Performance Requirements for Fuel System Tubing Assemblies PDF Download
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Author: Fuel Systems Standards Committee
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
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Book Description
This SAE Standard encompasses the recommended minimum requirements for non-metallic tubing and/or combinations of metallic tubing to non-metallic tubing assemblies manufactured as a liquid- and/or vapor-carrying systems designed for use in gasoline, alcohol blends with gasoline, or diesel fuel systems. This SAE Standard is intended to cover tubing assemblies for any portion of a fuel system which operates above 40 °C (40 °F) and below 115 °C (239 °F), and up to a maximum working gage pressure of 690 kPa (100 psi). The peak intermittent temperature is 115 °C (239 °F). For long-term continuous usage, the temperature shall not exceed 90 °C (194 °F). It should be noted that temperature extremes can affect assemblies in various manners and every effort must be made to determine the operating temperature to which a specific fuel line assembly will be exposed, and design accordingly. The applicable SAE standards should be referenced when designing liquid-carrying and/or vapor-carrying systems which are described in this document. Wherever possible or unless stated otherwise, systems tested to this document shall be in the final design intent configuration.
Author: Fuel Systems Standards Committee
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
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Book Description
This SAE Standard encompasses the recommended minimum requirements for non-metallic tubing and/or combinations of metallic tubing to non-metallic tubing assemblies manufactured as a liquid- and/or vapor-carrying systems designed for use in gasoline, alcohol blends with gasoline, or diesel fuel systems. This SAE Standard is intended to cover tubing assemblies for any portion of a fuel system which operates above 40 °C (40 °F) and below 115 °C (239 °F), and up to a maximum working gage pressure of 690 kPa (100 psi). The peak intermittent temperature is 115 °C (239 °F). For long-term continuous usage, the temperature shall not exceed 90 °C (194 °F). It should be noted that temperature extremes can affect assemblies in various manners and every effort must be made to determine the operating temperature to which a specific fuel line assembly will be exposed, and design accordingly. The applicable SAE standards should be referenced when designing liquid-carrying and/or vapor-carrying systems which are described in this document. Wherever possible or unless stated otherwise, systems tested to this document shall be in the final design intent configuration.
Author: Fuel Systems Standards Committee
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
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Book Description
This SAE Standard covers the performance requirements for protective covers for gasoline fuel tubing. The ultimate performance of the protective cover can be highly dependant on the interaction of the fuel line tubing and protective cover. Therefore, it is recommended that specific tubing and cover combinations be tested as an assembly to qualify to this document. This document is intended to provide guidance to the engineer on the key performance parameters for protective covers for gasoline fuel tubing. This document is designed to allow selection of predetermined performance levels for these key performance parameters. The engineer may select a specification by the use of a line call-out designation, which will denote the pertinent characteristics of the cover material and/or the tube/cover assembly and their corresponding performance criteria. The engineer is not required to select every characteristic, but only those deemed important to the application. Characteristics not covered by this document and deemed important to the engineer should be added using 'Z' suffixes. This document may involve hazardous materials, operations, and equipment. This document does not address the safety problems associated with its use. It is the responsibility of the user of this document to consult and establish appropriate safety and health practices and determine the applicability of regulatory limitations prior to use.
Author: Air Brake Tubing and Tube Ftg Committee
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
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Book Description
This standard is intended to establish uniform methods of testing SAE J844d tubing and fitting assemblies as used in automotive air brake systems.This standard also establishes minimum qualifications for tensile and pressure capabilities, vibrational durability under cyclic temperatures, serviceability, and fitting compatibility requirements. The specific tests and performance criteria applicable to the tubing are set forth in SAE J844d.Note: The test values contained in this performance standard are for test purposes only. For environmental and usage limitations see SAE J844d. Fittings A type of fitting for use with SAE J844d nonmetallic tubing is included in SAE J246b, however, it is not intended to restrict or preclude the use of other designs of fittings that comply with this standard.
Author: https://www.chinesestandard.net
Publisher: https://www.chinesestandard.net
ISBN:
Category : Technology & Engineering
Languages : en
Pages : 22
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Book Description
This standard specifies the requirements such as terms and definitions, dimensions and tolerances, materials and colors, technical requirements, test methods, marking, inspection rules, packaging, transportation, storage for single-layer nylon hose and hose assemblies for automotive fuel systems. This standard applies to single-layer nylon hose and hose assemblies for automotive fuel systems.
Author: Air Brake Tubing and Tube Ftg Committee
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
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Book Description
This SAE Standard is intended to establish uniform methods of testing SAE J844 tubing and fitting assemblies as used in automotive air brake systems.This document also establishes minimum qualifications for tensile and pressure capabilities, vibrational durability under cyclic temperatures, serviceability, and fitting compatibility requirements. The specific tests and performance criteria applicable to the tubing are set forth in SAE J844.NOTEThe test values contained in this document are for test purposes only. For environmental and usage limitations see SAE J844. FittingsA type of fitting for use with SAE J844 nonmetallic tubing is included in SAE J246; however, it is not intended to restrict or preclude the use of other designs of fittings that comply with this document. There was a change to 3.4.1.
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 Type classification for those hose assemblies commonly used in aerospace fuel, lubricating oil, and hydraulic fluid systems.
Author: Fuel Systems Standards Committee
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
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Book Description
This SAE Standard covers the minimum requirements for nonmetallic tubing as manufactured for use in gasoline or diesel fuel systems. It is not intended to cover tubing for any portion of the system which operates below -40 degrees C, above 115 degrees C, or above a maximum working gage pressure of 690 kPa.
Author: Metallic Tubing Committee
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
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Book Description
These recommended practices provide recommendations for general specifications and performance requirements of carbon, alloy and high strength low alloy steel tube assemblies for fluid power applications utilizing commonly available manufacturing methods and general guidelines for tube selection and application. The verbiage in this document has been modified to clarify the intent of the information presented. Additional information has been provided relating to performance tests and quality assurance.
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 Recommended Practice (ARP) establishes the suggested requirements and test methods for the evaluation, qualification testing, and/or acceptance testing of fuel and pneumatic couplings, quick disconnects, hydraulic fittings, and hose assemblies. The paragraphs noted herein are general words and may be modified to fit specific hardware, materials, and usage which will appear in procurement specifications.
Author: G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
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Book Description
This international standard establishes flexure and pressure impulse test procedures for determining and classifying the fatigue strengths of bent aircraft hydraulic tubing. The procedures are intended for use with high- and low-pressure system assemblies for evaluation of new materials or for qualification purposes. MA2006 has been reaffirmed to comply with the SAE five-year review policy.
