VERMEVEXLARE VID GASTURBIN

Heat exchanger apparatus for a gas turbine which is provided with a heat exchanger of the formed plate counterflow type including a core having a gas turbine exhaust gas inlet surface with integral air outlet manifolds, and an inlet gas temperature controller which controls the temperature of the ga...

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Bibliographische Detailangaben
Hauptverfasser:	PARKER K O, MARKSBERRY C L
Format:	Patent
Sprache:	swe
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:	Heat exchanger apparatus for a gas turbine which is provided with a heat exchanger of the formed plate counterflow type including a core having a gas turbine exhaust gas inlet surface with integral air outlet manifolds, and an inlet gas temperature controller which controls the temperature of the gas impinging on the manifolds and core surface. The temperature controller consists of a housing defining a gas flow path to the heat exchanger core surface, fluid passages within the housing which direct the gas at substantially full gas temperature onto the manifolds, and heat absorber structure within the housing which absorbs heat from the gas to reduce the temperature to less than full gas temperature during transient conditions, such as turbine start-up, and directs the gas onto the core surface.