Invention Application
US20160222982A1 FLUID INJECTOR FOR COOLING A GAS TURBINE ENGINE COMPONENT 审中-公开
用于冷却气体涡轮发动机部件的流体注射器

FLUID INJECTOR FOR COOLING A GAS TURBINE ENGINE COMPONENT
Abstract:
An example method of cooling a compressor of a gas turbine includes, among other things, diverting a flow from a compressor, and directing the flow at the compressor in a direction, the direction having a circumferential component and an axial component.
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