A multi-disk brake system comprises an electrical generator (105) disposed therein. The electrical generator is configured to convert mechanical energy to electrical energy. The mechanical energy may be generated during a braking event of the multi-disk brake system. The electric generator may power various electrical components on the aircraft or store the electrical energy in a capacitor bank. The electric generator may also act as a motor and/or power a landing gear in a motor configuration.
HYBRID REGENERATION BRAKE SYSTEM
HYBRIDES REGENERATIONSBREMSSYSTEM
SYSTÈME DE FREIN À RÉGÉNÉRATION HYBRIDE
2021-08-04
Patent
Electronic Resource
English
European Patent Office | 2020
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