CN212458065U

CN212458065U - Variable-section airfoil-shaped efficient heat exchange channel for supercritical carbon dioxide PCHE

Info

Publication number: CN212458065U
Application number: CN201922117018.0U
Authority: CN
Inventors: 李红智; 杨玉; 张磊; 吴家荣; 吴帅帅
Original assignee: Xian Thermal Power Research Institute Co Ltd
Current assignee: Xian Thermal Power Research Institute Co Ltd
Priority date: 2019-12-02
Filing date: 2019-12-02
Publication date: 2021-02-02
Anticipated expiration: 2029-12-02

Abstract

The variable cross-section airfoil type efficient heat exchange channel for the supercritical carbon dioxide PCHE comprises a unit body formed by airfoil molded lines, wherein the size of the unit body is gradually changed along the flow direction by a certain proportionality coefficient, and the shape of the unit body is kept unchanged, so that a contraction type or expansion type variable flow sectional area arrangement is formed and is used for providing the flow of cold and hot fluids. The development of a thermal boundary layer can be inhibited by adopting the existing airfoil profile, the increase of flow resistance caused by enhanced heat transfer is reduced, and the comprehensive flow heat transfer performance of a heat exchange channel is improved; by aiming at different changes of density or speed of cold and hot fluid along the flow direction, an expansion or contraction type variable flow sectional area arrangement mode is pertinently adopted, so that the fluid flows at a nearly constant speed along the flow direction, the flow resistance is further reduced, and the optimal flow heat transfer comprehensive performance is achieved.

Description

Variable-section airfoil-shaped efficient heat exchange channel for supercritical carbon dioxide PCHE

Technical Field

The utility model relates to a high-efficient compact heat exchanger technical field, in particular to high-efficient heat transfer passageway of variable cross section wing section for supercritical carbon dioxide PCHE.

Background

The supercritical carbon dioxide cyclic power generation system can realize higher cyclic power generation efficiency at lower heat absorption temperature and has the characteristics of compact structure and good flexibility. The supercritical carbon dioxide cycle power generation system needs to recover heat to preheat a working medium by adopting a high-efficiency low-resistance compact heat exchanger when the heat exchange capacity is large (about 3-4 times of the generated energy), so that the energy loss is reduced, and the economical efficiency is improved. The available high-efficiency low-resistance compact heat exchangers include Printed Circuit Heat Exchangers (PCHEs) and microchannel shell-and-tube heat exchangers, which use diffusion bonding technology (diffusion bonding).

The fluid in the cold and hot flow channels of the supercritical carbon dioxide heat exchanger is in a supercritical state, and the flowing heat transfer processes of two variable-physical-property double supercritical fluids with different pressures and temperatures are mutually influenced. The physical properties of the cold and hot supercritical carbon dioxide on two sides of a flow passage of the heat exchanger, such as density, specific heat capacity and viscosity, are changed constantly, the flow rate is also changed constantly, the heat flow density in different areas between the cold and hot fluid flow passages also shows nonlinear change, particularly, the density and specific heat capacity of working media on two sides are greatly different, and the temperature pinch effect (the temperature difference of the cold and hot fluid is nearly infinite and small, so that the problems of heat transfer failure and the like) is easy to occur in the flow passage, thereby influencing the safe operation of the system. At present, the knowledge of the supercritical carbon dioxide coupling heat transfer law is insufficient, a reasonable calculation method is lacked, the characteristics are hardly considered in the existing heat exchanger heat exchange channel, and the design deviation is large.

Disclosure of Invention

In order to solve the technical problem, the utility model aims to provide a high-efficient heat transfer passageway of variable cross section wing section for supercritical carbon dioxide PCHE for the heat exchanger design is more accurate.

In order to realize the purpose, the utility model discloses a technical scheme is:

a variable cross-section wing type efficient heat exchange channel for a supercritical carbon dioxide PCHE comprises a unit body formed by wing molded lines, wherein the size of the unit body is gradually changed along the flow direction by a certain proportionality coefficient, the shape of the unit body is kept unchanged, the upper part and the lower part of the wing type unit body are respectively provided with an upper frame area and a lower frame area, and a channel with a certain depth is etched on a plate except the wing type unit body and the upper frame area and the lower frame area by adopting a photochemical etching method to form a fluid channel; adopting an expansion or contraction type arrangement mode with variable flow sectional area;

the airfoil type unit bodies can be arranged in a staggered mode or in a row mode.

The number of the airfoil type unit bodies on the cross section is kept unchanged along the flow direction, but the sizes of the unit bodies are gradually reduced to form a heat transfer plate with a gradually expanded flow sectional area, namely an expanded type arrangement form of the flow sectional area, and the airfoil type unit bodies are suitable for the condition that the fluid density is gradually reduced along the flow direction.

The number of the airfoil type unit bodies on the cross section is kept unchanged along the flow direction, but the sizes of the unit bodies are gradually increased to form heat transfer plates with gradually reduced flow sectional areas, namely, the heat transfer plates are arranged in a contraction type variable flow section, and the heat transfer plates are suitable for the condition that the fluid density is gradually increased along the flow direction.

The number of the airfoil type unit bodies on the cross section can be increased along the flow direction in the expanding type arrangement mode of the variable flow cross section, but the total flow cross section is still gradually increased.

The number of the airfoil type unit bodies on the cross section can be reduced along the flow direction in the contraction type arrangement mode of the variable flow cross section area, but the total flow cross section area is still gradually reduced.

The utility model has the advantages that:

the development of a thermal boundary layer can be inhibited by adopting the existing airfoil profile, the increase of flow resistance caused by enhanced heat transfer is reduced, and the comprehensive flow heat transfer performance of a heat exchange channel is improved;

by aiming at different changes of density or speed of cold and hot fluid along the flow direction, an expansion or contraction type variable flow sectional area arrangement mode is pertinently adopted, so that the fluid flows at a nearly constant speed along the flow direction, the flow resistance is reduced, and the optimal flow heat transfer comprehensive performance is achieved.

In general, through the innovative method, the cold and hot heat exchange channels can be specially designed according to the physical property or speed change of the supercritical carbon dioxide, so that the heat exchanger is designed more accurately, and more efficient comprehensive flowing heat transfer performance is obtained.

Drawings

FIG. 1 is a schematic view of a variable cross-section airfoil-shaped efficient heat exchange channel for heating fluid along a flow direction.

FIG. 2 is a schematic view of a variable cross-section airfoil-shaped efficient heat exchange channel in which fluid is cooled along a flow direction.

Detailed Description

The present invention will be described in further detail with reference to the accompanying drawings.

Fig. 1 and fig. 2 show a variable cross-section airfoil type efficient heat exchange channel adopted by a supercritical carbon dioxide heat exchanger. The variable cross-section airfoil type efficient heat exchange channel is characterized in that a certain specific airfoil molded line forms a unit body, the size of the unit body is gradually changed along the flow direction by a certain proportionality coefficient, and the shape of the unit body is kept unchanged, so that a variable flow cross-section area arrangement form of a contraction type from large to small or an expansion type from small to large is formed. In the case of a fluid which is cooled in the flow direction, a narrowing variable flow cross-sectional arrangement which decreases from the largest to the smallest is formed in the flow direction. For the case where the fluid is heated in the flow direction, a divergent variable flow cross-sectional arrangement that becomes smaller and larger is formed in the flow direction.

The utility model discloses a theory of operation:

the utility model provides a be applicable to high-efficient heat transfer passageway design method of supercritical carbon dioxide heat exchanger variable cross section wing section. The new method enables the cold and hot heat exchange channels to be specially designed according to the physical property or speed change of the supercritical carbon dioxide, so that the heat exchanger is more accurately designed, and more efficient comprehensive flowing heat transfer performance is obtained. The variable cross-section airfoil type efficient heat exchange channel is characterized in that a certain specific airfoil molded line forms a unit body, the size of the unit body is gradually changed along the flowing direction by a certain proportionality coefficient, the shape of the unit body is kept unchanged, and a contraction type or expansion type variable flow cross-sectional area arrangement is formed, so that the flow velocity of fluid along each cross section of the flowing direction is consistent as much as possible, and the flowing resistance is reduced.

For cold fluid (heated) fluid, the fluid density gradually decreases along the flow direction, the volume flow rate gradually increases, and an expansion arrangement is adopted; for hot (cooled) fluids, the fluid density gradually increases and the volumetric flow rate gradually decreases in the direction of flow, with a converging arrangement. The specific expansion or contraction proportionality coefficient is specially designed and determined according to different design working conditions. The development of a thermal boundary layer can be inhibited by adopting the existing airfoil profile, the increase of flow resistance caused by enhanced heat transfer is reduced, and the comprehensive flow heat transfer performance of a heat exchange channel is improved; by aiming at different changes of density or speed of cold and hot fluid along the flow direction, an expansion or contraction type variable flow sectional area arrangement mode is pertinently adopted, so that the fluid flows at a nearly constant speed along the flow direction, the flow resistance is further reduced, and the optimal flow heat transfer comprehensive performance is achieved.

Claims

1. The variable cross-section airfoil type efficient heat exchange channel for the supercritical carbon dioxide PCHE is characterized by comprising an airfoil profile forming unit body, wherein the size of the unit body is gradually changed along the flow direction by a certain proportionality coefficient, the shape of the unit body is kept unchanged, a contraction type or expansion type variable flow cross-section area arrangement is formed and is used for providing the flow of cold and hot fluids, the upper part and the lower part of the airfoil type unit body are respectively provided with an upper frame area and a lower frame area, and a channel with a certain depth is etched on a plate except the airfoil type unit body and the upper frame area and the lower frame area by adopting a photochemical etching method to form a channel of the fluids; the expansion or contraction type arrangement mode with variable flow cross section area is adopted;

2. The variable cross-section airfoil type efficient heat exchange channel for the supercritical carbon dioxide PCHE as claimed in claim 1, wherein the number of the airfoil type unit bodies on the cross section is kept unchanged along the flow direction, but the sizes of the unit bodies are gradually reduced to form heat transfer plates with gradually expanded flow cross-sectional areas, namely an expanded variable flow cross-sectional area arrangement form, which is suitable for the condition that the fluid density is gradually reduced along the flow direction.

3. The variable cross-section airfoil type efficient heat exchange channel for the supercritical carbon dioxide PCHE according to claim 1, is characterized in that the number of the airfoil type unit bodies on the cross section is kept unchanged along the flow direction, but the sizes of the unit bodies are gradually increased to form heat transfer plates with flow cross sections gradually reduced, namely, a contraction type variable flow cross section arrangement is suitable for the condition that the fluid density is gradually increased along the flow direction.

4. The variable cross-section airfoil type high-efficiency heat exchange channel for the supercritical carbon dioxide PCHE as claimed in claim 1, wherein the number of airfoil type unit bodies on the cross section can be increased along the flow direction in the expanding type variable flow cross-sectional area arrangement mode, but the total flow cross-sectional area is still gradually increased.

5. The variable cross-section airfoil type high-efficiency heat exchange channel for the supercritical carbon dioxide PCHE as claimed in claim 1, wherein the number of airfoil type unit bodies on the cross section can be reduced along the flow direction in the arrangement form of the variable flow cross-section area of the contraction type, but the total flow cross-section area is still gradually reduced.