WO2013104091A1 - Segmented volute casing with guide vanes - Google Patents

Segmented volute casing with guide vanes Download PDF

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Publication number
WO2013104091A1
WO2013104091A1 PCT/CN2012/000429 CN2012000429W WO2013104091A1 WO 2013104091 A1 WO2013104091 A1 WO 2013104091A1 CN 2012000429 W CN2012000429 W CN 2012000429W WO 2013104091 A1 WO2013104091 A1 WO 2013104091A1
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WO
WIPO (PCT)
Prior art keywords
volute
intake
flow passage
passage
air
Prior art date
Application number
PCT/CN2012/000429
Other languages
French (fr)
Chinese (zh)
Inventor
王航
王艳霞
袁道军
朱智富
李永泰
宋丽华
Original Assignee
Wang Hang
Wang Yanxia
Yuan Daojun
Zhu Zhifu
Li Yongtai
Song Lihua
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 Wang Hang, Wang Yanxia, Yuan Daojun, Zhu Zhifu, Li Yongtai, Song Lihua filed Critical Wang Hang
Publication of WO2013104091A1 publication Critical patent/WO2013104091A1/en
Priority to US14/328,676 priority Critical patent/US20140321992A1/en

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D17/00Regulating or controlling by varying flow
    • F01D17/10Final actuators
    • F01D17/12Final actuators arranged in stator parts
    • F01D17/14Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
    • F01D17/141Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of shiftable members or valves obturating part of the flow path
    • F01D17/145Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of shiftable members or valves obturating part of the flow path by means of valves, e.g. for steam turbines
    • 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
    • F02B37/24Control of the pumps by using pumps or turbines with adjustable guide vanes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D9/00Stators
    • F01D9/02Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/026Scrolls for radial machines or engines
    • 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
    • F02B37/02Gas passages between engine outlet and pump drive, e.g. reservoirs
    • F02B37/025Multiple scrolls or multiple gas passages guiding the gas to the pump drive
    • 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
    • F02B37/22Control of the pumps by varying cross-section of exhaust passages or air passages, e.g. by throttling turbine inlets or outlets or by varying effective number of guide conduits
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00Application
    • F05D2220/40Application in turbochargers
    • 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

Definitions

  • the present invention relates to a segmented volute, and more particularly to a segmented volute with guide vanes that can work independently and work together to meet the performance requirements of various operating conditions of the engine, and belongs to the field of internal combustion engines. Background technique:
  • variable-section turbocharger can effectively control the exhaust pressure of the engine.
  • the supercharger and the engine achieve good performance matching under various working conditions and become the focus of research and development.
  • the low-speed torque of the engine using the variable-section supercharger is greatly improved.
  • the problem is that the engine's intake and exhaust negative pressure difference is very high, and the pumping loss is too high, resulting in low-speed engine operating conditions.
  • the fuel consumption is high.
  • Patent CN101694166A discloses a two-layer flow passage variable-section turbine control device, which comprises a turbine casing, and two inner and outer intake runners are arranged in the turbine casing, and the valve adjusts the opening of the valve through a valve control mechanism under high operating conditions in the engine.
  • the degree of intake air entering the outer flow passage of the volute intake air is adjusted to realize the function of variable cross section.
  • the structure has a limited increase in the boost ratio under high-speed engine conditions.
  • the problem to be solved by the present invention is to provide a method for effectively solving the hysteresis of the supercharger when the engine is in a low speed condition, and to improve the supercharging ratio when the engine is in a high speed condition, in order to solve the limitation of the variable section supercharger.
  • the present invention adopts the following technical solutions:
  • a segmented volute with guide vanes including a turbine volute;
  • the turbine volute is provided with a volute inlet flow passage and a volute expansion passage, and the turbine volute is respectively provided with a volute air inlet communicating with the volute intake flow passage and communicating with the volute diffusion passage a volute air outlet;
  • a left side pneumatic partition and a right side pneumatic partition are arranged in the volute inlet flow passage;
  • the ⁇ the side pneumatic baffle and the right pneumatic baffle partition the volute inlet flow passage into the volute left intake air flow passage, the volute intake air flow passage and the volute right intake air flow passage;
  • An air intake adjustment control device is respectively disposed at a position of the outer ventilating outer flow passage on the left side of the volute and the outer air intake outer flow passage on the right side of the volute near the vent inlet of the volute.
  • the air intake adjusting control device includes an air intake adjusting valve respectively installed at an air inlet of the left outer air intake passage of the volute and the outer air flow passage of the right side of the volute,
  • the intake adjustment valve drive is connected with an intake adjustment control actuator;
  • the two intake regulating valves are closed at the same time, that is, the left outer air intake passage of the volute and the outer helium outer flow passage of the volute are simultaneously closed; the volute helium inner flow passage is separately Working status
  • the intake adjustment valve installed at the intake port of the intake air passage on the left side of the volute is closed, and the intake air flow passage on the left side of the volute is closed, and the intake air flow on the right side of the volute
  • the inner passage of the passage and the volute intake air are in working condition
  • the two intake regulating valves are simultaneously opened, and the inner flow passage of the volute casing, the outer flow passage of the left side of the volute and the outer flow passage of the right side of the volute are simultaneously in working state.
  • the air inlet of the inner flow passage of the volute air inlet communicates with the air inlet of the volute, and the air inlet of the left outer air inlet of the volute and the air inlet of the outer air flow of the right side of the volute respectively
  • the air inlets of the inner air passage of the shell inlet are connected.
  • the left outer air intake flow passage of the volute and the right outer air intake outer flow passage of the volute are respectively located on both sides of the inner flow passage of the volute casing and are arranged side by side in parallel.
  • the left outer air intake outer flow passage of the volute and the right outer air intake outer flow passage of the volute are respectively located at two sides of the inner flow passage of the volute casing, and the cross section of the left outer air intake passage of the volute is curved, and the outer portion thereof The end extends to the outside of the inner flow passage of the volute intake.
  • the cross-sectional area of the outer air intake passage on the left side of the volute is larger than the cross-sectional area of the outer air flow passage on the right side of the volute.
  • the sum of the cross-sectional areas of the left outer air intake passage and the right outer air passage of the right side of the volute is a volute
  • the cross-sectional area of the inner flow passage of the intake air is 0.3-1.1 times.
  • a vane-free nozzle is respectively disposed at a position of the outer ventilating outer flow passage on the left side of the volute, the outer side outer flow passage of the volute casing, and the inner flow passage of the volute casing near the volute diffusing passage.
  • a plurality of airfoil-type pneumatic guide vanes are uniformly arranged in a ring shape near the vaneless nozzle in the left outer air inlet passage of the volute.
  • one end of the guiding vane is integrally casted and connected with the inner wall of the outer side of the outer side of the volute, and the other end is integrally casted with the inner wall of the left side of the outer side of the outer side of the volute.
  • a left outer flow passage control chamber is provided between the left outer air intake outer flow passage of the volute and the air inlet of the left outer air intake passage of the volute; the outer right outer flow passage of the volute
  • a right outer flow channel control chamber is arranged between the air inlets of the outer air intake passage on the right side of the volute.
  • the intake air regulating valve installed at the intake port of the intake air flow passage on the left side of the volute is located in the left outer flow passage control room;
  • the intake air regulating valve installed at the intake port of the intake air flow passage on the right side of the volute is located in the right outer flow passage control chamber.
  • Step-by-step improvement The upper outer runner control chamber and the right outer runner control chamber are respectively provided with upper outer runner end caps to achieve sealing of the intake air flow and limit of the intake air regulating valve.
  • the inner flow passage of the volute casing is a normally open intake flow passage
  • the outer air inlet outer passage of the volute and the right outer air passage of the volute are open under the control of the intake regulation control actuator or Closed
  • the intake air regulating wide door is driven by the air intake adjusting control actuator, and the outer air inlet outer flow passage of the volute and the outer air inlet outer flow passage of the volute are simultaneously closed, at this time, All the exhaust gas discharged from the engine only flows through the inner flow passage of the volute casing.
  • the intake regulating valve of the outer air intake passage of the right side of the volute When the engine is in the medium speed condition range, the intake regulating valve of the outer air intake passage of the right side of the volute is fully opened by the air intake adjusting control actuator, thereby opening the outer air inlet passage of the right side of the volute.
  • the inner flow passage of the volute inlet and the outer flow passage of the right side of the volute work together, and the cross-sectional area of the intake passage of the volute becomes larger, which can effectively satisfy the intake air amount entering the turbine impeller at the medium rotation speed of the engine, and improve the engine discharge.
  • the utilization of exhaust gas energy meets the supercharging requirements of the engine at medium speed.
  • the intake regulating valve When the engine is in the high-speed working condition, the intake regulating valve is fully opened under the driving of the intake adjusting control actuator, thereby opening the left outer air inlet and the outer air inlet of the volute. At this time, the inner flow passage of the volute inlet, the outer flow passage of the left side of the volute and the outer flow passage of the right side of the volute are simultaneously in working state.
  • the high-speed exhaust gas discharged from the engine enters the inner flow passage of the volute casing, the outer flow passage of the left side of the volute and the outer flow passage of the right side of the volute.
  • the cross-sectional area of the snail inlet flow passage increases, and the volute Guide vanes are provided at the vaneless nozzle of the left intake air flow passage, which can effectively guide the intake air flow into the turbine impeller at a suitable air flow angle, thereby improving the turbine intake efficiency and thereby increasing the boost ratio.
  • the structure of the turbine volute of the invention is basically the same as that of the ordinary supercharger volute structure, the structure is simple, the inheritance is good, the cost is low, and the engineering is easy and fast, the structure of the air intake adjusting device in the structure is simple, and the control method is easy to realize. , high reliability.
  • the invention will be further described below in conjunction with the accompanying drawings.
  • FIG. 1 is a schematic cross-sectional view showing a segmented volute with a guide vane in Embodiment 1 of the present invention
  • Figure 2 is a schematic cross-sectional view of a 0-180 degree flow path of a segmented volute with a guide vane according to Embodiment 1 of the present invention
  • Figure 3 is a flow guide vane with a guide vane according to Embodiment 1 of the present invention
  • FIG. 4 is a schematic cross-sectional structural view of a 0-180 degree flow path of a segmented volute with a guide vane according to Embodiment 2 of the present invention
  • FIG. 5 is a schematic view of the present invention.
  • FIG. 6 is a sectional structural view of the segmented volute with guide vanes in the low speed condition of the engine;
  • FIG. 6 is a sectional volute with guide vanes in the engine of the second embodiment of the present invention.
  • FIG. 7 is a schematic cross-sectional structural view of a segmented volute with a guide vane in a high speed condition of the engine according to Embodiment 2 of the present invention;
  • Embodiment 1 as shown in FIG. 1 and FIG. 2, a segmented volute with a guide vane, comprising: a turbine volute 1 having a volute inlet flow passage and a volute inside the turbine volute 1 a diffuser passage 4, wherein the turbine volute 1 is respectively provided with a volute air inlet 2 communicating with the volute inlet flow passage and a volute air outlet 3 communicating with the volute diffusing passage 4;
  • the volute inlet flow passage is provided with a left side pneumatic partition 5 and a right side pneumatic partition 6;
  • the left side pneumatic partition 5 and the right side pneumatic partition 6 divide the volute inlet flow passage into a volute left intake air flow passage 7, a volute intake inner flow passage 8 and a volute right intake air flow passage 9;
  • An air intake adjustment control device is respectively disposed at a position near the left outer air intake passage 7 of the volute and the outer air intake outer flow passage 9 of the volute near the volute intake port 2.
  • the air intake adjusting control device includes an air intake adjusting valve 10 installed at an air inlet of the left outer air intake runner 7 and the right outer air intake runner 9 of the volute, and the air intake adjusting valve 10 is driven. Connected with an air intake control actuator;
  • the two intake regulating valves 10 are simultaneously closed, that is, the left outer air intake passage 7 of the volute and the outer right outer air passage 9 of the volute are simultaneously closed; the volute intake air flow Road 8 is working alone;
  • the intake air regulating valve 10 installed at the intake port of the intake air flow passage 7 on the left side of the volute is closed, and the air intake outer flow passage 7 on the left side of the volute is closed, and the right side of the volute
  • the intake outer flow passage 9 and the volute intake inner flow passage 8 are in an operating state
  • the two intake air conditioning wide doors 10 are simultaneously opened, the volute air intake inner flow passage 8, the volute left air intake outer flow passage 7 and the volute right outer air intake outer flow passage 9 simultaneously Is working.
  • the left pneumatic diaphragm 5 and the right pneumatic diaphragm 6 are integrally coupled with the turbine volute 1; the volute air inlet 2 is a single air inlet, and the volute intake inner flow passage 8 is advanced.
  • the air port is in communication with the volute air inlet 2, and the air inlet of the left outer air intake passage 7 of the volute and the outer air inlet outer flow passage 9 of the volute is respectively connected with the inner flow passage 8 of the volute air intake The air inlets are connected.
  • the cross-sectional area of the left intake air flow passage 7 on the left side of the volute is larger than the cross-sectional area of the outer air flow passage 9 on the right side of the volute.
  • the sum of the cross-sectional areas of the left outer air intake runner 7 and the right outer air intake runner 9 of the volute is the inside of the volute intake air.
  • the cross-sectional area of the flow path 8 is 0.3-1.1 times.
  • the left outer air inlet passage 7 and the right outer air passage 9 of the volute are respectively located at two sides of the inner flow passage 8 of the volute, and the cross section of the outer air passage 7 on the left side of the volute is an arc.
  • the outer end extends to the outer side of the inner flow passage 8 of the volute casing.
  • a vaneless nozzle 15 is disposed at a position of the outer ventilating outer flow passage 7 on the left side of the volute, the outer side outer flow passage 9 on the right side of the volute, and the inner flow passage 8 of the volute casing near the volute diffusing passage 4, respectively.
  • the airflow flowing through the outer airflow passage on the left side of the volute enters the turbine impeller at a suitable airflow angle to improve the intake efficiency.
  • a plurality of airfoil-type air guide vanes 16 are uniformly disposed annularly in the outer air flow passage 7 on the left side of the volute near the vaneless nozzle 15 .
  • One end of the guide vane) 6 is integrally casted with the inner wall 17 of the left outer air inlet of the volute, and the other end is integrally formed with the left side pneumatic partition 5 on the inner side of the outer side of the outer flow passage 7 on the left side of the volute. Cast connection.
  • a left outer flow passage control chamber 11 is disposed between the left outer air intake outer flow passage 7 of the volute and the air inlet of the left outer air intake outer flow passage 7 of the volute; the outer right outer air passage 9 and the volute of the volute
  • a right outer flow passage control chamber 12 is provided between the intake ports of the intake air outer passage 9 on the right side of the casing.
  • the intake air regulating valves 10 are installed in the left outer flow path control chamber 11 and the right outer flow path control chamber 12, respectively.
  • the intake regulating valve 10 is respectively provided with an intake adjusting wide door fitting surface 13 at an intake port of the intake outer flow passage 7 on the left side of the volute and an intake U of the right outer intake passage 9 of the volute, thereby realizing The intake air regulates the sealing of the wide door.
  • the left outer flow passage control chamber 11 and the right outer flow passage control chamber 12 are respectively provided with an outer flow passage upper end cover 14 to achieve sealing of the intake air flow and restriction of the intake air regulating valve.
  • Embodiment 2 As shown in Fig. 4, in the above-described Embodiment 1, the left outer air intake passage 7 and the right outer air flow passage 9 of the volute may be arranged side by side in parallel.
  • the intake adjusting valve 10 is simultaneously closed by the intake adjusting control actuator, that is, the left outer side of the volute and the outer side of the volute
  • the intake air flow passage 9 is simultaneously closed, and at this time, all the exhaust gas discharged from the engine flows only through the volute intake inner flow passage 8, Since the cross-sectional area of the inner flow passage 8 of the volute casing is relatively small, the intake flow rate of the turbine impeller can be effectively increased, the available energy in the exhaust gas can be fully utilized, the turbine output work at the low speed condition of the engine can be increased, and the supercharging pressure can be increased. Meets the need for higher boost pressure at low engine speeds, improves engine low speed performance and reduces emissions, while increasing engine acceleration responsiveness and reducing the effects of boost hysteresis.
  • the intake regulating valve 10 of the left outer air inlet passage 7 of the volute is in the off state, and the outer air inlet runner 7 on the left side of the volute does not work.
  • the intake regulating valve 10 of the right outer side air flow passage 9 of the volute is opened under the driving of the air intake adjusting control actuator, thereby opening the outer air inlet outer flow passage 9 of the volute, and at this time, the volute enters
  • the gas inner flow passage 8 and the outer air intake outer flow passage 9 of the volute casing work together, and the cross-sectional area of the volute intake air passage passage becomes large, which can effectively satisfy the intake air flow rate entering the turbine impeller at a medium engine speed, and improve the utilization of the exhaust gas energy of the engine. Rate, to meet the supercharging requirements of the engine at medium speed.
  • the two intake air regulating valves 10 are simultaneously opened under the action of the intake air conditioning control actuator, thereby the outer air intake passage 7 on the left side of the volute.
  • the outer flow passage 9 on the right side of the volute is opened.
  • the inner flow passage 8 of the volute intake, the outer flow passage 7 of the left side of the volute, and the outer flow passage 9 of the right side of the volute are simultaneously in an operating state.
  • the high-speed exhaust gas discharged from the engine enters the volute intake inner flow passage 8, the volute left outer intake outer flow passage 7 and the volute right outer intake outer flow passage 9, respectively, and the outer flow passage 7 on the left side of the volute
  • the vaneless nozzle 16 is provided with a guide vane 16 which can effectively guide the intake air flow into the turbine impeller at a suitable air flow angle, thereby improving the turbine intake efficiency.
  • the inner flow passage of the volute casing is a constant intake air passage
  • the outer air inlet outer passage of the volute and the right outer air passage of the spiral outer casing are under the control of the air intake adjustment control actuator. Open or closed state.
  • the volute structure design is based on the improvement of the traditional volute, the structure is simple, the inheritance is good, and the product is easy to be engineered.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Supercharger (AREA)

Abstract

Disclosed is a segmented volute casing with guide vanes, comprising a turbine volute casing (1); a volute intake flow path and a volute diffusion path (4) provided within the turbine volute casing (1); and a volute intake port (2) in communication with the volute intake flow path and a volute air outlet (3) in communication with the volute diffusion path (4) respectively provided on the turbine volute casing (1). A left pneumatic baffle (5) and a right pneumatic baffle (6) are provided within the volute intake flow path, wherein the left pneumatic baffle (5) and the right pneumatic baffle (6) separate the volute intake flow path into a volute left intake outer flow path (7), a volute intake inner flow path (8) and a volute right intake outer flow path (9). An intake adjustment and control device is provided respectively at the position where the volute left intake outer flow path (7) and the volute right intake outer flow path (9) are adjacent to the volute intake port (2). The segmented volute casing with guide vanes improves the boost ratio when the engine is working at high speed, and satisfies the boost requirements within the full operating range of the engine.

Description

带导流叶片的分段式蜗壳 技术领域:  Segmented volute with guide vanes
本发明涉及一种分段式蜗壳, 具体地说是一种通过不同流道单独工作和共 同工作来满足发动机各工况性能要求的带导流叶片的分段式蜗壳, 属于内燃机 领域。 背景技术:  The present invention relates to a segmented volute, and more particularly to a segmented volute with guide vanes that can work independently and work together to meet the performance requirements of various operating conditions of the engine, and belongs to the field of internal combustion engines. Background technique:
近年来, 随着排放法规的日益严格, 人们对能够兼顾发动机全工况性能的 增压器的需求越来越强烈, 可变截面涡轮增压器因能有效控制发动机的排气压 力, 可使增压器和发动机在各个工况下实现良好的性能匹配, 成为了研发的重 点。 但在实际应用中, 采用可变截面增压器的发动机的低速扭矩有较大提高, 存在的问题是, 发动机的进排气负压差很高, 泵气损失过高, 导致发动机低速 工况油耗量偏高。专利 CN101694166A公开了一种双层流道变截面涡轮机控制装 置, 该结构包括涡轮壳, 涡轮壳内设有内外两个进气流道, 发动机中高工况下, 该装置通过阀门控制机构调节阀门的开度来调节进入蜗壳进气外流道的进气 量, 实现了变截面的功能。 但该结构在发动机高速工况下的增压比提高受限。  In recent years, with the increasingly strict emission regulations, there is an increasing demand for superchargers that can balance the performance of the engine. The variable-section turbocharger can effectively control the exhaust pressure of the engine. The supercharger and the engine achieve good performance matching under various working conditions and become the focus of research and development. However, in practical applications, the low-speed torque of the engine using the variable-section supercharger is greatly improved. The problem is that the engine's intake and exhaust negative pressure difference is very high, and the pumping loss is too high, resulting in low-speed engine operating conditions. The fuel consumption is high. Patent CN101694166A discloses a two-layer flow passage variable-section turbine control device, which comprises a turbine casing, and two inner and outer intake runners are arranged in the turbine casing, and the valve adjusts the opening of the valve through a valve control mechanism under high operating conditions in the engine. The degree of intake air entering the outer flow passage of the volute intake air is adjusted to realize the function of variable cross section. However, the structure has a limited increase in the boost ratio under high-speed engine conditions.
因此, 希望设计一种结构简单、 可靠性高的带导流叶片的分段式蜗壳, 来 满足发动机全工况范围内的性能要求, 提高发动机低速工况的进气量, 降低发 动机低速迟滞性, 并能在发动机高速工况下, 有效利用发动机的排气能量, 提 高发动机的进气量并有效提高增压比。 发明内容:  Therefore, it is desirable to design a segmented volute with guide vanes with simple structure and high reliability to meet the performance requirements of the engine under full working conditions, improve the intake air volume of the engine under low speed conditions, and reduce the low speed hysteresis of the engine. Sexuality, and can effectively utilize the exhaust energy of the engine under high-speed engine conditions, increase the intake air volume of the engine and effectively increase the boost ratio. Summary of the invention:
本发明要解决的问题是为了针对可变截面增压器的局限性, 提供一种能够 有效解决发动机低速工况时增压器的迟滞性, 并能提高发动机高速工况时的增 压比, 满足发动机全工况范围内的增压要求的带导流叶片的分段式蜗壳。  The problem to be solved by the present invention is to provide a method for effectively solving the hysteresis of the supercharger when the engine is in a low speed condition, and to improve the supercharging ratio when the engine is in a high speed condition, in order to solve the limitation of the variable section supercharger. A segmented volute with guide vanes that meets the boost requirements of the full operating range of the engine.
为了解决上述问题, 本发明采用以下技术方案:  In order to solve the above problems, the present invention adopts the following technical solutions:
一种带导流叶片的分段式蜗壳, 包括涡轮蜗壳; 所述涡轮蜗壳内设有蜗壳进气流道及蜗壳扩压通道, 所述涡轮蜗壳上分别 设有与蜗壳进气流道连通的蜗壳进气口和与蜗壳扩压通道连通的蜗壳出气口; 所述蜗壳进气流道内设有左侧气动隔板和右侧气动隔板; A segmented volute with guide vanes, including a turbine volute; The turbine volute is provided with a volute inlet flow passage and a volute expansion passage, and the turbine volute is respectively provided with a volute air inlet communicating with the volute intake flow passage and communicating with the volute diffusion passage a volute air outlet; a left side pneumatic partition and a right side pneumatic partition are arranged in the volute inlet flow passage;
所述 Γ:侧气动隔板和右侧气动隔板将蜗壳进气流道间隔成为蜗壳左侧进气 外流道, 蜗壳进气内流道和蜗壳右侧进气外流道;  The Γ: the side pneumatic baffle and the right pneumatic baffle partition the volute inlet flow passage into the volute left intake air flow passage, the volute intake air flow passage and the volute right intake air flow passage;
所述蜗壳左侧进气外流道和蜗壳右侧进气外流道靠近蜗壳进气口处的位置 分别设有进气调节控制装置。  An air intake adjustment control device is respectively disposed at a position of the outer ventilating outer flow passage on the left side of the volute and the outer air intake outer flow passage on the right side of the volute near the vent inlet of the volute.
以下是本发明对上述方案的进一步改进- 所述进气调节控制装置包括分别安装在蜗壳左侧进气外流道和蜗壳右侧进 气外流道的进气口处的进气调节阀门, 所述进气调节阀门传动连接有进气调节 控制执行器;  The following is a further improvement of the above-mentioned solution by the present invention - the air intake adjusting control device includes an air intake adjusting valve respectively installed at an air inlet of the left outer air intake passage of the volute and the outer air flow passage of the right side of the volute, The intake adjustment valve drive is connected with an intake adjustment control actuator;
当发动机处于低速工况范围时, 两个进气调节阀门同时关闭, 即蜗壳左侧 进气外流道和蜗壳右侧迸气外流道同时处于关闭状态; 蜗壳迸气内流道单独处 于工作状态;  When the engine is in the low speed range, the two intake regulating valves are closed at the same time, that is, the left outer air intake passage of the volute and the outer helium outer flow passage of the volute are simultaneously closed; the volute helium inner flow passage is separately Working status
当发动机处于中速工况范围时, 安装在蜗壳左侧进气外流道进气口处的进 气调节阀门关闭, 蜗壳左侧进气外流道处于关闭状态, 蜗壳右侧进气外流道和 蜗壳进气内流道处于工作状态;  When the engine is in the medium speed condition range, the intake adjustment valve installed at the intake port of the intake air passage on the left side of the volute is closed, and the intake air flow passage on the left side of the volute is closed, and the intake air flow on the right side of the volute The inner passage of the passage and the volute intake air are in working condition;
当发动机处于高速工况范围内时, 两个进气调节阀门同时打开, 蜗壳进气 内流道、 蜗壳左侧进气外流道和蜗壳右侧进气外流道同时处于工作状态。  When the engine is in the high-speed working range, the two intake regulating valves are simultaneously opened, and the inner flow passage of the volute casing, the outer flow passage of the left side of the volute and the outer flow passage of the right side of the volute are simultaneously in working state.
进 歩改进:  Advance improvement:
所述蜗壳进气内流道的进气口与蜗壳进气口相连通, 所述蜗壳左侧进气外 流道和所述蜗壳右侧进气外流道的进气口分别与蜗壳进气内流道的进气口相连 通。  The air inlet of the inner flow passage of the volute air inlet communicates with the air inlet of the volute, and the air inlet of the left outer air inlet of the volute and the air inlet of the outer air flow of the right side of the volute respectively The air inlets of the inner air passage of the shell inlet are connected.
进一步改进: 所述蜗壳左侧进气外流道和蜗壳右侧进气外流道分别位于蜗 壳进气内流道的两侧且并排平行设置。  Further improvement: the left outer air intake flow passage of the volute and the right outer air intake outer flow passage of the volute are respectively located on both sides of the inner flow passage of the volute casing and are arranged side by side in parallel.
另一种改进: , 所述蜗壳左侧进气外流道和蜗壳右侧进气外流道分别位于蜗壳进气内流道 的两侧, 所述蜗壳左侧进气外流道的截面为弧形, 其外端延伸至蜗壳进气内流 道的外侧。 Another improvement: The left outer air intake outer flow passage of the volute and the right outer air intake outer flow passage of the volute are respectively located at two sides of the inner flow passage of the volute casing, and the cross section of the left outer air intake passage of the volute is curved, and the outer portion thereof The end extends to the outside of the inner flow passage of the volute intake.
进 步改进: 所述蜗壳左侧进气外流道的截面积大于所述蜗壳右侧进气外 流道的截面积。  Further improvement: the cross-sectional area of the outer air intake passage on the left side of the volute is larger than the cross-sectional area of the outer air flow passage on the right side of the volute.
进一歩改迸: 为保证所设计的流道截面符合 A/R值的设计要求, 所述蜗壳 左侧进气外流道和! ¾壳右侧进气外流道的截面积之和是蜗壳进气内流道的截面 积的 0.3-1.1倍。  Further improvement: In order to ensure that the designed cross-section of the flow channel meets the design requirements of the A/R value, the sum of the cross-sectional areas of the left outer air intake passage and the right outer air passage of the right side of the volute is a volute The cross-sectional area of the inner flow passage of the intake air is 0.3-1.1 times.
进- 歩改进: 所述蜗壳左侧进气外流道、 蜗壳右侧进气外流道及蜗壳进气 内流道靠近蜗壳扩压通道的位置处分别设有无叶喷嘴。  In-mesh improvement: a vane-free nozzle is respectively disposed at a position of the outer ventilating outer flow passage on the left side of the volute, the outer side outer flow passage of the volute casing, and the inner flow passage of the volute casing near the volute diffusing passage.
进一步改进: 所述蜗壳左侧进气外流道内靠近无叶喷嘴处呈环形均匀设有 若干片机翼型气动式导流叶片。  Further improvement: a plurality of airfoil-type pneumatic guide vanes are uniformly arranged in a ring shape near the vaneless nozzle in the left outer air inlet passage of the volute.
进一步改进: 所述导流叶片的一端与蜗壳左侧进气外流道内壁一体铸造连 接,另一端与左侧气动隔板位于蜗壳左侧进气外流道一侧的内壁一体铸造连接。  Further improvement: one end of the guiding vane is integrally casted and connected with the inner wall of the outer side of the outer side of the volute, and the other end is integrally casted with the inner wall of the left side of the outer side of the outer side of the volute.
进- 歩改进: 所述蜗壳左侧进气外流道与蜗壳左侧进气外流道的进气口之 间设有左侧外流道控制室; 所述蜗壳右侧进气外流道与蜗壳右侧进气外流道的 进气口之间设有右侧外流道控制室。  In-mesh improvement: a left outer flow passage control chamber is provided between the left outer air intake outer flow passage of the volute and the air inlet of the left outer air intake passage of the volute; the outer right outer flow passage of the volute A right outer flow channel control chamber is arranged between the air inlets of the outer air intake passage on the right side of the volute.
进一步改进: 安装在蜗壳左侧进气外流道的进气口处的进气调节阀门位于 左侧外流道控制室内;  Further improvement: The intake air regulating valve installed at the intake port of the intake air flow passage on the left side of the volute is located in the left outer flow passage control room;
安装在蜗壳右侧进气外流道的进气口处的进气调节阀门位于右侧外流道控 制室内。  The intake air regulating valve installed at the intake port of the intake air flow passage on the right side of the volute is located in the right outer flow passage control chamber.
进- 步改进: 所述左侧外流道控制室和右侧外流道控制室上分别设有外流 道上端盖, 以实现对进气流的密封和进气调节阀门的限位。  Step-by-step improvement: The upper outer runner control chamber and the right outer runner control chamber are respectively provided with upper outer runner end caps to achieve sealing of the intake air flow and limit of the intake air regulating valve.
本发明采用上述方案, 蜗壳进气内流道是常开进气流道, 蜗壳左侧进气外 流道和蜗壳右侧进气外流道在进气调节控制执行器的控制下处于打开或闭合状 发动机处于低速工况范围内时, 进气调节阔门在进气调节控制执行器的带 动下, 将蜗壳左侧进气外流道和蜗壳右侧进气外流道同时关闭, 此时, 从发动 机排出的所有废气仅流经蜗壳进气内流道, 由于蜗壳进气内流道的截面积比较 小, 可有效提高涡轮叶轮的进气流速, 充分利用废气中的可用能量, 增大发动 机低速工况时的涡轮输出功, 提升增压压力, 满足发动机低速时的较高增压压 力的需求, 提高发动机的低速性能并能降低排放, 同时提高了发动机的加速响 应性, 减少了增压迟滞的影响。 The invention adopts the above scheme, the inner flow passage of the volute casing is a normally open intake flow passage, and the outer air inlet outer passage of the volute and the right outer air passage of the volute are open under the control of the intake regulation control actuator or Closed When the engine is in the low speed condition range, the intake air regulating wide door is driven by the air intake adjusting control actuator, and the outer air inlet outer flow passage of the volute and the outer air inlet outer flow passage of the volute are simultaneously closed, at this time, All the exhaust gas discharged from the engine only flows through the inner flow passage of the volute casing. Since the cross-sectional area of the inner flow passage of the volute casing is relatively small, the intake flow rate of the turbine impeller can be effectively increased, and the available energy in the exhaust gas can be fully utilized to increase. Turbine output work at low engine speed, boosting boost pressure, meeting the need for higher boost pressure at low engine speeds, improving engine low speed performance and reducing emissions, while increasing engine acceleration responsiveness and reducing The effect of pressure hysteresis.
发动机处于中速工况范围内时, 蜗壳右侧进气外流道的进气调节阀门在进 气调节控制执行器的带动下处于完全打开状态, 从而将蜗壳右侧进气外流道打 开, 此时, 蜗壳进气内流道和蜗壳右侧进气外流道共同工作, 蜗壳进气流道截 面积变大, 可有效满足发动机中等转速下进入涡轮叶轮的进气量, 提高发动机 排出废气能量的利用率, 满足发动机中等转速下的增压要求。  When the engine is in the medium speed condition range, the intake regulating valve of the outer air intake passage of the right side of the volute is fully opened by the air intake adjusting control actuator, thereby opening the outer air inlet passage of the right side of the volute. At this time, the inner flow passage of the volute inlet and the outer flow passage of the right side of the volute work together, and the cross-sectional area of the intake passage of the volute becomes larger, which can effectively satisfy the intake air amount entering the turbine impeller at the medium rotation speed of the engine, and improve the engine discharge. The utilization of exhaust gas energy meets the supercharging requirements of the engine at medium speed.
发动机处于高速工况范围内时, 进气调节阀门在进气调节控制执行器的带 动下同时处于完全打开状态, 从而将蜗壳左侧进气外流道和蜗壳右侧进气外流 道打开, 此时蜗壳进气内流道、 蜗壳左侧进气外流道和蜗壳右侧进气外流道同 时处于工作状态。 从发动机排出的高速废气分别进入蜗壳进气内流道、 蜗壳左 侧进气外流道和蜗壳右侧进气外流道, 蜗壳进气流道工作截面积增大, 又由于 在蜗壳左侧进气外流道的无叶喷嘴处设置了导流叶片, 可有效引导进气流以合 适的气流角进入涡轮叶轮, 提高了涡轮进气效率, 从而提高了增压比。  When the engine is in the high-speed working condition, the intake regulating valve is fully opened under the driving of the intake adjusting control actuator, thereby opening the left outer air inlet and the outer air inlet of the volute. At this time, the inner flow passage of the volute inlet, the outer flow passage of the left side of the volute and the outer flow passage of the right side of the volute are simultaneously in working state. The high-speed exhaust gas discharged from the engine enters the inner flow passage of the volute casing, the outer flow passage of the left side of the volute and the outer flow passage of the right side of the volute. The cross-sectional area of the snail inlet flow passage increases, and the volute Guide vanes are provided at the vaneless nozzle of the left intake air flow passage, which can effectively guide the intake air flow into the turbine impeller at a suitable air flow angle, thereby improving the turbine intake efficiency and thereby increasing the boost ratio.
本发明中的涡轮蜗壳结构与普通的增压器蜗壳结构基本相同, 结构简单、 继承性好、 成本低、 容易快速实现工程化, 结构中的进气调节装置结构简单, 控制方式容易实现, 可靠性高。 下面结合附图和对本发明做进一步说明。  The structure of the turbine volute of the invention is basically the same as that of the ordinary supercharger volute structure, the structure is simple, the inheritance is good, the cost is low, and the engineering is easy and fast, the structure of the air intake adjusting device in the structure is simple, and the control method is easy to realize. , high reliability. The invention will be further described below in conjunction with the accompanying drawings.
附图说明: BRIEF DESCRIPTION OF THE DRAWINGS:
附图 1 是本发明实施例 1 中的带导流叶片的分段式蜗壳的剖面结构示意 图; 附图 2是本发明实施例 1中的带导流叶片的分段式蜗壳的 0-180度流道截 面结构示意图; 附图 3是本发明实施例 1中的带导流叶片的分段式蜗壳的径向剖面结构示 意图; 附图 4是本发明实施例 2中的带导流叶片的分段式蜗壳的 0-180度流道截 面结构示意图; 附图 5是本发明实施例 2中的带导流叶片的分段式蜗壳在发动机低速工况 下的剖面结构示意图; 附图 6是本发明实施例 2中的带导流叶片的分段式蜗壳在发动机中速工况 下的剖面结构示意 1 ; 附图 7是本发明实施例 2中的带导流叶片的分段式蜗壳在发动机高速工况 下的剖面结构示意图; 图中: 1-涡轮蜗壳; 2-蜗壳迸气口; 3-蜗壳出气口; 4-蜗壳扩压通道; 5 - 左侧气动隔板; 6-右侧气动隔板; 7-蜗壳左侧进气外流道; 8-蜗壳进气内流道; 9-蜗壳右侧进气外流道; 10-进气调节阀门; 11-左侧外流道控制室; 12-右侧外 流道控制室; 13-进气调节阀门配合面; 14-外流道上端盖; 15-无叶喷嘴; 16- 导流叶片; 17-蜗 左侧进气外流道内壁。 具体实施方式: 1 is a schematic cross-sectional view showing a segmented volute with a guide vane in Embodiment 1 of the present invention; Figure 2 is a schematic cross-sectional view of a 0-180 degree flow path of a segmented volute with a guide vane according to Embodiment 1 of the present invention; Figure 3 is a flow guide vane with a guide vane according to Embodiment 1 of the present invention; FIG. 4 is a schematic cross-sectional structural view of a 0-180 degree flow path of a segmented volute with a guide vane according to Embodiment 2 of the present invention; FIG. 5 is a schematic view of the present invention. FIG. 6 is a sectional structural view of the segmented volute with guide vanes in the low speed condition of the engine; FIG. 6 is a sectional volute with guide vanes in the engine of the second embodiment of the present invention. FIG. 7 is a schematic cross-sectional structural view of a segmented volute with a guide vane in a high speed condition of the engine according to Embodiment 2 of the present invention; FIG. 1 : Turbine volute 2- volute vent; 3- volute outlet; 4- volute diffuser; 5 - left pneumatic diaphragm; 6-right pneumatic diaphragm; 7- volute left intake air passage; 8- volute inlet flow passage; 9- volute right intake air passage; 10-intake regulating valve; 11-left outer runner control room; 12-right side Road control chamber; 13- intake air regulating valve mating surface; 14- outflow track cover; no leaves the nozzle 15; 16- guide vane; 17- cochlear inner wall of the left outer channel. detailed description:
实施例 1, 如图 1、 图 2所示, 一种带导流叶片的分段式蜗壳, 包括: 涡轮蜗壳 1,所述涡轮蜗壳 1内设有蜗壳进气流道及蜗壳扩压通道 4,所述涡 轮蜗壳 1上分别设有与蜗壳进气流道连通的蜗壳进气口 2和与蜗壳扩压通道 4连 通的蜗壳出气口 3 ; 所述蜗壳进气流道内设有左侧气动隔板 5和右侧气动隔板 6; Embodiment 1, as shown in FIG. 1 and FIG. 2, a segmented volute with a guide vane, comprising: a turbine volute 1 having a volute inlet flow passage and a volute inside the turbine volute 1 a diffuser passage 4, wherein the turbine volute 1 is respectively provided with a volute air inlet 2 communicating with the volute inlet flow passage and a volute air outlet 3 communicating with the volute diffusing passage 4; The volute inlet flow passage is provided with a left side pneumatic partition 5 and a right side pneumatic partition 6;
所述左侧气动隔板 5和右侧气动隔板 6将蜗壳进气流道间隔成为蜗壳左侧进 气外流道 7, 蜗壳进气内流道 8和蜗壳右侧进气外流道 9;  The left side pneumatic partition 5 and the right side pneumatic partition 6 divide the volute inlet flow passage into a volute left intake air flow passage 7, a volute intake inner flow passage 8 and a volute right intake air flow passage 9;
所述蜗壳左侧进气外流道 7和蜗壳右侧进气外流道 9靠近蜗壳进气口 2处的 位置分别设有进气调节控制装置。  An air intake adjustment control device is respectively disposed at a position near the left outer air intake passage 7 of the volute and the outer air intake outer flow passage 9 of the volute near the volute intake port 2.
所述进气调节控制装置包括分别安装在蜗壳左侧进气外流道 7和蜗壳右侧 进气外流道 9的进气口处的进气调节阀门 10,所述进气调节阀门 10传动连接有进 气调节控制执行器;  The air intake adjusting control device includes an air intake adjusting valve 10 installed at an air inlet of the left outer air intake runner 7 and the right outer air intake runner 9 of the volute, and the air intake adjusting valve 10 is driven. Connected with an air intake control actuator;
当发动机处于低速工况范围时, 两个进气调节阀门 10同时关闭, 即蜗壳左 侧进气外流道 7和蜗壳右侧进气外流道 9同时处于关闭状态; 蜗壳进气内流道 8 单独处于工作状态;  When the engine is in the low speed range, the two intake regulating valves 10 are simultaneously closed, that is, the left outer air intake passage 7 of the volute and the outer right outer air passage 9 of the volute are simultaneously closed; the volute intake air flow Road 8 is working alone;
当发动机处于中速工况范围时,安装在蜗壳左侧进气外流道 7进气口处的进 气调节阀门 10关闭,蜗壳左侧进气外流道 7处于关闭状态,蜗壳右侧进气外流道 9和蜗壳进气内流道 8处于工作状态;  When the engine is in the medium speed condition range, the intake air regulating valve 10 installed at the intake port of the intake air flow passage 7 on the left side of the volute is closed, and the air intake outer flow passage 7 on the left side of the volute is closed, and the right side of the volute The intake outer flow passage 9 and the volute intake inner flow passage 8 are in an operating state;
当发动机处于高速工况范围内时, 两个进气调节阔门 10同时打开, 蜗壳进 气内流道 8、 蜗壳左侧进气外流道 7和蜗壳右侧进气外流道 9同时处于工作状态。  When the engine is in the high speed working condition, the two intake air conditioning wide doors 10 are simultaneously opened, the volute air intake inner flow passage 8, the volute left air intake outer flow passage 7 and the volute right outer air intake outer flow passage 9 simultaneously Is working.
所述左侧气动隔板 5和右侧气动隔板 6与涡轮蜗壳 1铸造一体连接; 所述蜗壳进气口 2为单进气口, 所述蜗壳进气内流道 8的进气口与蜗壳进气 口 2相连通,所述蜗壳左侧进气外流道 7和所述蜗壳右侧进气外流道 9的进气口分 别与蜗壳进气内流道 8的进气口相连通。  The left pneumatic diaphragm 5 and the right pneumatic diaphragm 6 are integrally coupled with the turbine volute 1; the volute air inlet 2 is a single air inlet, and the volute intake inner flow passage 8 is advanced. The air port is in communication with the volute air inlet 2, and the air inlet of the left outer air intake passage 7 of the volute and the outer air inlet outer flow passage 9 of the volute is respectively connected with the inner flow passage 8 of the volute air intake The air inlets are connected.
所述蜗壳左侧进气外流道 7的截面积大于所述蜗壳右侧进气外流道 9的截面 积。  The cross-sectional area of the left intake air flow passage 7 on the left side of the volute is larger than the cross-sectional area of the outer air flow passage 9 on the right side of the volute.
为保证所设 il的流道截面符合 A/R值的设计要求, 所述蜗壳左侧进气外流 道 7和蜗壳右侧进气外流道 9的截面积之和是蜗壳进气内流道 8的截面积的 0.3-1.1倍。 所述蜗壳左侧进气外流道 7和蜗壳右侧进气外流道 9分别位于蜗壳进气内流 道 8的两侧, 所述蜗壳左侧进气外流道 7的截面为弧形, 其外端延伸至蜗壳进气 内流道 8的外侧。 In order to ensure that the flow path section of the il is in accordance with the design requirements of the A/R value, the sum of the cross-sectional areas of the left outer air intake runner 7 and the right outer air intake runner 9 of the volute is the inside of the volute intake air. The cross-sectional area of the flow path 8 is 0.3-1.1 times. The left outer air inlet passage 7 and the right outer air passage 9 of the volute are respectively located at two sides of the inner flow passage 8 of the volute, and the cross section of the outer air passage 7 on the left side of the volute is an arc. The outer end extends to the outer side of the inner flow passage 8 of the volute casing.
所述蜗壳左侧进气外流道 7、蜗壳右侧进气外流道 9及蜗壳进气内流道 8靠近 蜗壳扩压通道 4的位置处分别设有无叶喷嘴 15。  A vaneless nozzle 15 is disposed at a position of the outer ventilating outer flow passage 7 on the left side of the volute, the outer side outer flow passage 9 on the right side of the volute, and the inner flow passage 8 of the volute casing near the volute diffusing passage 4, respectively.
如图 2、 图 3所示, 发动机高速工况时, 为充分利用发动机的排气能量, 保 证流经蜗壳左侧进气外流道的气流以合适的气流角进入涡轮叶轮, 提高进气效 率,在所述蜗壳左侧进气外流道 7内靠近无叶喷嘴 15处呈环形均匀设有若干片机 翼型气动式导流叶片 16。  As shown in Fig. 2 and Fig. 3, in the high-speed engine condition, in order to make full use of the exhaust energy of the engine, the airflow flowing through the outer airflow passage on the left side of the volute enters the turbine impeller at a suitable airflow angle to improve the intake efficiency. A plurality of airfoil-type air guide vanes 16 are uniformly disposed annularly in the outer air flow passage 7 on the left side of the volute near the vaneless nozzle 15 .
所述导流叶 ) ΊΊ 6的一端与蜗壳左侧进气外流道内壁 17—体铸造连接, 另一 端与左侧气动隔板 5位于蜗壳左侧进气外流道 7—侧的内壁一体铸造连接。  One end of the guide vane) 6 is integrally casted with the inner wall 17 of the left outer air inlet of the volute, and the other end is integrally formed with the left side pneumatic partition 5 on the inner side of the outer side of the outer flow passage 7 on the left side of the volute. Cast connection.
所述蜗壳左侧进气外流道 7与蜗壳左侧进气外流道 7的进气口之间设有左侧 外流道控制室 11 ; 所述蜗壳右侧进气外流道 9与蜗壳右侧进气外流道 9的进气口 之间设有右侧外流道控制室 12。  a left outer flow passage control chamber 11 is disposed between the left outer air intake outer flow passage 7 of the volute and the air inlet of the left outer air intake outer flow passage 7 of the volute; the outer right outer air passage 9 and the volute of the volute A right outer flow passage control chamber 12 is provided between the intake ports of the intake air outer passage 9 on the right side of the casing.
所述进气调节阀门 10分别安装在左侧外流道控制室 11和右侧外流道控制室 12内。  The intake air regulating valves 10 are installed in the left outer flow path control chamber 11 and the right outer flow path control chamber 12, respectively.
所述进气调节阀门 10靠近蜗壳左侧进气外流道 7的进气口和蜗壳右侧进气 外流道 9的进气 U处分别设有进气调节阔门配合面 13,从而实现进气调节阔门的 密封性。  The intake regulating valve 10 is respectively provided with an intake adjusting wide door fitting surface 13 at an intake port of the intake outer flow passage 7 on the left side of the volute and an intake U of the right outer intake passage 9 of the volute, thereby realizing The intake air regulates the sealing of the wide door.
所述左侧外流道控制室 11和右侧外流道控制室 12上分别设有外流道上端盖 14, 以实现对进气流的密封和进气调节阀门的限位。  The left outer flow passage control chamber 11 and the right outer flow passage control chamber 12 are respectively provided with an outer flow passage upper end cover 14 to achieve sealing of the intake air flow and restriction of the intake air regulating valve.
实施例 2, 如图 4所示, 上述实施例 1中, 所述蜗壳左侧进气外流道 7和蜗壳 右侧进气外流道 9还可以并排平行设置。  Embodiment 2 As shown in Fig. 4, in the above-described Embodiment 1, the left outer air intake passage 7 and the right outer air flow passage 9 of the volute may be arranged side by side in parallel.
如图 5所示, 当发动机处于低速工况范围时,进气调节阀门 10在进气调节控 制执行器的带动下同时处于关闭状态,即将蜗壳左侧进气外流道 7和蜗壳右侧进 气外流道 9同时关闭,此时,从发动机排出的所有废气仅流经蜗壳进气内流道 8, 由于蜗壳进气内流道 8的截面积比较小,可有效提高涡轮叶轮的进气流速,充分 利用废气中的可用能量,增大发动机低速工况时的涡轮输出功,提升增压压力, 满足发动机低速时的较高增压压力的需求, 提高发动机的低速性能并能降低排 放, 同时提高了发动机的加速响应性, 减少了增压迟滞的影响。 As shown in FIG. 5, when the engine is in the low speed range, the intake adjusting valve 10 is simultaneously closed by the intake adjusting control actuator, that is, the left outer side of the volute and the outer side of the volute The intake air flow passage 9 is simultaneously closed, and at this time, all the exhaust gas discharged from the engine flows only through the volute intake inner flow passage 8, Since the cross-sectional area of the inner flow passage 8 of the volute casing is relatively small, the intake flow rate of the turbine impeller can be effectively increased, the available energy in the exhaust gas can be fully utilized, the turbine output work at the low speed condition of the engine can be increased, and the supercharging pressure can be increased. Meets the need for higher boost pressure at low engine speeds, improves engine low speed performance and reduces emissions, while increasing engine acceleration responsiveness and reducing the effects of boost hysteresis.
如图 6所示, 、"1发动机处于中速工况范围时, 蜗壳左侧进气外流道 7的进气 调节阀门 10处于关 | 状态,蜗壳左侧进气外流道 7并不工作。而蜗壳右侧进气外 流道 9的进气调节阀门 10在进气调节控制执行器的带动下处于打开状态,从而将 蜗壳右侧进气外流道 9打开, 此时, 蜗壳进气内流道 8和蜗壳右侧进气外流道 9 共同工作, 蜗壳进气流道截面积变大, 可有效满足发动机中等转速下进入涡轮 叶轮的进气流量, 提高发动机排出废气能量的利用率, 满足发动机中等转速下 的增压要求。  As shown in Fig. 6, when the engine is in the medium speed range, the intake regulating valve 10 of the left outer air inlet passage 7 of the volute is in the off state, and the outer air inlet runner 7 on the left side of the volute does not work. The intake regulating valve 10 of the right outer side air flow passage 9 of the volute is opened under the driving of the air intake adjusting control actuator, thereby opening the outer air inlet outer flow passage 9 of the volute, and at this time, the volute enters The gas inner flow passage 8 and the outer air intake outer flow passage 9 of the volute casing work together, and the cross-sectional area of the volute intake air passage passage becomes large, which can effectively satisfy the intake air flow rate entering the turbine impeller at a medium engine speed, and improve the utilization of the exhaust gas energy of the engine. Rate, to meet the supercharging requirements of the engine at medium speed.
如图 7所示, 当发动机处于高速工况范围内时,两个进气调节阀门 10在进气 调节控制执行器的 ^动下同时处于打开状态,从而将蜗壳左侧进气外流道 7和蜗 壳右侧进气外流道 9打开, 此时,蜗壳进气内流道 8、蜗壳左侧进气外流道 7和蜗 壳右侧进气外流道 9同时处于工作状态。从发动机排出的高速废气分别进入蜗壳 进气内流道 8、蜗壳左侧进气外流道 7和蜗壳右侧进气外流道 9,又由于在蜗壳左 侧进气外流道 7的无叶喷嘴 15处设置了导流叶片 16,可有效引导进气流以合适的 气流角进入涡轮叶轮, 提高了涡轮进气效率。  As shown in FIG. 7, when the engine is in the high speed working condition range, the two intake air regulating valves 10 are simultaneously opened under the action of the intake air conditioning control actuator, thereby the outer air intake passage 7 on the left side of the volute. The outer flow passage 9 on the right side of the volute is opened. At this time, the inner flow passage 8 of the volute intake, the outer flow passage 7 of the left side of the volute, and the outer flow passage 9 of the right side of the volute are simultaneously in an operating state. The high-speed exhaust gas discharged from the engine enters the volute intake inner flow passage 8, the volute left outer intake outer flow passage 7 and the volute right outer intake outer flow passage 9, respectively, and the outer flow passage 7 on the left side of the volute The vaneless nozzle 16 is provided with a guide vane 16 which can effectively guide the intake air flow into the turbine impeller at a suitable air flow angle, thereby improving the turbine intake efficiency.
本发明采用上述方案, 所述蜗壳进气内流道是常幵进气流道, 蜗壳左侧进 气外流道和蜗売右侧进气外流道在进气调节控制执行器的控制下处于打开或闭 合状态。 通过调节蜗壳进气截面积, 满足不同工况下, 进入蜗壳进气流道的进 气量, 实现变截面涡轮机的功能, 满足发动机全工况下的增压需求。 该蜗壳结 构设计是在传统蜗壳基础上进行的改进, 结构简单, 继承性好, 容易实现产品 的工程化。  According to the above aspect of the invention, the inner flow passage of the volute casing is a constant intake air passage, and the outer air inlet outer passage of the volute and the right outer air passage of the spiral outer casing are under the control of the air intake adjustment control actuator. Open or closed state. By adjusting the intake cross-sectional area of the volute, it can meet the intake air volume of the volute inlet flow passage under different working conditions, realize the function of the variable-section turbine, and meet the supercharging demand under the full working condition of the engine. The volute structure design is based on the improvement of the traditional volute, the structure is simple, the inheritance is good, and the product is easy to be engineered.

Claims

权利要求 Rights request
1、 一种带导流叶片的分段式蜗壳, 包括:  1. A segmented volute with guide vanes, comprising:
涡轮蜗壳( 1 ),所述涡轮蜗壳( 1 )内设有蜗壳进气流道及蜗壳扩压通道( 4 ), 所述涡轮蜗壳 (1 ) 上分别设有与蜗壳进气流道连通的蜗壳进气口 (2) 和与蜗 壳扩压通道 (4) 连通的蜗壳出气口 (3);  a turbine volute (1), wherein the turbine volute (1) is provided with a volute inlet flow passage and a volute expansion passage (4), and the turbine volute (1) is respectively provided with a volute intake flow a volute inlet (2) connected to the volute and a vent outlet (3) communicating with the volute diffuser passage (4);
其特征在于:  It is characterized by:
所述蜗壳进气流道内设有左侧气动隔板 (5) 和右侧气动隔板 (6 );  The volute inlet flow passage is provided with a left side pneumatic partition (5) and a right side pneumatic partition (6);
所述左侧气动隔板 (5 ) 和右侧气动隔板 (6) 将蜗壳进气流道间隔成为蜗 壳左侧进气外流道 (7 ), 蜗壳进气内流道 (8) 和蜗壳右侧进气外流道 (9); 所述蜗壳左侧进气外流道 (7) 和蜗壳右侧进气外流道 (9) 靠近蜗壳进气 口 (2) 处的位置分别设有进气调节控制装置。  The left pneumatic diaphragm (5) and the right pneumatic diaphragm (6) partition the volute intake flow passage into a volute left intake air flow passage (7), a volute intake inner flow passage (8) and The outer ventilating outer flow passage of the volute (9); the outer venting outer flow passage (7) of the volute and the outer venting outer flow passage (9) of the volute close to the volute inlet (2) respectively It has an air intake control device.
2、 根据权利要求 1所述的带导流叶片的分段式蜗壳, 其特征在于: 所述进气调节控制装置包括分别安装在蜗壳左侧进气外流道(7)和蜗壳右 侧进气外流道(9)的进气口处的进气调节阀门 (10), 所述进气调节阀门(10) 传动连接有进气调节控制执行器;  2. The segmented volute with a guide vane according to claim 1, wherein: said intake adjustment control device comprises an outer intake outer flow passage (7) and a volute right side respectively mounted on the left side of the volute An intake adjusting valve (10) at an intake port of the side intake outer flow passage (9), wherein the intake adjusting valve (10) is connected to an intake adjusting control actuator;
当发动机处于低速工况范围时, 两个进气调节阀门 (10) 同时关闭, 即蜗 壳左侧进气外流道 (7 ) 和蜗壳右侧进气外流道 (9) 同时处于关闭状态; 蜗壳 进气内流道 (8) 单独处于工作状态;  When the engine is in the low speed range, the two intake regulating valves (10) are simultaneously closed, that is, the left outer air intake passage (7) of the volute and the outer air inlet outer flow passage (9) of the volute are simultaneously closed; The inner flow passage (8) of the volute intake is in a working state alone;
当发动机处于中速工况范围时, 安装在蜗壳左侧进气外流道(7)进气口处 的进气调节阀门 (10 )关闭, 蜗壳左侧进气外流道(7)处于关闭状态, 蜗壳右 侧进气外流道 (9) 和蜗壳进气内流道 (8) 处于工作状态;  When the engine is in the medium speed range, the intake adjustment valve (10) installed at the intake port of the intake outer flow passage (7) on the left side of the volute is closed, and the intake outer flow passage (7) on the left side of the volute is closed. State, the outer ventilating outer flow passage (9) of the volute and the inner flow passage (8) of the volute intake are in operation;
当发动机处于高速工况范围时, 两个进气调节阀门 (10) 同时打开, 蜗壳 进气内流道 (8 )、 蜗壳左侧进气外流道 (7) 和蜗壳右侧进气外流道 (9) 同时 处于工作状态。  When the engine is in the high speed range, the two intake adjustment valves (10) are simultaneously opened, the volute intake inner flow passage (8), the volute left intake air passage (7) and the volute right intake. The outer flow path (9) is in working condition at the same time.
3、 根据权利要求 2所述的带导流叶片的分段式蜗壳, 其特征在于: 所述蜗壳进气内流道 (8) 的进气口与蜗壳进气口 (2) 相连通, 所述蜗壳 左侧进气外流道 (7) 和所述蜗壳右侧进气外流道 (9) 的进气口分别与蜗壳进 气内流道 (8) 的进气口相连通。 3. The segmented volute with a guide vane according to claim 2, wherein: An intake port of the volute intake inner flow passage (8) communicates with a volute intake port (2), and the volute left intake air passage (7) and the volute right intake The intake ports of the outer flow passage (9) are respectively connected to the intake ports of the inner flow passage (8) of the volute intake.
4、 根据权利要求 3所述的带导流叶片的分段式蜗壳, 其特征在于: 所述蜗壳左侧进气外流道 (7) 和蜗壳右侧进气外流道 (9) 分别位于蜗壳 进气内流道 (8) 的两侧且并排平行设置。  The segmented volute with a guide vane according to claim 3, wherein: the left outer air intake outer flow passage (7) and the outer side outer air intake outer flow passage (9) of the volute are respectively It is located on both sides of the inner flow passage (8) of the volute casing and arranged side by side in parallel.
5、 根据权利要求 3所述的带导流叶片的分段式蜗壳, 其特征在于: 所述蜗壳左侧进气外流道 (7)和蜗壳右侧进气外流道 (9) 分别位于蜗壳 进气内流道 (8) 的两侧, 所述蜗壳左侧进气外流道 (7) 的截面为弧形, 其外 端延伸至蜗壳进气内流道 (8) 的外侧。  The segmented volute with a guide vane according to claim 3, wherein: the left outer air intake outer flow passage (7) and the outer right outer air intake outer passage (9) of the volute are respectively Located on both sides of the inner flow passage (8) of the volute casing, the left outer air inlet passage (7) has an arc-shaped cross section, and the outer end extends to the inner flow passage (8) of the volute intake air. Outside.
6、 根据权利要求 4或 5所述的带导流叶片的分段式蜗壳, 其特征在于: 所述蜗壳左侧进气外流道(7)的截面积大于所述蜗壳右侧进气外流道(9) 的截面积。  The segmented volute with a guide vane according to claim 4 or 5, wherein: the cross-sectional area of the left outer air intake passage (7) of the volute is larger than the right side of the volute The cross-sectional area of the gas flow path (9).
7、 根据权利要求 6所述的带导流叶片的分段式蜗壳, 其特征在于- 所述蜗壳左侧进气外流道 (7) 和蜗壳右侧进气外流道 (9) 的截面积之和 是蜗壳进气内流道 (8) 的截面积的 0.3-1.1倍。  The segmented volute with a guide vane according to claim 6, characterized in that - the left outer intake outer flow passage (7) of the volute and the right outer air intake outer passage (9) of the volute The sum of the cross-sectional areas is 0.3-1.1 times the cross-sectional area of the inner flow passage (8) of the volute intake.
8、 根据权利要求 7所述的带导流叶片的分段式蜗壳, 其特征在于: 所述蜗 壳左侧进气外流道 (7)、 蜗壳右侧进气外流道 (9) 及蜗壳进气内流道 (8) 靠 近蜗壳扩压通道 (1) 的位置处分别设有无叶喷嘴 (15)。  The segmented volute with a guide vane according to claim 7, wherein: the left outer air inlet passage (7) of the volute, the outer air inlet outer flow passage (9) of the volute and The volute inlet inner flow passage (8) is provided with a vaneless nozzle (15) at a position close to the volute diffuser passage (1).
9、 根据权利要求 8所述的带导流叶片的分段式蜗壳, 其特征在于: 所述蜗 壳左侧进气外流道(7) 内靠近无叶喷嘴(15)处呈环形均匀设有若干片机翼型 气动式导流叶片 (16)。  The segmented volute with a guide vane according to claim 8, wherein: the outer ventilating outer flow passage (7) of the volute is annularly arranged adjacent to the no-blade nozzle (15). There are several airfoil pneumatic guide vanes (16).
10、 根据权利要求 9所述的带导流叶片的分段式蜗壳, 其特征在于- 所述导流叶片 (16) 的一端与蜗壳左侧进气外流道内壁 (17) —体铸造连 接, 另一端与左侧气动隔板 (5) 位于蜗壳左侧进气外流道 (7) —侧的内壁一 体铸造连接。 ^ 10. The segmented volute with a guide vane according to claim 9, characterized in that - one end of the guide vane (16) is integrally cast with the inner wall of the outer flow passage (17) of the left side of the volute Connected, the other end is connected to the left side pneumatic partition (5) on the left side of the outer side of the volute (7). ^
11、 根据权利要求 10所述的带导流叶片的分段式蜗壳, 其特征在于: 所述蜗壳左侧进气外流道 (7) 与蜗壳左侧进气外流道 (7) 的进气口之间 设有左侧外流道控制室 (11 ); 所述蜗壳右侧进气外流道 (9) 与蜗壳右侧进气 外流道 (9) 的进气口之间设有右侧外流道控制室 (12)。 The segmented volute with a guide vane according to claim 10, characterized in that: the left outer air inlet outer flow passage (7) of the volute and the left outer air intake outer flow passage (7) of the volute A left outer flow channel control chamber (11) is disposed between the air inlets; and a right outer air intake outer flow passage (9) of the volute is disposed between the air inlet of the outer air intake outer flow passage (9) of the right side of the volute Right outer flow channel control room (12).
12、 根据权利要求 11所述的带导流叶片的分段式蜗壳, 其特征在于: 安装在蜗壳左侧进气外流道(7)的进气口处的进气调节阀门(10)位于左 侧外流道控制室 (11 ) 内;  The segmented volute with a guide vane according to claim 11, characterized in that: an intake regulating valve (10) installed at an intake port of the intake outer flow passage (7) on the left side of the volute Located in the left outer flow channel control room (11);
安装在蜗壳右侧进气外流道(9)的进气口处的进气调节阀门(10)位于右 侧外流道控制室 (12) 内。  The intake regulating valve (10) installed at the intake port of the intake outer flow passage (9) on the right side of the volute is located in the right outer flow path control chamber (12).
13、 根据权利要求 12所述的带导流叶片的分段式蜗壳, 其特征在于: 所述 左侧外流道控制室 (11 ) 和右侧外流道控制室 (12) 上分别设有外流道上端盖 The segmented volute with a guide vane according to claim 12, wherein: the left outer flow channel control chamber (11) and the right outer flow channel control chamber (12) are respectively provided with an outflow Upper end cap
( 14), 以实现对进气流的密封和进气调节阀门的限位。 (14), to achieve the sealing of the intake air flow and the limit of the intake air regulating valve.
PCT/CN2012/000429 2012-01-11 2012-03-31 Segmented volute casing with guide vanes WO2013104091A1 (en)

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