CN2419375Y - Mixed flow blade rotation and cross section variable turbosupercharger - Google Patents
Mixed flow blade rotation and cross section variable turbosupercharger Download PDFInfo
- Publication number
- CN2419375Y CN2419375Y CN 99257634 CN99257634U CN2419375Y CN 2419375 Y CN2419375 Y CN 2419375Y CN 99257634 CN99257634 CN 99257634 CN 99257634 U CN99257634 U CN 99257634U CN 2419375 Y CN2419375 Y CN 2419375Y
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- fish tail
- blade
- passive
- turbosupercharger
- fork
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Abstract
The utility model relates to a turbosupercharger of a mixed flow blade rotation type with variable cross sections. The utility model is composed of a spiral case, a turbine wheel, rotatable blades of a turbine nozzle ring and a set of mechanical drive mechanism driving rotary nozzle ring blades to rotate around a blade shaft. The utility model reaches the goal of changing free section of turbines by changing the angle of the nozzle ring blades, and thus, matching performance of the turbosupercharger and the engines is improved. The utility model and an actuator are a whole body. The utility model has the advantages of compact structure, reliability, stable and compliant change of free section of turbines, small loss of flow resistance, high turbine efficiency, and low cost.
Description
The utility model is a kind of mixed flow blade-rotation variable-area turbocharger, and it mainly is suitable for the motor on the automobile, engineering machinery, special vehicle of requirement low-speed big, belongs to technical field of engines.
The turbocharging technology of internal-combustion engine can make engine performance be significantly improved.Therefore turbosupercharging not only be used for marine engine, locomotive with internal-combustion engine, transportation formula vehicle with internal-combustion engine, stationary power generation unit with internal-combustion engine, also be used for the various internal-combustion engines in each field of national economy.But turbocharging technology is used to transport formula vehicle internal combustion engine field than later, up to early sixties since radial-flow type small sized turbine pressurized machine succeed in developing and commercialization just developed rapidly, its main cause is that the characteristics of vehicle internal combustion engine require the turbosupercharger size little, reliable in structure, good aeroperformance, can satisfy road and load variations condition extremely complicated in the vehicle driving, and low price etc.In recent years, because haulage vehicle is with the performance improvement of supercharged diesel engine, the increasing substantially of mean effective pressure, thereby ubiquity the low speed torque deficiency, the acceleration extreme difference quickens to smolder, defectives such as cold starting difficulty.The appearance of these problems is different with the working method of pressurized machine mainly due to diesel engine, and the two is difficult to good coupling.Solve these problems targetedly, obtain a kind ofly should the low speed torque performance well requiring the high-speed working condition condition that the good power character and the vehicle power of fuel economy are arranged again, it be the most suitable selecting the variable cross section turbo-charged diesel.
The purpose of this utility model is to provide a kind of turbosupercharger of efficient, reliable, practical novel changable cross section turbine.It has overcome the turbosupercharger that in the past adopts variable geometry turbocharger owing to reasons such as air-flow path shape sudden change gas dams cause turbine efficiency to be lower than conventional defectives such as turbosupercharger, make supercharged diesel engine when low speed, obtain higher boost pressure, keep supercharged diesel engine that good low speed torque performance is arranged, the acceleration of reasonable solution supercharged diesel engine problem such as smolder.On structural configuration, can be accepted by Vehicle Turbocharged diesel engine user on the performance simultaneously.
The utility model is the target that realizes mixed flow blade-rotation variable cross section by following measure: this turbosupercharger is made up of spiral case, rotatable nozzle blade, turbine wheel and rotation controlling mechanism; Rotate controlling mechanism and be arranged on the end of intermediate by turbine, comprising: blade installation dish, drive plate, passive fish tail fork, passive fish tail jaw, active fish tail fork, active fish tail jaw, installing and locating supporting ring, power transmission shaft, transmission shaft Sealing, final controlling element link arm; The passive fish tail fork of nozzle blade and drive blade rotation angle connects; Initiatively one of fish tail jaw is contained in the active fish tail fork, and one is contained in the drive plate, and one of passive fish tail jaw is contained in the drive plate, and one is contained in the passive fish tail fork; The installing and locating supporting ring is housed between pressurized machine intermediate and drive plate; Between power transmission shaft and intermediate, Sealing is housed; Blade installation dish side is an arc step surface, and the blade installation dish compresses mutually by volute and intermediate and is installed on the intermediate.
The utlity model has following advantage: it has kept mixed flow or the high intrinsic advantage of radial-flow turbine booster turbine efficient, has mixed flow and radial-flow turbine pressurized machine can solve supercharged diesel engine low-speed big, instant getaway difference and acceleration specific question such as smolder again.And at serviceability of structures, there are many novel characteristics aspects such as manufacture cost.It obviously is better than with bleed valve adjustable mixed flow and radial-flow turbine pressurized machine.
Description of drawings: Fig. 1 mixed flow rotary blade type variable-area turbocharger structure chart Fig. 2 runoff rotary blade type variable-area turbocharger structure chart Fig. 3 mixed flow rotary blade type variable-area turbocharger governor motion side view Fig. 4 runoff rotary blade type variable-area turbocharger governor motion side view 1 jet blade 2 spiral cases 3 turbine wheels 4 blades installation dishes 5 driving-discs 6 passive fish tails are pitched initiatively fish tail fork 9 active fish tail jaws 10 installation positioning support carrier rings 11 power transmission shafts 12 seals 13 actuator linking arms 14 intermediates 15 pneumatic control actuators of 7 passive fish tail jaws 8
This turbosupercharger is made up of spiral case 2, rotatable nozzle blade 1, turbine wheel 3 and rotation controlling mechanism; The rotation controlling mechanism is arranged on the end of intermediate by turbine, comprising: blade installation dish 4, drive plate 5, passive fish tail fork 6, passive fish tail jaw 7, active fish tail fork 8, active fish tail jaw 9, installing and locating supporting ring 10, power transmission shaft 11, transmission shaft Sealing 12, final controlling element link arm 13.The passive fish tail fork 6 of nozzle blade 1 and drive blade rotation angle connects; Initiatively 9 one of fish tail jaws are contained in the active fish tail fork 8, and one is contained in the drive plate 5, and 7 one of passive fish tail jaws are contained in the drive plate 5, and one is contained in the passive fish tail fork 6; Initiatively fish tail fork 8 is stirred active fish tail jaw 9 and is made drive plate 5 rotations, and drive plate 5 rotates passive fish tail fork 6 by passive fish tail jaw 7; Passive fish tail jaw 7 can slide in passive fish tail fork 6, and initiatively fish tail jaw 9 can slide in active fish tail fork 8; Between pressurized machine intermediate 14 and drive plate 5, installing and locating supporting ring 10 is housed; Between power transmission shaft 11 and intermediate 14, Sealing 12 is housed; Blade installation dish 4 sides are an arc step surface, and blade installation dish 4 is to compress mutually by volute 2 and intermediate 14 to be installed on the intermediate 14.The a whole set of blade-rotation adjustable structure of this turbosupercharger also can be used for the radial-flow turbine pressurized machine.The course of action of entire mechanism is realized as follows: the pressure signal of turbocharger air compressor outlet is by pneumatic actuator link arm 13 rotation angles, driving power transmission shaft 11 rotates with active fish tail fork 8, initiatively fish tail fork 8 is stirred initiatively fish tail jaw 9, because initiatively fish tail jaw 9 is installed on the drive plate 5, make drive plate 5 rotation angles, the passive fish tail jaw 7 that is installed in simultaneously on the drive plate 5 drives passive fish tail fork 6 rotations, nozzle blade 1 is with passive fish tail fork 6 rotations that be connected as a single entity, so the variation of turbocharger air compressor boost pressure can be controlled the variation of nozzle blade 1 angle by this transmission of overlapping mechanism.In this cover mechanism, adopted active jaw, active fork, passive jaw and the passive fork of fish tail type, make whole adjusting more flexible, structure is lighter and handier, has increased the practicability of adjusting mechanism.This blade-rotation variable cross section mixed flow or radial-flow turbine pressurized machine are except parts such as turbine volute, turbine wheel, thermal baffle, in that a cover rotation controlling mechanism has been installed in intermediate near an end of intermediate, nozzle blade can and be rotated around the blade axle center.This cover rotates in the controlling mechanism and comprises: passive fish tail fork, passive fish tail jaw, drive plate, active fish tail fork and compositions such as active fish tail jaw, power transmission shaft and installing and locating supporting ring, to realize changing the angle of nozzle blade, reach the purpose that changes the turbine passage section.The utility model is realized the sealing of high-temperature fuel gas and the reliability of mechanism by following measure.The installing and locating supporting ring at first is housed on drive plate, makes the drive plate loss of stably working and reduce friction.
Claims (1)
1. mixed flow blade-rotation variable-area turbocharger is characterized in that: this turbosupercharger is made up of snail (2), rotatable nozzle blade (1), turbine wheel (3) and rotation controlling mechanism; The rotation controlling mechanism is arranged on the end of intermediate (14) by turbine, comprising: blade installation dish (4), drive plate (5), passive fish tail fork (6), passive fish tail jaw (7), active fish tail fork (8), active fish tail jaw (9), installing and locating supporting ring (10), power transmission shaft (11), transmission shaft Sealing (12), final controlling element link arm (13); The passive fish tail fork (6) of nozzle blade (1) and drive blade rotation angle connects; Initiatively (9) one of fish tail jaws are contained in the active fish tail fork (8), and one is contained in the drive plate (5), and (7) one of passive fish tail jaws are contained in the drive plate (5), and one is contained in the passive fish tail fork (6); Between pressurized machine intermediate (14) and drive plate (5), installing and locating supporting ring (10) is housed; Between power transmission shaft (11) and intermediate (14), Sealing (12) is housed; Blade installation dish (4) side is an arc step surface, and blade installation dish (4) is to compress mutually by volute (2) and intermediate (14) to be installed on the intermediate (14).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN 99257634 CN2419375Y (en) | 1999-12-23 | 1999-12-23 | Mixed flow blade rotation and cross section variable turbosupercharger |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN 99257634 CN2419375Y (en) | 1999-12-23 | 1999-12-23 | Mixed flow blade rotation and cross section variable turbosupercharger |
Publications (1)
Publication Number | Publication Date |
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CN2419375Y true CN2419375Y (en) | 2001-02-14 |
Family
ID=34040473
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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CN 99257634 Expired - Fee Related CN2419375Y (en) | 1999-12-23 | 1999-12-23 | Mixed flow blade rotation and cross section variable turbosupercharger |
Country Status (1)
Country | Link |
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CN (1) | CN2419375Y (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102182546A (en) * | 2011-04-22 | 2011-09-14 | 北京理工大学 | Mixed flow turbocharger with variable nozzle ring |
CN101663472B (en) * | 2007-05-04 | 2012-06-20 | 博格华纳公司 | Variable turbine geometry turbocharger |
CN103806948A (en) * | 2012-11-12 | 2014-05-21 | 霍尼韦尔国际公司 | Turbocharger and variable-nozzle cartridge therefor |
CN104704217A (en) * | 2012-09-28 | 2015-06-10 | 株式会社Ihi | Variable nozzle unit, variable-capacity supercharger, and manufacturing method for power transmission members |
CN106460624A (en) * | 2014-05-19 | 2017-02-22 | 丰田自动车株式会社 | Engine system and control apparatus and control method for engine system |
-
1999
- 1999-12-23 CN CN 99257634 patent/CN2419375Y/en not_active Expired - Fee Related
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN101663472B (en) * | 2007-05-04 | 2012-06-20 | 博格华纳公司 | Variable turbine geometry turbocharger |
CN102182546A (en) * | 2011-04-22 | 2011-09-14 | 北京理工大学 | Mixed flow turbocharger with variable nozzle ring |
CN104704217A (en) * | 2012-09-28 | 2015-06-10 | 株式会社Ihi | Variable nozzle unit, variable-capacity supercharger, and manufacturing method for power transmission members |
CN104704217B (en) * | 2012-09-28 | 2017-04-26 | 株式会社Ihi | Variable nozzle unit, variable-capacity supercharger, and manufacturing method for power transmission members |
US9759086B2 (en) | 2012-09-28 | 2017-09-12 | Ihi Corporation | Variable nozzle unit, variable geometry system turbocharger, and power transmission member manufacturing method |
CN103806948A (en) * | 2012-11-12 | 2014-05-21 | 霍尼韦尔国际公司 | Turbocharger and variable-nozzle cartridge therefor |
CN106460624A (en) * | 2014-05-19 | 2017-02-22 | 丰田自动车株式会社 | Engine system and control apparatus and control method for engine system |
CN106460624B (en) * | 2014-05-19 | 2018-10-23 | 丰田自动车株式会社 | Engine system and control device and control method for engine system |
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Legal Events
Date | Code | Title | Description |
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C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
C19 | Lapse of patent right due to non-payment of the annual fee | ||
CF01 | Termination of patent right due to non-payment of annual fee |