HEAT EXCHANGER FOR A GAS TURBINE ENGINE

The heat exchanger (5) comprises a pressure vessel (6) with an inlet (7) for air, an outlet (8) for air and a bundle of pipes (9) housed within the pressure vessel (6) for a thermo-vector fluid. A gas/solid separator (10) is provided within the pressure vessel (6) for separating particles drawn by t...

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Bibliographische Detailangaben
Hauptverfasser:	PONCA, Daniel, STRUEKEN, Stephan, BRICAUD, Cyrille, ESCUDERO OLANO, Marcos
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OFGENERAL APPLICATION GAS-TURBINE PLANTS HEAT EXCHANGE IN GENERAL HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS,IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
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Beschreibung
Zusammenfassung:	The heat exchanger (5) comprises a pressure vessel (6) with an inlet (7) for air, an outlet (8) for air and a bundle of pipes (9) housed within the pressure vessel (6) for a thermo-vector fluid. A gas/solid separator (10) is provided within the pressure vessel (6) for separating particles drawn by the air.