Media pads with mist elimination features

US9551282B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9551282-B2
Application numberUS-201414516663-A
CountryUS
Kind codeB2
Filing dateOct 17, 2014
Priority dateOct 17, 2014
Publication dateJan 24, 2017
Grant dateJan 24, 2017

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

The present application provides a media pad for cooling an inlet air flow to a compressor of a gas turbine engine. The media pad may include a first media sheet with a chevron corrugated surface having a first mist eliminator and a second media sheet with a wavy corrugated surface having a second mist eliminator.

First claim

Opening claim text (preview).

We 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. 2. The media pad of claim 1 , wherein the leading edge faces the inlet air flow. 3. The media pad of claim 1 , wherein the first mist eliminator and the second mist eliminator are positioned about the trailing edge. 4. The media pad of claim 1 , wherein the leading edge and the trailing edge comprise a diamond like shape. 5. The media pad of claim 4 , wherein a leading edge chevron angle is about 17degrees and a trailing edge chevron angle is about 18 degrees. 6. The media pad of claim 4 , wherein the diamond like shape comprises a bonding portion and an expanded portion. 7. The media pad of claim 1 , wherein the first media sheet and the second media sheet extend from a top edge to a bottom edge. 8. The media pad of claim 7 , wherein the top edge faces a flow of water. 9. The media pad of claim 1 , wherein the first mist eliminator extends from the diagonally lowering portion at a sharp angle. 10. The media pad of claim 1 , wherein the wavy corrugated surface comprises a plurality of wavy channels with peaks and valleys. 11. The media pad of claim 10 , wherein the second mist eliminator extends from a valley at a sharp angle. 12. The media pad of claim 1 , wherein the first mist eliminator and the second mist eliminator comprise an integral mist eliminator. 13. A method of cooling an inlet air flow for a gas turbine engine, comprising: positioning a media pad with a first corrugated surface having a chevron configuration, a second corrugated surface having a sinusoidal wavy configuration, and an integral mist eliminator about an inlet of the gas turbine engine, wherein the first corrugated surface and the second corrugated surface 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; flowing water from a top to a bottom of the media pad through the first corrugated surface and the second corrugated surface; exchanging heat between the inlet air flow and the flow of water; capturing any mist from the flow of water in the integral mist eliminator; and flowing the captured mist back to the first corrugated surface and the second corrugated surface. 14. 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 plurality of chevron channels leading to a first mist eliminator, the plurality of chevron channels comprising a diagonally rising portion in 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; the second media sheet comprising a plurality of substantially horizontal wavy channels leading to a second mist eliminator; wherein the first mist eliminator and the second mist eliminator form an integral mist eliminator; and wherein the first media sheet and the second media sheet extend from a leading edge facing an inlet air flow to a trailing edge with the integral mist eliminator, and wherein the plurality of chevron channels and the plurality of wavy channels 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. 15. The media pad of claim 14 , wherein the leading edge and the trailing edge comprise a diamond like shape. 16. The media pad of claim 14 , wherein the plurality of wavy channels comprises peaks and valleys.

Assignees

Inventors

Classifications

  • characterised by the material treated · CPC title

  • by impingement against baffle separators · CPC title

  • having means for purifying air before leaving crankcase, e.g. removing oil · CPC title

  • F02C7/185Primary

    Cooling means for reducing the temperature of the cooling air or gas · CPC title

  • Control or regulation (conjointly with fuel supply control F02C9/50, with nozzle area control F02K1/16) · CPC title

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Frequently asked questions

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What does patent US9551282B2 cover?
The present application provides a media pad for cooling an inlet air flow to a compressor of a gas turbine engine. The media pad may include a first media sheet with a chevron corrugated surface having a first mist eliminator and a second media sheet with a wavy corrugated surface having a second mist eliminator.
Who is the assignee on this patent?
Gen Electric
What technology area does this patent fall under?
Primary CPC classification F02C7/185. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Jan 24 2017 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 1 related publication on this page (citations in our corpus or others sharing the same primary CPC).