FR2591728A1 - Heat exchanger, particularly for internal combustion engine - Google Patents
Heat exchanger, particularly for internal combustion engine Download PDFInfo
- Publication number
- FR2591728A1 FR2591728A1 FR8518475A FR8518475A FR2591728A1 FR 2591728 A1 FR2591728 A1 FR 2591728A1 FR 8518475 A FR8518475 A FR 8518475A FR 8518475 A FR8518475 A FR 8518475A FR 2591728 A1 FR2591728 A1 FR 2591728A1
- Authority
- FR
- France
- Prior art keywords
- exchanger
- fluid
- fluids
- heat exchanger
- internal combustion
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F9/00—Casings; Header boxes; Auxiliary supports for elements; Auxiliary members within casings
- F28F9/22—Arrangements for directing heat-exchange media into successive compartments, e.g. arrangements of guide plates
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F9/00—Casings; Header boxes; Auxiliary supports for elements; Auxiliary members within casings
- F28F9/22—Arrangements for directing heat-exchange media into successive compartments, e.g. arrangements of guide plates
- F28F2009/222—Particular guide plates, baffles or deflectors, e.g. having particular orientation relative to an elongated casing or conduit
- F28F2009/226—Transversal partitions
Abstract
Description
ECHANGEUR THERMIQUE, NOTAMMENT POUR MOTEUR A
COMBUSTION INTERNE.HEAT EXCHANGER, ESPECIALLY FOR A MOTOR
INTERNAL COMBUSTION.
La présente invention se rapporte à la conception d' un échangeur thermique utilisable en particulier pour les moteurs à combustion interne.The present invention relates to the design of a heat exchanger which can be used in particular for internal combustion engines.
Dans les échangeurs de type connu, le fluide refroidisseur circule à l'intérieur de tubes, ceux-ci formant un faisceau caractérisant le type ou modèle de 1' échangeur. Le fluide à refroidir est canalisé dans la partie externe de ces tubes et généralement, le sens d' écoulement des fluides est croisé pour accroître 1' efficacité thermique.In exchangers of known type, the coolant circulates inside tubes, these forming a bundle characterizing the type or model of one exchanger. The fluid to be cooled is channeled into the external part of these tubes and generally, the direction of flow of the fluids is crossed to increase thermal efficiency.
L' efficacité thermique d' un échangeur dépend essentiellement - de la nature, géométrie et disDosition des tubes formant le faisceau ; - de la forme et importance du volume délimité par la partie externe
des tubes - et de l' organisation du sens d' écoulement du fluide refroidisseur et
fluide à refroidir.The thermal efficiency of an exchanger essentially depends on - the nature, geometry and arrangement of the tubes forming the bundle; - the shape and size of the volume delimited by the external part
tubes - and the organization of the direction of flow of the coolant and
fluid to cool.
un un des buts de la présente invention est précisément d'organiser méthodiquement le sens d' écoulement des fluides afin d'obtenir d' obtenir - une vitesse optimale des fluides, facteur caractérisant la valeur du
coefficient d' échange thermique fluide-parois - et une différence de température maximale entre fluide à
refroidir et fluide refroidisseur.one of the aims of the present invention is precisely to organize methodically the direction of flow of the fluids in order to obtain an optimal speed of the fluids, a factor characterizing the value of the
fluid-wall heat exchange coefficient - and a maximum temperature difference between fluid at
cool and coolant.
Généralement, ces deux conditions imposent - un débit important du fluide refroidisseur - et un sens d'écoulement dit "à courant croisé", ce qui amène
généralement sur l' ensemble échangeur
des orifices entrée et sortie de fluide disposés aux extrémités du
faisceau d' échangeur expliquant une modification de leurs implantations
dès qu'il y a changement du faisceau d' échangeur imposé notamment
par une exigence différente de puissance cie refroidissement.Generally, these two conditions impose - a large flow rate of the coolant - and a direction of flow called "cross-current", which brings
generally on the exchanger assembly
fluid inlet and outlet ports disposed at the ends of the
exchanger bundle explaining a modification of their locations
as soon as there is a change in the heat exchanger harness imposed in particular
by a different requirement of cooling power.
Pour pallier ces exigences, la présente invention présente une solution selon laquelle, suivant une particularité essentielle, - l' ensemble des orifices sortie et entrée des fluides est situé sur une
même face ou extrémité de l' échangeur ; - il est possible de modifier la taille du faisceau sans conséquences au
niveau des implantations de ces orifices ; - une cloison médiane séDare cet échangeur en deux demi-échangeurs
couplés en série pour organiser la circulation des fluides ; - et cette cloison est calorifugée pour éviter un transfert thermique du
fluide à refroidir.To overcome these requirements, the present invention presents a solution according to which, according to an essential characteristic, - the assembly of the outlet and inlet ports for the fluids is located on a
same face or end of the exchanger; - it is possible to modify the size of the beam without consequences
level of the locations of these orifices; - a central partition separates this exchanger into two half-exchangers
coupled in series to organize the circulation of fluids; - and this partition is insulated to avoid thermal transfer of the
fluid to cool.
Suivant une autre particularité de l'invention, cet échangeur thermique comporte un clapet monté sur cette cloison médiane pour éviter à ce fluide à refroidir, toute chute de pression importante.According to another feature of the invention, this heat exchanger includes a valve mounted on this central partition to prevent this fluid to cool, any significant pressure drop.
D' autres buts, particularités et avantages de l' invention apparaîtront plus clairement à la lecture de la description qui suit de deux modes de réalisation- préférés, donnés à titre d' exemples non limitatifs en référence aux dessins annexés dans lesquels - la figure 1 représente une vue en coupe axiale cl' un échangeur
thermique suivant un premier mode de réalisation ; - les figures 2, 3 et 4 représentent trois sections droites respectives de
cet échangeur thermique suivant les plans A-A, B-B et C-C de la
figure 1 ; - et les figures 5, 6 et 7 représentent trois sections droites respectives
d' un second mode de réalisation de cet échangeur, suivant les mêmes
plans 4-A, 9-B et C-C.Other objects, features and advantages of the invention will appear more clearly on reading the following description of two preferred embodiments, given by way of nonlimiting examples with reference to the appended drawings in which - Figure 1 shows an axial sectional view of an exchanger
thermal according to a first embodiment; - Figures 2, 3 and 4 show three respective cross sections of
this heat exchanger according to the plans AA, BB and CC of the
figure 1 ; - And Figures 5, 6 and 7 show three respective cross sections
of a second embodiment of this exchanger, according to the same
plans 4-A, 9-B and CC.
L' ensemble échangeur de la figure l présente un carter externe l et un orifice d'entrée 2 qui permet au fluide refroidisseur d'atteindre un faisceau tubulaire 3. Le nombre de tubes de ce faisceau qui est défini pour claque tyne d' échangeur, est divisé en deux parties égales, une première moitié assurant le passage du fluide de l' entrée 2 vers une partie d' extrémité 4 du faisceau tubulaire.Le fluide refroidisseur ernprunte l' autre moitié des tubes pour etre dirigé vers un orifice de sortie 5. r,e fluide à refroidir pénètre dans l'échangeur par un orifice 6 et se voit diriger vers la partie de l' échangeur (figures 3 et 6, section B-9), délimitée par une cloison médiane 7 du faisceau 3 et le carter externe 1. Ce fluide circule entre les tubes formant la moitié du faisceau ramenant le fluide refroidisseur de la partie 4 vers l'orifice de sortie 5.The exchanger assembly of FIG. 1 has an external casing l and an inlet orifice 2 which allows the cooling fluid to reach a tube bundle 3. The number of tubes of this bundle which is defined for each type of exchanger, is divided into two equal parts, a first half ensuring the passage of the fluid from the inlet 2 to an end portion 4 of the tube bundle. The cooling fluid ernprunts the other half of the tubes to be directed to an outlet orifice 5 r, e fluid to cool enters the exchanger through an orifice 6 and is directed towards the part of the exchanger (Figures 3 and 6, section B-9), delimited by a central partition 7 of the bundle 3 and the external casing 1. This fluid circulates between the tubes forming half of the bundle bringing the coolant from part 4 to the outlet orifice 5.
Pour accélérer et organiser le courant du fluide à refroidir selon l'invention, des cloisons 8 sont disposées de part et d' autre de la cloison médiane 7. Le nombre de ces cloisons est défini pour chaque type d' échangeur. Le passage du fluide à refroidir de la première moitié vers la seconde moitié du faisceau tubulaire se fait au niveau d' un orifice 9 (figures 4 et 7, section C-C). Ensuite, le fluide à refroidir circule entre les tubes formant le demi-faisceau canalisant le fluide refroidisseur de I' orifice d' entrée 2 vers la partie 4. Comme précédemment, des cloisons
S assurent une circulation rnéthodique du fluide de l'orifice 9 vers une sortie 10.To accelerate and organize the flow of the fluid to be cooled according to the invention, partitions 8 are arranged on either side of the central partition 7. The number of these partitions is defined for each type of exchanger. The passage of the fluid to be cooled from the first half to the second half of the tube bundle takes place at the level of an orifice 9 (FIGS. 4 and 7, section CC). Then, the fluid to be cooled circulates between the tubes forming the half-beam channeling the coolant from the inlet orifice 2 to the part 4. As before, partitions
S ensure a methodical circulation of the fluid from the orifice 9 to an outlet 10.
Une autre particularité de l'invention est obtenue par le mode de réalisation de la cloison médiane 7. Cette dernière est réalisée à l'aide d'iin matériau susceptible d' assurer une isolation thermiaue afin que que le liquide à refroidir ne puisse transférer thermiquement par conduction au travers de la cloison médiane 7. Another particular feature of the invention is obtained by the embodiment of the central partition 7. The latter is produced using a material capable of providing thermal insulation so that the liquid to be cooled cannot heat transfer by conduction through the middle partition 7.
Suivant une autre particularité de l'invention, un clapet Il peut être monté sur la cloison médiane 7. Le rôle de ce clapet est de permettre le by-pass du fluide à refroidir dans le cas où ce dernier étant à basse température présente une viscosité élevée et, par là, entraîne une perte de pression importante par le passage obligé au travers du faisceau tubulaire. According to another particular feature of the invention, a valve It can be mounted on the central partition 7. The role of this valve is to allow the by-pass of the fluid to be cooled in the case where the latter being at low temperature has a viscosity high and thereby causes a significant pressure loss by the forced passage through the tube bundle.
Claims (2)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR8518475A FR2591728B1 (en) | 1985-12-13 | 1985-12-13 | HEAT EXCHANGER, ESPECIALLY FOR AN INTERNAL COMBUSTION ENGINE |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR8518475A FR2591728B1 (en) | 1985-12-13 | 1985-12-13 | HEAT EXCHANGER, ESPECIALLY FOR AN INTERNAL COMBUSTION ENGINE |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2591728A1 true FR2591728A1 (en) | 1987-06-19 |
FR2591728B1 FR2591728B1 (en) | 1989-05-19 |
Family
ID=9325752
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR8518475A Expired FR2591728B1 (en) | 1985-12-13 | 1985-12-13 | HEAT EXCHANGER, ESPECIALLY FOR AN INTERNAL COMBUSTION ENGINE |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR2591728B1 (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0428920A1 (en) * | 1989-11-17 | 1991-05-29 | Behr GmbH & Co. | Oil-cooler |
GB2424945A (en) * | 2005-03-16 | 2006-10-11 | Detroit Diesel Corp | Two pass heat exchanger |
Citations (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1648646A (en) * | 1926-06-22 | 1927-11-08 | Newton Process Mfg Co | Heat exchanger |
US1722109A (en) * | 1927-10-26 | 1929-07-23 | Foster Wheeler Corp | Heat-exchange apparatus |
US2352704A (en) * | 1939-11-24 | 1944-07-04 | Serck Radiators Ltd | Oil cooler |
US2419634A (en) * | 1942-09-03 | 1947-04-29 | United Aircraft Prod | Congealable liquid conditioning device |
FR1066418A (en) * | 1952-11-10 | 1954-06-04 | Chausson Usines Sa | heat exchanger in particular for aircraft and similar applications |
GB1187366A (en) * | 1968-03-12 | 1970-04-08 | Westinghouse Electric Corp | Heat Exchanger |
US3958630A (en) * | 1975-01-24 | 1976-05-25 | Exxon Research And Engineering Company | Heat exchanger baffle arrangement |
DE2543074A1 (en) * | 1974-12-20 | 1976-06-24 | Modine Mfg Co | HEAT EXCHANGER |
US4029145A (en) * | 1976-03-05 | 1977-06-14 | United Aircraft Products, Inc. | Brazeless heat exchanger of the tube and shell type |
-
1985
- 1985-12-13 FR FR8518475A patent/FR2591728B1/en not_active Expired
Patent Citations (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1648646A (en) * | 1926-06-22 | 1927-11-08 | Newton Process Mfg Co | Heat exchanger |
US1722109A (en) * | 1927-10-26 | 1929-07-23 | Foster Wheeler Corp | Heat-exchange apparatus |
US2352704A (en) * | 1939-11-24 | 1944-07-04 | Serck Radiators Ltd | Oil cooler |
US2419634A (en) * | 1942-09-03 | 1947-04-29 | United Aircraft Prod | Congealable liquid conditioning device |
FR1066418A (en) * | 1952-11-10 | 1954-06-04 | Chausson Usines Sa | heat exchanger in particular for aircraft and similar applications |
GB1187366A (en) * | 1968-03-12 | 1970-04-08 | Westinghouse Electric Corp | Heat Exchanger |
DE2543074A1 (en) * | 1974-12-20 | 1976-06-24 | Modine Mfg Co | HEAT EXCHANGER |
US3958630A (en) * | 1975-01-24 | 1976-05-25 | Exxon Research And Engineering Company | Heat exchanger baffle arrangement |
US4029145A (en) * | 1976-03-05 | 1977-06-14 | United Aircraft Products, Inc. | Brazeless heat exchanger of the tube and shell type |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0428920A1 (en) * | 1989-11-17 | 1991-05-29 | Behr GmbH & Co. | Oil-cooler |
GB2424945A (en) * | 2005-03-16 | 2006-10-11 | Detroit Diesel Corp | Two pass heat exchanger |
Also Published As
Publication number | Publication date |
---|---|
FR2591728B1 (en) | 1989-05-19 |
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CA | Change of address | ||
CD | Change of name or company name | ||
CJ | Change in legal form |