49.080 航空航天用流体系统和零部件 标准查询与下载



共找到 2370 条与 航空航天用流体系统和零部件 相关的标准,共 158

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Fitting, Elbow, 90 Degree, Integral Weld Ring, 3000 psi

ICS
49.080
CCS
J13
发布
2013-10-20
实施

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Ring, Weld, 3000 psi, Cres

ICS
49.080
CCS
J13
发布
2013-10-20
实施

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Sleeve, Tube End, Acorn to Weld, Short Flareless

ICS
49.080
CCS
发布
2013-10-20
实施

This specification establishes the common requirements for variable delivery electric motor driven, hydraulic pump units, suitable for use in aircraft hydraulic systems.

Pump Units, Hydraulic, Electric Motor Driven, Variable Delivery

ICS
49.080
CCS
发布
2013-10-04
实施

This SAE Aerospace Recommended Practice (ARP) provides analytical and test methods for determining pressure drop in fluid systems such as hydraulic, fluid, oil, and coolant used in aerospace vehicles. Determining pressure drop by analytical and test results will be discussed.

Determination of Hydraulic Pressure Drop

ICS
49.080
CCS
发布
2013-10-04
实施

The importance of adequate component procurement specifications to the success of a hardware development program cannot be overemphasized. Specifications which are too stringent can be as detrimental as specifications which are too lax. Performance specifications, for instance, must not only identify all the component requirements, but they must also include sufficient quality assurance provisions so that compliance can be verified. It should be understood that in almost every case specifications for components will ultimately become part of a BINDING, WRITTEN CONTRACT (PO). The purpose of this document is to describe specifications, provide guidance for th

Fluid-System-Component Specification Preparation Criteria

ICS
49.080
CCS
发布
2013-10-04
实施

This SAE Aerospace Information Report (AIR) provides design data reliability information relative to the long-term storage of gas containers or pressure vessels charged with nitrogen or helium at pressures ranging from 6000 to 12 000 psi. The gas containers are cylindrical, spherical, or toroidal in shape. Internal volumes range up to 1385 in3. Applications for this type cold gas actuation system include tactical missiles, guided projectiles, and smart bombs. A typical system is described.

Long-Term Storage Reliability of High Pressure Gas Containers for Pneumatic Actuation Systems

ICS
49.080
CCS
发布
2013-10-04
实施

The purpose of this SAE Aerospace Recommended Practice (ARP) is to provide guide lines for allowable leakage for in-service aircraft hydraulic components at a nominal 100 °F (38 °C) temperature and to outline the procedure for measuring such leakage. The limits to be applied to any specific aircraft should be adjusted before inclusion in a maintenance manual.

External Hydraulic Leakage for In-Service Components

ICS
49.080
CCS
发布
2013-10-04
实施

This SAE Aerospace Standard (AS) defines contamination classes and levels for particulate contamination of hydraulic fluids and includes methods of reporting related data (Appendix A). The contamination levels selected are based on the widely accepted NAS 1638 cleanliness classes. The conversion from NAS 1638 cleanliness class specifications to AS4059 class specifications is defined. The comparison of the NAS 1638 classes to AS4059 classes and levels is provided and are defined and the differences explained (Appendix B). NAS 1638 classes based on weight of particles are not applicable to these classes and are not included. A contamination code has been adde

Aerospace Fluid Power - Contamination Classification for Hydraulic Fluids

ICS
49.080
CCS
发布
2013-09-27
实施

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Long Term Storage for Missile Hydraulic Control Systems - Design and Operational Practices Guide

ICS
49.080
CCS
发布
2013-09-26
实施

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HOSE ASSEMBLY, LINED SILICONE, HEATED, FLARELESS TO FIXED CAVITY, 125 PSI, POTABLE WATER

ICS
49.080
CCS
发布
2013-09-19
实施

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ELBOW, 90 DEGREE, REDUCER AND STANDARD, REDUCED BODY, FLARELESS

ICS
49.080
CCS
发布
2013-08-22
实施

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TEE, BULKHEAD ON RUN, STANDARD AND REDUCER, REDUCED BODY, FLARELESS

ICS
49.080
CCS
发布
2013-08-22
实施

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TEE, BULKHEAD ON SIDE, STANDARD AND REDUCER, REDUCED BODY, FLARELESS

ICS
49.080
CCS
发布
2013-08-22
实施

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CROSS, STANDARD AND REDUCER, REDUCED BODY, FLARELESS

ICS
49.080
CCS
发布
2013-08-22
实施

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TEE, STANDARD AND REDUCER, REDUCED BODY, FLARELESS

ICS
49.080
CCS
发布
2013-08-22
实施

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ELBOW, 90 DEGREE, BULKHEAD, STANDARD AND REDUCER, REDUCED BODY, FLARELESS

ICS
49.080
CCS
发布
2013-08-22
实施

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

ICS
49.080
CCS
发布
2013-08-15
实施

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

This document has been declared ""Stabilized"" and will no longer be subjected to periodic reviews for currency. Users are responsible for verifying references and continued suitability or technical requirements. New technology may exist. This SAE Aerospace Recommended Practice (ARP) presents two BASIC language computer programs to promote and standardize the computation of installed O-ring cross-section deflection hereafter referred to as ""squeeze"" and the computation of gland volume. The two programs were written with line numbers and without use of any system specific BASIC commands to allow usage with as many systems as possible with a minimum of edit

Gland Design, Computation of Seal Squeeze and Gland Volume

ICS
49.080
CCS
V21
发布
2013-06-18
实施



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