CN108167074A - A kind of Two Stage Turbocharging System height is arbitrarily downgraded booster support construction - Google Patents
A kind of Two Stage Turbocharging System height is arbitrarily downgraded booster support construction Download PDFInfo
- Publication number
- CN108167074A CN108167074A CN201711177012.1A CN201711177012A CN108167074A CN 108167074 A CN108167074 A CN 108167074A CN 201711177012 A CN201711177012 A CN 201711177012A CN 108167074 A CN108167074 A CN 108167074A
- Authority
- CN
- China
- Prior art keywords
- booster
- pressure stage
- exhaust pipe
- engine
- low
- 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
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
- F02B67/00—Engines characterised by the arrangement of auxiliary apparatus not being otherwise provided for, e.g. the apparatus having different functions; Driving auxiliary apparatus from engines, not otherwise provided for
- F02B67/10—Engines characterised by the arrangement of auxiliary apparatus not being otherwise provided for, e.g. the apparatus having different functions; Driving auxiliary apparatus from engines, not otherwise provided for of charging or scavenging apparatus
-
- 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
- F02B37/00—Engines characterised by provision of pumps driven at least for part of the time by exhaust
- F02B37/004—Engines characterised by provision of pumps driven at least for part of the time by exhaust with exhaust drives arranged in series
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Exhaust Silencers (AREA)
- Supercharger (AREA)
Abstract
The present invention provides a kind of Two Stage Turbocharging System height to arbitrarily downgrade booster support construction, including hiigh pressure stage booster, hiigh pressure stage turbine outlet smoke exhaust pipe, booster supporter and low-pressure stage booster；Hiigh pressure stage booster connects the exhaust pipe of engine；Described booster supporter one end is fixed on the engine, and the other end connects hiigh pressure stage turbine outlet smoke exhaust pipe, the hollow space of flange is gas channel below by supporting connection low-pressure stage booster above hollow flange；The hiigh pressure stage turbine outlet smoke exhaust pipe is equipped with can be with the hose construction of adjustment length and angle.The present invention has the advantage that：It is of the invention to be applied to the installation support of secondary engine pressure charging system, in compactedness connection procedure, by a booster supporter with hollow flange, realize that booster support of just arbitrarily downgrading is independent of each other；There is adjustable bellows design structure in two supports of hiigh pressure stage booster simultaneously, can avoid the occurrence of and support positioning.
Description
Technical field
The invention belongs to turbo-charger technical field, arbitrarily downgrade booster more particularly, to a kind of Two Stage Turbocharging System height
Support construction.
Background technology
Turbocharger is to improve engine charge density using the energy of engine discharge exhaust gas, since supercharging is started
The characteristics of high power of machine, low oil consumption, low emission, on the engine using quite extensively.Two Stage Turbocharging System is to adapt at present
Maximum discharge requirement, the gas system scheme of small-sized high-power output engine, can using the boost pressure after two-stage supercharging
It increasing substantially, each independent plenums device can be operated in the working region of greater efficiency, when two boosters work, hair
Motivation range of flow is widened significantly, and the raising of high pressure ratio operating mode boost pressure is that single stage supercharging is unapproachable, can be met very well
Diesel engine improves power and meets the needs of discharge.
But two-stage supercharging is the working method of two boosters, and system bulk weight can increase.Especially two superchargings
The installation fixed form of device on the engine is compared with the increasingly complex difficulty of single-stage supercharger.Hiigh pressure stage booster is smaller, can be by sending out
Motivation exhaust pipe supports, and fixed exhaust connection, low-pressure stage whirlpool are needed between lower pressure stage turbine case and hiigh pressure stage turbine box
After roller box import is fixedly connected with the outlet of hiigh pressure stage turbine box, in order to ensure that booster is solid and reliable, another branch is also needed
Support point.The center of gravity of booster is generally tended on turbine box, fixed supporting point is usually in addition looked on lower pressure stage turbine case, at this time such as
Fruit support is unreliable, it may appear that low-pressure stage booster cantilever vibration causes booster to connect unreliable failure and occurs, while low pressure
Grade turbine box import adds another hiigh pressure stage booster supporting point after being fixed with hiigh pressure stage turbine box outlet connection, it may appear that
Positioning scenarios are crossed, lead to the appearance of initial connection pretightning force.
Invention content
In view of this, the booster support construction the present invention is directed to propose a kind of Two Stage Turbocharging System height is arbitrarily downgraded, to realize
The compact reliability connection of secondary engine pressure charging system, while avoided the occurrence of positioning scenarios.
In order to achieve the above objectives, the technical proposal of the invention is realized in this way：
A kind of Two Stage Turbocharging System height is arbitrarily downgraded booster support construction, and including hiigh pressure stage booster, hiigh pressure stage turbine goes out
Mouth smoke exhaust pipe, booster supporter and low-pressure stage booster；Hiigh pressure stage booster connects the exhaust pipe of engine；The booster branch
Support body one end is fixed on the engine, and the other end is by supporting connection low-pressure stage booster above hollow flange, connection is high below
It arbitrarily downgrades turbine outlet smoke exhaust pipe, the hollow space of flange is gas channel；The hiigh pressure stage turbine outlet smoke exhaust pipe is equipped with can
With the hose construction of adjustment length and angle.
Further, the booster supporter include engine end connector, low-pressure stage booster end connector and in
Between connector, the intermediate connecting body is broken line type, and one end is welded and fixed with engine end connector, the other end and low-pressure stage increasing
Depressor end connector is welded and fixed；The low-pressure stage booster end connector is hollow flange, is pressurized by screw and low-pressure stage
Device and hiigh pressure stage turbine outlet smoke exhaust pipe link together.
Further, the hiigh pressure stage turbine outlet smoke exhaust pipe is equipped with the bellows structure that can be adjusted.
Relative to the prior art, the present invention has the advantage that：
The present invention is applied to the installation support of secondary engine pressure charging system, in compactedness connection procedure, passes through a band
The booster supporter of hollow flange realizes that booster support of just arbitrarily downgrading is independent of each other, realizes secondary engine pressure charging system
Compact reliability connection；There is adjustable bellows design structure in two supports of hiigh pressure stage booster simultaneously, can keep away
Exempt to occur supporting positioning.
Description of the drawings
The attached drawing for forming the part of the present invention is used to provide further understanding of the present invention, schematic reality of the invention
Example and its explanation are applied for explaining the present invention, is not constituted improper limitations of the present invention.In the accompanying drawings：
Fig. 1 arbitrarily downgrades booster support construction schematic diagram for a kind of Two Stage Turbocharging System of embodiment of the present invention height.
Fig. 2 is that a kind of Two Stage Turbocharging System of embodiment of the present invention height is arbitrarily downgraded the vertical view of booster support construction.
Reference sign：
The 1- exhaust pipes of engine, 2- hiigh pressure stage boosters, 3- hiigh pressure stage turbine outlet smoke exhaust pipes, 4- booster supporters,
5- low-pressure stage boosters.
Specific embodiment
It should be noted that in the absence of conflict, the feature in embodiment and embodiment in the present invention can phase
Mutually combination.
The present invention will be described in detail below with reference to the accompanying drawings and in conjunction with the embodiments.
A kind of present invention Two Stage Turbocharging System height is arbitrarily downgraded booster support construction, as shown in Figure 1, 2, is increased including hiigh pressure stage
Depressor 2, hiigh pressure stage turbine outlet smoke exhaust pipe 3, booster supporter 4 and low-pressure stage booster 5；The connection hair of hiigh pressure stage booster 2
Motivation exhaust pipe 1；Described 4 one end of booster supporter is fixed on the engine, and the other end passes through the company of support above hollow flange
Low-pressure stage booster 5 is connect, connects hiigh pressure stage turbine outlet smoke exhaust pipe 3 below, the hollow space of flange is gas channel；The height
Turbine outlet smoke exhaust pipe (3) of arbitrarily downgrading is equipped with can be with the hose construction of adjustment length and angle.
The booster supporter 4 includes engine end connector, low-pressure stage booster end connector and intermediate connecting body,
The intermediate connecting body is broken line type, and one end is welded and fixed with engine end connector, and the other end connects with low-pressure stage booster end
Junctor is welded and fixed；The low-pressure stage booster end connector is hollow flange, passes through screw and low-pressure stage booster 5 and height
Turbine outlet smoke exhaust pipe 3 of arbitrarily downgrading links together.
In order to avoid positioning, the hiigh pressure stage turbine outlet smoke evacuation are crossed in the connection of two supporting points of hiigh pressure stage booster 2
Pipe 3 is equipped with the bellows structure that can be adjusted.
Hiigh pressure stage booster 2 is first connect with the exhaust pipe of engine 1, and hiigh pressure stage booster 2 has been fixed at this time.Starting again
Booster supporter 4 on machine is installed, low-pressure stage booster 5 is installed on booster supporter 4, two boosters can be consolidated
It is fixed, then hiigh pressure stage turbine outlet smoke exhaust pipe 3 is installed.Hiigh pressure stage turbine outlet smoke exhaust pipe 3 is with low-pressure stage booster 5 by hollow
Flange realizes the connection function of tracheae.
The present invention draws a booster supporter 4 with hollow flange from engine, low to carry top support
It arbitrarily downgrades booster 5, it is following to connect hiigh pressure stage turbine outlet smoke exhaust pipe 3, it can be carried to avoid the mutual vibration effect of two boosters
High blower is installed and the reliability of ontology, the hollow space of flange undertake gas channel function simultaneously.Hiigh pressure stage booster
Main support point is on the exhaust pipe of engine 1.
The foregoing is merely illustrative of the preferred embodiments of the present invention, is not intended to limit the invention, all essences in the present invention
With within principle, any modification, equivalent replacement, improvement and so on should all be included in the protection scope of the present invention god.
Claims (4)
- The booster support construction 1. a kind of Two Stage Turbocharging System height is arbitrarily downgraded, it is characterised in that：Including hiigh pressure stage booster (2), Hiigh pressure stage turbine outlet smoke exhaust pipe (3), booster supporter (4) and low-pressure stage booster (5)；Hiigh pressure stage booster (2) connects The exhaust pipe of engine (1)；Described booster supporter (4) one end is fixed on the engine, and the other end is by supporting connection low pressure above hollow flange Grade booster (5) connects hiigh pressure stage turbine outlet smoke exhaust pipe (3) below, and the hollow space of flange is gas channel；The high pressure Grade turbine outlet smoke exhaust pipe (3) is equipped with can be with the hose construction of adjustment length and angle.
- The booster support construction 2. a kind of Two Stage Turbocharging System height according to claim 1 is arbitrarily downgraded, it is characterised in that：Institute It states booster supporter (4) and includes engine end connector, low-pressure stage booster end connector and intermediate connecting body, the centre Connector is broken line type, and one end is welded and fixed with engine end connector, and the other end is welded with low-pressure stage booster end connector It is fixed；The low-pressure stage booster end connector is hollow flange, passes through screw and low-pressure stage booster (5) and hiigh pressure stage whirlpool Wheel outlet smoke exhaust pipe (3) links together.
- The booster support construction 3. a kind of Two Stage Turbocharging System height according to claim 1 is arbitrarily downgraded, it is characterised in that：Institute It states hiigh pressure stage turbine outlet smoke exhaust pipe (3) and is equipped with the bellows structure that can be adjusted.
- The assembly method of booster support construction 4. a kind of Two Stage Turbocharging System height described in claim 1 is arbitrarily downgraded, feature It is to include the following steps：1) hiigh pressure stage booster 2 is first connect with the exhaust pipe of engine 1；2) booster supporter 4 is installed on the engine again；3) low-pressure stage booster 5 on booster supporter 4 is installed, then hiigh pressure stage turbine outlet smoke exhaust pipe 3 is installed.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711177012.1A CN108167074A (en) | 2017-11-22 | 2017-11-22 | A kind of Two Stage Turbocharging System height is arbitrarily downgraded booster support construction |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711177012.1A CN108167074A (en) | 2017-11-22 | 2017-11-22 | A kind of Two Stage Turbocharging System height is arbitrarily downgraded booster support construction |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108167074A true CN108167074A (en) | 2018-06-15 |
Family
ID=62527437
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711177012.1A Pending CN108167074A (en) | 2017-11-22 | 2017-11-22 | A kind of Two Stage Turbocharging System height is arbitrarily downgraded booster support construction |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108167074A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109322736A (en) * | 2018-12-12 | 2019-02-12 | 中国北方发动机研究所(天津) | A kind of two stage turbocharging system |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3576102A (en) * | 1969-05-08 | 1971-04-27 | Allis Chalmers Mfg Co | Turbocharger system |
| US20120255528A1 (en) * | 2009-11-06 | 2012-10-11 | Rolf Gunkel | Pipe arrangement |
| CN202768140U (en) * | 2012-08-29 | 2013-03-06 | 东风汽车有限公司 | Two-stage turbocharging system of engine |
| CN204003079U (en) * | 2011-09-15 | 2014-12-10 | 通用电气公司 | Turbo-charger sytem, engine system and the equipment flowing for delivery of fluid |
| CN102312721B (en) * | 2010-06-30 | 2015-05-27 | 马自达汽车株式会社 | Turbo-charging apparatus for vehicle engine |
| CN104100571B (en) * | 2013-04-09 | 2017-03-22 | Abb涡轮***有限公司 | Housing of a radial compressor |
| JP2017125431A (en) * | 2016-01-13 | 2017-07-20 | 日野自動車株式会社 | Two-stage turbocharger system |
-
2017
- 2017-11-22 CN CN201711177012.1A patent/CN108167074A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3576102A (en) * | 1969-05-08 | 1971-04-27 | Allis Chalmers Mfg Co | Turbocharger system |
| US20120255528A1 (en) * | 2009-11-06 | 2012-10-11 | Rolf Gunkel | Pipe arrangement |
| CN102312721B (en) * | 2010-06-30 | 2015-05-27 | 马自达汽车株式会社 | Turbo-charging apparatus for vehicle engine |
| CN204003079U (en) * | 2011-09-15 | 2014-12-10 | 通用电气公司 | Turbo-charger sytem, engine system and the equipment flowing for delivery of fluid |
| CN202768140U (en) * | 2012-08-29 | 2013-03-06 | 东风汽车有限公司 | Two-stage turbocharging system of engine |
| CN104100571B (en) * | 2013-04-09 | 2017-03-22 | Abb涡轮***有限公司 | Housing of a radial compressor |
| JP2017125431A (en) * | 2016-01-13 | 2017-07-20 | 日野自動車株式会社 | Two-stage turbocharger system |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109322736A (en) * | 2018-12-12 | 2019-02-12 | 中国北方发动机研究所(天津) | A kind of two stage turbocharging system |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN106795805B (en) | Supercharging equipment for internal combustion engine and the operating method for supercharging equipment | |
| CN213743665U (en) | Engine air inlet pipe and engine | |
| KR20060101288A (en) | Internal combustion engine | |
| CN108167074A (en) | A kind of Two Stage Turbocharging System height is arbitrarily downgraded booster support construction | |
| CN107002551A (en) | Two-stage exhaust gas turbocharge device for internal combustion engine | |
| US20120227400A1 (en) | Method and system for improving efficiency of multistage turbocharger | |
| CN203098039U (en) | Two-stage turbocharger applicable to heavy-duty diesel engine | |
| CN109339938A (en) | Three condition two-stage consecutive pressurization system and its control method | |
| CN206942870U (en) | A kind of automobile turbocharger silencer | |
| CN105849384B (en) | Internal-combustion engine system | |
| CN107044326A (en) | A kind of nuclear power generating sets muffler | |
| CN207499955U (en) | Engine turbine heel row tracheae | |
| CN106368800B (en) | A kind of supercharger structure that single shaft dual-air compressor is controllable | |
| CN207161216U (en) | The gas compressor system of supercharger among a kind of band | |
| CN103573386A (en) | A waste gas boost and aftertreatment module for a combustion engine and the combustion engine | |
| CN205349509U (en) | Compound pressure intensifying structure in succession of supercharged diesel engine | |
| CN108087110A (en) | A kind of Two Stage Turbocharging System turbine by-pass self-adaptive regulating | |
| CN103967540B (en) | A kind of turbine cylinder and explosive motor | |
| CN210239936U (en) | Low pressure supercharging device to waste gas reuse | |
| CN206972342U (en) | A kind of nuclear power generating sets muffler | |
| CN103883537A (en) | Turbocharging-type air compressor | |
| CN109322736A (en) | A kind of two stage turbocharging system | |
| CN206309471U (en) | A kind of two-stage supercharging device of engine | |
| CN203488250U (en) | Two-stage turbo-supercharger adopting variable-cross-section supercharger | |
| CN112377295A (en) | Multi-cylinder engine capable of stopping cylinder |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20180615 |
|
| RJ01 | Rejection of invention patent application after publication |