Contoured evaporative cooling medium

US10495000B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-10495000-B2
Application numberUS-201715463680-A
CountryUS
Kind codeB2
Filing dateMar 20, 2017
Priority dateMar 20, 2017
Publication dateDec 3, 2019
Grant dateDec 3, 2019

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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 gas turbine engine. The gas turbine engine may include a compressor and an inlet air system positioned upstream of the compressor. The inlet air system may include a wetted media pad for evaporative cooling. The wetted media pad may include a contoured configuration.

First claim

Opening claim text (preview).

We claim: 1. A gas turbine engine, comprising: a compressor; and an inlet air system positioned upstream of the compressor; the inlet air system comprising a wetted media pad for evaporative cooling; wherein the wetted media pad comprises a contoured configuration; wherein the contoured configuration comprises a curved configuration extending from an upper section to a lower section along at least one of a leading edge and a trailing edge. 2. The gas turbine engine of claim 1 , wherein the wetted media pad comprises polyethylene terephthalate (PET), polytrimethylene terephthalate (PTT), nylon, polyester, polypropylene, or cellulose. 3. A gas turbine engine of claim 1 , comprising: a compressor; and an inlet air system positioned upstream of the compressor; the inlet air system comprising a wetted media pad for evaporative cooling; wherein the wetted media pad comprises a plurality of channels therethrough with a branched configuration; wherein the branched configuration comprises at least one of a larger, single channel branching into smaller, multiple channels and smaller, multiple channels merging into a larger, single channel. 4. The gas turbine engine of claim 3 , wherein the plurality of channels with the branched configuration extend from a leading edge to a trailing edge or from a top edge to a bottom edge. 5. The gas turbine engine of claim 1 , wherein the wetted media pad comprises: a first media sheet; the first media sheet comprising a chevron corrugated surface; and a second media sheet; the second media sheet comprising a wavy corrugated surface. 6. The gas turbine engine of claim 5 , wherein the chevron corrugated surface and the wavy corrugated surface extend from a leading edge towards a trailing edge and wherein the leading edge and the trailing edge comprise a diamond like shape. 7. The gas turbine engine of claim 6 , wherein the diamond like shape comprises a bonding portion and an expanded portion. 8. The gas turbine engine of claim 5 , wherein the chevron corrugated surface comprises a plurality of chevron channels with diagonally rising portions and diagonally lowering portions. 9. The gas turbine engine of claim 5 , wherein the wavy corrugated surface comprises a plurality of wavy channels with peaks and valleys. 10. A gas turbine engine, comprising: a compressor; and an inlet air system positioned upstream of the compressor; the inlet air system comprising a wetted media pad for evaporative cooling; wherein the wetted media pad comprises curved configuration; wherein the curved configuration extends from an upper section to a lower section along at least one of a leading edge and a trailing edge. 11. The gas turbine engine of claim 10 , wherein the wetted media pad comprise polyethylene terephthalate (PET), polytrimethylene terephthalate (PTT), nylon, polyester, polypropylene, or cellulose.

Assignees

Inventors

Classifications

  • using a phase changing mass, e.g. heat absorbing by melting or boiling · CPC title

  • F28F3/025Primary

    the means being corrugated, plate-like elements · CPC title

  • having provisions for obviating the penetration of damaging objects or particles · CPC title

  • before or between the compressor stages · CPC title

  • with change of state, e.g. absorption, evaporation, condensation (generating steam under pressure F22) · CPC title

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Frequently asked questions

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What does patent US10495000B2 cover?
The present application provides a gas turbine engine. The gas turbine engine may include a compressor and an inlet air system positioned upstream of the compressor. The inlet air system may include a wetted media pad for evaporative cooling. The wetted media pad may include a contoured configuration.
Who is the assignee on this patent?
Gen Electric
What technology area does this patent fall under?
Primary CPC classification F28F3/025. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Dec 03 2019 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 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).