FR2853938A1 - Reactor has auxiliary engine turning electricity generator and compressor, and cam shaft opening or closing valve for providing multiple ram effects in second, where ram effects increase final force of reactor - Google Patents
Reactor has auxiliary engine turning electricity generator and compressor, and cam shaft opening or closing valve for providing multiple ram effects in second, where ram effects increase final force of reactor Download PDFInfo
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- FR2853938A1 FR2853938A1 FR0304840A FR0304840A FR2853938A1 FR 2853938 A1 FR2853938 A1 FR 2853938A1 FR 0304840 A FR0304840 A FR 0304840A FR 0304840 A FR0304840 A FR 0304840A FR 2853938 A1 FR2853938 A1 FR 2853938A1
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- Prior art keywords
- reactor
- compressor
- ram effects
- force
- auxiliary engine
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K5/00—Plants including an engine, other than a gas turbine, driving a compressor or a ducted fan
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Exhaust Gas After Treatment (AREA)
Abstract
Description
La présente demande de brevet a pour objet de faire marcherThe purpose of this patent application is to operate
un réacteur avec un moteur auxiliaire dont les dix brevets qui suivent ont été déposés: (1457337 le 17/06/65) ; (7539920 le 29/12175) ; (8215312 le 02/11/82) ; (8717038 le 08/12/87) (?213582 le 09/11/92) ; (9314428 le 30/11/93) ; (9412262 le 12/ 10/94) ; (0013196 le 12/10/00) ; (0014432 le 08/11/00) ; (0016 348 le 12/12/00). Ces brevets concernent le moteur, rotatif, à explosions, à travail latéral, à cylindre tournant, à compresseur plusieurs fois plus grand que le propulseur, constitué de 10 deux groupes, l'un conpresseur l'autre propulseur, chaque groupe comprenant deux rotors dont l'un, intérieur, fait fonction de piston et l'autre, extérieur, fait fonction de cylindre. Les deux rotors tournent conjointement l'un dans l'autre et sont excentrés l'un par rapport à l'autre de façon à ce que le rotor15 piston touche la voûte du rotor-cylindre en un point x. L'excentricité des deux rotors définit, pour le compresseur, les chambres d'aspiration et de compression et pour le propulseur, les chambres de détentes et d'échappements. a reactor with an auxiliary engine of which the following ten patents have been filed: (1457337 on 06/17/65); (7539920 on 12/29,175); (8215312 on 02/11/82); (8717038 on 08/12/87) (? 213582 on 09/11/92); (9314428 on 11/30/93); (9412262 on 12/10/94); (0013196 on 12/10/00); (0014432 on 08/11/00); (0016 348 on 12/12/00). These patents relate to the rotary, explosion, side-working, rotating cylinder, compressor engine several times larger than the propellant, consisting of two groups, one compressor the other propeller, each group comprising two rotors, one, inside, acts as a piston and the other, outside, acts as a cylinder. The two rotors rotate together and are offset from each other so that the piston rotor touches the roof of the rotor-cylinder at a point x. The eccentricity of the two rotors defines, for the compressor, the suction and compression chambers and for the propellant, the expansion and exhaust chambers.
Ce moteur tire sa puissance extraordinaire du fait que mar20 chant latéralement, il bénéficie des "coups de bélier" de ses explosions et de ses échappements, ce qui lui donne la force fabuleuse de plus de 500 fois supérieure à celle de n'importe quel autre moteur, à consommation égale de carburant. This engine draws its extraordinary power from the fact that mar20 sings sideways, it benefits from the pressure surges of its explosions and its exhausts, which gives it the fabulous force of more than 500 times greater than that of any other. engine, with equal fuel consumption.
Le réacteur faisant l'objet du présent brevet, bénéficie é25 gaiement des "coups de bélier" de ses échappements et a une poussée fabuleuse de plusieurs centaines de fois supérieure. The reactor which is the subject of this patent also benefits from the "water hammer" of its exhausts and has a fabulous thrust of several hundred times greater.
Il est donc utile de savoir ce que représente cette force fabuleuse des "coups de bélier" qui est la plus grande force qui existe dans l'Univers. It is therefore useful to know what represents this fabulous force of "water hammer" which is the greatest force that exists in the Universe.
Voici deux preuves parmi cinq autres, qui ont été retenues, Première preuve, Le "coup de bélier",d'une explosion, d'un gaz qui se libère brutalement ou d'un choc, est la plus grande force qui puisse se faire, puisqu'elle a été assez forte pour engendrer l'Uni35 vers tel que nous le voyons. Here are two proofs among five others, which were retained, First proof, The "water hammer", of an explosion, of a gas which is suddenly released or of a shock, is the greatest force which can be done , since it was strong enough to generate the Uni35 towards as we see it.
En effet, le GRAND BOUM (bing bang) produit par l'explosion du GRAND OBJET, a provoqué le PREMIER "COUP DE BELIER" qui a réussi à faire LA CHOSE que nulle autre force n'était capable de faire, c'est-à-dire: - De vaincre la gravité de L'OBJET qui a explosé et - De disperser sa matière dans l'Espace, - Matière qui est d'ailleurs toujours en expansion. Indeed, the BIG BOMB produced by the explosion of the BIG OBJECT, caused the FIRST "COUP DE BELIER" which succeeded in doing THE THING that no other force was able to do, that is- to say: - To overcome the gravity of the OBJECT which exploded and - To disperse its matter in Space, - Matter which is besides always in expansion.
Le moteur de l'invention dont le travail se fait laté5 ralement dans un cylindre tournant, bénéficie des "coups de bélier" de ses explosions et de ses échappements, dispose donc doublement de cette force de la nature, ainsi que le réacteur qui bénéficie aussi des "coups de bélier". The engine of the invention, the work of which is done laterally in a rotating cylinder, benefits from "water hammer" from its explosions and from its exhausts, therefore has doubly this force of nature, as does the reactor which also benefits "water hammer".
Ce réacteur est donc, tout comme le GRAND OBJET, capable 10 de vaincre la gravité de la terre, en emportant une charge de plus de 100 fois son poids. This reactor is therefore, just like the BIG OBJECT, capable of overcoming the gravity of the earth, by carrying a load of more than 100 times its weight.
Deuxième preuve, La force du "coup de bélier" a été prouvée par une expérience consistant à enfoncer un clou à 3 mm environ de pro15 fondeur dans un bloc de bois placé sur une balance avec un marteau produisant un "coup de bélier" de 100 grammes. Second proof, The force of the "water hammer" was proven by an experiment consisting of driving a nail about 3 mm deep in a block of wood placed on a scale with a hammer producing a "water hammer" of 100 grams.
Ensuite, il a été essayé de planter le clou en lui posant dessus un poids de 10 kg, sans même marquer le bois. Il y faut un poids de plus de 30 kg, démontrant ainsi que la force 20 du "coup de bélier" est plus de 3I0G fois supérieure à la force qui frappe. Then, it was tried to plant the nail by placing a 10 kg weight on it, without even marking the wood. It requires a weight of more than 30 kg, thus demonstrating that the force 20 of the "water hammer" is more than 3I0G times greater than the force which strikes.
La description qui va suivre en regard des dessins annexés, donnée à titre d'exemple non limitatif, fera bien comprendre comment l'invention peut être réalisée, les particularités qui 25 ressortent tant des dessins quedu teXte faisant, bien entendu, partie de la dite invention. The description which follows with reference to the appended drawings, given by way of nonlimiting example, will make it clear how the invention can be implemented, the features which emerge both from the drawings and from the text forming, of course, part of said invention.
Numérotage des éléments de ce réacteur, (1) Moteur auxiliaire, faisant tourner, le générateur d'électricité 2, le compresseur 3 et actionnant la soupape 30 7, (2) Générateur d'électricité permettant de chauffer la chambre de compression 4 et de maintenir dans tout son volume une pression de 5 bars, (3) Compresseur permettant de compléter la pression de 5 35 bars dans la chambre de compression 4, (4) Chambre de compression, d'un volume d'une cylindrée du compresseur, (5) Entrée de l'azote pour marche hors atmosphère, (6) Entrée de-l'àir atmesphériquç (7) Soupape permettant de donner environ 15 "coups de bélier" à la seconde, (8) Commande hydraulique venant de la came 9, ouvrant et fermant la soupape, pour donner les "coups de bélier", (9) Came commandant l'ouverture et la fermeture de la soupape, (10) Ressort de rappel de la soupape. Numbering of the elements of this reactor, (1) Auxiliary motor, rotating, the electricity generator 2, the compressor 3 and actuating the valve 30 7, (2) Electricity generator allowing to heat the compression chamber 4 and maintain a pressure of 5 bars throughout its volume, (3) Compressor making it possible to complete the pressure of 5 35 bars in the compression chamber 4, (4) Compression chamber, with a volume of one displacement of the compressor, ( 5) Nitrogen inlet for operation outside the atmosphere, (6) Atmospheric air inlet (7) Valve allowing approximately 15 "water hammer" to be given per second, (8) Hydraulic control coming from cam 9 , opening and closing the valve, to give the pressure surges, (9) Cam controlling the opening and closing of the valve, (10) Return spring of the valve.
La figure 1, représente une vue du réacteur avec le moteur auxilliaire 1, faisant tourner, le générateur d'électricité 2, le compresseur 3, tout en actionnant la soupape 7 pour provoquer les "coups de bélier", environ 15 fois par seconde. Figure 1 shows a view of the reactor with the auxiliary motor 1, rotating, the electricity generator 2, the compressor 3, while actuating the valve 7 to cause "water hammer", about 15 times per second.
La figure 2, représente une vue du moteur auxiliaire 1, qui fait marcher tout le réacteur et lui permet d'avoir une force prodigieuse en lui permettant de bénéficier des "coups 15 de bélier". Figure 2 shows a view of the auxiliary engine 1, which operates the entire reactor and allows it to have a prodigious force allowing it to benefit from "water hammer".
Ce système fonctionne de la façon suivante Le moteur auxiliaire 1 bénéficiant des "coups de bélier" de ses explosions et de ses échappements, entraîne le réacteur, lui permettant ainsi de bénéficier lui-même des "coups 20 de b4lier" de ses échappements. This system works in the following manner. The auxiliary engine 1 benefiting from "water hammer" from its explosions and from its exhausts, drives the reactor, thereby enabling it to benefit itself from the "blows 20" from its exhausts.
Donc le moteur 1 comprime et chauffe, à chaque tour, dans la chambre de compression 4 une cylindrée du compresseur 3, lui donnant ainsi une pression de 5 bars environ, ce qui fait que à chaque échappement, il se produit une poussée de 30 kg et donc, s'il fait 15 échappements par seconde poûr une rotation de 28 tours par seconde, par exemple, sa force serait de kg x 15 = une poussée de 450 kg et comme selon l'exemple du clou que l'on enfonce, les "coups de bélier" multiplient cette force par 300, la force finale de ce réacteur serait de 30 450 kg x 300 = 135 tonnes de poussée par seconde. Therefore the motor 1 compresses and heats, in each revolution, in the compression chamber 4 a displacement of the compressor 3, thus giving it a pressure of approximately 5 bars, which means that with each exhaust, a thrust of 30 kg is produced and therefore, if it makes 15 exhausts per second for a rotation of 28 revolutions per second, for example, its force would be kg x 15 = a thrust of 450 kg and as according to the example of the nail that we drive, "water hammer" multiplies this force by 300, the final force of this reactor would be 30 450 kg x 300 = 135 tonnes of thrust per second.
Il va de soi que la présente invention a été décrite cidessus à titre explicatif mais nullement limitatif et qu'on pourrait y apporter toutes modifications de détail sans sortir de son cadre. It goes without saying that the present invention has been described above for explanatory purposes but in no way limitative and that any modification of detail could be made without departing from its scope.
Claims (1)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0304840A FR2853938A1 (en) | 2003-04-17 | 2003-04-17 | Reactor has auxiliary engine turning electricity generator and compressor, and cam shaft opening or closing valve for providing multiple ram effects in second, where ram effects increase final force of reactor |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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FR0304840A FR2853938A1 (en) | 2003-04-17 | 2003-04-17 | Reactor has auxiliary engine turning electricity generator and compressor, and cam shaft opening or closing valve for providing multiple ram effects in second, where ram effects increase final force of reactor |
Publications (1)
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FR2853938A1 true FR2853938A1 (en) | 2004-10-22 |
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FR0304840A Withdrawn FR2853938A1 (en) | 2003-04-17 | 2003-04-17 | Reactor has auxiliary engine turning electricity generator and compressor, and cam shaft opening or closing valve for providing multiple ram effects in second, where ram effects increase final force of reactor |
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Citations (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB572876A (en) * | 1943-09-01 | 1945-10-26 | Frank Henry Stark | Improvements in or relating to fluid reaction apparatus for propelling purposes |
FR1457337A (en) * | 1965-06-17 | 1966-11-04 | Rotary internal combustion engine | |
FR2337253A1 (en) * | 1975-12-29 | 1977-07-29 | Gil Noel | Rotary piston engine with compressor and motor stages - has sliding vanes mounted by ball and socket joints with seal maintained by pistons |
FR2647505A1 (en) * | 1987-12-08 | 1990-11-30 | Gil Noel | Internal combustion turbine with endless effect piston |
FR2697793A1 (en) * | 1992-11-09 | 1994-05-13 | Gil Noel | Jet engine system for helicopter - has ducting passing air to rear with compression chamber, and shutters to control air flow and direction |
US5361581A (en) * | 1993-04-21 | 1994-11-08 | Clark Barre A M | Pulsed piston-compressor jet engine |
FR2713283A1 (en) * | 1993-11-30 | 1995-06-09 | Gil Noel | Rotary IC engine with two assemblies |
FR2725756A1 (en) * | 1994-10-12 | 1996-04-19 | Gil Noel | Rotary combustion engine with associated air compressor |
DE19621878A1 (en) * | 1996-05-31 | 1997-12-04 | Michael Jensen | Thermodynamic energy conversion system |
FR2815381A1 (en) * | 2000-10-12 | 2002-04-19 | Noel Gil | Control mechanism, for rotary internal combustion engine, is such that it allows controlled delay of the introduction of air into the combustion chamber. |
FR2816351A1 (en) * | 2000-11-08 | 2002-05-10 | Noel Gil | Fixings, for rotary engine, are applied to fix pistons to shafts, to prevent piston from applying pressure to slider. |
FR2817910A1 (en) * | 2000-12-12 | 2002-06-14 | Noel Gil | Rotary i.c. engine with lateral operation has gas fuel feed through fixed flange and seal between fixed and rotary sections |
-
2003
- 2003-04-17 FR FR0304840A patent/FR2853938A1/en not_active Withdrawn
Patent Citations (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB572876A (en) * | 1943-09-01 | 1945-10-26 | Frank Henry Stark | Improvements in or relating to fluid reaction apparatus for propelling purposes |
FR1457337A (en) * | 1965-06-17 | 1966-11-04 | Rotary internal combustion engine | |
FR2337253A1 (en) * | 1975-12-29 | 1977-07-29 | Gil Noel | Rotary piston engine with compressor and motor stages - has sliding vanes mounted by ball and socket joints with seal maintained by pistons |
FR2647505A1 (en) * | 1987-12-08 | 1990-11-30 | Gil Noel | Internal combustion turbine with endless effect piston |
FR2697793A1 (en) * | 1992-11-09 | 1994-05-13 | Gil Noel | Jet engine system for helicopter - has ducting passing air to rear with compression chamber, and shutters to control air flow and direction |
US5361581A (en) * | 1993-04-21 | 1994-11-08 | Clark Barre A M | Pulsed piston-compressor jet engine |
FR2713283A1 (en) * | 1993-11-30 | 1995-06-09 | Gil Noel | Rotary IC engine with two assemblies |
FR2725756A1 (en) * | 1994-10-12 | 1996-04-19 | Gil Noel | Rotary combustion engine with associated air compressor |
DE19621878A1 (en) * | 1996-05-31 | 1997-12-04 | Michael Jensen | Thermodynamic energy conversion system |
FR2815381A1 (en) * | 2000-10-12 | 2002-04-19 | Noel Gil | Control mechanism, for rotary internal combustion engine, is such that it allows controlled delay of the introduction of air into the combustion chamber. |
FR2816351A1 (en) * | 2000-11-08 | 2002-05-10 | Noel Gil | Fixings, for rotary engine, are applied to fix pistons to shafts, to prevent piston from applying pressure to slider. |
FR2817910A1 (en) * | 2000-12-12 | 2002-06-14 | Noel Gil | Rotary i.c. engine with lateral operation has gas fuel feed through fixed flange and seal between fixed and rotary sections |
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