AIR7975 Aircraft Fuel System Design Guidelines

Current

12/05/2019

Features
Issuing Committee
Scope
Content
This document describes the major design drivers and considerations when designing a fuel system for a large commercial aircraft. It discusses the design at a system/aircraft level, and is not intended as a design manual for individual system components, though it does refer out to other SAE specifications where more detail on specific components and sub-systems is given. It does include examples of a number of calculations associated with sizing of fuel systems, based on those given in NAV-AIR-06-5-504, as well as an appendix summarizing basic fluid mechanical equations which are key for fuel system design. It is acknowledged that most of these calculations would today be performed by modelling tools, rather than by hand, but it is considered important for the designer to understand the principles.
It is intended that later issues of this document will include appendices which give specific considerations for military aircraft, smaller commercial aircraft, and rotorcraft.
Meta TagsDetails
DOI
https://doi.org/10.4271/AIR7975
Pages
85
Citation
SAE International Information Report, Aircraft Fuel System Design Guidelines, SAE Standard AIR7975, Issued December 2019, https://doi.org/10.4271/AIR7975.
Additional Details
Publisher
Published
Dec 5, 2019
Product Code
AIR7975
Content Type
Information Report
Status
Current
Language
English

Revisions