Add to ORKGThis paper describes the basic design, refinement, and verification using finite-element analysis, and operational simulation using the Virtual Test Bed, of a linear machine for an electromagnetic aircraft launcher, for the aircraft carrier of the future. Choices of basic machine format and procedures for determining basic dimensions are presented. A detailed design for a permanent-magnet version is presented, and wound-field coil and induction machine versions are briefly discussed. The long armature-short field geometry is justified, and in particular the impact of this geometry on the scale of the power electronic drive system is examined
The purpose of this paper is to use the Lorentz force to generate repulsion forces to drive aircraft...
The application of more electrified systems in aircraft is required to achieve the target of a more ...
The paper presents a concept of a magnetic coil launcher for unmanned aerial vehicles of mass up to ...
This paper describes the basic design, refinement, and verification using finite-element analysis, a...
This paper deals with the design of an electromagnetic aircraft launch system (EMALS). The system st...
The engine size of modern passenger transport aircraft is principally determined by take-off conditi...
This paper considers the feasibility of different technologies for an electromagnetic launcher to as...
The engine size of modern aircraft is principally determined by take-off conditions, since initial a...
This paper presents design and prototyping studies for coreless and slotless permanent magnet (PM) m...
The engine size of modern passenger transport aircraft is principally determined by take-off conditi...
The engine size of modern passenger transport aircraft is principally determined by take-off conditi...
Electromagnetic launcher (EML) is an electromagnetic accelerator which uses electrical pulse power i...
This paper compares three possible linear motor topologies for an electromagnetic launch system to a...
This paper summarizes the results of a design study investigating the use of linear electric motors ...
The electromagnetic launcher consists of a system of stator coils producing a traveling field which ...
The purpose of this paper is to use the Lorentz force to generate repulsion forces to drive aircraft...
The application of more electrified systems in aircraft is required to achieve the target of a more ...
The paper presents a concept of a magnetic coil launcher for unmanned aerial vehicles of mass up to ...
This paper describes the basic design, refinement, and verification using finite-element analysis, a...
This paper deals with the design of an electromagnetic aircraft launch system (EMALS). The system st...
The engine size of modern passenger transport aircraft is principally determined by take-off conditi...
This paper considers the feasibility of different technologies for an electromagnetic launcher to as...
The engine size of modern aircraft is principally determined by take-off conditions, since initial a...
This paper presents design and prototyping studies for coreless and slotless permanent magnet (PM) m...
The engine size of modern passenger transport aircraft is principally determined by take-off conditi...
The engine size of modern passenger transport aircraft is principally determined by take-off conditi...
Electromagnetic launcher (EML) is an electromagnetic accelerator which uses electrical pulse power i...
This paper compares three possible linear motor topologies for an electromagnetic launch system to a...
This paper summarizes the results of a design study investigating the use of linear electric motors ...
The electromagnetic launcher consists of a system of stator coils producing a traveling field which ...
The purpose of this paper is to use the Lorentz force to generate repulsion forces to drive aircraft...
The application of more electrified systems in aircraft is required to achieve the target of a more ...
The paper presents a concept of a magnetic coil launcher for unmanned aerial vehicles of mass up to ...
