A galley insert for an aircraft galley. The galley insert include heating equipment and an exhaust arrangement configured to pass an exhaust air stream out of the galley insert. The exhaust arrangement comprises a plurality of deflection lamellas configured to adjust a direction of the exhaust air stream. At least some of the deflection lamellas are angularly adjusted on the basis of a temperature of the exhaust air stream using one or more temperature-dependent actors.
AIRCRAFT GALLEY INSERT
2024-05-23
Patent
Electronic Resource
English
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