GB2305974A - Reducing turbocharger lag - Google Patents

Reducing turbocharger lag Download PDF

Info

Publication number
GB2305974A
GB2305974A GB9511830A GB9511830A GB2305974A GB 2305974 A GB2305974 A GB 2305974A GB 9511830 A GB9511830 A GB 9511830A GB 9511830 A GB9511830 A GB 9511830A GB 2305974 A GB2305974 A GB 2305974A
Authority
GB
United Kingdom
Prior art keywords
charge
turbocharger
compressor
heat
compressed
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.)
Granted
Application number
GB9511830A
Other versions
GB9511830D0 (en
GB2305974B (en
Inventor
Adrian Graham Alford
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 GB9511830A priority Critical patent/GB2305974B/en
Publication of GB9511830D0 publication Critical patent/GB9511830D0/en
Publication of GB2305974A publication Critical patent/GB2305974A/en
Application granted granted Critical
Publication of GB2305974B publication Critical patent/GB2305974B/en
Anticipated expiration legal-status Critical
Expired - Fee Related 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
    • F02B37/04Engines with exhaust drive and other drive of pumps, e.g. with exhaust-driven pump and mechanically-driven second pump
    • F02B37/10Engines with exhaust drive and other drive of pumps, e.g. with exhaust-driven pump and mechanically-driven second pump at least one pump being alternatively or simultaneously driven by exhaust and other drive, e.g. by pressurised fluid from a reservoir or an engine-driven 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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D25/00Pumping installations or systems
    • F04D25/02Units comprising pumps and their driving means
    • F04D25/04Units comprising pumps and their driving means the pump being fluid-driven
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D27/00Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids
    • F04D27/02Surge control
    • F04D27/0207Surge control by bleeding, bypassing or recycling fluids
    • 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

For reducing turbocharger lag when increased power is required from a so-equipped engine 7, operating at part load, its compressor 8, is provided with nozzles or directing devices 3, designed to increase the speed of the rotor (9)(figures 1 and 2) or to rotate the charge entering the compressor. The devices 3, are supplied by recirculating compressed charged, via a distributor valve 2. A heat source such as a heat exchanger 4, (with a shunt 5, controlled by a distributor valve 6) using waste heat from exhaust gases, can heat the recirculating charge, thereby increasing the energy of the recirculated charge to further increase the rotational speed of the rotor or charge. Compressed air supplied to the engine 7, may pass through a cooler 10. The tendency of the turbocharger to surge may also be reduced.

Description

DEVICE FOR IMPROVING TURBOCHARGER DYNAMIC CHARACTERISTICS This invention relates to a turbocharger system for an internal combustion engine.
The problems with the use of the turbocharger with the internal combustion engine are well documented. One is known as "throttle lag and is caused by the low speed of the turbocharger rotor when the engine is operated at part load, combined with the energy required to overcome its inertia and accelerate the rotor to a speed where sufficient boost is created when increased power is required. If the rotor can be made to rotate at a greater speed at engine part load requirement by a reduction in compressor work and/or some additional work input, this problem could be alleviated very substantially.
Other benefits can accrue from this course of action, including a reduced tendency to turbocharger surge, and reduction of losses to throttling in the spark ignition engine.
According to the present invention the induction system of an internal combustion engine is provided with valve means to recirculate some portion of the compressed charge to the low pressure side of the compressor with some recovery of the energy expended in its compression by means of one or more nozzles or directing devices arranged so that the stream of this charge should impinge on the blades of the impellor so as to impart energy on them in their direction of rotation or cause the charge entering the compressor to rotate in the aforementioned direction.
This devised approach will have the effect of increasing the rotational speed of the rotor. A heat source, possibly a heat exchanger using waste heat from exhaust gases, can be provided to heat the recirculating charge between the two pressure regimes, the increase in the energy of this recirculated charge causing a further increase in the rotational speed of the rotor.
There will also be an additional effect due to the heating of the charge being delivered to the compressor and engine with further advantages accruing. Heated air, though requiring greater energy per unit mass for compression through a given ratio, has a lower energy requirement per unit volume for a similar compression, due to its lower density. It logically follows from this that for a given charge air density requirement at the engine, operating at some part of its rating, less throttling of the charge is required, reducing pumping losses at the engine and increasing turbocharger rotor speed.
With use with engines using variable valve timing as a load control means, the deficiency in charge temperature prior to ignition, which can have adverse effects on ignition and combustion, can be reduced.
Occurence of surge in the compressor can be reduced, due to the increase in mass flowrate through the compressor when this type of charge recirculation is operated, and a reduction in turbocharger pressure ratio is also anticipated within embodiments of the invention.
By means of a shunt and distributor valve to bypass the heat source of the recirculatory system and/or a shunt and distributor valve to bypass any chargecooler, the optimum temperature and density of charge reaching the cylinders can be provided.
A circumferentially split volute with more than one chamber where one chamber is arranged to be able to cause the charge to be compressed to a greater pressure - to be recirculated in any of the manners described in the above paragraphs - could be used within the context of this invention to achieve greater efficiency of operation.
Valve means can be provided to allow inflow of charge from the substantially atmospheric side of the induction system to the nozzle(s) or directing device(s) to increase the flow capacity of the compressor and decrease the incidence of compressor choke. The valve means shall be arranged to prevent compressed charge from venting through the recirculatory system to the substantially atmospheric side of the induction system.
One embodiment of the turbocharger system according to the invention is shown in figures 1, 2 and 3. Figure 1 shows a section of a turbocharger compressor 8 with impellor 9 and nozzles 3. Figure 2 shows another section through a similarly equiped compressor. Figure 3 shows the turbocharger system diagrammatically with reference numeral 1 indicating a turbocharger and 7 an internal combustion engine. The engine feed charge passes into the centrifugal compressor 8 from which it passes into inlet manifold 11. From here it passes to distributor valve 2 where some portion can be diverted to the charge recycling apparatus at engine part load. The remainder of the charge passes to the engine. The charge in the recycling apparatus then encounters distributor valve 6 where it can be directed in variable proportions to exhaust gas heat exchanger 4 and shunt 5. The charge then passes to nozzles 3 where it re-enters compressor 8, impingeing on the blades of the impellor, causing the impellor to rotate at greater speed.
Numeral 10 indicates a chargecooler.

Claims (5)

1) A turbocharger provided with valve means to recirculate some portion of the compressed charge to the low pressure side of the compressor with some recovery of the energy expended in its compression by means of one or more nozzles or directing devices arranged so that the stream of this charge should impinge on the blades of the impellor so as to impart energy upon them in their direction of rotation or cause the charge entering the compressor to rotate in this direction.
2) A turbocharger as claimed in claim 1) characterised in that a heat source, possibly a heat exchanger using waste heat from exhaust gases, is provided to heat the recirculating charge between the two pressure regimes.
3) A turbocharger as claimed in claim 2) characterised in that a shunt and distributor valve are provided to bypass the heat source of the recirculatory system.
4) A turbocharger as claimed in claim 1), claim 2) or claim 3) characterised in that a circumferentially split volute with more than one chamber is used, where one chamber is arranged to be able to cause the charge to be compressed to a greater pressure for subsequent recirculation.
5) A turbocharger as claimed in claim 1), claim 2), claim 3) or claim 4) characterised in that valve means are provided to allow inflow of charge from the substantially atmospheric side of the induction system to the nozzles or directing devices. The valve means shall be arranged to prevent compressed charge from venting through the recirculatory system to the substantially atmospheric side of the induction system.
GB9511830A 1995-06-10 1995-06-10 Device for improving turbocharger dynamic characteristics Expired - Fee Related GB2305974B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB9511830A GB2305974B (en) 1995-06-10 1995-06-10 Device for improving turbocharger dynamic characteristics

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB9511830A GB2305974B (en) 1995-06-10 1995-06-10 Device for improving turbocharger dynamic characteristics

Publications (3)

Publication Number Publication Date
GB9511830D0 GB9511830D0 (en) 1995-08-09
GB2305974A true GB2305974A (en) 1997-04-23
GB2305974B GB2305974B (en) 1999-08-11

Family

ID=10775871

Family Applications (1)

Application Number Title Priority Date Filing Date
GB9511830A Expired - Fee Related GB2305974B (en) 1995-06-10 1995-06-10 Device for improving turbocharger dynamic characteristics

Country Status (1)

Country Link
GB (1) GB2305974B (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1998040613A1 (en) * 1997-03-11 1998-09-17 Adrian Graham Alford Device for improving turbocharger dynamic characteristics
US7010916B2 (en) * 2003-06-07 2006-03-14 Daimlechrysler Ag Exhaust-gas turbocharger
US20120266593A1 (en) * 2007-01-19 2012-10-25 Cummins Turbo Technologies Limited Compressor
US9157446B2 (en) 2013-01-31 2015-10-13 Danfoss A/S Centrifugal compressor with extended operating range
US10962016B2 (en) 2016-02-04 2021-03-30 Danfoss A/S Active surge control in centrifugal compressors using microjet injection

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1510070A (en) * 1975-10-17 1978-05-10 Bbc Brown Boveri & Cie Two-stage exhaust-gas turbocharger with two coaxial shafts one inside the other
US4517803A (en) * 1983-04-22 1985-05-21 The Garrett Corporation Turbocharger compressor valve
EP0174867A2 (en) * 1984-09-14 1986-03-19 AlliedSignal Inc. Hydraulic assist turbocharger system and method for its operation
GB2170866A (en) * 1985-02-09 1986-08-13 Man B & W Diesel Gmbh Turbocharger
US4817387A (en) * 1986-10-27 1989-04-04 Hamilton C. Forman, Trustee Turbocharger/supercharger control device
GB2268228A (en) * 1992-06-24 1994-01-05 Rover Group A compressor surge control system.
GB2277129A (en) * 1993-04-13 1994-10-19 Daimler Benz Ag Exhaust gas turbocharger
GB2282643A (en) * 1993-10-09 1995-04-12 Abb Management Ag Exhaust gas turbocharger

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1510070A (en) * 1975-10-17 1978-05-10 Bbc Brown Boveri & Cie Two-stage exhaust-gas turbocharger with two coaxial shafts one inside the other
US4517803A (en) * 1983-04-22 1985-05-21 The Garrett Corporation Turbocharger compressor valve
EP0174867A2 (en) * 1984-09-14 1986-03-19 AlliedSignal Inc. Hydraulic assist turbocharger system and method for its operation
GB2170866A (en) * 1985-02-09 1986-08-13 Man B & W Diesel Gmbh Turbocharger
US4817387A (en) * 1986-10-27 1989-04-04 Hamilton C. Forman, Trustee Turbocharger/supercharger control device
GB2268228A (en) * 1992-06-24 1994-01-05 Rover Group A compressor surge control system.
GB2277129A (en) * 1993-04-13 1994-10-19 Daimler Benz Ag Exhaust gas turbocharger
GB2282643A (en) * 1993-10-09 1995-04-12 Abb Management Ag Exhaust gas turbocharger

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1998040613A1 (en) * 1997-03-11 1998-09-17 Adrian Graham Alford Device for improving turbocharger dynamic characteristics
US7010916B2 (en) * 2003-06-07 2006-03-14 Daimlechrysler Ag Exhaust-gas turbocharger
US20120266593A1 (en) * 2007-01-19 2012-10-25 Cummins Turbo Technologies Limited Compressor
US8820073B2 (en) * 2007-01-19 2014-09-02 Cummins Turbo Technologies Limited Compressor
US9157446B2 (en) 2013-01-31 2015-10-13 Danfoss A/S Centrifugal compressor with extended operating range
US10184481B2 (en) 2013-01-31 2019-01-22 Danfoss A/S Centrifugal compressor with extended operating range
US10962016B2 (en) 2016-02-04 2021-03-30 Danfoss A/S Active surge control in centrifugal compressors using microjet injection

Also Published As

Publication number Publication date
GB9511830D0 (en) 1995-08-09
GB2305974B (en) 1999-08-11

Similar Documents

Publication Publication Date Title
US6625986B2 (en) IC engine-turbocharger unit for a motor vehicle, in particular an industrial vehicle, with turbine power control
US7127893B2 (en) Internal combustion engine comprising a compressor in the induction tract
US10107180B2 (en) Two-stage supercharging internal combustion engine having an exhaust-gas aftertreatment arrangement, and method for operating a two-stage supercharged internal combustion engine
US4404805A (en) Method of and system for power generation by supercharged internal combustion engine
US6901759B2 (en) Method for operating a partially closed, turbocharged gas turbine cycle, and gas turbine system for carrying out the method
US8281587B2 (en) Supercharged boost-assist engine brake
US8312720B2 (en) Method for controlling an engine braking device of an internal combustion engine and internal combustion engine for a motor vehicle
US6701710B1 (en) Turbocharged engine with turbocharger compressor recirculation valve
US4428192A (en) Turbocharged internal combustion engine
JPS61164039A (en) Multistage turbo supercharged engine
EP1348849A2 (en) Engine turbocompressor controllable bypass system and method
US20060059909A1 (en) Supercharged internal combustion engine
SE517844C2 (en) Combustion engine arrangement and procedure for reducing harmful emissions
GB2425332A (en) Providing swirl to the compressor of a turbocharger
US3570240A (en) Supercharging apparatus for diesel and multifuel engines
US5400597A (en) Turbocharger system with electric blower
CN111102064A (en) Method for operating an internal combustion engine system
JP2598060B2 (en) Method for controlling the working cycle of an internal combustion engine and its implementation
JPS58187521A (en) Exhaust gas turbo overcharger
GB2305974A (en) Reducing turbocharger lag
JPS63309727A (en) Exhaust gas treatment device for internal combustion engine with exhaust turbosupercharger
WO1998040613A1 (en) Device for improving turbocharger dynamic characteristics
JPH03164526A (en) Compound internal combustion engine
JPH09256814A (en) Diesel engine plant
EP4206446A1 (en) Air intake system for a vehicle's internal combustion engine

Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee

Effective date: 19991111