SYSTEM FOR PREVENTING OVERHEATING IN AIRCRAFT GALLEY INSERTS

A system may include a heating element (104) configured to heat a fluid, the fluid configured to heat a food or drink product (110). The system may include one or more fluid temperature monitoring components (120) configured to monitor a temperature of the fluid while the fluid is heated by the heat...

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Bibliographische Detailangaben
1. Verfasser:	CIESIELSKI, Filip
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS PARACHUTES PERFORMING OPERATIONS TRANSPORTING
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Beschreibung
Zusammenfassung:	A system may include a heating element (104) configured to heat a fluid, the fluid configured to heat a food or drink product (110). The system may include one or more fluid temperature monitoring components (120) configured to monitor a temperature of the fluid while the fluid is heated by the heating element and configured to control the fluid temperature by controlling the heating element. The system may include one or more control units (116) configured to control operation of an aircraft galley insert via one or more control signals. The system may include one or more heating element temperature rise slope limiters (112) configured to maintain a heating temperature rise speed below a select heating temperature rise speed limit. The system may include one or more heating element temperature monitoring components (114) configured to provide information of a heating element temperature to the one or more heating element temperature rise slope limiters.