Heat transfer fin

US11333397B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-11333397-B2
Application numberUS-201916567349-A
CountryUS
Kind codeB2
Filing dateSep 11, 2019
Priority dateOct 15, 2018
Publication dateMay 17, 2022
Grant dateMay 17, 2022

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  1. Title

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  2. Abstract

    A short plain-language summary of the technical disclosure.

  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.

A heat transfer fin (1) includes a plurality of heat-transfer-tube insertion holes (10) aligned in a single stage, a downstream cut portion (3) formed so as to be recessed toward an upstream side of a gas flow passage of combustion exhaust gas, a downstream flange (13) formed on a peripheral edge of the downstream cut portion (3) so as to protrude from one surface of the heat transfer fin (1), and a plurality of first protruding pieces (4a) (4b) (4c) formed between the heat-transfer-tube insertion hole (10) and the downstream flange (13) so as to protrude alternately from both surfaces of the heat transfer fin (1).

First claim

Opening claim text (preview).

What is claimed is: 1. A heat transfer fin having a flat plate shape and arranged in a heat exchanger through which combustion exhaust gas flows, the heat transfer fin comprising: a plurality of heat-transfer-tube insertion holes aligned in a single stage; a downstream cut portion provided downstream of a gas flow passage of the combustion exhaust gas between an adjacent pair of the plurality of heat-transfer-tube insertion holes, the downstream cut portion being formed so as to be recessed toward an upstream side of the gas flow passage of the combustion exhaust gas; a downstream flange formed on a peripheral edge of the downstream cut portion so as to protrude from a first surface of the heat transfer fin; and a plurality of protruding pieces formed between the downstream flange and a first heat-transfer-tube insertion hole of the adjacent pair of the plurality of heat-transfer-tube insertion holes located adjacent to the downstream flange so as to protrude alternately from the first surface and a second surface of the heat transfer fin, wherein each of the plurality of protruding pieces is a cut-and-raised portion protruding only in a downstream direction of the gas flow passage of the combustion exhaust gas. 2. The heat transfer fin according to claim 1 , wherein the plurality of protruding pieces is a plurality of first protruding pieces, the heat transfer fin further comprising a plurality of second protruding pieces formed between the adjacent pair of the plurality of heat-transfer-tube insertion holes so as to protrude alternately from the first surface and the second surface of the heat transfer fin. 3. The heat transfer fin according to claim 2 , wherein the plurality of first protruding pieces are configured to be substantially orthogonal to the gas flow passage of the combustion exhaust gas flowing from the upstream side to a downstream side between the first heat-transfer-tube insertion hole of the adjacent pair of the plurality of heat-transfer-tube insertion holes and the downstream flange, and wherein the plurality of second protruding pieces are configured to be substantially orthogonal to the gas flow passage of the combustion exhaust gas flowing from the upstream side to the downstream side between the adjacent pair of the plurality of heat-transfer-tube insertion holes. 4. The heat transfer fin according to claim 2 , wherein each of the plurality of first protruding pieces is a first cut-and-raised portion, wherein each of the plurality of second protruding pieces is a second cut-and-raised portion protruding only in a downstream direction of the gas flow passage of the combustion exhaust gas, and wherein the downstream flange has a protrusion height greater than protrusion heights of the first cut-and-raised portions and the second cut-and-raised portions protruding from the first surface of the heat transfer fin. 5. The heat transfer fin according to claim 1 , further comprising an upstream protrusion formed between the first heat-transfer-tube insertion hole of the adjacent pair of the plurality of heat-transfer-tube insertion holes and an upstream edge of the heat transfer fin so as to protrude from the first surface of the heat transfer fin. 6. The heat transfer fin according to claim 1 , further comprising an upstream cut portion upstream of the gas flow passage of the combustion exhaust gas between the adjacent pair of the plurality of heat-transfer-tube insertion holes, the upstream cut portion being formed so as to be recessed toward a downstream side of the gas flow passage of the combustion exhaust gas.

Assignees

Inventors

Classifications

  • Energy efficient heating, ventilation or air conditioning [HVAC] · CPC title

  • for water heaters · CPC title

  • F24H1/145Primary

    using fluid fuel · CPC title

  • Spacing means · CPC title

  • the means being only outside the tubular element · CPC title

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Frequently asked questions

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What does patent US11333397B2 cover?
A heat transfer fin (1) includes a plurality of heat-transfer-tube insertion holes (10) aligned in a single stage, a downstream cut portion (3) formed so as to be recessed toward an upstream side of a gas flow passage of combustion exhaust gas, a downstream flange (13) formed on a peripheral edge of the downstream cut portion (3) so as to protrude from one surface of the heat transfer fin (1), …
Who is the assignee on this patent?
Rinnai Kk
What technology area does this patent fall under?
Primary CPC classification F24H1/145. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue May 17 2022 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).