公开(公告)号：US10066632B2

公开(公告)日：2018-09-04

申请号：US14964620

申请日：2015-12-10

Applicant: GENERAL ELECTRIC COMPANY

Inventor： Joseph Philip Klosinski ,  Sanji Ekanayake ,  John Clisby Blanton ,  Alston Ilford Scipio

IPC: F04D27/02 ,  F02C7/047 ,  F02C7/052 ,  F02C7/24 ,  F02C9/18

Abstract: The present application provides an inlet bleed heat control system for a compressor of a gas turbine engine. The inlet bleed heat control system provides an inlet bleed heat manifold and an ejector in communication with the inlet bleed heat manifold such that the ejector is in communication with a flow of compressor discharge air and a flow of ambient air.