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JP2004516423A5 - - Google Patents

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Publication number
JP2004516423A5
JP2004516423A5 JP2002553064A JP2002553064A JP2004516423A5 JP 2004516423 A5 JP2004516423 A5 JP 2004516423A5 JP 2002553064 A JP2002553064 A JP 2002553064A JP 2002553064 A JP2002553064 A JP 2002553064A JP 2004516423 A5 JP2004516423 A5 JP 2004516423A5
Authority
JP
Japan
Prior art keywords
support member
recuperator
turbine
chamber
housing
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Withdrawn
Application number
JP2002553064A
Other languages
Japanese (ja)
Other versions
JP2004516423A (en
Filing date
Publication date
Priority claimed from US09/749,267 external-priority patent/US20020079085A1/en
Application filed filed Critical
Publication of JP2004516423A publication Critical patent/JP2004516423A/en
Publication of JP2004516423A5 publication Critical patent/JP2004516423A5/ja
Withdrawn legal-status Critical Current

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Claims (12)

ハウジングと、
該ハウジング内に配置され、該ハウジングとの間に通路を形成する支持部材と、
対向する2つの端部及び対向する2つの側部を有し、該側部が互いに近接するようにそれ自体が折り重ねられ、該側部が前記支持部材に固定され、前記端部がシールされて、チャンバを形成するようになった波形材料のシートを各々が含み、前記支持部材に固定された複数の熱伝導セルと、
入口ヘッダと、
各々が前記入口ヘッダ及び前記チャンバと流体連通する、前記支持部材に形成された複数の入口と、
出口ヘッダと、
各々が前記出口ヘッダ及び前記チャンバと流体連通する、前記支持部材に形成された複数の出口と、
を組み合わせて含むことを特徴とするタービンの復熱装置。
A housing;
A support member disposed within the housing and defining a passage therewith;
It has two opposite end portions and two opposite side portions, and is folded itself so that the side portions are close to each other, the side portions are fixed to the support member, and the end portions are sealed. A plurality of heat conducting cells each including a sheet of corrugated material adapted to form a chamber and secured to the support member;
An inlet header;
A plurality of inlets formed in the support member, each in fluid communication with the inlet header and the chamber;
An exit header;
A plurality of outlets formed in the support member, each in fluid communication with the outlet header and the chamber;
A recuperator for a turbine comprising a combination of
前記チャンバが、予熱される空気が通過する低温セルを形成することを特徴とする、請求項1に記載のタービンの復熱装置。The turbine recuperator of claim 1, wherein the chamber forms a cold cell through which preheated air passes. 前記ハウジングが円筒形断面を有することを特徴とする、請求項1に記載のタービンの復熱装置。The recuperator for a turbine according to claim 1, wherein the housing has a cylindrical cross section. 前記支持部材が円筒形断面を有し、前記ハウジングに対し同軸に延びることを特徴とする、請求項3に記載のタービンの復熱装置。The turbine recuperator according to claim 3, wherein the support member has a cylindrical cross section and extends coaxially with respect to the housing. 円筒形ハウジングと、
該ハウジング内に同軸に配置され、高温の排気空気が通過する環状通路を前記ハウジングとの間に形成する円筒形支持部材と、
対向する2つの端部及び対向する2つの側部を有し、該側部が互いに近接するようにそれ自体が折り重ねられ、該側部が前記支持部材に固定され、前記端部がシールされて、チャンバを形成するようになった波形材料のシートを各々が含み、前記支持部材に固定された複数の熱伝導セルと、
入口ヘッダと、
各々が前記入口ヘッダ及び前記チャンバと流体連通して予熱される低温空気を前記チャンバに導入する、前記支持部材に形成された複数の入口と、
出口ヘッダと、
各々が前記出口ヘッダ及び前記チャンバと流体連通する、前記支持部材に形成された複数の出口と、
を組み合わせて含むことを特徴とするタービンの復熱装置。
A cylindrical housing;
A cylindrical support member disposed coaxially within the housing and forming an annular passage between the housing and the passage of hot exhaust air;
It has two opposite end portions and two opposite side portions, and is folded itself so that the side portions are close to each other, the side portions are fixed to the support member, and the end portions are sealed. A plurality of heat conducting cells each including a sheet of corrugated material adapted to form a chamber and secured to the support member;
An inlet header;
A plurality of inlets formed in the support member, each for introducing cold air into the chamber that is preheated in fluid communication with the inlet header and the chamber;
An exit header;
A plurality of outlets formed in the support member, each in fluid communication with the outlet header and the chamber;
A recuperator for a turbine comprising a combination of
前記熱伝導セルが、その半径方向寸法に沿って、前記支持部材に対して湾曲していることを特徴とする、請求項4又は請求項5に記載のタービンの復熱装置。The recuperator for a turbine according to claim 4 or 5, wherein the heat conduction cell is curved with respect to the support member along a radial dimension thereof. 前記入口ヘッダから前記入口、前記チャンバ及び前記出口ヘッダを経て、前記出口ヘッダに通る低温空気の流れと逆方向に、高温の排気空気の流れを与えるように、前記通路が構成されることを特徴とする、請求項1に記載のタービンの復熱装置。The passage is configured to provide a flow of hot exhaust air from the inlet header through the inlet, the chamber and the outlet header in a direction opposite to the flow of cold air passing through the outlet header. The recuperator for a turbine according to claim 1. 前記波形材料が金属であることを特徴とする、請求項1又は請求項5に記載のタービンの復熱装置。The recuperator for a turbine according to claim 1, wherein the corrugated material is a metal. 前記側部が前記支持部材に溶接されていることを特徴とする、請求項8に記載のタービンの復熱装置。The turbine recuperator according to claim 8, wherein the side portion is welded to the support member. 前記端部を互いに溶接して、シールを形成することを特徴とする、請求項8に記載のタービンの復熱装置。The turbine recuperator according to claim 8, wherein the ends are welded together to form a seal. 前記波形材料が鉄であることを特徴とする、請求項1又は請求項5に記載のタービンの復熱装置。The recuperator for a turbine according to claim 1 or 5, wherein the corrugated material is iron. 前記波形材料がニッケル基合金であることを特徴とする、請求項1又は請求項5に記載のタービンの復熱装置。The turbine recuperator according to claim 1 or 5, wherein the corrugated material is a nickel-based alloy.
JP2002553064A 2000-12-27 2001-12-12 Turbine recuperator Withdrawn JP2004516423A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US09/749,267 US20020079085A1 (en) 2000-12-27 2000-12-27 Turbine recuperator
PCT/US2001/048132 WO2002052211A2 (en) 2000-12-27 2001-12-12 Turbine recuperator

Publications (2)

Publication Number Publication Date
JP2004516423A JP2004516423A (en) 2004-06-03
JP2004516423A5 true JP2004516423A5 (en) 2005-01-20

Family

ID=25013017

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2002553064A Withdrawn JP2004516423A (en) 2000-12-27 2001-12-12 Turbine recuperator

Country Status (5)

Country Link
US (1) US20020079085A1 (en)
EP (1) EP1348098A2 (en)
JP (1) JP2004516423A (en)
KR (1) KR20020077921A (en)
WO (1) WO2002052211A2 (en)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6904747B2 (en) * 2002-08-30 2005-06-14 General Electric Company Heat exchanger for power generation equipment
US6966173B2 (en) * 2002-11-06 2005-11-22 Elliott Energy Systems, Inc. Heat transfer apparatus
TWI496918B (en) * 2013-02-05 2015-08-21 Adpv Technology Ltd Intetrust Gas release device for coating process
US9724746B2 (en) * 2013-03-14 2017-08-08 Pratt & Whitney Canada Corp. Aerodynamically active stiffening feature for gas turbine recuperator
CN106091757B (en) * 2016-07-22 2018-02-09 甘肃蓝科石化高新装备股份有限公司 A kind of package assembly and assemble method of full welding corrugated board cluster
NL2017947B1 (en) * 2016-12-07 2018-06-19 Recair Holding B V Recuperator
KR102097209B1 (en) * 2018-07-31 2020-04-03 주식회사 이노윌 Heat exchanger for gas turbine

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3507115A (en) * 1967-07-28 1970-04-21 Int Harvester Co Recuperative heat exchanger for gas turbines
DE2805912A1 (en) * 1978-02-13 1979-08-23 Linde Ag Plate type heat exchanger - has folded rectangular sheet metal plates sealed at connecting edges
DE3029000C2 (en) * 1980-07-31 1982-07-22 Gartemann & Hollmann Gmbh, 4800 Bielefeld Ring heat exchanger
GB9027994D0 (en) * 1990-12-22 1991-02-13 Atomic Energy Authority Uk Heat exchanger
JP3685890B2 (en) * 1996-10-17 2005-08-24 本田技研工業株式会社 Heat exchanger
GB2343641A (en) * 1998-11-10 2000-05-17 Centrax Ltd Heat exchanger

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