HEAT EXCHANGER WITH HEAT RESISTANT CENTER BODY

A heat exchanger (102) for use in a gas turbine engine has a central body including an inlet manifold (126) and at least one tube providing an outlet manifold (128), and a plurality of tubes communicating holes (133) in an outer periphery of the inlet manifold (126) to holes (131) in an outer periph...

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Bibliographische Detailangaben
Hauptverfasser:	DUESLER, Paul W, SCHWARZ, Frederick M
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 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 JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
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Beschreibung
Zusammenfassung:	A heat exchanger (102) for use in a gas turbine engine has a central body including an inlet manifold (126) and at least one tube providing an outlet manifold (128), and a plurality of tubes communicating holes (133) in an outer periphery of the inlet manifold (126) to holes (131) in an outer periphery of the outlet manifold (128), and passages for cooling air to pass across the tubes.