CLOSED LOOP ICING CONTROL FOR HEAT EXCHANGERS

A heat exchanger has a heat exchanger body (39), an inlet (24) for a fluid to be cooled, and an outlet (26) for the fluid to be cooled. There is also an inlet (30) for a cooling fluid and an outlet (32) for the cooling fluid. The cooling fluid and the fluid to be cooled connects to the heat exchange...

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Bibliographische Detailangaben
1. Verfasser:	RHODEN, William E
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BLASTING COSMONAUTICS DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OFGENERAL APPLICATION EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS HEAT EXCHANGE IN GENERAL HEATING LIGHTING MECHANICAL ENGINEERING PARACHUTES PERFORMING OPERATIONS TRANSPORTING WEAPONS
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Beschreibung
Zusammenfassung:	A heat exchanger has a heat exchanger body (39), an inlet (24) for a fluid to be cooled, and an outlet (26) for the fluid to be cooled. There is also an inlet (30) for a cooling fluid and an outlet (32) for the cooling fluid. The cooling fluid and the fluid to be cooled connects to the heat exchanger, but are maintained separate in the heat exchanger such that the cooling fluid lowers the temperature of the fluid to be cooled. The cooling fluid and the fluid to be cooled connects to pass through the heat exchanger, but are maintained separate such that the cooling fluid lowers the temperature of the fluid to be cooled. An ice detector (34) detects an undesirable amount of ice particles in the cooling fluid. A control receives information from the ice detector and controls electric heating elements should an undesirable amount of ice particles be detected. An aircraft is also described.