Download or read book Fittings Tube Fluid Systems Separable High Pressure Dynamic Beam Seal 5000 8000 Psi General Specification For written by G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies and published by . This book was released on 2015 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: This specification covers the design requirements and test procedures for separable beam seal fittings which include end fittings (see 2.4.2), connectors (see 2.4.3), and boss fittings for use in aerospace fluid systems. Design requirements are for Class 5000 and 8000 in titanium, and corrosion resistant steel (CRES). Definition of fittings and related terms are defined in 2.4. This standard is revised to correct minor errors and to provide for PRI-QPL requirements and to establish PRI-QPL-AS85720.

Download or read book Fittings Tube Fluid Systems Separable High Pressure Dynamic Beam Seal General Specification For written by G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies and published by . This book was released on 2004 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: This specification covers the basic test and design requirements for one style separable high pressure beam seal fittings including boss or port seal connectors for use in 5000/8000 psi aerospace fluid systems. Definitions of fitting and related terms are included in 6.4.

Download or read book Fittings Tube Fluid Systems Separable High Pressure Beam Seal 5000 8000 Psi General Specification For written by G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies and published by . This book was released on 2018 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: This specification covers the design requirements and test procedures for separable beam seal fittings which include end fittings (see 2.4.2), connectors (see 2.4.3), and boss fittings for use in aerospace fluid systems. Design requirements are for Class 5000 and 8000 in titanium, and corrosion resistant steel (CRES). Definition of fittings and related terms are defined in 2.4. This specification is revised to incorporate allowances for shape fittings (Elbows, Tees and Crosses) to be manufactured from either: a) bar-stock per dimensions specified in AS1376 or b) near-net forgings or c) oversize forgings per dimensions specified in AS1376. It is also being revised to replace the lot-to-lot destructive testing with periodic testing.

Download or read book Index of Specifications and Standards written by and published by . This book was released on with total page 960 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book FITTINGS TUBE FLUID SYSTEMS SEPARABLE HIGH PRESSURE DYNAMIC BEAM SEAL DESIGN STANDARD FOR MALE END written by G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies and published by . This book was released on 2020 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: CORRECT THREAD PROFILE CALLOUT FOR SIZES 12 AND 16. CORRECT FIGURE TO SHOW DIMENSION "C" LEADER LINE.

Download or read book Fittings Tube Fluid Systems Separable Beam Seal 3000 4000 Psi General Specification For Supplement 1 written by G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies and published by . This book was released on 2013 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: This supplement forms a part of SAE Aerospace Specification AS85421. It shall be used to identify fitting standards citing this procurement specification. AS85421SUP1 has been reaffirmed to comply with the SAE five-year review policy.

Download or read book Fittings Tube Fluid Systems Separable Beam Seal 3000 4000 Psi General Specification For written by G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies and published by . This book was released on 1998 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: This specification covers the design requirements and test procedures for separable beam seal fittings which includes end fittings (see 6.10.3), fitting bodies (see 6.10.6), and boss fittings (see 6.10.1) for use in aerospace fluid systems. Design requirements are for class 3000 in corrosion resistant steel (CRES) only and for class 4000 in titanium alloy (Ti) only. Definition of fittings and related terms are defined in 6.10. This document has been reaffirmed to comply with the SAE 5-year Review policy.

Download or read book Separable Fittings Permanent Fittings Tubing Fluid Systems 8000 Psi Qualification Test Standard For written by G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies and published by . This book was released on 2013 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: This Performance Standard covers the Qualification Test Requirements for separable fittings, permanent fittings, and tubing suitable for use in 8000 psi aerospace fluid power systems. The standard treats each of these elements as part of a "system" in which each element has a specific critical relationship one to the other This document is applicable to both the pressure (8000 psi) and the return (4000 psi) portions of an 8000 psi rated system. Rationale for tests, testing philosophy, and key words are covered in Sections 5 and 6. AS4401 has been reaffirmed to comply with the SAE five-year review policy.

Download or read book Fittings Weld Fluid Connection 5000 Psi Maximum written by G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies and published by . This book was released on 2019 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: This SAE Aerospace Standard (AS) establishes the requirements for weld fluid connection fittings and rings to be orbital arc welded to tubing for use in aircraft fluid systems up to a maximum operating pressure of 5000 psi. Qualification specifics for weld-to-beam seal reduced-wall/reduced-pressure fittings are not included in AS85421, AS85720, AS4510, or AS4510/2. This revision will clarify qualification requirements for those fitting versions. Additionally, dash codifications that are on current detail standards, but not in AS4510, are being added.

Download or read book Separable Tube Fittings for Fluid Systems 24 0D Cone General Specification written by British Standards Institute Staff and published by . This book was released on 1998-12-01 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt: Fluid equipment components, Aircraft components, Space technology components, Fluid equipment, Pipe fittings, Hydraulic equipment, Threads, Defects, Surface defects, Pressure, Grades (quality), Dimensions, Colour codes, Marking, Performance, Finishes, Classification systems, Test pressure, Bend testing, Test specimens, Inspection, Leak tests, Stress corrosion, Corrosion tests, Mechanical testing, Pressure testing, Sampling methods, Quality assurance, Approval testing, Quality control, Statistical quality control, Packaging, Specimen preparation, Angles (geometry)

Download or read book TUBE FITTINGS METRIC AEROSPACE FLUID SYSTEMS SEPARABLE GENERAL SPECIFICATION FOR written by G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies and published by . This book was released on 1983 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: This standard establishes the basic performance and quality criteria for screw-together tube fitting assemblies and port connectors. It was prepared to standardize on the qualification test and procurement requirements for ISO standard tube fittings. The test requirements are intended to satisfy the most strenuous demands encountered in a high performance aircraft hydraulic system. The procurement requirements are intended to assure that fittings which are bought to this specification are of the same quality as the fittings used during the original qualification testing. Compliance with these test and procurement requirements is necessary for fittings which are used in control systems where a malfunction could affect the safety of flight.

Download or read book TUBE FITTINGS FLUID SYSTEMS SEPARABLE GENERAL SPECIFICATION FOR written by G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies and published by . This book was released on 1981 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: This document establishes the basic performance and quality criteria for screw-together tube fitting assemblies and port connectors used in aircraft fluid systems.

Download or read book Fittings Axially Swaged Tube with Flareless Separable Fluid System For Operating Pressures Up to and Including 5080 Psi 35 000 KPa Specification for written by G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies and published by . This book was released on 2013 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: This SAE Aerospace Standard (AS) establishes the requirements for externally swaged titanium tube fittings on titanium and CRES tubing with flareless separable fitting for use in hydraulic supply and return aerospace fluid systems up to operating pressure of 5080 psig (35 000 kPa) maximum and an operating temperature range of 65 to +275 °F (54 to +135 °C).This specification covers a common 5080 psi pressure titanium fitting that may be used for a range of operating pressures up to 5080 psi with different tubing materials and tubing wall thicknesses, and is assembled with the same tooling in accordance with AS5959. The fitting operating pressure is based on the fitting thread pitch. Extra fine pitch for 5080 psi operating pressure and fine pitch for operating pressures 3000 psi and less. Table 12 shows applicable aerospace fitting part number standard and tubing materials and operating pressures. Add Blue Anodize and Ink-Jet Options as Identification and Marking methods to 3.4.2.3 and 3.5.2, and correct the joint strength conversion values to Newton in Tables 3A and 3B.

Download or read book FITTING PLUG BEAM SEAL HYDRAULIC written by G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies and published by . This book was released on 2018 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: REMOVE "DUAL" PROCUREMENT SPECIFICATION REQUIREMENTS BY REMOVING AS85720 AND 5000 PSI PRESSURE REQUIREMENTS. MAKE REFERENCE TO AS8440 (5000 PSI) ALTERNATIVE. FIXED TYPOS AND GENERAL UPDATES.

Download or read book Fittings Axially Swaged Tube with Flareless Separable Fluid System 5080 Psi 35 000 KPa Specification for written by G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies and published by . This book was released on 2009 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: This SAE Aerospace Standard (AS) establishes the requirements for externally swaged titanium tube fittings on titanium tubing with flareless separable fitting for use in hydraulic supply and return aerospace fluid systems up to operating pressure of 5080 psig (35 000 kPa) maximum and an operating temperature range of -65 to +275 °F (-54 to +135 °C). AS5958 Rev. C is an exact duplication of AS5958 Rev. A. AS5958 Rev. B had been issued prematurely and has been removed from circulation.Rationale from Rev. A: Added -20 size and requirements and corrected errors.

Download or read book Aerospace Separable Tube Fittings for Fluid Systems for 24 0D Cones for Pressures Up to 3 000 Psi Or 21 000 KPa Procurement Specification Inch metric written by British Standards Institute Staff and published by . This book was released on 1914-11-30 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt: Aircraft components, Hydraulic equipment, Fluid equipment components, Fluid equipment, Pipe fittings, Threads, Defects, Surface defects, Pressure, Grades (quality), Performance, Dimensions, Angles (geometry), Colour codes, Marking, Finishes, Classification systems, Test pressure, Bend testing, Leak tests, Stress corrosion, Corrosion tests, Mechanical testing, Pressure testing, Sampling methods, Quality assurance, Inspection, Approval testing, Quality control, Statistical quality control, Packaging, Test specimens

Download or read book Fittings Axially Swaged Tube with Flareless Separable Fluid System for Operating Pressures Up to and Including 5080 Psi 35000 KPa Specification for written by G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies and published by . This book was released on 2017 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: This SAE Aerospace Standard (AS) establishes the requirements for axially swaged titanium fittings on titanium, CRES, and aluminum tubing with flareless separable fitting ends for use in hydraulic supply and return aerospace fluid systems up to operating pressure of 5080 psig (35000 kPa) maximum. The operating temperature range for titanium tubing and CRES tubing is 65 to +275 °F (54 to +135 °C) and the operating temperature range for aluminum return system tubing is 65 to +225 °F (54 to +107 °C).This specification covers a common 5080 psi pressure titanium fitting that may be used for a range of operating pressures up to 5080 psi with different tubing materials and tubing wall thicknesses, and is assembled with the same tooling in accordance with AS5959. The flareless fitting operating pressure is based on the fitting thread pitch. Extra fine pitch is used for 5080 psi operating pressure and fine pitch for operating pressures 3000 psi and less. Table 14 shows applicable aerospace fitting part number standard and tubing materials and operating pressures. Add performance requirements for aluminum tubing, class designation for tubing, update and correct existing text and figures.