Heat exchanger of exhaust heat recovery apparatus
11603782 · 2023-03-14
Assignee
Inventors
Cpc classification
F28F2001/027
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N3/0205
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F28F1/40
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N2470/22
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N2240/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F28F2009/226
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F28D21/0003
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N2240/20
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N13/1872
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N2260/14
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N2260/024
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y02T10/12
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
F01N13/08
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F28D7/1684
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N2470/20
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F01N3/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
The present invention relates to a heat exchanger of an exhaust heat recovery apparatus having a simple structure which is configured such that exhaust gas is evenly distributed, thereby preventing a boiling phenomenon wherein coolant water is boiling, and improving efficiency of heat exchange and durability of the apparatus.
Claims
1. A heat exchanger of an exhaust heat recovery apparatus comprising: a housing extending in one direction, with both sides thereof being opened to allow exhaust gas to be introduced from one side thereof and discharged to the other side thereof; at least two tube parts spaced apart from each other at a predetermined distance in a height direction while being accommodated inside the housing to form a flow path in a direction in which the housing extends to allow the exhaust gas introduced from the one side of the housing to pass therethrough; an exhaust gas inlet formed in a lower portion of the one side of the housing; an exhaust gas outlet formed in a lower portion of the other side of the housing and having a smaller area than the exhaust gas inlet; a coolant inlet formed in a side surface of the housing to introduce coolant between the tube parts; and a coolant outlet formed in the side surface of the housing to discharge the coolant introduced between the tube parts, wherein one end of the exhaust gas inlet is opened and the exhaust gas outlet has an end portion formed at the other side thereof to be closed.
2. The heat exchanger of the exhaust heat recovery apparatus of claim 1, further comprising a baffle fixing the plurality of tube parts to be spaced apart from each other and extending a flow path for the coolant introduced through the coolant inlet and discharged through the coolant outlet.
3. The heat exchanger of the exhaust heat recovery apparatus of claim 2, wherein the baffle includes: a support portion extending in one direction to be disposed in the height direction of the housing; and a plurality of extension portions extending in a direction perpendicular to the direction in which the support portion extends, while being spaced apart from each other at a predetermined distance along the support portion, to be inserted into spaces between the tube parts.
4. The heat exchanger of the exhaust heat recovery apparatus of claim 1, wherein a parallel distance from the exhaust gas inlet to a tube part farthest away therefrom is no more than 1.5 times a one-side width of the exhaust gas inlet.
5. The heat exchanger of the exhaust heat recovery apparatus of claim 4, wherein the exhaust gas inlet has an area that is no less than 99% and no more than 105% of a sum of inlet end areas of the plurality of tube parts.
6. The heat exchanger of the exhaust heat recovery apparatus of claim 1, wherein the exhaust gas outlet has an area that is 70% or more of that of the exhaust gas inlet.
7. The heat exchanger of the exhaust heat recovery apparatus of claim 1, wherein the coolant inlet is formed at a lower position than the coolant outlet on the basis of the gravity direction.
8. The heat exchanger of the exhaust heat recovery apparatus of claim 1, wherein a coolant flow path formed by a space between the tube parts adjacent to each other and a coolant flow path formed by a space between the housing and the tube part are identical to each other in height.
9. The heat exchanger of the exhaust heat recovery apparatus of claim 8, wherein each of the coolant flow paths has a height that is no less than 95% and no more than 100% of a value obtained by dividing an inner diameter of the coolant inlet by a total number of coolant flow paths.
10. The heat exchanger of the exhaust heat recovery apparatus of claim 1, wherein each of the tube parts includes a plurality of fins spaced apart from each other at a predetermined distance in a width direction of the housing, with first waves curved in one direction and second waves curved in the opposite direction being repeatedly formed, while extending in the direction in which the housing extends and in the height direction.
11. The heat exchanger of the exhaust heat recovery apparatus of claim 10, wherein the number of repetitions of first waves and second waves is 13 to 15 per 100 mm in length of each of the fins.
12. The heat exchanger of the exhaust heat recovery apparatus of claim 10, wherein the fins extend to be 6 to 8 mm in the height direction.
13. The heat exchanger of the exhaust heat recovery apparatus of claim 10, wherein a parallel distance from end points of the first waves to end points of the second waves of another adjacent fin is 0.20 to 0.25 mm.
14. The heat exchanger of the exhaust heat recovery apparatus of claim 10, wherein the first waves have a curvature radius of 3.8 to 4.2 mm, and the second waves have a curvature radius of 2.5 to 2.9 mm.
15. The heat exchanger of the exhaust heat recovery apparatus of claim 3, wherein the housing includes a first housing and a second housing that are assembled together.
16. The heat exchanger of the exhaust heat recovery apparatus of claim 15, wherein the first housing and the second housing are assembled together by inserting an end of the second housing into an end of the first housing, and the support portion is located at a position where the ends of the first housing and the second housing overlap each other to contact an inner surface of the second housing.
17. An exhaust heat recovery apparatus comprising: the heat exchanger of the exhaust heat recovery apparatus of claim 1; an outer housing in which the heat exchanger of the exhaust heat recovery apparatus is accommodated; and a valve installed inside the outer housing to control the exhaust gas to be introduced into or blocked from the heat exchanger of the exhaust heat recovery apparatus depending on an operation mode.
Description
DESCRIPTION OF DRAWINGS
(1)
(2)
(3)
(4)
(5)
(6)
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(8)
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BEST MODE
(10) Hereinafter, a heat exchanger of an exhaust heat recovery apparatus according to a preferred exemplary embodiment of the present invention will be described in detail with reference to the accompanying drawings.
First Exemplary Embodiment
(11)
(12) As illustrated in
(13) As illustrated in
(14) As illustrated in
(15) As illustrated in
(16)
(17) As illustrated in
(18) A space between the tube parts 200 spaced apart from each other at the predetermined distance as illustrated in
(19) The coolant is heated by exchanging heat with the exhaust gas passing through adjacent tube parts 200 while being introduced into and discharged from the space between the tube parts 200, thereby obtaining heat for heating during an initial operation of an engine in winter.
(20) As illustrated in
(21) As illustrated in
(22) The baffle 700 is provided not only for the plurality of tube parts 200 to be spaced apart from each other at the predetermined distance in the Z-axis direction, like the connectors 220, but also to set a flow path allowing the coolant to be introduced from the left side thereof and discharged to the right side thereof on the basis of the X-axis direction. As illustrated in
(23) As illustrated in
(24) As illustrated in
(25) Since the extension portions 720 are spaced apart from each other at the predetermined distance along the direction in which the support portion 710 extends, spaces are formed between adjacent extension portions 720. The side surfaces of the tube parts 200 are inserted into the spaces between the adjacent extension portions 720, thereby fixing the plurality of tube parts 200 to be spaced apart from each other at the predetermined distance in the height direction.
(26) An extending length of the extension portion 720 is shorter than a Y-axis length of the tube part 200. This is for the extension portion 720 to set and expand the coolant flow path so that the coolant and the exhaust gas may exchange heat with each other for a longer period of time. That is, the extension portion 720 makes it possible to form a coolant introducing space and a coolant discharging space on the left side and on the right side, respectively, on the basis of the X-axis direction, so that the coolant may flow in a “U” shape on and under the tube part 200.
(27)
(28) As illustrated in
(29) As illustrated in
(30) The first wave 211 and the second wave 212 are provided to prolong a period of time for which the exhaust gas passes through the inside of the tube part 200, thereby increasing heat exchange efficiency.
(31) The first wave 211 and the second wave 212 illustrated in
(32) The number of repetitions of first waves 211 and second waves 212 formed on each of the fins 210 illustrated in
(33) Since 13 to 15 first waves 211 and second wave 212 are repeatedly formed per 100 mm in length of each of the fins 210, a length of one cycle (a first wave and a second wave) may be 6.6 to 7.6 mm, and the length of one cycle in the present exemplary embodiment may be about 7 mm.
(34) A Y-axis distance W1 (parallel distance) from end points of the first waves 211 to end points of the second waves 212 as illustrated in
(35) The reason for specifically limiting the numerical values of the tube part 200 as described above is to improve the flow and the heat exchange efficiency of the exhaust gas inside the tube part 200.
(36) As illustrated in
(37) As illustrated in
(38) As illustrated in
(39) As illustrated in
(40) As illustrated in
(41)
(42) As illustrated in
(43) On the other hand, since the exhaust gas outlet 400 is a part for discharging the heat-exchanged exhaust gas, which has already been distributed, through the other ends of the tube parts 200, the other end of the exhaust gas outlet 400 is closed, while the inner wall of the outer housing of the exhaust heat recovery apparatus also serves as a guide partition when the exhaust gas having passed through the tube parts 200 flows into the exhaust gas outlet 400. That is, according to the present invention, the exhaust gas inlet 300 and the exhaust gas outlet 400 are asymmetric with different shapes.
(44) Referring to
(45) The exhaust gas outlet 400 illustrated in
(46) The exhaust gas inlet 300 may have an area that is no less than 99% and no more than 105% of a sum of inlet end areas of the plurality of tube parts 200.
(47)
(48) As illustrated in
(49) Each of the coolant flow paths 20 illustrated in
Second Exemplary Embodiment
(50) Hereinafter, a heat exchanger of an exhaust heat recovery apparatus according to a second exemplary embodiment of the present invention will be described in detail with reference to the accompanying drawings.
(51) The difference of the heat exchanger of the exhaust heat recovery apparatus according to the second exemplary embodiment of the present invention from that according to the first exemplary embodiment of the present invention is the housing 100. The other parts, excluding the housing 100 and the components associated therewith, are identical between the first exemplary embodiment and the second exemplary embodiment, and therefore, the description thereof is omitted.
(52)
(53) As illustrated in
(54) As illustrated in
(55)
(56) As illustrated in
(57) In the heat exchanger of the exhaust heat recovery apparatus according to the second exemplary embodiment of the present invention, the reason why the center portion of the housing 100 has a triple structure as described above is that there is a problem that when rapid external cooling occurs in a state where the heat exchanger overheats, the heat exchanger may be damaged due to deformation such as swelling. Therefore, the durability of the heat exchanger is improved by configuring the center portion of the heat exchanger in a triple-overlap structure.
(58)
(59) As illustrated in
(60) The outer housing 40 serves to guide the exhaust gas and to accommodate the heat exchanger 10 of the exhaust heat recovery apparatus therein as described above, and forms a separate exhaust gas flow path 30 connected in parallel with the flow path in the heat exchanger 10 of the exhaust heat recovery apparatus.
(61) Referring to
(62)
(63)
(64) The present invention is not limited to the above-described exemplary embodiments, and may be applied in a wide range and variously modified without departing from the gist of the present invention claimed in the claims.
DESCRIPTION OF REFERENCE NUMERALS
(65) 10: heat exchanger for exhaust heat recovery apparatus 20: coolant flow path 30: exhaust gas flow path 40: outer housing 50: exhaust gas controller 100: housing 110: first housing 120: second housing 200: tube part 210: fin 211: first wave 212: second wave 220: connector 300: exhaust gas inlet 400: exhaust gas outlet 500: coolant inlet 600: coolant outlet 700: baffle 710: support portion 720: extension portion