ES436135A1 - Instalacion motriz perfeccionada. - Google Patents

Instalacion motriz perfeccionada.

Info

Publication number
ES436135A1
ES436135A1 ES436135A ES436135A ES436135A1 ES 436135 A1 ES436135 A1 ES 436135A1 ES 436135 A ES436135 A ES 436135A ES 436135 A ES436135 A ES 436135A ES 436135 A1 ES436135 A1 ES 436135A1
Authority
ES
Spain
Prior art keywords
arm
engine
orifices
combustion chamber
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.)
Expired
Application number
ES436135A
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.)
Etat Francais
Original Assignee
Etat Francais
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 Etat Francais filed Critical Etat Francais
Publication of ES436135A1 publication Critical patent/ES436135A1/es
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B37/00Engines characterised by provision of pumps driven at least for part of the time by exhaust
    • F02B37/12Control of the pumps
    • F02B37/16Control of the pumps by bypassing charging air
    • F02B37/164Control of the pumps by bypassing charging air the bypassed air being used in an auxiliary apparatus, e.g. in an air turbine
    • F02B37/166Control of the pumps by bypassing charging air the bypassed air being used in an auxiliary apparatus, e.g. in an air turbine the auxiliary apparatus being a combustion chamber, e.g. upstream of turbine
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/26Controlling the air flow
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B3/00Engines characterised by air compression and subsequent fuel addition
    • F02B3/06Engines characterised by air compression and subsequent fuel addition with compression ignition
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/12Improving ICE efficiencies

Abstract

Instalación motriz perfeccionada que comprende un motor de combustión interna, de preferencia del tipo de encendido por compresión que, por una parte, está sobrealimentado por un grupo turbo-compresor que comprende un compresor, una turbina que arrastra este compresor y un paso que comunica, de preferencia de modo permanente, con la salida del compresor y la entrada de la turbina y que es capaz de llevar a la turbina la totalidad del caudal del compresor no atravesando el motor, y que, por otra parte, comprende una cámara de trabajo de volumen variable que comunica por un conducto de admisión con la salida del compresor y por un conducto de escape con la entrada de la turbina, de tal manera que la cámara de trabajo esté en paralelo con una parte, al menos, del paso una cámara de combustión auxiliar dividida, desde aguas arriba hacia aguas abajo, en una zona primaria de combustión alimentada de aire fresco por el paso y de combustible por un sistema de alimentación de combustible, y en una zona secundaria de dilución, alimentada de aire fresco por el paso y de gas de combustión por el conducto de escape y que suministra gases calientes a la turbina para contribuir a arrastrarla, y en el paso, medios de estrangulación apropiados para establecer, entre el aire que sale del compresor y el gas que entra en la turbina, una disminución de presión que es prácticamente independiente de la relación entre el caudal de aire que sigue el paso y el caudal total de aire suministrado por el compresor, pero que varía en el mismo sentido que la presión que reina en este paso aguas arriba de los medios de estrangulación caracterizada por el hecho de que el paso está dividido en dos ramas paralelas, de las cuales la primera está provista de los citados medios de estrangulación y termina aguas abajo de la zona primaria de combustión y de las cuales la segunda está unida a la zona primaria por al menos un orificio de sección tal que la citada disminución de presión sea establecida prácticamente también entre la parte aguas arriba y la parte aguas abajo de este orificio y por el hecho de que el sistema de alimentación de combustible desemboca en la zona primaria al nivel de las turbulencias que son creadas allí por la llegada del aire a través de dicho orificio.
ES436135A 1974-03-29 1975-03-29 Instalacion motriz perfeccionada. Expired ES436135A1 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7411011A FR2265979B1 (es) 1974-03-29 1974-03-29

Publications (1)

Publication Number Publication Date
ES436135A1 true ES436135A1 (es) 1976-12-01

Family

ID=9137024

Family Applications (1)

Application Number Title Priority Date Filing Date
ES436135A Expired ES436135A1 (es) 1974-03-29 1975-03-29 Instalacion motriz perfeccionada.

Country Status (30)

Country Link
US (1) US4026115A (es)
JP (1) JPS5421483B2 (es)
AR (1) AR202747A1 (es)
AT (1) AT376767B (es)
BE (1) BE827256A (es)
CA (1) CA1026570A (es)
CH (1) CH585843A5 (es)
CS (1) CS209854B2 (es)
DD (1) DD116893A5 (es)
DE (1) DE2513889C2 (es)
DK (1) DK144648C (es)
ES (1) ES436135A1 (es)
FI (1) FI60060C (es)
FR (1) FR2265979B1 (es)
GB (1) GB1491561A (es)
HK (1) HK6979A (es)
HU (1) HU171875B (es)
IL (1) IL46940A (es)
IN (1) IN143030B (es)
IT (1) IT1044276B (es)
LU (1) LU72168A1 (es)
MY (1) MY7800392A (es)
NL (2) NL162714C (es)
NO (2) NO148460C (es)
PL (1) PL108892B1 (es)
RO (1) RO69767A (es)
SE (2) SE435646B (es)
SU (1) SU698543A3 (es)
YU (1) YU37382B (es)
ZA (1) ZA751944B (es)

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2308792A2 (fr) * 1975-04-24 1976-11-19 France Etat Perfectionnements apportes aux installations a moteur a combustion interne suralimente, notamment a moteur diesel suralimente
JPS584059Y2 (ja) * 1978-02-22 1983-01-24 株式会社小松製作所 過給機付内燃機関における過給機増力用の燃焼器
FR2441057A1 (fr) * 1978-11-09 1980-06-06 Melchior Jean Moteurs a combustion interne a rendement et remplissage ameliores par recuperation d'une partie de l'energie des bouffees qui sont produites lors de l'ouverture des orifices d'echappement
FR2472082A1 (fr) * 1979-12-19 1981-06-26 France Etat Perfectionnements apportes aux moteurs a combustion interne suralimentes, notamment aux moteurs diesel
FR2484536A1 (fr) * 1980-06-17 1981-12-18 France Etat Perfectionnements aux moteurs a combustion interne suralimentes, notamment aux moteurs diesel, et aux procedes de mise en marche de ces moteurs et de reglage de leur vitesse
CA1188111A (en) * 1980-12-02 1985-06-04 William F. Helmrich Variable area means for air systems of air blast type fuel nozzle assemblies
FR2585072A1 (fr) * 1985-07-18 1987-01-23 Melchior Cie Perfectionnements aux moteurs a combustion interne suralimentes
FR2618528B1 (fr) * 1987-07-23 1992-10-16 France Etat Armement Perfectionnements aux chambres de combustion auxiliaires, pour moteurs a combustion interne suralimentes, et moteurs a combustion interne equipes d'une telle chambre
EP0474007A3 (en) * 1990-09-06 1993-04-14 Krupp Mak Maschinenbau Gmbh Running up device for diesel engine turbo charges
DE4215046C3 (de) * 1992-05-07 1999-10-21 Audi Ag Auspuffanlage für eine Diesel-Brennkraftmaschine
AP2001002032A0 (en) * 1998-07-09 2001-03-31 Guy Negre Method for operating pollution-free engine expansion chamber and expansion chamber therefor.
GB2351343A (en) * 1999-06-22 2000-12-27 Alstom Gas Turbines Ltd Telescopically-moveable combustion chamber
US7040094B2 (en) * 2002-09-20 2006-05-09 The Regents Of The University Of California Staged combustion with piston engine and turbine engine supercharger
GB0308013D0 (en) 2003-04-07 2003-05-14 Prodrive 2000 Ltd Turbocharger
US20060283187A1 (en) * 2004-04-06 2006-12-21 Roland Broadbent Combustion unit for turbocharger
FR2896566B1 (fr) * 2006-01-25 2008-05-02 Renault Sas Regulateur de debit pour systeme d'injection de gaz traceur
US8291886B2 (en) * 2007-02-12 2012-10-23 Honeywell International Inc. Actuator flow compensated direct metering fuel control system and method
US11002185B2 (en) * 2019-03-27 2021-05-11 Pratt & Whitney Canada Corp. Compounded internal combustion engine

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2633698A (en) * 1948-02-05 1953-04-07 Nettel Frederick Turbosupercharger means to heat intake of compression-ignition engine for starting
US2669090A (en) * 1951-01-13 1954-02-16 Lanova Corp Combustion chamber
DE1929126A1 (de) * 1968-06-15 1970-06-18 Uzina 23 August Verfahren zur Abgasturboladung in Abzweigung fuer Verbrennungsmotoren
FR2179309A5 (es) * 1972-04-06 1973-11-16 France Etat

Also Published As

Publication number Publication date
NL7810391A (nl) 1979-02-28
IL46940A (en) 1977-07-31
SE8201512L (sv) 1982-03-10
CA1026570A (en) 1978-02-21
RO69767A (ro) 1981-08-17
IL46940A0 (en) 1975-06-25
AU7961775A (en) 1976-09-30
GB1491561A (en) 1977-11-09
NL162714B (nl) 1980-01-15
FI60060B (fi) 1981-07-31
AT376767B (de) 1984-12-27
ZA751944B (en) 1976-03-31
NO823373L (no) 1975-09-30
DE2513889C2 (de) 1982-11-25
DD116893A5 (es) 1975-12-12
MY7800392A (en) 1978-12-31
FI750946A (es) 1975-09-30
NO152763B (no) 1985-08-05
SU698543A3 (ru) 1979-11-15
NL7503684A (nl) 1975-10-01
FR2265979A1 (es) 1975-10-24
SE450902B (sv) 1987-08-10
AR202747A1 (es) 1975-07-15
NO148460B (no) 1983-07-04
FI60060C (fi) 1981-11-10
NO750753L (es) 1975-09-30
YU37382B (en) 1984-08-31
HU171875B (hu) 1978-04-28
CS209854B2 (en) 1981-12-31
DK144648B (da) 1982-04-26
YU76075A (en) 1983-04-27
US4026115A (en) 1977-05-31
DK144648C (da) 1982-10-04
CH585843A5 (es) 1977-03-15
IN143030B (es) 1977-09-24
JPS50133317A (es) 1975-10-22
JPS5421483B2 (es) 1979-07-31
NO148460C (no) 1983-10-12
SE7503460L (sv) 1975-09-30
NO152763C (no) 1985-11-13
ATA242875A (de) 1984-05-15
PL108892B1 (en) 1980-05-31
LU72168A1 (es) 1975-08-20
HK6979A (en) 1979-02-16
SE435646B (sv) 1984-10-08
IT1044276B (it) 1980-03-20
BE827256A (fr) 1975-09-29
FR2265979B1 (es) 1977-10-14
NL162714C (nl) 1980-06-16
DE2513889A1 (de) 1975-10-09
DK131475A (es) 1975-09-30

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