METHOD AND SYSTEM FOR RADIAL TUBULAR HEAT EXCHANGERS

A method and a system for a heat exchanger assembly (60) are provided. The heat exchanger assembly (60) includes one or more arcuate heat exchanger segments (106) each including an inlet header (504) configured to extend circumferentially about a circumference of an inner surface (108) of a fluid fl...

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Hauptverfasser: MARTINEZ, RAMON, HURT, MATTHEW JOHN, JOHNSON, PAUL CHARLES, JOERGER, KEITH ALAN, BREIG, BENJAMIN PAUL, WILSON, GREGG HUNT, CORSMEIER, DONALD MICHAEL
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creator MARTINEZ, RAMON
HURT, MATTHEW JOHN
JOHNSON, PAUL CHARLES
JOERGER, KEITH ALAN
BREIG, BENJAMIN PAUL
WILSON, GREGG HUNT
CORSMEIER, DONALD MICHAEL
description A method and a system for a heat exchanger assembly (60) are provided. The heat exchanger assembly (60) includes one or more arcuate heat exchanger segments (106) each including an inlet header (504) configured to extend circumferentially about a circumference of an inner surface (108) of a fluid flow duct (109), and an outlet header (502) configured to extend circumferentially about the fluid flow duct (109). The heat exchanger assembly (60) also includes a first serpentine heat exchanger tube extending between the inlet header (504) and the outlet header (502) and including a series of flow path segments haying a gradually changing direction defined by a bend radius of the tube such that a direction of flow through the serpentine heat exchanger tube reverses between the inlet (504) and the outlet headers (502) and a second serpentine heat exchanger tube extending between the inlet header (504) and the outlet header (502), the second serpentine heat exchanger tube co-planar with the first serpentine heat exchanger tube.
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The heat exchanger assembly (60) also includes a first serpentine heat exchanger tube extending between the inlet header (504) and the outlet header (502) and including a series of flow path segments haying a gradually changing direction defined by a bend radius of the tube such that a direction of flow through the serpentine heat exchanger tube reverses between the inlet (504) and the outlet headers (502) and a second serpentine heat exchanger tube extending between the inlet header (504) and the outlet header (502), the second serpentine heat exchanger tube co-planar with the first serpentine heat exchanger tube.</description><language>eng ; fre</language><subject>AIR INTAKES FOR JET-PROPULSION PLANTS ; BLASTING ; CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TOTRANSPORTATION ; COMBINED OPERATIONS ; COMBUSTION ENGINES ; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ; DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OFGENERAL APPLICATION ; ENGINE PLANTS IN GENERAL ; GAS-TURBINE PLANTS ; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC ; GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS ; HEAT EXCHANGE IN GENERAL ; HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS,IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT ; HEATING ; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS ; INDEXING SCHEME FOR ASPECTS RELATING TONON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES ORJET-PROPULSION PLANTS ; INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUSSUBCLASSES OF CLASSES F01-F04 ; JET-PROPULSION PLANTS ; LIGHTING ; MACHINE TOOLS ; MACHINES OR ENGINES IN GENERAL ; MECHANICAL ENGINEERING ; METAL-WORKING NOT OTHERWISE PROVIDED FOR ; NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES ; OTHER WORKING OF METAL ; PERFORMING OPERATIONS ; STEAM ENGINES ; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS ; TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINSTCLIMATE CHANGE ; TRANSPORTING ; UNIVERSAL MACHINE TOOLS ; WEAPONS</subject><creationdate>2015</creationdate><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20151230&amp;DB=EPODOC&amp;CC=CA&amp;NR=2895602A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20151230&amp;DB=EPODOC&amp;CC=CA&amp;NR=2895602A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>MARTINEZ, RAMON</creatorcontrib><creatorcontrib>HURT, MATTHEW JOHN</creatorcontrib><creatorcontrib>JOHNSON, PAUL CHARLES</creatorcontrib><creatorcontrib>JOERGER, KEITH ALAN</creatorcontrib><creatorcontrib>BREIG, BENJAMIN PAUL</creatorcontrib><creatorcontrib>WILSON, GREGG HUNT</creatorcontrib><creatorcontrib>CORSMEIER, DONALD MICHAEL</creatorcontrib><title>METHOD AND SYSTEM FOR RADIAL TUBULAR HEAT EXCHANGERS</title><description>A method and a system for a heat exchanger assembly (60) are provided. 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The heat exchanger assembly (60) also includes a first serpentine heat exchanger tube extending between the inlet header (504) and the outlet header (502) and including a series of flow path segments haying a gradually changing direction defined by a bend radius of the tube such that a direction of flow through the serpentine heat exchanger tube reverses between the inlet (504) and the outlet headers (502) and a second serpentine heat exchanger tube extending between the inlet header (504) and the outlet header (502), the second serpentine heat exchanger tube co-planar with the first serpentine heat exchanger tube.</abstract><oa>free_for_read</oa></addata></record>
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subjects AIR INTAKES FOR JET-PROPULSION PLANTS
BLASTING
CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TOTRANSPORTATION
COMBINED OPERATIONS
COMBUSTION ENGINES
CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OFGENERAL APPLICATION
ENGINE PLANTS IN GENERAL
GAS-TURBINE PLANTS
GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS
HEAT EXCHANGE IN GENERAL
HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS,IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
INDEXING SCHEME FOR ASPECTS RELATING TONON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES ORJET-PROPULSION PLANTS
INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUSSUBCLASSES OF CLASSES F01-F04
JET-PROPULSION PLANTS
LIGHTING
MACHINE TOOLS
MACHINES OR ENGINES IN GENERAL
MECHANICAL ENGINEERING
METAL-WORKING NOT OTHERWISE PROVIDED FOR
NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES
OTHER WORKING OF METAL
PERFORMING OPERATIONS
STEAM ENGINES
TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINSTCLIMATE CHANGE
TRANSPORTING
UNIVERSAL MACHINE TOOLS
WEAPONS
title METHOD AND SYSTEM FOR RADIAL TUBULAR HEAT EXCHANGERS
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