FR2567570A1 - Moteur rotatif - Google Patents

Moteur rotatif Download PDF

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Publication number
FR2567570A1
FR2567570A1 FR8317367A FR8317367A FR2567570A1 FR 2567570 A1 FR2567570 A1 FR 2567570A1 FR 8317367 A FR8317367 A FR 8317367A FR 8317367 A FR8317367 A FR 8317367A FR 2567570 A1 FR2567570 A1 FR 2567570A1
Authority
FR
France
Prior art keywords
engine
blades
fact
gases
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.)
Pending
Application number
FR8317367A
Other languages
English (en)
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to FR8317367A priority Critical patent/FR2567570A1/fr
Publication of FR2567570A1 publication Critical patent/FR2567570A1/fr
Pending legal-status Critical Current

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
    • F02B53/00—Internal-combustion aspects of rotary-piston or oscillating-piston engines
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
    • F01C1/00—Rotary-piston machines or engines
    • F01C1/30—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members
    • F01C1/34—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F01C1/08 or F01C1/22 and relative reciprocation between the co-operating members
    • F01C1/356—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F01C1/08 or F01C1/22 and relative reciprocation between the co-operating members with vanes reciprocating with respect to the outer member
    • F01C1/3566—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F01C1/08 or F01C1/22 and relative reciprocation between the co-operating members with vanes reciprocating with respect to the outer member the inner and outer member being in contact along more than one line or surface
    • 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
    • Y—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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00—Road transport of goods or passengers
    • Y02T10/10—Internal combustion engine [ICE] based vehicles
    • Y02T10/12—Improving ICE efficiencies

Abstract

L'INVENTION CONCERNE LES MOTEURS A EXPLOSION A QUATRE TEMPS. C'EST UN ROTATIF EQUILIBRE, APPARAISSENT DE NOUVELLES PIECES:-LE PLONGEUR, MOVIBLE DE BAS EN HAUT SOUS L'IMPULSION DES PALES DU ROTOR DONT IL SUIT LES COURBURES;-LE TRANSFERT, PERMETTANT L'ADMISSION DES GAZ COMPRESSES EN CHAMBRE D'EXPLOSION (RACCORDEMENT FIXE DE LA CHAMBRE DE COMBUSTION A LA CHAMBRE D'EXPLOSION);-LE ROTOR, COMPOSE DE QUATRE PALES, PIVOTE AUTOUR D'UN AXE CENTRAL, IL PERMET LES QUATRE TEMPS MOTEUR. MOTEUR QUI PARAIT INTERESSANT DU FAIT DE SA GRANDE SIMPLICITE, DE L'ENORME ALLEGEMENT QU'IL PROPOSE. REDUISANT TOUTES CAUSES DE FREINAGE (VILBREQUIN, BIELLES, PISTONS, ETC.) QUI DISPARAISSENT. PERMETTANT UN BALAYAGE A 100 DES GAZ BRULES. POUVANT EXPLOSER HUIT FOIS PAR 360. L'EMPLOI D'UN TEL MOTEUR SEMBLE ILLIMITE.

Description

D E S C R I P T I O N
La présente invention @oncerne les moteurs à explosion à 4 t@mps.
Selcn l'invention @e moteur est un moteur rotatif équilibré simpl@, schéma de prineipe joint.
Selon l'invention apparraissent des pièces nouv@lles:
- une mobile de bas en haut " le plongeur ",il blcque les gaz.
- une fixe " le transfert " permettant aux ga@ compressés l'accès
à la chambre d'explosion.
L'admission,l'échappement,ne nécessitent pas de soupapes.
L'allumage est classique.
Selon le moteur prop@sé,le principe de foncticnnement est simple(schéma II)
Le moteur est lançé
- temps I - admission
par dépression de A en B (pale 1)
- temps II - compression
en B le plongeur,s'enfcnce,blcque les gaz,les fait scus l'impulsion
de la pale 2 se compresser,et passer dans le transfert.
- temps III - expl@sion détente
position de la pale 2 en B',les gaz compressés guidés par le trans
fert ont été libérés en @ B B' -explosion détente jusqu'@n C.
- temps IV - échappement
la pale 3 pousoe la totalité des gaz brûlés qui s'echappent en C .
Ce type de moteur peut exploser 8 fois par 360 .
Nota. Les croquis joints ne sont que schémas de principe .

Claims (1)

  1. REVENDICATIONS
    -moteur rotatif équilibré -caractérisé par le fait qu'apparait une pièce ncuvelle très imp@rtant@
    simplifiant à l'extrême le mcuvement " le pl@ngeur".
    -caractérisé par le fait qu'spparait un raccordement fixe " le transfert "
    permettant au@ gaz compressés l'admission à la chambre de combustion . -caractérisé par le fait que le plongeur permet le bal@yage à 100 das
    gaz brûlés .
    -caractérisé par le fait que le pl@ngeur supprime : pist@ns,bielles,vil-
    br@quin,etc..... .
FR8317367A 1983-10-27 1983-10-27 Moteur rotatif Pending FR2567570A1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR8317367A FR2567570A1 (fr) 1983-10-27 1983-10-27 Moteur rotatif

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8317367A FR2567570A1 (fr) 1983-10-27 1983-10-27 Moteur rotatif

Publications (1)

Publication Number Publication Date
FR2567570A1 true FR2567570A1 (fr) 1986-01-17

Family

ID=9293688

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8317367A Pending FR2567570A1 (fr) 1983-10-27 1983-10-27 Moteur rotatif

Country Status (1)

Country Link
FR (1) FR2567570A1 (fr)

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR418470A (fr) * 1910-07-21 1910-12-10 Guillaume Bouret Moteur rotatif à glissières multiples
FR13427E (fr) * 1910-07-21 1911-04-07 Guillaume Bouret Moteur rotatif à glissières multiples
US2409141A (en) * 1944-08-30 1946-10-08 Eugene Berger Rotary internal-combustion engine
FR1131238A (fr) * 1955-09-13 1957-02-19 Moteur rotatif à combustion interne

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR418470A (fr) * 1910-07-21 1910-12-10 Guillaume Bouret Moteur rotatif à glissières multiples
FR13427E (fr) * 1910-07-21 1911-04-07 Guillaume Bouret Moteur rotatif à glissières multiples
US2409141A (en) * 1944-08-30 1946-10-08 Eugene Berger Rotary internal-combustion engine
FR1131238A (fr) * 1955-09-13 1957-02-19 Moteur rotatif à combustion interne

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