Patent ID: 9650956
Date: 2017-05-16
CPC Classifications: B01F,F01K,F02C,F05D

Claim:
1. An intake arrangement for a compressor in a gas turbine power plant, the intake arrangement, comprising: a passageway having an elongated portion, and a circular portion at an end portion of the elongated portion, the circular portion being arranged in proximity to the compressor at a compressor inlet; the passageway divided at least circumferentially and radially across the entire elongated portion and at least partially across the circular portion to configure, a plurality of flue gas inlet segments, each adapted to convey a flue gas stream therethrough; and a plurality of air inlet segments, each adapted to convey a fresh air stream therethrough, wherein the flue gas stream and the fresh air stream from each of the respective plurality of flue gas and air inlet segments, converge at a region (P) around and after the circular portion, to be blended into a target mass stream for being conveyed into the compressor through the compressor inlet.