Heat transfer surface with nested tabs
US-9958215-B2 · May 1, 2018 · US
US11512909B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11512909-B2 |
| Application number | US-202117174454-A |
| Country | US |
| Kind code | B2 |
| Filing date | Feb 12, 2021 |
| Priority date | Mar 14, 2018 |
| Publication date | Nov 29, 2022 |
| Grant date | Nov 29, 2022 |
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Heat exchanger fins and heat exchangers are disclosed. The heat exchanger fins disclosed herein comprise louvers and winglet-type vortex generators arranged to improve heat transfer efficiency.
Opening claim text (preview).
What is claimed is: 1. A heat exchanger fin comprising: a base having a fin leading edge and a fin trailing edge, the fin leading edge being configured to be upstream of the fin trailing edge when the heat exchanger fin is installed in a heat exchanger; a plurality of apertures disposed in the base, each of the plurality of apertures being configured to receive a corresponding heat transfer tube of the heat exchanger; a first louver disposed on the base and comprising a first louver leading edge and a first louver trailing edge, the first louver leading edge being convex and the first louver trailing edge being concave; a pair of leading edge winglet-type vortex generators flanking each aperture of the plurality of apertures and located nearer the fin leading edge than the fin trailing edge; and a pair of trailing edge winglet-type vortex generators flanking each aperture of the plurality of apertures and located nearer the fin trailing edge than the fin leading edge; wherein the pair of leading edge winglet-type vortex generators defines a first angle therebetween, and the pair of trailing edge winglet-type vortex generators defines a second angle therebetween, wherein the first angle and the second angle are between about 35° to about 75°. 2. The heat exchanger fin of claim 1 further comprising: a second louver disposed on the base, the second louver comprising a second louver leading edge and a second louver trailing edge, wherein a second distance between the second louver leading edge and the second louver trailing edge is greater than a first distance between the first louver leading edge and the first louver trailing edge. 3. The heat exchanger fin of claim 1 further comprising: a second louver disposed on the base, the second louver comprising a second louver leading edge and a second louver trailing edge, the second louver leading edge being convex and the second louver trailing edge being concave. 4. The heat exchanger fin of claim 1 further comprising: a winglet-type vortex generator located between the fin leading edge and the first louver leading edge. 5. The heat exchanger fin of claim 4 , wherein the winglet-type vortex generator comprises a rectangular winglet. 6. The heat exchanger fin of claim 4 , wherein the winglet-type vortex generator comprises a triangular winglet. 7. The heat exchanger fin of claim 1 , wherein the first angle between the pair of leading edge winglet-type vortex generators is about 40°. 8. The heat exchanger fin of claim 1 , wherein the second angle between the pair of trailing edge winglet-type vortex generators is about 40°. 9. The heat exchanger fin of claim 1 , wherein each aperture of the plurality of apertures is oblong and oriented such that a longitudinal axis of the aperture is parallel with an average direction of upstream to downstream flow of gas over the heat exchanger fin when the heat exchanger fin is installed in the heat exchanger. 10. The heat exchanger fin of claim 1 , wherein a section of the fin leading edge between adjacent apertures of the plurality of apertures is concave. 11. The heat exchanger fin of claim 1 , wherein a first section of the fin leading edge that is upstream of an aperture of the plurality of apertures is convex and a second section of the fin trailing edge that is downstream of an aperture of the plurality of apertures is concave.
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