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US 2026/0285488 A1Published application
Unpressurised bay compartment in an aircraft having a ventilation system
AssigneeAirbus Operations GmbH
InventorSasank KOMARLA
Life of this patent
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Abstract
An unpressurised bay compartment in an aircraft with a ventilation system. The ventilation system includes a single air inlet in an outer skin of the aircraft, two ducts, a conveying device arranged in the first duct, a duct furcation, where the first duct and the second duct branch off from one another upstream of the conveying device, a duct junction, where the first duct and the second duct join one another downstream of the conveying device, and a valve arranged in the first duct between the duct furcation and the conveying device.
Claims12
An unpressurised bay compartment in an aircraft, comprising:
- a portion of an outer skin of the aircraft;
- and
- a ventilation system comprising:
- a single air inlet in the outer skin,
- a first duct,
- a conveying device arranged in the first duct and configured to convey air from the single air inlet through the first duct,
- a second duct arranged to bypass at least the conveying device,
- a duct furcation, where the first duct and the second duct branch off from one another, the duct furcation being disposed between the single air inlet and the conveying device,
- a duct junction, where the first duct and the second duct join one another, the duct junction being disposed downstream of the conveying device, and
- a valve arranged in the first duct between the duct furcation and the conveying device.
7 more elements
Dependencies are inferred from the claim text.