Description / Abstract:
This SAE Aerospace Information Report (AIR) is a compilation of
engineering references and data useful to the technical community
that can be used to ensure fuel system compatibility with composite
structure. This AIR is not a complete detailed design guide and is
not intended to satisfy all potential fuel system applications.
Extensive research, design, and development are required for each
individual application.
Purpose
This document is intended to serve as guidance to airframe and
equipment manufacturers for the design and installation of fuel
systems into composite structure. This document is not intended to
be a fully definitive specification, but concentrates on areas
where it is felt guidance is needed.
The purpose of this AIR is to compile one definitive source of
the references, rules, regulations, and preferred practices for the
development of a fuel system in composite structure. This AIR sets
forth some useful design considerations for work with composites as
it relates to the fuel system.
Background
The development and installation of a fuel system in composite
structure introduces a variety of design situations which are
different from aluminum. The differences are related to the
properties of the composite material. As an example these may
include low electrical and thermal conductivity, greater design
sensitivity to penetrations, reduced shielding from electromagnetic
radiation, reduced conductivity of lightning, and potential
corrosion in graphite aluminum interfaces.
Field of Application
This AIR applies to the aerospace industry and specifically to
aircraft that use common petroleum fuels.