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Author: G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
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Languages : en
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Book Description
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.
Author: G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
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ISBN:
Category :
Languages : en
Pages : 0
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Book Description
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.
Author: G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
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ISBN:
Category :
Languages : en
Pages : 0
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Book Description
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.
Author: G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
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Languages : en
Pages : 0
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Book Description
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.
Author: G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
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ISBN:
Category :
Languages : en
Pages : 0
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Book Description
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.
Author: G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
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Category :
Languages : en
Pages : 0
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Book Description
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.
Author: G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
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Languages : en
Pages : 0
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Book Description
This ARP establishes the basic test and design requirements for permanently attached tube fittings for use in aerospace fluid systems. Definitions of fitting and related terms are included in 6.3.
Author: G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
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Languages : en
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Book Description
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.
Author: G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
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Languages : en
Pages : 0
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Book Description
This specification covers the design requirements and test procedures for separable beam seal fittings which includes end fittings (see 2.3.4), fitting bodies (see 2.3.7), and boss fittings (see 2.3.2) for use in aerospace fluid systems. Design requirements are for class 3000 in corrosion resistant steel (15-5 PH, 17-4 PH CRES) only and for class 4000 in titanium alloy (Ti) and corrosion and heat-resistant steel (nickel alloy 718 CRES) only. Definition of fittings and related terms are defined in 2.3. Corrected error to sample numbers in burst test (4.6.3); modified periodic control testing procedures/tests (4.4.3); clarified flexure Tables 2A, 2B, and 2C; and added new tubing material options to Table 1.
Author: G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
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Book Description
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). This specification was prepared to provide the performance requirements for axially swaged, field attachable, 5080 psi, tube fittings.
Author: G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Publisher:
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Category :
Languages : en
Pages : 0
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Book Description
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.
