A gas turbine engine component includes a heat exchange structure (96) having an upstream end and a downstream end. A diffusing duct (68) is associated with the upstream end. A throttle member (102) controls air flow through the heat exchange structure (96), wherein the throttle member (102) has a non-circular cross section and is mounted to the downstream end of the heat exchange structure (96) or is mounted between the upstream end and the diffusing duct (68).
HEAT EXCHANGER FOR GAS TURBINE ENGINE
WÄRMETAUSCHER FÜR GASTURBINENTRIEBWERK
ECHANGEUR DE CHALEUR POUR MOTEUR À TURBINE À GAZ
2019-08-21
Patent
Electronic Resource
English
GAS TURBINE ENGINE WITH LOWER BIFURCATION HEAT EXCHANGER
European Patent Office | 2018
|GAS TURBINE ENGINE WITH THERMOELECTRIC COOLING AIR HEAT EXCHANGER
European Patent Office | 2017
|