Electrical protection system for aircraft, with superconductive fuse connection

Abstract

An electrical protection system for an electrical connection of an electrical circuit of an aircraft, for example an aircraft powered by hydrogen, comprising a fuse element made of a material which exhibits superconducting properties in a superconducting state, and non-superconducting properties in a normal state, the transition from the superconducting state to the normal state releasing transition energy, the protection system also comprising a device, called the safety device, designed to open the electrical connection when the fuse element changes from the superconducting state to the normal state.

Dependencies are inferred from the claim text.