Pre-cooler

Claim 2

In a gas compression system having first and second gas compressors, an intercooler connecting said compressors, at least one power turbine to drive said compressors, a combustion chamber to supply combusted gas to drive said turbine, and an air compressor to supply compressed air to said combustion chamber, the improvement comprising: an indirect evaporating film heat exchanger having separated dry and wet sides and formed with a first conduit for exhausting cool dry air from the dry side of said heat exchanger, and a second conduit for exhausting cool moist air from the wet side of said heat exchanger; mans for connecting said first heat exchanger conduit to the air compressor of said power turbine conveying said cool dry air from the heat exchanger to said turbine air compressor for supply thereby to said combustion chamber; and means for connecting said second heat exchanger conduit to said intercooler for heat exchange between said intercooler and the cool moist air from said heat exchanger.

Claim 3

In a gas compression system having first and second gas compressors, an intercooler connecting said compressors, at least one power turbine to drive said compressors, a combustion chamber to supply combusted gas to drive said turbine, and an air compressor to supply compressed air to said combustion chamber, the improvement comprising: an indirect evaporating film heat exchanger having separated dry and set sides and formed with a first conduit for exhausting cool dry air from the dry side of said heat exchanger, and a second conduit for exhausting cool moist air from the wet side of said heat exchanger; means for connecting said first heat exchanger conduit to the air compressor of said power turbine whereby said cool dry air from the heat exchanger is conveyed to said turbine air compressor to be supplied thereby to said combustion chamber; means for connecting said second heat exchanger conduit to said intercooler for heat exchange between said intercooler and the cool moist air from said heat exchanger; a third compressor for further compressing said gas as it exhausts from said second compressor; a second intercooler connecting said second and third compressors; and the further improvement comprising means for connecting said second heat exchanger conduit to said second intercooler for providing heat exchange between said second intercooler and the cool moist air from said heat exchanger.

Claim 4

In a gas compression system having first and second gas compressors, an intercooler connecting said compressors, at least one power turbine to drive said compressors, a combustion chamber to supply combusted gas to drive said turbine, and an air compressor to supply compressed air to said combustion chamber, the improvement comprising: an indirect evaporating film heat exchanger having separated dry and set sides and formed with a first conduit for exhausting cool dry air from the dry side of said heat exchanger, and a second conduit for exhausting cool moist air from the wet side of said heat exchanger; means for connecting said first heat exchanger conduit to the air compressor of said power turbine whereby said cool dry air from the heat exchanger is conveyed to said turbine air compressor to be supplied thereby to said combustion chamber; means for connecting said second heat exchanger conduit to said intercooler for heat exchange between said intercooler and the cool moist air from said heat exchanger; a third compressor for further compressing said gas as it exhausts from said second compressor; a second intercooler connecting said second and third compressors; and the further improvement comprising means for connecting said second heat exchanger conduit to said second intercooler for providing heat exchange between said second intercooler and the cool moist air from said heat exchanger.

Claim 5

The improvement of claim 1 including a second indirect evaporating film heat exchanger, means whereby the cool dry air from said first heat exchanger is utilized as the input air for said second heat exchanger, and means for combining in said second conduit the cool moist air from said first and second heat exchangers.

Claim 6

In a power turbine system having at least one power turbine, a combustion chamber to supply combusted gas to drive said turbine, and an air compressor to supply compressed air to said combustion chamber, the improvement comprising: an indirect evaporating film heat exchanger having separated dry and wet sides and formed with a first conduit for exhausting cool dry air from the dry side of said heat exchanger, and a second conduit for exhausting cool moist air from the wet side of said heat exchanger; means for combining the air contained in said first and second conduits and exhausting through a third conduit; and means for connecting said air compressor to said third conduit routing said cool dry air and said cool moist air to said air compressor for supply thereby to said combustion chamber.

Claim 7

In a power turbine system having at least one power turbine, a combustion chamber to supply combusted gas to drive said turbine, and an air compressor to supply compressed air to said combustion chamber, the improvement comprising: an indirect evaporating film heat exchanger having separated dry and wet sides and formed with a first conduit for exhausting cool dry air from the dry side of said heat exchanger, and a second conduit for exhausting cool moist air from the wet side of said heat exchanger; means for combining the air contained in said first and second conduits and exhausting through a third conduit; and means for connecting said air compressor to said third conduit routing said cool dry air and said cool moist air to said air compressor for supply thereby to said combustion chamber.

Claim 8

The improvement of claim 4 further comprising means for forming a film of water of predetermined thickness on said heat exchanger wet side.

Claim 9

The improvement of claim 5 wherein said thickness is about 0.1 to about 2 millimeters.

Claim 10

In a power turbine system having at least one power turbine, a combustion chamber to supply combusted gas to drive said turbine, and an air compressor to supply compressed air to said combustion chamber, the improvement comprising: an indirect evaporating film heat exchanger having separated dry and wet sides in the form of an array of vertically directed, spaced hollow elongated conduits wherein said dry and wet sides constitute outer an inner condduit surfaces, respective, and formed with a first conduit for exhausting cool dry air from the dry side of said heat exchanger, and a second conduit for exhausting cool moist air from the wet side of said heat exchanger; means for connecting said air compressor to said third conduit whereby said cool dry air and said cool moist air are routed to said air compressor to be supplied thereby to said combustion chamber; and means for forming a film of water of predetermined thickness on said heat exchanger wet side comprising means for applying said film of water to said inner conduit surfaces for flow by gravity therethrough.

Claim 11

In a power turbine system having at least one power turbine, a combustion chamber to supply combusted gas to drive said turbine, and an air compressor to supply compressed air to said combustion chamber, the improvement comprising: an indirect evaporating film heat exchanger having separated dry and wet sides in the form of an array of vertically directed, spaced hollow elongated conduits wherein said dry and wet sides constitute outer an inner condduit surfaces, respective, and formed with a first conduit for exhausting cool dry air from the dry side of said heat exchanger, and a second conduit for exhausting cool moist air from the wet side of said heat exchanger; means for connecting said air compressor to said third conduit whereby said cool dry air and said cool moist air are routed to said air compressor to be supplied thereby to said combustion chamber; and means for forming a film of water of predetermined thickness on said heat exchanger wet side comprising means for applying said film of water to said inner conduit surfaces for flow by gravity therethrough.

Claim 12

An improved method of gas compression utilizing a first and second gas compressor, an intercooler connecting said compressors, at least one power turbine to drive said compressors, a combustion chamber to supply combusted gas to drive said turbine, and an air compressor to supply compressed air to said combustion chamber, the improvement comprising: exhausting cool dry air from the dry side of a first indirect evaporating film heat exchanger having separated dry and wet side walls; exhausting cool moist air from the wet side of said first indirect evaporating film heat exchanger having separated dry and wet side walls; conveying said cool dry air to said air compressor and then to said combustion chamber; and, conveying said cool moist air to said intercooler for heat exchange between said intercooler and said cool moist air.

Claim 13

An improved method of gas compression utilizing a first and second gas compressor, an intercooler connecting said compressors, at least one power turbine to drive said compressors, a combustion chamber to supply combusted gas to drive said turbine, and an air compressor to supply compressed air to said combustion chamber, the improvement comprising: exhausting cool dry air from the dry side of a first indirect evaporating film heat exchanger having separated dry and wet side walls; exhausting cool moist air from the wet side of said first indirect evaporating film heat exchanger having separated dry and wet side walls; conveying said cool dry air to said air compressor and then to said combustion chamber; and, conveying said cool moist air to said intercooler for heat exchange between said intercooler and said cool moist air.

Claim 14

In the method of claim 8 wherein a third compressor is utilized for gas compression and a second intercooler connecting said second and third compressors is utilized, the further improvement comprising conveying said cool moist air to said second intercooler for providing heat exchange between said second intercooler and said cool moist air.

Claim 15

In the method of claim 8, the further improvement comprising: using cool dry air output from a second evaporating film heat exchanger as input air to said first evaporating film heat exchanger; and combining cool moist air output from said second evaporating film heat exchanger with said cool moist air from said first evaporating film heat exchanger.

Claim 16

An improved method of supplying input air to a power turbine system utilizing at least one power turbine, a combustion chamber to supply combusted gas to drive said turbine, and an air compressor to supply compressed air to said combustion chamber, the improvement comprising: exhausting cool dry air from the dry side of an indirect evaporating film heat exchanger having separated dry and wet side walls; exhausting cool moist air from the wet side of an indirect evaporating film exchanger having separated dry and wet side walls; combining said cool dry air with said cool moist air; and using said combined air as the input to said air compressor to be supplied thereby to said combustion chamber.

Claim 17

An improved method of supplying input air to a power turbine system utilizing at least one power turbine, a combustion chamber to supply combusted gas to drive said turbine, and an air compressor to supply compressed air to said combustion chamber, the improvement comprising: exhausting cool dry air from the dry side of an indirect evaporating film heat exchanger having separated dry and wet side walls; exhausting cool moist air from the wet side of an indirect evaporating film exchanger having separated dry and wet side walls; combining said cool dry air with said cool moist air; and using said combined air as the input to said air compressor to be supplied thereby to said combustion chamber.

Claim 18

The method of claim 11, the further improvement comprising forming a film of water of predetermined thickness on said heat exchanger wet side.

Claim 19

The improvement of claim 2 wherein said thickness is about 0.1 to 2 millimeters.

Claim 20

In the method of claim 12, the further improvement comprising: orienting said wet side wall to a vertical disposition, and applying said film of water to said wet side wall for flow by gravity thereon.