FR2683856A1 - Heat engine with four supplemented stroke cycle. Gain in power by reintroduction, to the cycle, of the exhaust gases, and conversion of their energy into a motive force - Google Patents
Heat engine with four supplemented stroke cycle. Gain in power by reintroduction, to the cycle, of the exhaust gases, and conversion of their energy into a motive force Download PDFInfo
- Publication number
- FR2683856A1 FR2683856A1 FR9114159A FR9114159A FR2683856A1 FR 2683856 A1 FR2683856 A1 FR 2683856A1 FR 9114159 A FR9114159 A FR 9114159A FR 9114159 A FR9114159 A FR 9114159A FR 2683856 A1 FR2683856 A1 FR 2683856A1
- Authority
- FR
- France
- Prior art keywords
- energy
- chamber
- gases
- cycle
- turbo
- 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
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B41/00—Engines characterised by special means for improving conversion of heat or pressure energy into mechanical power
- F02B41/02—Engines with prolonged expansion
- F02B41/06—Engines with prolonged expansion in compound cylinders
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B75/00—Other engines
- F02B75/02—Engines characterised by their cycles, e.g. six-stroke
- F02B2075/022—Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle
- F02B2075/027—Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle four
Abstract
Description
MOTEUR THERMIQUE cycle à 4 temps complétés
La présente invention a pour objet l'augmentation du rendement thermodynamique dans un moteurthermique cycle à 4temps par l'utilisation dans le cycle, de l'énergie cinétique des gaz d'échappement et la transformation de cette énergie en force motrice.THERMAL ENGINE 4-cycle cycle completed
The object of the present invention is to increase the thermodynamic efficiency in a 4-stroke cycle thermal engine by the use in the cycle of the kinetic energy of the exhaust gases and the transformation of this energy into a driving force.
Dans les moteurs de conception classique, les gaz rejetés dans l'atmosphère représentent une perte de 35% de l'énergie produite par la combustion du carburant, perte supérieure à l'énergie motrice utilisée estimée à 25 % environ, I'énergie restante étant dissipée en rayonnement refroidissement, et entrainement mécanique des différents équipements propres au moteur. In engines of conventional design, the gases released into the atmosphere represent a loss of 35% of the energy produced by the combustion of the fuel, a loss greater than the driving energy used estimated at around 25%, the remaining energy being dissipated in cooling radiation, and mechanical drive of the various equipment specific to the engine.
Dans le moteur conforme à l'invention la nouveauté porte sur la création, à la base des cylindres d'une chambre secondaire dans laquelle les gaz arrivant à vitesse élevée de la chambre d'explosion agissent sur le fond du piston, ou leur énergie cinétique se transforme, en force motrice; les gaz rejetés pouvant être dirigés vers un turbo-générateur d'électricité pour utilisation totale de l'énergie restante. In the engine according to the invention the novelty relates to the creation, at the base of the cylinders of a secondary chamber in which the gases arriving at high speed from the explosion chamber act on the bottom of the piston, or their kinetic energy turns into a driving force; the exhaust gases can be directed to a turbo-generator of electricity for total use of the remaining energy.
II y a lieu de préciser que, les quatre temps du cycle étant conservés, le mécanisme de commande des soupapes dans la partie haute des cylindres reste inchangé, le fonctionnement de l'ensemble demeure donc conforme aux techniques actuellement développées. It should be noted that, the four cycle times being preserved, the valve control mechanism in the upper part of the cylinders remains unchanged, the operation of the assembly therefore remains in accordance with the techniques currently developed.
Les dessins annexés sur planches 1/2 et 2/2 illustrent l'invention. The accompanying drawings on plates 1/2 and 2/2 illustrate the invention.
PI 1/2 La figure 1 représente, selon l'invention, le cylindre moteur vu en
coupe sur deux plans précisés en B.B. sur figure 4 PI. 2/2.PI 1/2 Figure 1 shows, according to the invention, the engine cylinder seen in
section on two planes specified in BB on figure 4 PI. 2/2.
La figure 2 représente ie bloc cylindre, vu en coupe suivant A.A.,
avec, au centre la culasse inférieure, les entrées et sortie des gaz et
la prise d'air de balayage. FIG. 2 represents the cylinder block, seen in section along AA,
with, in the center the lower cylinder head, the gas inlets and outlets and
the purge air intake.
PI 2/2 La figure 3 est une représentation graphique du cycle à 4temps
selon l'invention.PI 2/2 Figure 3 is a graphical representation of the 4-stroke cycle
according to the invention.
La figure 4 est la représentation schématique d'un ensemble moteur
turbo-générateur selon l'invention.Figure 4 is a schematic representation of an engine assembly
turbo generator according to the invention.
En référence à ces dessins l'invention s'explique de la façon suivante. With reference to these drawings, the invention can be explained as follows.
L'évacuation des gaz de la chambre principale (chambre d'explosion) 1 s'effectuera par la plus large ouverture admissible, deux soupapes par exemple,afin qu'ils acquièrent, dès leur sortie, la plus grande vitesse possible; ils seront alors transférés dans la chambre secondaire 2 située à la base du cylindre, par une tubulure 3 de forme, de section, et en un matériau tels qu'ils ne devront subir que très peu de perte en vitesse et température. The gases from the main chamber (explosion chamber) 1 are evacuated by the widest admissible opening, two valves for example, so that they acquire, as soon as they exit, the highest possible speed; they will then be transferred to the secondary chamber 2 located at the base of the cylinder, by a tube 3 of shape, section, and of a material such that they should only suffer very little loss in speed and temperature.
La culasse 4 formant cette chambre comportera une gouttière d'entrée 5 dont le profil sera étudié de façon que les gaz arrivant par 8 soient dirigés vers le fond du piston sur lequel ils exerceront une forte poussée en direction du point mort haut, ils y perdront sous forme de travail moteur, une grande partie de leur énergie et seront renvoyés, par inversion, vers la gouttière de sortie 6 et l'ouverture déchappement 9 puis dirigés par le collecteur Il soit vers un turbo-générateur d'électricité dans lequel ils céderont utilement le reste de leur force vive, soit à l'air libre, par pot d'échappement interposé. The cylinder head 4 forming this chamber will include an inlet gutter 5 whose profile will be studied so that the gases arriving by 8 are directed towards the bottom of the piston on which they will exert a strong thrust towards the top dead center, they will lose there in the form of engine work, a large part of their energy and will be returned, by inversion, to the outlet gutter 6 and the exhaust opening 9 then directed by the collector It is to a turbo-generator of electricity in which they will yield usefully the rest of their live force, either in the open air, by interposed exhaust.
Afin d'assurer le balayage de la chambre secondaire 2 une entrée d'air 10 sera prévue dans le bloc cylindre, à l'opposé des entrées 8 et sortie 9 des gaz chauds et en correspondance avec une encoche 7 prévue dans la culasse 4 pour assurer la répartition de l'airs aspiré
Cette prise d'air sera fermée à toute pression intérieure par un clapet à ressort 12 qui ne s'ouvrira, par dépression dans la chambre 2 que lors de la remontée du piston vers le point mort haut. (temps compression) manoeuvre d'ouverture assistée, si besoin était, par commande électro magnétique ou autre afin de favoriser l'entrée de l'air. In order to ensure the sweeping of the secondary chamber 2, an air inlet 10 will be provided in the cylinder block, opposite the hot gas inlets 8 and outlet 9 and in correspondence with a notch 7 provided in the cylinder head 4 for ensure the distribution of air sucked
This air intake will be closed at any internal pressure by a spring valve 12 which will only open, by vacuum in the chamber 2, when the piston is raised to top dead center. (compression time) assisted opening maneuver, if necessary, by electromagnetic or other control in order to favor the entry of air.
Le dispositif mécanique autorisant, selon l'invention le plein emploi de la puissance des gaz dits d'échappement est représenté schématiquement sur fig.1 PL. 1/2, il est de conception technique classique; le piston n'étant plus soumis qu'à des efforts axiaux peut ne pas comporter de jupe sa hauteur sera suffisante pour y situer les segments indispensables à l'étanchéité, à la lubrification, et pour les deux extrêmes, résister à la chaleur du fait des températures élevées dans chacune des deux chambres. The mechanical device according to the invention allowing full use of the power of the so-called exhaust gases is shown diagrammatically in FIG. 1 PL. 1/2, it is of classic technical design; the piston being no longer subjected to axial forces may not have a skirt its height will be sufficient to locate the segments essential for sealing, lubrication, and for the two extremes, to resist heat due to the fact high temperatures in each of the two rooms.
La culasse 4fera corps avec la glissière de pied de bielle. Elle comportera, en son centre une chambre à joints d'étanchéité 13 sans pour autant servir de guidage à la tige du piston qui la traverse, tige tubulaire qui assurera le transfert de l'huile de graissage au piston
Le graphique représenté fig.3 PL 212 précise pour chacun des quatre temps les opérations respectives dans chacune des deux chambres; les courbes ne sont qu'indicatives pour chaque fonction, sans précision quant aux valeurs.The cylinder head 4 will form a body with the connecting rod slide. It will include, in its center a chamber with seals 13 without serving as a guide for the piston rod which passes through it, tubular rod which will ensure the transfer of the lubricating oil to the piston
The graph shown in fig. 3 PL 212 specifies for each of the four times the respective operations in each of the two chambers; the curves are only indicative for each function, without specifying the values.
La cote X figure l'angle de rotation du vilebrequin entre le point d'ouverture de la soupape d'échappement et sa position au moment où les gaz prennent contact avec le fond du piston. Dimension X represents the angle of rotation of the crankshaft between the point of opening of the exhaust valve and its position when the gases make contact with the bottom of the piston.
Pour un fonctionnement correct, la poussée des gaz sur la face inférieure du piston ne devra s'effectuer qu'au cours de sa remontée vers le point mort haut, régime ralenti inclus, I'angle d'avance à l'échappement sera déterminé en conséquence. For correct operation, the thrust of the gases on the underside of the piston should only take place during its ascent to top dead center, idle speed included, the angle of advance to the exhaust will be determined in result.
L'emploi des technologies nouvelles et produits nouveaux, les céramiques par exemple, ne pourront qu'accroître les performances du moteur réalisé selon l'invention. The use of new technologies and new products, ceramics for example, can only increase the performance of the engine produced according to the invention.
La figure 4 PL. 2/2 schématise à titre d'exemple un ensemble moteur turbogénérateur (2 blocs bi-cylindres à 90 ): dans cette version, la réalisation de certains éléments du turbo (éléments mobiles, fixes, ou spécialement ajoutés) en des matériaux catalyseurs peut assurer une moindre nocivité des gaz résiduels à leur sortie dans l'atmosphère. Figure 4 PL. 2/2 schematically shows, for example, a turbogenerator engine assembly (2 twin-cylinder blocks at 90): in this version, the production of certain elements of the turbo (mobile, fixed, or specially added elements) in catalyst materials can ensure less harmful residual gases when they exit the atmosphere.
Claims (4)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR9114159A FR2683856B1 (en) | 1991-11-18 | 1991-11-18 | FULL-TIME 4-CYCLE HEAT ENGINE. GAIN OF POWER BY REINTRODUCTION, INTO THE CYCLE, OF EXHAUST GASES AND TRANSFORMATION OF THEIR ENERGY INTO MOTOR FORCE. |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR9114159A FR2683856B1 (en) | 1991-11-18 | 1991-11-18 | FULL-TIME 4-CYCLE HEAT ENGINE. GAIN OF POWER BY REINTRODUCTION, INTO THE CYCLE, OF EXHAUST GASES AND TRANSFORMATION OF THEIR ENERGY INTO MOTOR FORCE. |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2683856A1 true FR2683856A1 (en) | 1993-05-21 |
FR2683856B1 FR2683856B1 (en) | 1993-12-31 |
Family
ID=9419031
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR9114159A Expired - Fee Related FR2683856B1 (en) | 1991-11-18 | 1991-11-18 | FULL-TIME 4-CYCLE HEAT ENGINE. GAIN OF POWER BY REINTRODUCTION, INTO THE CYCLE, OF EXHAUST GASES AND TRANSFORMATION OF THEIR ENERGY INTO MOTOR FORCE. |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR2683856B1 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2010119246A1 (en) * | 2009-04-18 | 2010-10-21 | Richard Lloyd Leslie Daniel | Internal combustion engine |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB276087A (en) * | 1925-12-01 | 1927-09-01 | Henry Ernest Le Mesurier | Improvements in the construction and method of working internal combustion engines |
FR1021084A (en) * | 1949-07-07 | 1953-02-13 | Further training in internal combustion and internal combustion engines | |
FR1068152A (en) * | 1952-11-27 | 1954-06-23 | Snecma | Motor with variable characteristics |
US3075507A (en) * | 1960-03-17 | 1963-01-29 | John L Betzen | Quadruple acting internal combustion engines |
FR2413547A1 (en) * | 1977-12-29 | 1979-07-27 | Ruyer Charles | IMPROVED REDUCED LOAD OPERATING CYCLE FOR FOUR STROKE EXPLOSION ENGINES AND ENGINES USING THIS CYCLE |
GB2062112A (en) * | 1979-10-17 | 1981-05-20 | Dornier C | Device for Utilization of Residual Energy in Machinery |
-
1991
- 1991-11-18 FR FR9114159A patent/FR2683856B1/en not_active Expired - Fee Related
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB276087A (en) * | 1925-12-01 | 1927-09-01 | Henry Ernest Le Mesurier | Improvements in the construction and method of working internal combustion engines |
FR1021084A (en) * | 1949-07-07 | 1953-02-13 | Further training in internal combustion and internal combustion engines | |
FR1068152A (en) * | 1952-11-27 | 1954-06-23 | Snecma | Motor with variable characteristics |
US3075507A (en) * | 1960-03-17 | 1963-01-29 | John L Betzen | Quadruple acting internal combustion engines |
FR2413547A1 (en) * | 1977-12-29 | 1979-07-27 | Ruyer Charles | IMPROVED REDUCED LOAD OPERATING CYCLE FOR FOUR STROKE EXPLOSION ENGINES AND ENGINES USING THIS CYCLE |
GB2062112A (en) * | 1979-10-17 | 1981-05-20 | Dornier C | Device for Utilization of Residual Energy in Machinery |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2010119246A1 (en) * | 2009-04-18 | 2010-10-21 | Richard Lloyd Leslie Daniel | Internal combustion engine |
Also Published As
Publication number | Publication date |
---|---|
FR2683856B1 (en) | 1993-12-31 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US7383797B2 (en) | Double piston cycle engine | |
US7273023B2 (en) | Steam enhanced double piston cycle engine | |
FR2683856A1 (en) | Heat engine with four supplemented stroke cycle. Gain in power by reintroduction, to the cycle, of the exhaust gases, and conversion of their energy into a motive force | |
US5299537A (en) | Metered induction two cycle engine | |
US20070181101A1 (en) | Internal combustion engine | |
US6463731B1 (en) | Two stroke regenerative external combustion engine | |
JP2009222060A (en) | Exchanging (scavenging) method for combustion gas of two stroke engine | |
US2463308A (en) | Multiple opposed piston propulsive engine | |
JPH0541214Y2 (en) | ||
EP2531708B1 (en) | Two-stage engine exhaust system | |
US20100095662A1 (en) | Rechargeable reciprocating pneumatic piston engine | |
GB2069594A (en) | A compound expansion internal combustion engine | |
EP0006747A1 (en) | Internal-combustion engine with additional expansion | |
US11828238B2 (en) | Method in a two-stroke engine and two-stroke engine | |
GB2112064A (en) | Piston power transmission in an internal or external combustion engine | |
FR2810373A1 (en) | Internal combustion engine without external cooling has additional air compression cylinder with ambient air suction and compressed air outlet to buffer bottle whose outlet connects to air inlets on cylinder head | |
US892790A (en) | Compound explosive-engine. | |
FR3065489A1 (en) | INTERNAL COMBUSTION ENGINE WITH DIVIDED CYCLE | |
US1387408A (en) | Internal-combustion engine | |
EP0043375A1 (en) | An internal combustion engine and operating method | |
US1450810A (en) | Internal-combustion engine | |
FR2668543A1 (en) | Hot gas engine | |
SU875111A1 (en) | Heat piston engine | |
FR3095672A3 (en) | AUXILIARY MOTOR | |
WO2009004185A2 (en) | Device and method for opening a lubrication and cooling valve for reciprocating piston engines |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |