Flugzeugtreibstoffzufuhrsystem

Details

Veröffentlichungs-Nr.

EP4806791

Anmeldetag

9. März 2026

Veröffentlichung

16. September 2026

Rechtsraum

EP

Abstract

The present invention relates to an aircraft fuel delivery system having a first tank for storing a first fluid, second tank for storing a second fluid and a shut-off valve. The shut-off valve comprises a first inlet port for introducing the first fluid into an internal valve chamber and a second inlet port for introducing the second fluid into the internal valve chamber such that the second fluid can be combined with the first fluid to create a fluid mixture. The shut-off valve also comprises a valve member the position of which can be adjusted for controlling the delivery of the first fluid and/or the fluid mixture to the aircraft power plant.

Anmelder

Firma

Airbus Operations Ltd

Land

🇬🇧 Großbritannien