2022
DOI: 10.1016/j.cryogenics.2022.103548
|View full text |Cite
|
Sign up to set email alerts
|

Design and finite volume evaluation of a counterflow recuperative spiral heat exchanger for additive manufacturing

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
3
1

Citation Types

0
4
0

Year Published

2023
2023
2024
2024

Publication Types

Select...
6

Relationship

0
6

Authors

Journals

citations
Cited by 6 publications
(4 citation statements)
references
References 27 publications
0
4
0
Order By: Relevance
“…22 Therefore, the proposed system presented herein is also modeled with the same d/p ratio of 4:1 to achieve the maximum heat transfer. Busch et al 23 devised a counter flow recuperative spiral heat exchanger to achieve a large temperature difference between the inlets (i.e. )., 30 K for cold inlet and 300 K for the hot inlet to maintain the temperature of electric components efficiently at a constant level.…”
Section: Validationmentioning
confidence: 99%
“…22 Therefore, the proposed system presented herein is also modeled with the same d/p ratio of 4:1 to achieve the maximum heat transfer. Busch et al 23 devised a counter flow recuperative spiral heat exchanger to achieve a large temperature difference between the inlets (i.e. )., 30 K for cold inlet and 300 K for the hot inlet to maintain the temperature of electric components efficiently at a constant level.…”
Section: Validationmentioning
confidence: 99%
“…The previous flow distribution, which mainly determines the boundary conditions for heat transfer, has been neglected (e.g. [3,4]). Investigations are typically conducted using large-volume distribution chambers, which often have unfavorable flow conditions but are not taken into account [5].…”
Section: Introductionmentioning
confidence: 99%
“…Liu, Z. T. et al introduced a composite heat exchanger combining a plate-fin heat exchanger and a front deflector, which effectively improves the heat conversion efficiency at high altitudes of an aircraft [16]. Bush, B. et al proposed a composite heat exchanger applied to aircraft, which includes a heat pump and a return heat exchanger, and it can realize smooth heat circulation at low temperatures [17]. Xu, Y. et al proposed a coupling of a vapor compression system and lubricating oil system to solve the problem of engine power loss due to heat supply on an aircraft and, to a certain extent, alleviate the engine power loss due to heat supply.…”
Section: Introductionmentioning
confidence: 99%