US 3,945,434 AGranted

Gas turbine heat exchanger apparatus

AssigneeThe Garrett Corporation

InventorsKenneth O. Parker, Clarence L. Marksberry

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Abstract

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.

Claims5

Dependent claims

A counterflow heat exchanger of the type including a core of substantially parallel stacked plates and a plurality of manifolds in parallel spaced relation to each other, said manifolds and said defining a gas inlet surface for receiving hot gases and directing said gases into alternate spaces between said plates and temperature controller means, the improvement wherein said temperature controller means comprises:

a body having an inlet side and an outlet side and including a plurality of plate members defining a plurality of gas passages communicating said inlet side and said outlet side, said inlet side being arranged for receiving said hot gases and said outlet side being in close proximity to said gas inlet surface;
first ones of said passages being arranged for conducting a portion of the hot gases to said stacked plates of said heat exchanger and including means reducing the temperature of the hot gases before such gases reach said stacked plates of said heat exchanger, and
second ones of said passages bypassing said first passages and being arranged for conducting the remainder of said hot gases into heat transmitting relationship with said manifolds so that hot gases from said second passages which heat said manifolds are at a higher temperature than the gases leaving said first passages during transient heat exchange conditions.

Dependencies are inferred from the claim text.