WO2012030311A1 - Installation motrice - Google Patents

Installation motrice Download PDF

Info

Publication number
WO2012030311A1
WO2012030311A1 PCT/UA2010/000062 UA2010000062W WO2012030311A1 WO 2012030311 A1 WO2012030311 A1 WO 2012030311A1 UA 2010000062 W UA2010000062 W UA 2010000062W WO 2012030311 A1 WO2012030311 A1 WO 2012030311A1
Authority
WO
WIPO (PCT)
Prior art keywords
engine
fuel
rotor
housing
compressed air
Prior art date
Application number
PCT/UA2010/000062
Other languages
English (en)
Russian (ru)
Inventor
Владимир Петрович БОНДАРЕНКО
Original Assignee
Bondarenko Vladimir Petrovich
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 Bondarenko Vladimir Petrovich filed Critical Bondarenko Vladimir Petrovich
Publication of WO2012030311A1 publication Critical patent/WO2012030311A1/fr

Links

Classifications

    • 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
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
    • F01C21/00—Component parts, details or accessories not provided for in groups F01C1/00 - F01C20/00
    • F01C21/10—Outer members for co-operation with rotary pistons; Casings

Definitions

  • the power plant contains an air cooling system 20, including eight cooling blades 5, which connect the rotor 4 to the shaft 6 and are fixed at an angle, for example, 45 ° to the axis of the rotor 4 (and shaft 6).

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Supercharger (AREA)

Abstract

L'invention se rapporte aux installations motrices à moteur rotatif. Le moteur comprend des chambres de combustion externes. Un rotor monté dans le corps comporte des pales. À l'extérieur et sur les côtés du rotor sont montés des pistons de type plaque. La chambre de combustion comprend une ouverture d'évacuation et des ouvertures d'admission d'air comprimé et de carburant et d'insertion d'un élément d'inflammation du carburant. La chambre de combustion comprend une soupape capable de fermer hermétiquement son ouverture d'évacuation. Les soupapes de la chambre de combustion, les systèmes d'alimentation en air comprimé et en carburant et l'élément d'inflammation sont connectés à une unité de commande. Le moteur comprend des clapets capables de fermer hermétiquement la chambre de travail, et des tiges de poussée qui sont reliées à l'unité de commande. Les clapets sont montés en aval de fenêtres de sortie et en amont des chambres de combustion dans le sens de rotation du rotor. Le corps est fermé par des couvercles d'extrémité comportant des nervures de rigidité et des fenêtres entre ces dernières. Le système de refroidissement est à air. Les couvercles d'extrémité comportent des joints. Le résultat technique consiste en un indice de performance plus élevé, en une plus grande fiabilité et en plus de ressources, en une simplification de la structure, en une diminution du temps nécessaire à l'entretien, de la masse métallique et de la main d'œuvre nécessaire à la fabrication de l'installation motrice.
PCT/UA2010/000062 2010-08-31 2010-09-14 Installation motrice WO2012030311A1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
UA2010010561 2010-08-31
UAA201010561 2010-08-31

Publications (1)

Publication Number Publication Date
WO2012030311A1 true WO2012030311A1 (fr) 2012-03-08

Family

ID=45773155

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/UA2010/000062 WO2012030311A1 (fr) 2010-08-31 2010-09-14 Installation motrice

Country Status (1)

Country Link
WO (1) WO2012030311A1 (fr)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ES2545972A1 (es) * 2014-02-17 2015-09-17 Diego ORELLANA HURTADO Motor de impulso circular con sistema de neutralización de los gases de la combustión
CN106574500A (zh) * 2014-06-04 2017-04-19 斯泰因·克瑞·蒙森 旋转马达
US10273879B2 (en) 2013-12-17 2019-04-30 Diego ORELLANA HURTADO Circular propulsion jet compressor-engine

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2079192A (en) * 1935-08-06 1937-05-04 Jr Lucius Forest Upshaw Rotary engine
US4782656A (en) * 1985-03-25 1988-11-08 Hansen Engine Corporation Rotary valve assembly for engine
RU2183754C2 (ru) * 1999-12-07 2002-06-20 Гордиенко Николай Николаевич Силовая установка
US8111988B1 (en) * 2008-06-10 2012-02-07 Lockheed Martin Corporation Method for monitoring wavelength-division multiplexed signal

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2079192A (en) * 1935-08-06 1937-05-04 Jr Lucius Forest Upshaw Rotary engine
US4782656A (en) * 1985-03-25 1988-11-08 Hansen Engine Corporation Rotary valve assembly for engine
RU2183754C2 (ru) * 1999-12-07 2002-06-20 Гордиенко Николай Николаевич Силовая установка
US8111988B1 (en) * 2008-06-10 2012-02-07 Lockheed Martin Corporation Method for monitoring wavelength-division multiplexed signal

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10273879B2 (en) 2013-12-17 2019-04-30 Diego ORELLANA HURTADO Circular propulsion jet compressor-engine
ES2545972A1 (es) * 2014-02-17 2015-09-17 Diego ORELLANA HURTADO Motor de impulso circular con sistema de neutralización de los gases de la combustión
CN106574500A (zh) * 2014-06-04 2017-04-19 斯泰因·克瑞·蒙森 旋转马达

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