Thermal Management of Advanced Aircraft Secondary Power Systems

Format:

Conference/Event

Author/Creator:

Iya, Sridhar K., author.

Conference Name:

Aerospace Technology Conference & Exposition (1990-10-01 : Long Beach, California, United States)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1990

Summary:

This paper presents a thermal management system study for a hydrocarbon-fueled Mach 6 aircraft equipped with the following three types of secondary power systems: (i) conventional system with hydraulic actuators and turbine-driven fuel pumps; (ii) more-electric system with electromechanical actuators and turbine-driven fuel pumps; and (iii) all-electric system with electromechanical actuators and electrically driven fuel pumps.The thermal management system was designed to provide environmental control for the crew cabin, avionics, flight controls, and electrical generators. Engine fuel was used as the ultimate heat sink for all cases.Details of thermal protection concepts for the three cases are discussed and compared in this paper. A brief overview of integrated thermal management for the total aircraft is also presented

Notes:

Vendor supplied data

Publisher Number:

901959

Access Restriction:

Restricted for use by site license