Luftlenkungsanordnung für ein Flugzeug mit Integriertem Wärmetauscher
Anmelder: Airbus Defence and Space GmbH 🇩🇪
Details
- Veröffentlichungs-Nr.
- EP3981689
- Aktenzeichen
- EP21200033
- Anmeldetag
- 30. September 2021
- Veröffentlichung
- 12. März 2025
- Erteilung
- 12. März 2025
- Rechtsraum
- EP
- IPC
- B64D33/02
Abstract
An air direction arrangement (100) for an aircraft is described. The air direction arrangement contains an inlet opening (110) and an inlet channel (111) which is connected thereto and which is at least partially surrounded by an outer wall (125). The inlet channel (111) is configured to guide air to an engine (30) of the aircraft. The outer wall (125) contains at least one outlet channel (135) and at least one outlet element (130). The outlet element (130) is configured to selectively release or close the outlet channel (135) for an air flow from the inlet channel (111) into the environment of the aircraft. The air direction arrangement (100) contains a heat exchanger (140) which is arranged in the outlet channel (135) in order to discharge thermal energy to the air flow which is flowing from the inlet channel into the environment of the aircraft.
Anmelder
- Firma
- Airbus Defence and Space GmbH
- Land
- 🇩🇪 Deutschland
Deutsche Sparte des Airbus-Konzerns, die militärische Flugzeuge, Satelliten, Raumfahrttechnik sowie Verteidigungs- und Sicherheitssysteme entwickelt.
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