Functional Compatibility Analysis of Aircraft - Engine Fuel Systems

Format:

Conference/Event

Author/Creator:

González, César, author.

Conference Name:

National Business Aircraft Meeting and Engineering Display (1969-03-26 : Wichita, Kansas, United States)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1969

Summary:

The range of performance demands placed on fuel systems incorporated on piston business aircraft is rapidly expanding with the continued rise in operating altitudes, rates of climb, cabin pressurization levels, and turbocharging capabilities. Fuel systems cannot be considered any longer as separate links of a chain leading the fuel from the tanks to the fuel injector or carburetor, since incompatible component characteristics at any point can defeat an otherwise ideal system.Compatibility requirements between engine and airframe supply systems are discussed in this paper, and several component features are analyzed in an effort to categorize and group these components in integrated systems with degrees of sophistication or simplicity in accord with the particular application

Notes:

Vendor supplied data

Publisher Number:

690308

Access Restriction:

Restricted for use by site license