Patent ID: 9551282
Date: 2017-01-24
CPC Classifications: B01D,C04B,F01M,F02C

Claim:
1. A media pad for cooling an inlet air flow to a compressor of a gas turbine engine, comprising: a first media sheet; the first media sheet comprising a chevron corrugated surface with a first mist eliminator, the chevron corrugated surface comprising a plurality of chevron channels with a diagonally rising portion and a positive Y-axis direction and a diagonally lowering portion in a negative Y-axis direction, wherein the first mist eliminator is adjacent to the diagonally lowering portion; and a second media sheet adjacent to the first media sheet; the second media sheet comprising a wavy corrugated surface with a second mist eliminator, the wavy corrugated surface comprising substantially lateral waves that are adjacent to the second mist eliminator; wherein the first media sheet and the second media sheet extend from a leading edge to a trailing edge, and wherein the chevron corrugated surface and the wavy corrugated surface extend from the leading edge towards the trailing edge; and wherein the inlet air flows in a positive X-axis direction that is perpendicular to the Y-axis.