Further cooling of pre-swirl flow entering cooled rotor aerofoils

摘要

A tangential on board injector with auxiliary supply of further cooled compressed air, from an external heat exchanger or air cooled bearing gallery for example, serves to reduce the volume of cooling air directed tangentially toward a cooled rotor of a gas turbine engine. The tangential on board injector has an array of injector blades between two injector walls defining circumferential main flow nozzles for directing a main compressed air flow tangentially. Each blade has an interior chamber in flow communication with a source of auxiliary compressed air with at least one bore extending between the chamber and an exterior surface of the blade. The bores eject further cooled air from the heat exchanger and merge with the primary compressed air flowing through the injector nozzles. The bores may also produce a cooling film of air that reduces drag over the injector blades. Advantages of the further cooling bores include: reduction in injector air temperature and corresponding reduction in cooling air flow requirements; added control over injector flow volume and temperature to fine tune the delivery of cooling air to the rotor blades; improved cooling air control results in extended durability and service life of air cooled rotor blades; and the ejection of air near the trailing edge of the injector blades results in less drag and air pressure requirements.