Recuperative exhaust-gas heat exchanger for a gas turbine engine
AssigneeMTU Aero Engines AG
InventorHarald Schoenenborn
Life of this patent
Estimating the term…
Abstract
A recuperative exhaust-gas heat exchanger for a gas turbine engine is provided which has a crossflow/counterflow matrix around which the hot turbine exhaust gas flows, a distributing tube for directing the air delivered by a compressor into the crossflow/counterflow matrix and a collecting tube which is arranged parallel to the distributing tube and is intended for discharging the compressor air, heated via the crossflow/counterflow matrix, to a consumer. End faces of the distributing and collecting tubes which are remote from the compressor and consumer are closed. The closed end face of the collecting tube is firmly connected axially and radially to the turbine casing.
Claims3
A recuperative exhaust-gas heat exchanger for a gas turbine engine, said recuperative exhaust-gas heat exchanger having a crossflow/counterflow matrix around which hot turbine exhaust gas flows, a distributing tube for directing air delivered by a compressor into the crossflow/counterflow matrix, and a collecting tube which is arranged parallel to the distributing tube and is intended for discharging the compressor air, heated via the crossflow/counterflow matrix, to a consumer, each of the distributing and collecting tubes having opposite ends, wherein one end of the collecting tube is firmly connected axially and radially to a turbine casing and the other end of the collecting tube has axial play with respect to the turbine casing, and wherein the one end of the collecting tube is closed by a cover plate.
A recuperative exhaust-gas heat exchanger for a gas turbine engine, said recuperative exhaust-gas heat exchanger having a crossflow/counterflow matrix around which hot turbine exhaust gas flows, a distributing tube for directing air delivered by a compressor into the crossflow/counterflow matrix, and a collecting tube which is arranged parallel to the distributing tube and is intended for discharging the compressor air, heated via the crossflow/counterflow matrix, to a consumer, end faces of the distributing and collecting tubes which are remote from the compressor and consumer being closed, wherein the closed end face of the collecting tube is firmly connected axially and radially to a turbine casing, wherein a region comprising the closed end face of the collecting tube is designed as a cover plate, and wherein the cover plate is releasably connected to the collecting tube.
Dependencies are inferred from the claim text.