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US 2024/0401535 A1Published application
Dihydrogen control assembly for an aircraft turbine engine
AssigneeSafran Aircraft Engines
InventorsYves EMPRIN, Jérémy Edmond FERT
Life of this patent
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Abstract
The present invention relates to an aircraft turbine engine (1) comprising a dihydrogen control assembly (10) having at least one dihydrogen retention zone (V) in which dihydrogen accumulates. The assembly comprises at least one spark plug (12) arranged at said retention zone (V) in order to burn at least some of the accumulated hydrogen.
Claims10
An aircraft turbine engine,
- the aircraft turbine engine comprising a dihydrogen control assembly having at least one retention zone configured so that dihydrogen accumulates in the retention zone,
- the dihydrogen control assembly comprising at least one spark plug arranged at the retention zone,
- the at least one spark plug being configurated to burn at least some of the dihydrogen that accumulates in the retention zone.
Dependencies are inferred from the claim text.