Plate-shaped heat exchanger for a cooling device comprising at least one heart exchanger package
US-9638476-B2 · May 2, 2017 · US
US11333397B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11333397-B2 |
| Application number | US-201916567349-A |
| Country | US |
| Kind code | B2 |
| Filing date | Sep 11, 2019 |
| Priority date | Oct 15, 2018 |
| Publication date | May 17, 2022 |
| Grant date | May 17, 2022 |
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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).
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.
Energy efficient heating, ventilation or air conditioning [HVAC] · CPC title
for water heaters · CPC title
using fluid fuel · CPC title
Spacing means · CPC title
the means being only outside the tubular element · CPC title
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