fuel systems, and similar applications. Information contained herein may be used for quality assurance testing to insure that a high performance filter grade wire mesh is acceptable for use in an aerospace application. This document pertains to meshes as coarse as 4 x 4 wires/cm (10 x 10 wires/in) or coarser, as well as to meshes as fine as 155 x 1100 wires/cm (400 x 2800 wires/in) or finer. Fine wire meshes refer to all wire meshes used for filtration, but also the coaser meshes used as a backup or supporting material.

Fine Wire Mesh for Filter Elements

SAE AS5009-1997 液压外部模压90°弯头配件

Fitting, Elbow, 90 Degree, External Swage, HydraulicTABLE 1 - DIMENSIONS AND WEIGHTS

Fitting, Elbow, 90 Degree, External Swage, Hydraulic

SAE AS4444/2-1997 液体连接24°锥形非扩口式和37°扩口式配件

This SAE Aerospace Standard (AS) establishes the requirements for fluid fittings that combine both 24?cone flareless and 37?flared connections for use in all types of fluid systems.

Fitting, 24?Cone Flareless to 37?Flared, Fluid Connection

SAE AS5013-1997 液压外部铸模直线无扩口适配器配件

FITTING, ADAPTER, STRAIGHT FLARELESS, EXTERNAL SWAGE, HYDRAULICTABLE 1A - DIMENSIONS A-GTABLE 1B - DIMENSIONS H-AATABLE 2- WEIGHTS

FITTING, ADAPTER, STRAIGHT FLARELESS, EXTERNAL SWAGE, HYDRAULIC

SAE AS5266-1997 液压外部收压扩口式直型适配器接头

Fitting, Adapter, Straight, Flared, External Swage, HydraulicTABLE 1 - DIMENSIONSTABLE 2 - WEIGHTS

Fitting, Adapter, Straight, Flared, External Swage, Hydraulic