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IL41922A - Supercharged internal combustion engines - Google Patents

Supercharged internal combustion engines

Info

Publication number
IL41922A
IL41922A IL41922A IL4192273A IL41922A IL 41922 A IL41922 A IL 41922A IL 41922 A IL41922 A IL 41922A IL 4192273 A IL4192273 A IL 4192273A IL 41922 A IL41922 A IL 41922A
Authority
IL
Israel
Prior art keywords
power unit
unit according
pressure
throttle
pass
Prior art date
Application number
IL41922A
Other versions
IL41922A0 (en
Inventor
J Melchior
Original Assignee
France Etat
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 France Etat filed Critical France Etat
Publication of IL41922A0 publication Critical patent/IL41922A0/en
Publication of IL41922A publication Critical patent/IL41922A/en

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
    • F02B37/04Engines with exhaust drive and other drive of pumps, e.g. with exhaust-driven pump and mechanically-driven second pump
    • 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
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B75/00Other engines
    • F02B75/02Engines characterised by their cycles, e.g. six-stroke
    • F02B2075/022Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle
    • F02B2075/025Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle two
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B2275/00Other engines, components or details, not provided for in other groups of this subclass
    • F02B2275/14Direct injection into combustion chamber
    • 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
    • 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
    • F23R2900/00Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/00001Arrangements using bellows, e.g. to adjust volumes or reduce thermal stresses
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Supercharger (AREA)
  • Output Control And Ontrol Of Special Type Engine (AREA)
  • Exhaust-Gas Circulating Devices (AREA)
  • Control Of The Air-Fuel Ratio Of Carburetors (AREA)
  • Fuel-Injection Apparatus (AREA)

Claims (29)

41922/3: WHA WE CLAIM IS :
1. A power unit comprising an internal combustion engine supercharged by a turbine-compressor unit v:hose turbine has an inlet connected to the exhaust of the engine and comprising a by-pass conduit permanently open in operation, communicating with the outlet of the compressor and with the turbine inlet for the engine to be in parallel air flow relation with the by-pass, said by-pass having automatically controlled throttle means to develop a pressure drop in the air flow passing through the by-pass which is substantially independent of the rate of flow traversing said by-pass and which is an increasing function of the pressure existing at the compressor outlet. · ■ ' '
2. A power unit according to claim 1, wherein the increasing function is a linear or substantially linear function.
3. A power unit comprising an internal combustion engine supercharged by a turbine-compressor unit whose compressor operates close to its surge line and whose turbine is connected to receive the exhaust gas of the engine and an air flow delivered by the compressor and which has circulated along a conduit permanently open in operation and by-passing the engine, the pressure drop of said air flow · being an increasing function of the pressure delivered by the compressor. 41922/3
4. A power unit according to claim 2, having automatically controlled throttle means in said by-pass conduit to develop said pressure drop.
5. A power unit according to claim 1, 2 or 4, wherein the throttle means comprises a movable throttle member which limits in said by-pass conduit a throttled . section whose cross-sectional area is determined by the position of said movable member and wherein 'the throttling action of said member tends to increase responsive to increase of the pressure which prevails at a point of the by-pass located upstream of said throttled section and to decrease v/hen the difference between, the pressures which prevail at points of the by-pass located upstream and downstream of said throe Lied section decreases.
6. A power unit according to claim 1, 2 or 4, wherein the throttle means comprises a movable throttle member which limits a throttled section in said by-pass conduit and said movable member is controlled by pressure forces exerted on surfaces which are subjected to the pressures which prevail in said by-pass conduit upstream and downstream of said throttled section, the resultant surface which is subjected to the pressure which prevails upstream of the throttled section being smaller than the - resultant surface subjected to the pressure which prevails donwstrea of the throttled section. 41922/:?
7. A power unit according to claim 1, 2 or 4, wherein the throttle means comprises a throttle member movable within the by-pass conduit and cooperating with a fixed seat for limiting a throttled air flow section of variable effective cross-sectional area.
8. A power unit according to claim 5, 6 or 7, v/herein said throttle member is oparatively connected to a balancing piston which is subjected to the pressure which prevails at a point of the by-pass conduit. '■■
9. A power unit according to anyone of claims 5 to 8, having resilient return means associated with said throttle member and which maintains the throttle means in open condition when atmospheric pressure prevails in the by-pass conduit on both sides of the throttled section.
10. A power uni according to claim 9, wherein said resilient return means is adjustable.
11. A power unit according to anyone of claims 1, 2 and 4-10, wherein said throttle means is provided v/ith viscous damping means.
12. A power uni according to any one of claims 1 to 11, having an auxiliary combustion chamber connected to receive air which has passed through the by-pass conduit and having its outlet connected to the inlet ■ . '.· , ..' , 41922/3
13. A power unit according to claim 12, wherein said auxiliary combustion chamber has a fuel inlet, a ^primary- air intake connected to receive fresh air derived from a point of said by-pass located upstream of said throttling means for combustion of the fuel injected into said auxiliary combustion chamber and a secondary air intake adapted to receive air from said by-pass conduit through throttling means providing said pressure drop. s
14. A power unit according to claim .13, having means for adjusting the flow rate of the primary air which is responsive to the pressure which prevails at a point of the by-pass conduit which is located upstream or downs 'cream o the throttling means.
15. A power unit according to claim 14, wherein said adjusting means comprises a f rst member and a second member movable with respect to each other to adjust the effective cross-sectional area of a passage for said primary air, the first member of the adjusting means being operatively connected to a movable throttle member Of said throttle means and the second member of said adjusting means being controlled by the pressure which prevails downstream of said throttle means.
16. A power unit according to claim 15, wherein said second member of the primary air adjusting means 41922/3 member of said primary air adjusting means which is fast with the movable member of the throttling means.
17. A power unit according to claim 16, wherein said first member of the primary air adjusting means comprises a tube having a first opening in its wall and wherein said second member is a tubular slide valve consisting of a blind tube formed with a second opening adapted to cooperate with said first opening and slidably received in said tube.
18. A power unit according to any one of claims 14-17, wherein the primary air adjusting means actuates a device for adjusting the flow-rate of fuel injected into the auxiliary combustion chamber so as to maintain a substantially stoechiorhetrlc ratio between the flow-rates of primary air and fuel.
19. A pov/er unit according to claim 18, wherein ' the primary air adjusting means and" the fuel flow adjusting device are located in a movable member of the throttle means.
20. A po er unit according to claim.15 or 16, wherein said movable throttle member is formed with a tubular extension and the,.primary air adjusting means comprises at least one port formed in said tubular extension and adapted to be covered by a slide valve having an actuation surface subjected to the pressure existing in the downstream or u stream art of the b - ass i e and 41922/3: another actuation surface subjected to a counter pressure and to the action o a spring, said slide valve being connected to the adjusting means.
21. A power unit according to claim 20, wherein said counter pressure is pneumatic.
22. A power unit according to claim 21, wherein Λ said counter pressure is equal to or greater than atmospheric pressure.
23. A power unit according to claim 21, wherein said counter pressure is the pressure' in a regulation chamber connected to the admission of the engine through a needle adjustment device and provided with a calibrated air leak.
24. A power unit according to claim S or 19, in which the auxiliary combustion chamber is supplied by an injector of the return type, as herein defined, the means for adjusting the flow rate of fuel comprises a movable member determining the effective cross- sectional area of a variable nozzle as a function of the position of said movable member, said nozzle being arranged on a return path from the injector.
25. A power unit according to claim 18 or 19, in which the auxiliary combustion chamber is supplied by an injector of the non return type, as herein defined, . ' 41922/3 / wherein the means for adjusting the flow rate of fuel comprises a movable member determining the effective cross-sectional area of a variable nozzle as a function of1. he position of said movable member, said' nozzle being arranged on a passage through which high pressure ' fuel flows to the injector.
26. Λ power unit according to claim 24 or 25, wherein the variable nozzle comprises a needle with a conical portion adapted to project into an orifice by a variable extent.
27. A power unit according to claim 25 or 26, comprising a sliding valve regulator comprising a chamber placed in communication with the pressure of fuel upstream of the fuel flow adjusting device,, and a chamber placed in communication with the pressure of fuel donwstrea of the regulating device, this slide valve regulator covering or uncovering a port placing the first of the tv/o said chambers in communication with a delivery pipe.
28. A power unit .according to claim 27, wherein the slide valve regulator comprises a piston separating the two said chambers and subjected to the action of a spring acting in a direction opposite to the difference of pressure existing in the two said chambers.
29.. A power unit constructed and arranged substantially as hereinbefore described with reference to and as illustrated in the accompanying drawings .' , For the Applicants '^1 DR. REINH0¾D C<¾ AND PARTNERS By:
IL41922A 1972-04-06 1973-03-30 Supercharged internal combustion engines IL41922A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7212113A FR2179310A5 (en) 1972-04-06 1972-04-06

Publications (2)

Publication Number Publication Date
IL41922A0 IL41922A0 (en) 1973-06-29
IL41922A true IL41922A (en) 1976-03-31

Family

ID=9096433

Family Applications (1)

Application Number Title Priority Date Filing Date
IL41922A IL41922A (en) 1972-04-06 1973-03-30 Supercharged internal combustion engines

Country Status (27)

Country Link
JP (2) JPS522041B2 (en)
AR (1) AR205327A1 (en)
AT (1) AT338567B (en)
AU (1) AU462539B2 (en)
BE (1) BE797857A (en)
BR (1) BR7302471D0 (en)
CA (1) CA990160A (en)
CH (1) CH565940A5 (en)
CS (1) CS207320B2 (en)
DD (1) DD103300A5 (en)
DK (2) DK140443C (en)
ES (2) ES413178A1 (en)
FI (1) FI55561C (en)
FR (1) FR2179310A5 (en)
GB (1) GB1429493A (en)
HK (1) HK43177A (en)
HU (1) HU168199B (en)
IL (1) IL41922A (en)
IN (1) IN138616B (en)
MY (1) MY8100102A (en)
NL (1) NL157688B (en)
NO (1) NO143816C (en)
PL (1) PL85207B1 (en)
SE (1) SE401236B (en)
SU (1) SU650517A3 (en)
YU (1) YU36797B (en)
ZA (1) ZA732223B (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS58195581A (en) * 1982-05-10 1983-11-14 ブラザー工業株式会社 Safety apparatus of sewing machine for stitching button hole
DE102009034510A1 (en) * 2009-07-24 2011-04-14 Bayerische Motoren Werke Aktiengesellschaft Vehicle with a supercharged combustion engine and method for operating a vehicle with a supercharged combustion engine
DE102014113550B3 (en) * 2014-09-19 2016-03-31 Pierburg Gmbh Adjusting element for a diverter valve

Also Published As

Publication number Publication date
CH565940A5 (en) 1975-08-29
ZA732223B (en) 1974-03-27
MY8100102A (en) 1981-12-31
ATA275673A (en) 1976-12-15
DK140443C (en) 1980-01-28
NL7304457A (en) 1973-10-09
ES413178A1 (en) 1976-01-16
CS207320B2 (en) 1981-07-31
JPS5018815A (en) 1975-02-27
AT338567B (en) 1977-09-12
JPS5874829A (en) 1983-05-06
DE2316027A1 (en) 1973-10-11
AR205327A1 (en) 1976-04-30
PL85207B1 (en) 1976-04-30
NO143816C (en) 1981-04-15
AU462539B2 (en) 1975-06-26
FI55561C (en) 1979-08-10
IN138616B (en) 1976-02-28
FR2179310A5 (en) 1973-11-16
SU650517A3 (en) 1979-02-28
NL157688B (en) 1978-08-15
YU89673A (en) 1982-02-25
BR7302471D0 (en) 1974-06-27
DE2316027B2 (en) 1977-07-07
JPS646328B2 (en) 1989-02-02
HU168199B (en) 1976-03-28
HK43177A (en) 1977-09-02
DD103300A5 (en) 1974-01-12
DK143518B (en) 1981-08-31
JPS522041B2 (en) 1977-01-19
CA990160A (en) 1976-06-01
BE797857A (en) 1973-10-08
GB1429493A (en) 1976-03-24
SE401236B (en) 1978-04-24
DK143518C (en) 1982-01-04
AU5414573A (en) 1974-10-10
DK140443B (en) 1979-08-27
ES131178A3 (en) 1933-08-16
NO143816B (en) 1981-01-05
FI55561B (en) 1979-04-30
IL41922A0 (en) 1973-06-29
YU36797B (en) 1984-08-31

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