DocumentCode
2030512
Title
Design and simulation of an electromagnetic aircraft launch system
Author
Bertoncelli, T. ; Monti, A. ; Patterson, D. ; Ougal, R.D.
Author_Institution
Dipt. di Elettronica, Politecnico di Milano, Italy
Volume
3
fYear
2002
fDate
2002
Firstpage
1475
Abstract
Electric actuators are increasingly supplanting or replacing mechanical actuators (steam or hydraulic) in ship systems. This trend started in commercial shipping, especially cruise ships, and there is now a move to adopt the benefits in military systems. This paper describes the design and analysis of a very large actuator for a military ship system an Electro-Magnetic Aircraft Launching System, or EMALS, which will accelerate aircraft to flight speeds in very short distances. The aim is to replace the steam catapult currently used on aircraft carriers with a linear electric motor. The entire system should fit within the confines of the existing steam catapult. The advantages of such a system are increased operational availability, lower airframe stress due to programmable acceleration profiles, and reduced maintenance (and hence reduced manning). The goal of the study described here is to investigate the many feasible solutions and to use simulations to compare their performance. This paper reports on the initial stages of the work, which uses the Virtual Test Bed (VTB) as the simulation and virtual prototyping environment. This yields substantial side benefits because the EMALS research program represents a meaningful test case for the VTB itself. Models of the different parts of the systems are being built up from the specifications and the characteristics required by the US Navy, and will be refined with increasing detail as the project is developed.
Keywords
CAD; aircraft; electric actuators; electromagnetic launchers; linear motors; machine theory; naval engineering computing; ships; CAD; EMALS; US Navy; Virtual Test Bed; electric actuators; electromagnetic aircraft launch system; performance; ship systems; simulation; virtual prototyping environment; Acceleration; Availability; Carrier confinement; Electric motors; Electromagnetic launching; Hydraulic actuators; Marine vehicles; Military aircraft; Stress; Testing;
fLanguage
English
Publisher
ieee
Conference_Titel
Power Electronics Specialists Conference, 2002. pesc 02. 2002 IEEE 33rd Annual
Print_ISBN
0-7803-7262-X
Type
conf
DOI
10.1109/PSEC.2002.1022384
Filename
1022384
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