Download or read book Fittings Tube Fluid System 3000 4000 Psig Rated Pressure Externally Swaged 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 SAE Aerospace Standard (AS) establishes the requirements for externally swaged tube fittings for use in hydraulic and other aerospace fluid systems in temperature range of -65 to 275 °F.

Download or read book Fittings Tube Fluid System 3000 Psig 21 000 KPa Rated Pressure Externally Swaged 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 tube-fitting assemblies used in aircraft fluid systems in the following pressure classes: B (1500 psi or 10 500 kPa), and D (3000 psi or 21 000 kPa), and in temperature types I (65 to 160 °F or 55 to 70 °C), and II (65 to 275 °F or 55 to 135 °C) of AS2001.This specification covers a common Cres, titanium, and aluminum fittings that may be used for a range of operating pressures up to 3000 psi with different tubing materials and tubing wall thicknesses, and is assembled with the same tooling in accordance with AS5902. Table 10 shows applicable aerospace fitting part number standard and tubing materials and operating pressures. Complete update of the procurement specification to prepare for QPL listing of part standards listed in Table 10 including corrections of material specification numbers, tube materials, wall thicknesses in Table 7, description of back-up seal, and updating quality conformance plans.

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 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 and CRES tubing with flareless separable fitting for use in hydraulic supply and return aerospace fluid systems up to a maximum operating pressure of 5080 psig (35 000 kPa) and a maximum 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 fitting number and tubing materials and operating pressures. Add performance requirements for additional tube materials, tube thicknesses and pressures.

Download or read book Aerospace Hydraulic Systems written by Wayne Stout, Phd and published by DesignAerospace LLC. This book was released on 2013-04-25 with total page 395 pages. Available in PDF, EPUB and Kindle. Book excerpt: The book addresses hydraulic system operation and design from an aerospace perspective. The book covers issues of fluids and fluid flow, component operation and system design. Component sizing methods, mathematical relationships and modeling equations are presented for each component. A methodology for system level modeling and simulation is also presented. Numerous examples and worked sample problems are included.

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 Flight Control Systems written by Wayne Stout, Phd and published by DesignAerospace LLC. This book was released on 2018-01-15 with total page 305 pages. Available in PDF, EPUB and Kindle. Book excerpt: This book covers aerospace flight control systems. Both primary and secondary flight control systems are covered in the book. The first chapters cover basic mechanism fundamentals that are relevant to flight control systems. Next is chapters on cable systems, gearing systems and power screws. Hydraulic and electromechanical actuation are also discussed. From here, the book addresses general aspects of flight control systems, including fly by wire systems. After this secondary systems (high lift, spoilers, trim) and primary flight control for each axis are discussed - each in stand-alone chapters. Reversible, irreversible and fly by wire systems are discussed for each axis. The final chapter goes into system fault detection.

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 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.

Download or read book Aluminum Fittings Axially Swaged Tube with Flareless Separable Fluid System Up to 1500 Psi 10 340 KPa Maximum Specification for written by G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies and published by . This book was released on 2011 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: This SAE Aerospace Standard (AS) establishes the requirements for externally swaged aluminum tube fittings on aluminum tubing with flareless separable fitting ends for use in hydraulic supply and return aerospace fluid systems including pneumatic, coolants, and fire extinguishers up to a maximum operating pressure of 1500 psig (10 340 kPa) and a maximum operating temperature range of 65 to +225 °F (54 to +107 °C).This specification covers a common aluminum fitting that may be used for a range of operating pressures up to 1500 psi with different tubing materials and tubing wall thicknesses, and is assembled with the same tooling in accordance with AS6124. Table 12 shows applicable aerospace fitting part number standard and tubing materials and operating pressures. This specification is being prepared to provide the performance requirements for aluminum axially swaged, field attachable, 1500 psi, tube fittings.

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 Aluminum Fittings Axially Swaged Tube with Flareless Separable Fluid System Up to 1500 Psi 10340 KPa Maximum Specification for written by G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies and published by . This book was released on 2016 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: This SAE Aerospace Standard (AS) establishes the requirements for externally swaged aluminum tube fittings on aluminum tubing with flareless separable fitting ends for use in hydraulic supply and return aerospace fluid systems including pneumatic, coolants, and fire extinguishers up to a maximum operating pressure of 1500 psig (10340 kPa) and a maximum operating temperature range of -65 to +225 °F (-54 to +107 °C).This specification covers a common aluminum fitting that may be used for a range of operating pressures up to 1500 psi with different tubing materials and tubing wall thicknesses, and is assembled with the same tooling in accordance with AS6124. Table 12 shows applicable aerospace fitting part number standard and tubing materials and operating pressures. Change operating pressure requirements of size 24 from 500 to 600 psi (including proof and burst pressures), add vibration curves requirements to Tables 10 and 11 for size 24, add the new configuration part number AS6323 to Table 12, and add size 24 dimensions to some of the standards configurations.

Download or read book FITTINGS TUBE FLUID SYSTEM 3000 Psig MAXIMUM PERMANENTLY ATTACHED SPECIFICATION FOR written by G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies and published by . This book was released on 1992 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: This SAE Aerospace Standard (AS) establishes the requirements for MIL-H-5440 Class II permanently attached tube fittings for use in hydraulic and other aerospace fluid systems.

Download or read book Fittings 24 Cone Flareless Fluid Connection 3000 Psi written by G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies and published by . This book was released on 2008 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: This SAE Aerospace Standard (AS) establishes the requirements for 24 degree cone flareless fluid connection fittings and nuts, internally or externally swaged, preset, or welded sleeves for use in aircraft fluid systems at nominal operating pressures up to and including 3000 psi. To correct material specification numbers in Table 1, to clarify fluorescent inspection for aluminum forgings, to add a thread requirement for ISO 3161, and periodic control test requirements under 4.5.3 have been clarified and simplified.

Download or read book Sleeve Internally Or Externally Swaged Or Welded 24 Cone Flareless Fitting 3000 Psi 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 SAE Aerospace Standard (AS) establishes the requirements for internally or externally swaged or welded sleeves or tube end adapters for use with 24° cone flareless fluid connection fittings per AS18280.

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 Test Methods for Tube Fitting Assemblies written by G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies and published by . This book was released on 2011 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: This SAE Aerospace Standard (AS) specifies test methods for tube-fitting assemblies used in aircraft fluid systems in the following pressure classes: B (1500 psi or 10500 kPa), D (3000 psi or 21000 kPa), E (4000 psi or 28000 kPa), and J (5000 psi or 35000 kPa) and in temperature types I (-65 to 160 °F or -55 to 70 °C), II (-65 to 275 °F or -55 to 135 °C), and III (-65 to 400 °F or -55 to 200 °C) of AS2001.This document applies each time that it is referred to in a procurement specification or other definition document.Fluids and materials used for the tests are listed in Section 2. Update the entire standard to include additional test methods and to support qualification test requirements for operating systems up to 5000 psi.

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.