WO2011096640A2 - Turbocharger actuator - Google Patents

Turbocharger actuator Download PDF

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Publication number
WO2011096640A2
WO2011096640A2 PCT/KR2010/008785 KR2010008785W WO2011096640A2 WO 2011096640 A2 WO2011096640 A2 WO 2011096640A2 KR 2010008785 W KR2010008785 W KR 2010008785W WO 2011096640 A2 WO2011096640 A2 WO 2011096640A2
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WO
WIPO (PCT)
Prior art keywords
insert body
shaft
terminal assembly
actuator
hole
Prior art date
Application number
PCT/KR2010/008785
Other languages
French (fr)
Korean (ko)
Other versions
WO2011096640A3 (en
Inventor
강지만
최남선
김차식
Original Assignee
주식회사 인팩
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
Priority claimed from KR1020100010704A external-priority patent/KR20110091067A/en
Priority claimed from KR1020100101432A external-priority patent/KR101160073B1/en
Priority claimed from KR1020100101426A external-priority patent/KR101160072B1/en
Priority claimed from KR1020100107475A external-priority patent/KR101205707B1/en
Application filed by 주식회사 인팩 filed Critical 주식회사 인팩
Publication of WO2011096640A2 publication Critical patent/WO2011096640A2/en
Publication of WO2011096640A3 publication Critical patent/WO2011096640A3/en

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    • 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
    • F01D17/20Devices dealing with sensing elements or final actuators or transmitting means between them, e.g. power-assisted
    • 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
    • F02B37/18Control of the pumps by bypassing exhaust from the inlet to the outlet of turbine or to the atmosphere
    • F02B37/183Arrangements of bypass valves or actuators therefor
    • F02B37/186Arrangements of actuators or linkage for bypass valves
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B39/00Component parts, details, or accessories relating to, driven charging or scavenging pumps, not provided for in groups F02B33/00 - F02B37/00
    • F02B39/16Other safety measures for, or other control of, pumps
    • 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 turbocharger actuator of an automobile, and more particularly to a turbocharger actuator having a position sensor unit for monitoring the state of the turbocharger.
  • a turbocharger is a supercharger for improving engine performance by using exhaust gas generated from an internal combustion engine.
  • a turbocharger is a device that increases the engine output by forcibly sending compressed air to a combustion chamber so that more fuel can be combusted. to be.
  • Such turbochargers are broadly classified into waste gate turbochargers (WGT) and variable geometry turbochargers (VGT), and recently, variable turbochargers have been widely applied.
  • This variable turbocharger changes the area of the turbine inlet by adjusting the vanes to maximize the amount of air in the low load region, which is lacking in the waste gate turbocharger. By maximizing, the exhaust gas is reduced by securing sufficient air amount while increasing the response in the low speed and low load region.
  • variable turbocharger is largely composed of a compressor and a turbine, and further includes a flow passage adjusting mechanism for controlling the flow of exhaust gas therebetween.
  • the flow path adjusting mechanism is to improve the exhaust gas flow performance by adjusting the angular position of the vanes.
  • the unison ring is installed inside the turbine housing and the turbine wheel and the equally spaced one side of the unison ring. Is a plurality of vanes and discs moving within a non-contact range, bushings and levers for operating the vanes and discs, and actuators connected to the levers using rods and operated by vacuum pressure provided by the vacuum pump of the engine. It consists of.
  • the vane is a structure in which the whole is integrally connected, and this integrated bale connection structure is called a cartridge, and the position of the actuator rod, the lever connected thereto, and the entire vane can be controlled by the control of the actuator.
  • another object of the present invention is to provide an actuator of a turbocharger which can improve the operability of the actuator by adding a component to the insert body of the actuator to facilitate the reciprocating motion of the shaft.
  • the actuator unit having a piston rod reciprocating according to the engine state; And a position sensor unit for sensing the piston rod, wherein the position sensor unit is mounted on an upper side of the actuator unit, an insert body integrally formed in the cover body and formed with a through hole, and in the through hole.
  • a terminal assembly having a shaft installed to reciprocate, a magnet provided inside the shaft, and a hall sensor responsive to the magnetic force of the magnet, wherein the actuator portion is integrally formed under the cover body. It is characterized in that the configuration.
  • the position sensor unit may further include a friction reducing unit provided in the insert body to reduce friction generated between the inside of the insert body and the shaft during the reciprocating motion of the shaft.
  • the friction reducing part is composed of a bearing provided in the through hole of the insert body.
  • the bearing is integrally formed with the insert body by insert molding during the injection molding of the insert body.
  • the insert body and the shaft are provided with a guide for guiding the shaft to prevent the shaft from being eccentric in the through hole.
  • the guide part includes one or more guide ribs formed on a protrusion formed at a predetermined height on an outer circumference of the shaft, and one or more guide grooves corresponding to the guide ribs and formed on an inner circumference of the through hole.
  • the terminal assembly includes a lead frame, a terminal fixed to an upper end of the lead frame, and a hall sensor fixed to a lower end of the lead frame, wherein the terminal assembly is integrally formed during injection molding of the insert body. do.
  • the terminal assembly further includes a protective cap inserted into the hall sensor to protect the terminal assembly when the terminal assembly is injection molded integrally with the insert body.
  • the terminal assembly When the terminal assembly is integrally formed on the insert body, an exposed part is formed on the insert body, and the hall sensor is protruded to the exposed part, and a protective cap is fitted to the hall sensor.
  • the protective cap is composed of epoxy (EPOSY) or ABS resin.
  • a coupling groove is formed at one side of the through hole of the insert body, and the terminal assembly is fitted into the coupling groove.
  • FIG. 1 is a cross-sectional view showing a turbocharger actuator according to the present invention.
  • Figure 2 is a cross-sectional view showing a sensor portion of the turbocharger actuator according to the present invention.
  • Figure 3 is a cross-sectional view showing a coupling state of the insert body and the shaft of the turbocharger actuator according to the first embodiment of the present invention.
  • FIG. 4 is a perspective view showing a terminal assembly provided with a protection unit in the turbocharger actuator according to the first embodiment of the present invention.
  • FIG. 5 is a detailed view of portion A of FIG. 3;
  • Figure 6 is a perspective view showing an example of the friction reducing unit in the turbocharger actuator according to the first embodiment of the present invention.
  • Figure 7 is an exploded perspective view showing a guide portion of the turbocharger actuator according to the first embodiment of the present invention.
  • FIG. 8 is a cross-sectional view illustrating a hall sensor structure of a terminal assembly in a turbocharger actuator according to a second exemplary embodiment of the present invention.
  • Figure 9 is an exploded cross-sectional view showing a fixing structure of the terminal assembly in the turbocharger actuator according to a third embodiment of the present invention.
  • FIG. 10 is an exploded perspective view of FIG. 9;
  • actuator portion 101 piston rod
  • terminal assembly 241 lead frame
  • terminal 243 hall sensor
  • cap member 621 protective protrusion
  • FIG. 1 is a cross-sectional view showing a turbocharger actuator according to an embodiment of the present invention
  • Figure 2 is a cross-sectional view showing a sensor portion of a turbocharger actuator according to an embodiment of the present invention.
  • the turbocharger actuator according to the embodiment of the present invention is provided in the position sensor unit 200 for monitoring the state of the turbocharger, and the position preliminary portion 200 in accordance with the state of the vehicle and engine
  • the piston rod 101 is composed of an actuator part 100 provided to reciprocate.
  • the position sensor unit 200 includes a cover body 210 mounted on an upper side of the actuator unit 100, an insert body 220 provided inside the cover body 210, and A shaft 230 provided reciprocally in the insert body 220, a terminal assembly 240 provided at one side of the insert body 220, and a magnet 270 provided at an inner center of the shaft 230. ), And a cap member 280 fixed to the top of the shaft 230 is configured.
  • the insert body 220 has a through hole 221 for reciprocating the shaft 230.
  • a hole sensor 243 reacts with the magnetism of the magnet 270 at one side of the through hole 221.
  • the terminal assembly 240 is injection molded integrally with the insert body 220.
  • the terminal assembly 240 includes a lead frame 241, a terminal 242 fixed to the upper end of the lead frame 241, and a hall sensor 243 fixed to the lower end of the lead frame 241.
  • the terminal assembly 240 fixes the terminal 242 and the hall sensor 243 to the upper and lower ends of the lead frame 241, respectively.
  • a protection unit for protecting the Hall sensor 243 is further provided.
  • the protection unit does not directly affect the high temperature of the hall sensor 243 during injection molding, so that the inherent function of the hall sensor 243 is improved. It is to prevent the loss. That is, the Hall sensor 243 is in response to the magnetism of the magnet 270 formed inside the shaft 230 so that the position sensor unit 200 can be operated smoothly.
  • the protective part is composed of a protective cap 300 that is fitted from the lower side of the hall sensor 243.
  • the protective cap 300 is formed by penetrating the upper and lower portions, is inserted from the lower side of the hall sensor 243 is a part of the lower end of the hall sensor 243 protrudes to the lower side of the protective cap 300.
  • the protective cap 300 is formed of epoxy (EPOXY), ABS resin, or the like, which has heat resistance and low thermal conductivity, in order to prevent loss of the function of the hall sensor 243 due to high temperature during injection molding.
  • the shaft 230 is interlocked with the drive of the piston rod 101 of the actuator unit 100, the magnet 270 is formed integrally by insert injection molding therein.
  • the position sensor unit 200 is a component related to the engine, there is a high risk of burnout due to heat, and thus, the hall sensor 243, the magnet 270, and the cover body 210 constituting the position sensor unit 200. Care must be taken in the selection of materials such as the insert body 220.
  • the magnet 270 is made of ferrite, neodium, cobalt, alnico, and the like, and has a small change in magnetic flux depending on temperature, a high magnetic flux density, and an alnico having a high hardness. Use a series of magnets.
  • the insert body 220 and the shaft 230 are made of PPS (Poly Pheylene Sulfide) or epoxy.
  • PPS Poly Pheylene Sulfide
  • epoxy epoxy
  • PPS is also referred to as a super plastic that is spotlighted as a next-generation material to replace metals due to its heat resistance and durability as a thermoplastic resin.
  • the position sensor unit 200 further includes a spring 290 for returning to the original state after the shaft 230 is raised from the through hole 221.
  • the spring 290 is configured to be elastically supported by the cap member 280 and the protrusion 231 protruding from the outer circumference of the shaft 230 by being fitted to the outer circumference of the shaft 230.
  • a lower end of the through hole 221 may be provided with a locking portion that prevents the shaft 230 from being separated from the through hole 221 by the elastic force of the spring 290 in the through hole 221.
  • the spring 290 is to ensure the allowable stress and the coil strength through the selection of a suitable spring constant and material to allow the operation to limit the maximum movement stroke of the shaft 230.
  • the Hall sensor 243 is a device that requires programming to output a linear output.
  • the magnet 270 is firmly fixed in the shaft 230 in consideration of the sensing area and sensitivity of the Hall sensor 243 during insert injection molding, and after the magnet 270 is fixed to the shaft 230, There is almost no.
  • the hole sensor 243 is fixed in a spot welding manner in consideration of the sensing range of the Hall sensor 243 and the polarity of the magnet 270.
  • the through hole 221 of the insert body 220 is in contact with the inner circumferential surface of the through hole 221 during reciprocating movement of the shaft 230 to prevent friction, thereby smoothly reciprocating.
  • a friction reducing portion 400 is provided.
  • the friction reducing part 400 includes a bearing fixed to an inner circumference of the through hole 221.
  • the bearing is integrally molded to the insert body by insert molding during the molding of the insert body 220.
  • the bearing may be configured as a ball bearing or a roller bearing, and any bearing may be applied as long as the shaft 230 is smoothly reciprocated in the through hole 221.
  • the bearing is provided on the inner periphery of the lower end of the through hole 221 and is configured to perform a role of a catching part that prevents the shaft 230 from being separated from the through hole 221 by being caught by the protrusion 231 of the shaft 230. It becomes.
  • the insert body 220 and the shaft 230 may include guide parts for guiding the shaft 230 when the shaft 230 reciprocates in the through hole 221 to prevent eccentricity. 500 is provided.
  • the guide part 500 corresponds to the shape of the one or more guide ribs 510 and the guide ribs 510 formed on the outer circumference of the protrusion 231 formed at a predetermined height on the outer circumference of the shaft 230 and the through hole (
  • the guide groove 520 is formed on the inner circumference of the 221.
  • the shaft 230 has a lower end connected to the piston rod 101 of the actuator unit 100, and the through hole 221 of the insert body 220 by the piston rod 101 reciprocated according to the engine state. It will be reciprocated from.
  • FIG. 8 is a cross-sectional view illustrating a hall sensor structure of a terminal assembly in a turbocharger actuator according to a second exemplary embodiment of the present invention.
  • the terminal assembly 240 is integrally molded to the insert body 220 during the injection molding of the insert body 220, the terminal assembly 240 An exposed portion 224 protruding from the hall sensor 243 is formed, and a separate cap member 300 is fitted to the hall sensor 243 protruding from the exposed portion 224.
  • the Hall sensor 243 is formed in a state protruding to the exposed portion 224, the cap member 300 is provided separately in the Hall sensor 243 is inserted into the It is configured to protect the hall sensor 243 from high temperatures during injection molding of the cover body 210.
  • 9 and 10 are an exploded cross-sectional view and a perspective view showing the fixing structure of the terminal assembly in the turbocharger actuator according to the third embodiment of the present invention.
  • the turbocharger actuator according to the third embodiment of the present invention forms a coupling groove 612 in the insert body 610, and after fitting the terminal assembly 240 to the coupling groove 612
  • the cap member 620 is coupled to the upper portion of the through hole 611 of the insert body 610.
  • a fixing groove 614 is formed is the terminal 242 is seated.
  • a protective protrusion 621 formed in the cap member 620 is fixed to the fixing groove 614 to cover and protect the terminal 242.
  • the hall sensor 243 welded to the lead frame 241 of the terminal assembly 240 detects a change in the magnetic force according to the position change of the magnet 270 to detect the change value of the magnetic force through the terminal 242.
  • the Hall sensor 243 of the position sensor unit 200 detects a change in the magnetic force according to the position change of the magnet 270 and outputs a change value of the magnetic force through the terminal 241.
  • the configuration for detecting the turbocharger is composed only of the magnet and the hall sensor, there is an effect that can reduce the manufacturing cost and the malfunction rate of the product by simplifying the components.
  • the sensor unit for detection is integrally overmolded in the component parts of the product, it is possible to prevent malfunction due to vibration or moisture inflow and to improve durability.
  • the Hall sensor constituting the position sensor unit integrally to the component parts with a protective cap when molding, it prevents the sensor from losing its function due to high temperature during injection molding, thereby improving the performance of the product. It has an effect.

Abstract

The present invention relates to a turbocharger actuator, which comprises: an actuator section provided with a piston rod that reciprocates according to an engine state; and a position sensor section for sensing the piston rod. The position sensor section includes: a cover body mounted at the upper portion of the actuator section; an insert body integrally formed into the cover body and formed with a through-hole; a shaft mounted into the though-hole to be able to reciprocate; a magnet provided in the shaft; and a terminal assembly having a hall sensor responding to the magnetic force of the magnet, wherein the actuator section is integrated into the lower side of the cover body. Therefore, the state of a turbocharger is detected by only the magnet and the hall sensor, so that it is possible to reduce manufacturing costs and a malfunction rate of a product via the simplification of components. In addition, the sensor section for detection is integrally over-molded into the components of a product, so that it is possible to prevent malfunction due to vibration or moisture inflow so as to improve durability.

Description

터보차저 액츄에이터Turbocharger actuator
본 발명은 자동차의 터보차저 액츄에이터에 관한 것으로, 더욱 상세하게는 터보차저의 상태를 모니터링 하는 포지션 센서부를 구비한 터보차저 액츄에이터에 관한 것이다. The present invention relates to a turbocharger actuator of an automobile, and more particularly to a turbocharger actuator having a position sensor unit for monitoring the state of the turbocharger.
일반적으로, 터보차저는 내연기관에서 발생되는 배기가스를 이용하여 엔진의 성능을 향상시키기 위한 과급기로서, 강제로 압축한 공기를 연소실로 보내 더 많은 연료가 연소될 수 있도록 하여 엔진의 출력을 높이는 장치이다. In general, a turbocharger is a supercharger for improving engine performance by using exhaust gas generated from an internal combustion engine. A turbocharger is a device that increases the engine output by forcibly sending compressed air to a combustion chamber so that more fuel can be combusted. to be.
이러한 터보차저는 웨이스트 게이트 터보차저(Waste Gate TurboCharger : WGT)와 가변형상 터보차저(Variable Geometry Turbocharger :VGT)로 크게 분류되며, 최근에는 가변형상 터보차저가 널리 적용되고 있다. Such turbochargers are broadly classified into waste gate turbochargers (WGT) and variable geometry turbochargers (VGT), and recently, variable turbochargers have been widely applied.
이 가변형상 터보차저는 웨이스트 게이트 터보차저에서 부족하였던 저부하 영역에서의 공기량을 최대한 확보하고자 베인을 조정하여 터빈 입구의 면적을 변화시키는데, 저속 영역에서는 유로면적을 최소화하고, 고속영역에서는 유로면적을 최대화함으로써, 저속·저부하 영역에서의 응답성 증대와 함께 충분한 공기량 확보로 배기가스를 저감시키게 된다. This variable turbocharger changes the area of the turbine inlet by adjusting the vanes to maximize the amount of air in the low load region, which is lacking in the waste gate turbocharger. By maximizing, the exhaust gas is reduced by securing sufficient air amount while increasing the response in the low speed and low load region.
이러한 가변형상 터보차저는 컴프레서와 터빈으로 크게 구성되며, 그 사이에서 배기가스의 유동을 제어하는 유로 조절기구를 더 포함하고 있다. The variable turbocharger is largely composed of a compressor and a turbine, and further includes a flow passage adjusting mechanism for controlling the flow of exhaust gas therebetween.
유로 조절기구는 베인의 각도 위치를 조절하여 배기가스의 흐름 성능을 향상시키기 위한 것으로, 터빈 하우징 내부에 설치되는 유니슨 링(Unison Ring)과, 유니슨 링의 한쪽 면에 등간격으로 설치되면서 터빈휠과는 접촉되지 않는 범위 내에서 움직이는 다수개의 베인 및 원판과, 상기 베인 및 원판을 동작시켜 주는 부싱 및 레버와, 로드를 이용하여 레버에 연결되며 엔진의 진공펌프가 제공하는 진공압력에 의해 작동되는 액츄에이터로 구성된다. The flow path adjusting mechanism is to improve the exhaust gas flow performance by adjusting the angular position of the vanes. The unison ring is installed inside the turbine housing and the turbine wheel and the equally spaced one side of the unison ring. Is a plurality of vanes and discs moving within a non-contact range, bushings and levers for operating the vanes and discs, and actuators connected to the levers using rods and operated by vacuum pressure provided by the vacuum pump of the engine. It consists of.
베인은 전체가 일체형으로 연결된 구조이고, 이러한 일체형 베일 연결구조를 카트리지라고 하며, 또한, 액츄에이터의 제어에 의해 액츄에이터 로드 및 이에 연결된 레버, 전체 베인의 위치를 제어될 수 있게 되어 있다. The vane is a structure in which the whole is integrally connected, and this integrated bale connection structure is called a cartridge, and the position of the actuator rod, the lever connected thereto, and the entire vane can be controlled by the control of the actuator.
본 발명의 목적은 터보 차저의 효율을 향상시키고 불필요한 엔진 구동을 방지하여 연비 개선 및 공기 오염원 방출을 줄일 수 있도록 터보 차저 액츄에이터의 상태를 모니터링하는 것과, 구조를 간소화하며서도 액츄에이터의 모니터링 기능은 실현하여 구성부품의 단순화를 통한 원가절감을 실현할 수 있는 터보 차저의 액츄에이터를 제공하는 것이다. It is an object of the present invention to monitor the condition of the turbocharger actuator to improve the efficiency of the turbocharger and to prevent unnecessary engine operation, thereby improving fuel economy and reducing the emission of air pollutants. It is to provide an actuator of a turbocharger that can realize cost reduction by simplifying the components.
또한, 본 발명의 다른 목적은, 액츄에이터의 인서트 바디에 부품을 추가하여 샤프트의 왕복운동을 원활하게 함으로써, 액츄에이터의 동작성을 향상시킬 수 있는 터보 차저의 액츄에이터를 제공하는 것이다. In addition, another object of the present invention is to provide an actuator of a turbocharger which can improve the operability of the actuator by adding a component to the insert body of the actuator to facilitate the reciprocating motion of the shaft.
상기 목적을 달성하기 위한 본 발명은, 엔진 상태에 따라 왕복 운동하는 피스톤 로드를 구비하는 액츄에이터부; 상기 피스톤 로드를 센싱하기 위한 포지션 센서부를 포함하는 것으로, 상기 포지션 센서부는 상기 액츄에이터부의 상측에 장착되는 커버바디와, 상기 커버바디에 일체로 성형되고 관통홀이 형성되는 인서트 바디와, 상기 관통홀에 왕복 이동 가능하게 설치되는 샤프트와, 상기 샤프트의 내측에 구비되는 마그네트와, 상기 마그네트의 자력에 반응하는 홀센서를 갖는 터미널 앗세이를 포함하여 구성되며, 상기 커버바디의 하측에 상기 액츄에이터부가 일체로 구성되는 것을 특징으로 한다. The present invention for achieving the above object, the actuator unit having a piston rod reciprocating according to the engine state; And a position sensor unit for sensing the piston rod, wherein the position sensor unit is mounted on an upper side of the actuator unit, an insert body integrally formed in the cover body and formed with a through hole, and in the through hole. And a terminal assembly having a shaft installed to reciprocate, a magnet provided inside the shaft, and a hall sensor responsive to the magnetic force of the magnet, wherein the actuator portion is integrally formed under the cover body. It is characterized in that the configuration.
상기 포지션 센서부에는 상기 인서트 바디에 구비되어 상기 샤프트의 왕복 운동시 상기 인서트 바디의 내측과 상기 샤프트 사이에 발생되는 마찰을 저감시키기 위한 마찰저감부가 더 구비된다. The position sensor unit may further include a friction reducing unit provided in the insert body to reduce friction generated between the inside of the insert body and the shaft during the reciprocating motion of the shaft.
상기 마찰저감부는 상기 인서트 바디의 관통홀에 구비되는 베어링으로 구성된다. The friction reducing part is composed of a bearing provided in the through hole of the insert body.
상기 베어링은 상기 인서트 바디의 사출 성형시 인서트 성형에 의하여 상기 인서트 바디에 일체로 구성된다. The bearing is integrally formed with the insert body by insert molding during the injection molding of the insert body.
상기 인서트 바디와 샤프트에는 상기 관통홀에서 상기 샤프트가 왕복 운동할 때 편심되는 것을 방지하기 위하여 가이드하는 가이드부가 구비된다. The insert body and the shaft are provided with a guide for guiding the shaft to prevent the shaft from being eccentric in the through hole.
상기 가이드부는 상기 샤프트의 외주에 일정높이로 형성되는 돌출부에 형성되는 하나 이상의 가이드 리브와, 상기 가이드 리브에 대응되며 상기 관통홀 내주에 형성되는 하나이상의 가이드홈을 포함하여 구성된다. The guide part includes one or more guide ribs formed on a protrusion formed at a predetermined height on an outer circumference of the shaft, and one or more guide grooves corresponding to the guide ribs and formed on an inner circumference of the through hole.
상기 터미널 앗세이는 리드프레임과, 상기 리드프레임의 상단에 고정되는 터미널과, 상기 리드프레임의 하단에 고정되는 홀센서를 포함하는 것으로, 상기 터미널 앗세이는 상기 인서트 바디의 사출 성형시 일체로 성형된다. The terminal assembly includes a lead frame, a terminal fixed to an upper end of the lead frame, and a hall sensor fixed to a lower end of the lead frame, wherein the terminal assembly is integrally formed during injection molding of the insert body. do.
상기 터미널 앗세이는 상기 인서트 바디에 상기 터미널 앗세이가 일체로 사출 성형될 때, 상기 홀센서에 끼워져 보호하는 보호캡을 더 구비한다. The terminal assembly further includes a protective cap inserted into the hall sensor to protect the terminal assembly when the terminal assembly is injection molded integrally with the insert body.
상기 인서트 바디에 상기 터미널 앗세이를 일체로 성형 할 때, 상기 인서트 바디에 노출부가 형성되되, 상기 노출부로 상기 홀센서가 돌출되도록 성형되고, 상기 홀센서에 보호캡이 끼워져 고정된다. When the terminal assembly is integrally formed on the insert body, an exposed part is formed on the insert body, and the hall sensor is protruded to the exposed part, and a protective cap is fitted to the hall sensor.
상기 보호캡은 에폭시(EPOSY)나 ABS 수지로 이루어져 구성된다. The protective cap is composed of epoxy (EPOSY) or ABS resin.
상기 인서트 바디의 관통홀 일측에 결합홈이 형성되고, 상기 결합홈에 상기 터미널 앗세이가 끼워져 결합된다. A coupling groove is formed at one side of the through hole of the insert body, and the terminal assembly is fitted into the coupling groove.
도 1은 본 발명에 따른 터보차저 액츄에이터를 보인 단면도.1 is a cross-sectional view showing a turbocharger actuator according to the present invention.
도 2는 본 발명에 따른 터보차저 액츄에이터의 센서부를 보인 단면도. Figure 2 is a cross-sectional view showing a sensor portion of the turbocharger actuator according to the present invention.
도 3은 본 발명의 제1실시예에 따른 터보차저 액츄에이터의 인서트 바디와 샤프트의 결합 상태를 보인 단면도. Figure 3 is a cross-sectional view showing a coupling state of the insert body and the shaft of the turbocharger actuator according to the first embodiment of the present invention.
도 4는 본 발명의 제1실시예에 따른 터보차저 액츄에이터에서 보호부가 구비되는 터미널 앗세이를 보인 사시도.4 is a perspective view showing a terminal assembly provided with a protection unit in the turbocharger actuator according to the first embodiment of the present invention.
도 5는 도 3의 A부 상세도.5 is a detailed view of portion A of FIG. 3;
도 6은 본 발명의 제1실시예에 따른 터보차저 액츄에이터에서 마찰저감부의 일예를 보인 사시도.Figure 6 is a perspective view showing an example of the friction reducing unit in the turbocharger actuator according to the first embodiment of the present invention.
도 7은 본 발명의 제1실시예에 따른 터보차저 액츄에이터의 가이드부를 보인 분해사시도.Figure 7 is an exploded perspective view showing a guide portion of the turbocharger actuator according to the first embodiment of the present invention.
도 8은 본 발명의 제2실시예에 따른 터보차저 액츄에이터에서 터미널 앗세이의 홀센서 구조를 보인 단면도이다. 8 is a cross-sectional view illustrating a hall sensor structure of a terminal assembly in a turbocharger actuator according to a second exemplary embodiment of the present invention.
도 9는 본 발명의 제3실시예에 따른 터보차저 액츄에이터에서 터미널 앗세이의 고정 구조를 보인 분해 단면도. Figure 9 is an exploded cross-sectional view showing a fixing structure of the terminal assembly in the turbocharger actuator according to a third embodiment of the present invention.
도 10은 도 9의 분해사시도.10 is an exploded perspective view of FIG. 9;
* 부호의 설명 ** Explanation of Codes *
100 : 액츄에이터부 101 : 피스톤 로드100: actuator portion 101: piston rod
200 : 포지션 센서부 210 : 커버바디200: position sensor unit 210: cover body
220 : 인서트 바디 221 : 관통홀220: insert body 221: through hole
224 : 노출부 230 : 샤프트224: exposed portion 230: shaft
240 : 터미널 앗세이 241 : 리드프레임240: terminal assembly 241: lead frame
242 : 터미널 243 : 홀센서242: terminal 243: hall sensor
270 : 마그네트 280 : 캡부재270: magnet 280: cap member
290 : 스프링 300 : 보호캡290: spring 300: protective cap
400 : 마찰저감부 500 : 가이드부400: friction reduction portion 500: guide portion
510 : 가이드 리브 520 : 가이드홈510: guide rib 520: guide groove
610 : 인서트 바디 611 : 관통홀610: insert body 611: through hole
612 : 결합홈 614 : 고정홈612: coupling groove 614: fixing groove
620 : 캡부재 621 : 보호돌부620: cap member 621: protective protrusion
이하, 본 발명의 바람직한 실시에에 따른 터보차저 액츄에이터를 첨부된 도면을 참조하여 상세히 설명한다. Hereinafter, a turbocharger actuator according to a preferred embodiment of the present invention will be described in detail with reference to the accompanying drawings.
도 1은 본 발명의 실시예에 따른 터보차저 액츄에이터를 보인 단면도이고, 도 2는 본 발명의 실시예에 따른 터보차저 액츄에이터의 센서부를 보인 단면도이다. 1 is a cross-sectional view showing a turbocharger actuator according to an embodiment of the present invention, Figure 2 is a cross-sectional view showing a sensor portion of a turbocharger actuator according to an embodiment of the present invention.
도시된 바와 같이, 본 발명의 실시예에 따른 터보차저 액츄에이터는 터보차저의 상태를 모니터링 하기 위한 포지션 센서부(200)와, 포지션 선세부(200)의 하부에 구비되어 차량 및 엔진의 상태에 따라 피스톤 로드(101)가 왕복 이동가능하게 구비되는 액츄에이터부(100)로 구성된다. As shown, the turbocharger actuator according to the embodiment of the present invention is provided in the position sensor unit 200 for monitoring the state of the turbocharger, and the position preliminary portion 200 in accordance with the state of the vehicle and engine The piston rod 101 is composed of an actuator part 100 provided to reciprocate.
상기 포지션 센서부(200)는 도 2에 도시된 바와 같이, 액츄에이터부(100)의 상측에 장착되는 커버바디(210)와, 커버바디(210)의 내측에 구비되는 인서트 바디(220)와, 인서트 바디(220) 내측에 왕복 이동가능하게 구비되는 샤프트(230)와, 인서트 바디(220)의 일측에 구비되는 터미널 앗세이(240)와, 샤프트(230)의 내부 중앙에 구비되는 마그네트(270)과, 샤프트(230) 상단에 고정되는 캡부재(280)를 포함하여 구성된다. As shown in FIG. 2, the position sensor unit 200 includes a cover body 210 mounted on an upper side of the actuator unit 100, an insert body 220 provided inside the cover body 210, and A shaft 230 provided reciprocally in the insert body 220, a terminal assembly 240 provided at one side of the insert body 220, and a magnet 270 provided at an inner center of the shaft 230. ), And a cap member 280 fixed to the top of the shaft 230 is configured.
상기 인서트 바디(220)에는 샤프트(230)의 왕복 운동을 안내하는 관통홀(221)이 형성되고, 관통홀(221)의 일측에는 마그네트(270)의 자성과 반응하는 홀센서(243)를 갖는 터미널 앗세이(240)가 인서트 바디(220)에 일체로 사출 성형된다. The insert body 220 has a through hole 221 for reciprocating the shaft 230. A hole sensor 243 reacts with the magnetism of the magnet 270 at one side of the through hole 221. The terminal assembly 240 is injection molded integrally with the insert body 220.
상기 터미널 앗세이(240)는 리드프레임(241)과, 리드프레임(241)의 상단에 고정되는 터미널(242)과, 리드프레임(241)의 하단에 고정되는 홀센서(243)로 구성된다. The terminal assembly 240 includes a lead frame 241, a terminal 242 fixed to the upper end of the lead frame 241, and a hall sensor 243 fixed to the lower end of the lead frame 241.
상기 터미널 앗세이(240)는 인서트 바디(220)에 일체로 성형되기 전에, 리드프레임(241) 상단과 하단에 터미널(242)과 홀센서(243)를 각각 고정하는 것이다. Before the terminal assembly 240 is integrally molded to the insert body 220, the terminal assembly 240 fixes the terminal 242 and the hall sensor 243 to the upper and lower ends of the lead frame 241, respectively.
한편, 상기 터미널 앗세이(240)는 인서트 바디(220)에 일체로 사출 성형될 때, 홀센서(243)를 보호하기 위한 보호부가 더 구비된다. On the other hand, when the terminal assembly 240 is injection molded integrally with the insert body 220, a protection unit for protecting the Hall sensor 243 is further provided.
상기 보호부는 터미널 앗세이(240)를 인서트 바디(220)와 일체로 성형할 때, 사출 성형시 홀센서(243)가 고온에 직접적으로 영향을 받지 않도록 하여 홀센서(243)의 고유의 기능이 상실되는 것을 방지하는 것이다. 즉, 홀센서(243)가 샤프트(230)의 내측에 성형된 마그네트(270)의 자성에 반응되어 포지션 센서부(200)의 작동이 원활하게 이루어질 수 있도록 한 것이다. When the protective part is integrally molded with the insert body 220, the protection unit does not directly affect the high temperature of the hall sensor 243 during injection molding, so that the inherent function of the hall sensor 243 is improved. It is to prevent the loss. That is, the Hall sensor 243 is in response to the magnetism of the magnet 270 formed inside the shaft 230 so that the position sensor unit 200 can be operated smoothly.
상기 보호부는 홀센서(243)의 하측에서 끼워지는 보호캡(300)으로 구성된다. 상기 보호캡(300)은 상하부가 관통되어 형성되는 것으로, 홀센서(243)의 하측에서 끼워져 홀센서(243)의 하단 일부가 보호캡(300)의 하측으로 돌출되는 것이다. The protective part is composed of a protective cap 300 that is fitted from the lower side of the hall sensor 243. The protective cap 300 is formed by penetrating the upper and lower portions, is inserted from the lower side of the hall sensor 243 is a part of the lower end of the hall sensor 243 protrudes to the lower side of the protective cap 300.
여기서, 상기 보호캡(300)은 사출 성형시 고온으로 인하여 홀센서(243)의 기능이 상실되는 것을 방지하기 위하여 내열성이 있으면서 열전도율이 낮은 재질인 에폭시(EPOXY)나 ABS 수지 등으로 성형되는 것이다. Here, the protective cap 300 is formed of epoxy (EPOXY), ABS resin, or the like, which has heat resistance and low thermal conductivity, in order to prevent loss of the function of the hall sensor 243 due to high temperature during injection molding.
상기 샤프트(230)는 액츄에이터부(100)의 피스톤 로드(101)의 구동과 연동하는 것으로, 그 내부에 마그네트(270)가 인서트 사출 성형에 의해 일체로 형성된다. The shaft 230 is interlocked with the drive of the piston rod 101 of the actuator unit 100, the magnet 270 is formed integrally by insert injection molding therein.
또한, 상기 포지션 센서부(200)는 엔진에 관련된 부품이기 때문에 열에 의한 소손의 우려가 높으므로, 포지션 센서부(200)를 구성하는 홀센서(243), 마그네트(270) 및 커버바디(210)와 인서트 바디(220) 등의 재질 선정에 주의를 필요로 한다. In addition, since the position sensor unit 200 is a component related to the engine, there is a high risk of burnout due to heat, and thus, the hall sensor 243, the magnet 270, and the cover body 210 constituting the position sensor unit 200. Care must be taken in the selection of materials such as the insert body 220.
상기 마그네트(270)는 그 재료로 페라이트, 네오듐, 코발트, 알니코 계열 등이 있으며, 온도에 따른 자속량의 변화가 작고, 높은 자속 밀도를 얻을 수 있으며, 높은 경도를 갖는 알니코(Alnico)계열의 마그네트를 사용한다. The magnet 270 is made of ferrite, neodium, cobalt, alnico, and the like, and has a small change in magnetic flux depending on temperature, a high magnetic flux density, and an alnico having a high hardness. Use a series of magnets.
상기 인서트 바디(220)와 샤프트(230)는 PPS(Poly Pheylene Sulfide), 또는 에폭시의 재질로 이루어진다. 여기서, PPS란 열가소성수지로서 열에 강하면서 내구성이 뛰어나 금속을 대체할 차세대 소재로 각광받고 있는 슈퍼 플라시틱으로도 불린다. The insert body 220 and the shaft 230 are made of PPS (Poly Pheylene Sulfide) or epoxy. Here, PPS is also referred to as a super plastic that is spotlighted as a next-generation material to replace metals due to its heat resistance and durability as a thermoplastic resin.
상기 포지션 센서부(200)는 관통홀(221)에서 샤프트(230)가 상승된 후에 원상태로 복귀시키기 위한 스프링(290)을 더 구비한다. 상기 스프링(290)은 샤프트(230)의 외주에 끼워져 캡부재(280)와 샤프트(230) 외주에 돌출 형성되는 돌출부(231)에 탄력 지지되도록 구성된다. 그리고, 관통홀(221)의 하단 내주에는 샤프트(230)가 관통홀(221)에서 스프링(290)의 탄성력에 의해 이탈되지 않도록 샤프트(230)의 이탈을 방지하는 걸림부가 형성된다. The position sensor unit 200 further includes a spring 290 for returning to the original state after the shaft 230 is raised from the through hole 221. The spring 290 is configured to be elastically supported by the cap member 280 and the protrusion 231 protruding from the outer circumference of the shaft 230 by being fitted to the outer circumference of the shaft 230. In addition, a lower end of the through hole 221 may be provided with a locking portion that prevents the shaft 230 from being separated from the through hole 221 by the elastic force of the spring 290 in the through hole 221.
여기서, 상기 스프링(290)은 적당한 스프링 상수 및 재질 선정을 통한 허용 응력 및 코일 강도를 확보하여 샤프트(230)의 최대 이동스트로크에 제한을 두며 동작을 할 수 있도록 한다. Here, the spring 290 is to ensure the allowable stress and the coil strength through the selection of a suitable spring constant and material to allow the operation to limit the maximum movement stroke of the shaft 230.
그리고, 상기 홀센서(243)는 리니어 아웃풋(linear output)출력을 위하여 프로그래밍이 필요한 소자이다. In addition, the Hall sensor 243 is a device that requires programming to output a linear output.
상기 마그네트(270)는 인서트 사출성형시에 홀센서(243)의 센싱범위(sensing area) 및 감도(sensitivity)를 고려하여 샤프트(230) 내에 확실히 고정되며, 고정된 후에는 샤프트(230)와 단차가 거의 없도록 한다. The magnet 270 is firmly fixed in the shaft 230 in consideration of the sensing area and sensitivity of the Hall sensor 243 during insert injection molding, and after the magnet 270 is fixed to the shaft 230, There is almost no.
상기 터미널 앗세이(240)의 리드프레임(241)에 홀센서(243)를 고정할 때에는 홀센서(243)의 센싱 범위와 마그네트(270)의 극성을 고려하여 스폿웰딩 방식으로 고정한다. When the Hall sensor 243 is fixed to the lead frame 241 of the terminal assembly 240, the hole sensor 243 is fixed in a spot welding manner in consideration of the sensing range of the Hall sensor 243 and the polarity of the magnet 270.
한편, 인서트 바디(220)의 관통홀(221)에는 도 3에 도시된 바와 같이, 샤프트(230)의 왕복 운동시 관통홀(221)의 내주면과 접촉되어 마찰을 일으키는 것을 방지하여 왕복 운동을 원활하게 하는 마찰저감부(400)가 구비된다. Meanwhile, as illustrated in FIG. 3, the through hole 221 of the insert body 220 is in contact with the inner circumferential surface of the through hole 221 during reciprocating movement of the shaft 230 to prevent friction, thereby smoothly reciprocating. A friction reducing portion 400 is provided.
상기 마찰저감부(400)는 도 5에 도시된 바와 같이, 관통홀(221)의 내주에 고정되는 베어링으로 구성된다. 상기 베어링은 인서트 바디(220)의 성형시 인서트 성형으로 인서트 바디에 일체로 성형되는 것이다. As shown in FIG. 5, the friction reducing part 400 includes a bearing fixed to an inner circumference of the through hole 221. The bearing is integrally molded to the insert body by insert molding during the molding of the insert body 220.
상기 베어링은 도 6에 도시된 바와 같이, 볼베어링이나 롤러베어링으로 구성될 수 있으며, 샤프트(230)가 상기 관통홀(221)에서 원활하게 왕복 운동할 수 있도록 가이하는 것이면 모두 적용 가능하다. As shown in FIG. 6, the bearing may be configured as a ball bearing or a roller bearing, and any bearing may be applied as long as the shaft 230 is smoothly reciprocated in the through hole 221.
또한, 상기 베어링은 관통홀(221) 하단 내주에 구비되어 샤프트(230)의 돌출부(231)가 걸려서 샤프트(230)가 관통홀(221)에서 이탈되는 것을 방지하는 걸림부의 역할도 함께 수행하도록 구성되는 것이다 .In addition, the bearing is provided on the inner periphery of the lower end of the through hole 221 and is configured to perform a role of a catching part that prevents the shaft 230 from being separated from the through hole 221 by being caught by the protrusion 231 of the shaft 230. It becomes.
도 7에 도시된 바와 같이, 상기 인서트 바디(220)와 샤프트(230)에는 관통홀(221)에서 샤프트(230)가 왕복 운동할 때에 샤프트(230)를 가이드하여 편심되는 것을 방지하기 위한 가이드부(500)가 구비된다. As illustrated in FIG. 7, the insert body 220 and the shaft 230 may include guide parts for guiding the shaft 230 when the shaft 230 reciprocates in the through hole 221 to prevent eccentricity. 500 is provided.
상기 가이드부(500)는 샤프트(230)의 외주에 일정높이로 형성되는 돌출부(231)의 외주에 형성되는 하나 이상의 가이드 리브(510)와, 가이드 리브(510)의 형상에 대응되며 관통홀(221)의 내주에 형성되는 가이드 홈(520)으로 구성된다. The guide part 500 corresponds to the shape of the one or more guide ribs 510 and the guide ribs 510 formed on the outer circumference of the protrusion 231 formed at a predetermined height on the outer circumference of the shaft 230 and the through hole ( The guide groove 520 is formed on the inner circumference of the 221.
상기 샤프트(230)는 그 하단이 액츄에이터부(100)의 피스톤 로드(101)와 연결되며, 엔진의 상태에 따라 왕복 이동되는 피스톤 로드(101)에 의하여 인서트 바디(220)의 관통홀(221)에서 왕복 이동되는 것이다. The shaft 230 has a lower end connected to the piston rod 101 of the actuator unit 100, and the through hole 221 of the insert body 220 by the piston rod 101 reciprocated according to the engine state. It will be reciprocated from.
도 8은 본 발명의 제2실시예에 따른 터보차저 액츄에이터에서 터미널 앗세이의 홀센서 구조를 보인 단면도이다. 8 is a cross-sectional view illustrating a hall sensor structure of a terminal assembly in a turbocharger actuator according to a second exemplary embodiment of the present invention.
도시된 바와 같이, 본 발명의 제2실시예에 따른 터보차저 액츄에이터는 인서트 바디(220)의 사출 성형시 터미널 앗세이(240)가 인서트 바디(220)에 일체로 성형되되, 터미널 앗세이(240)의 홀센서(243)가 돌출되는 노출부(224)가 형성되고, 상기 노출부(224)로 돌출되는 홀센서(243)에 별도의 캡부재(300)가 끼워져 구성된다. As shown, the turbocharger actuator according to the second embodiment of the present invention, the terminal assembly 240 is integrally molded to the insert body 220 during the injection molding of the insert body 220, the terminal assembly 240 An exposed portion 224 protruding from the hall sensor 243 is formed, and a separate cap member 300 is fitted to the hall sensor 243 protruding from the exposed portion 224.
즉, 인서트 바디(220)의 사출성형시 홀센서(243)가 노출부(224)로 돌출된 상태로 성형된 후에, 상기 홀센서(243)에 별도로 구비되는 캡부재(300)가 끼워져서 상기 커버바디(210)의 사출 성형시 고온으로부터 홀센서(243)를 보호하도록 구성되는 것이다.That is, after the injection molding of the insert body 220, the Hall sensor 243 is formed in a state protruding to the exposed portion 224, the cap member 300 is provided separately in the Hall sensor 243 is inserted into the It is configured to protect the hall sensor 243 from high temperatures during injection molding of the cover body 210.
상기 제2실시예의 나머지 구성은 제1실시예의 구성과 동일함으로 제1실시예와 동일한 구성에 대하여 동일한 부호를 붙이고 자세한 설명은 생략한다.The rest of the configuration of the second embodiment is the same as that of the first embodiment, and the same reference numerals are assigned to the same components as the first embodiment, and detailed description thereof will be omitted.
도 9와 도 10은 본 발명의 제3실시예에 따른 터보차저 액츄에이터에서 터미널 앗세이의 고정 구조를 보인 분해 단면도와 사시도이다. 9 and 10 are an exploded cross-sectional view and a perspective view showing the fixing structure of the terminal assembly in the turbocharger actuator according to the third embodiment of the present invention.
도시된 바와 같이, 본 발명의 제3실시예에 따른 터보차저 액츄에이터는 인서트 바디(610)에 결합홈(612)을 형성하고, 이 결합홈(612)에 터미널 앗세이(240)를 끼워서 결합한 후에, 인서트 바디(610)의 관통홀(611) 상부에 캡부재(620)가 결합되는 구성이다. As shown, the turbocharger actuator according to the third embodiment of the present invention forms a coupling groove 612 in the insert body 610, and after fitting the terminal assembly 240 to the coupling groove 612 The cap member 620 is coupled to the upper portion of the through hole 611 of the insert body 610.
상기 인서트 바디(610)의 관통홀(611) 상부 일측에는 상기 터미널 앗세이(240)가 결합홈(612)에 끼워질 때, 터미널(242)이 안착되는 고정홈(614)이 형성된다. 그리고, 상기 고정홈(614)에는 캡부재(620)에 형성되는 보호돌부(621)가 고정되어, 터미널(242)을 덮어 보호하게 된다. The upper side of the through-hole 611 of the insert body 610, when the terminal assembly 240 is fitted into the coupling groove 612, a fixing groove 614 is formed is the terminal 242 is seated. In addition, a protective protrusion 621 formed in the cap member 620 is fixed to the fixing groove 614 to cover and protect the terminal 242.
상기 제3실시예의 나머지 구성은 제1실시예의 구성과 동일함으로 제1실시예와 동일한 구성에 대하여 동일한 부호를 붙이고 자세한 설명은 생략한다.The rest of the configuration of the third embodiment is the same as that of the first embodiment, so that the same components as in the first embodiment will be denoted by the same reference numerals and detailed description thereof will be omitted.
이하에서는 상기와 같은 구성으로 이루어지는 본발명의 실시예에 따른 터보차저 액츄에이터의 포지션 센서부의 동작관계를 설명한다. Hereinafter, an operation relationship of the position sensor unit of the turbocharger actuator according to the embodiment of the present invention having the above configuration will be described.
차량이 고속 주행시에는 액츄에이터부(100)의 피스톤 로드(101)가 하측으로 이동하게 되며, 동시에 포지션 센서부(200)의 샤프트(230)는 피스톤 로드(101)에 의하여 스프링(290)과 함께 하측으로 이동하게 된다. When the vehicle is traveling at high speed, the piston rod 101 of the actuator unit 100 moves downward, and at the same time, the shaft 230 of the position sensor unit 200 is lowered together with the spring 290 by the piston rod 101. Will be moved to.
이때, 상기 터미널 앗세이(240)의 리드프레임(241)에 용접된 홀센서(243)는 마그네트(270)의 위치 변화에 따른 자력의 변화를 감지하여 터미널(242)을 통해 자력의 변화값을 출력한다. At this time, the hall sensor 243 welded to the lead frame 241 of the terminal assembly 240 detects a change in the magnetic force according to the position change of the magnet 270 to detect the change value of the magnetic force through the terminal 242. Output
또한, 차량이 저속 주행시에는 액츄에이터부(100)의 피스톤 로드(101)가 위로 이동하게 되며, 동시에 포지션 센서부(200)의 샤프트(230)는 피스톤 로드(101)에 연동하여 위로 이동하게 된다. In addition, when the vehicle is traveling at a low speed, the piston rod 101 of the actuator unit 100 moves upward, and at the same time, the shaft 230 of the position sensor unit 200 moves upward in association with the piston rod 101.
이때 포지션 센서부(200)의 홀센서(243)는 마그네트(270)의 위치 변화에 따른 자력의 변화를 감지하여 터미널(241)을 통해 자력의 변화값을 출력한다.  At this time, the Hall sensor 243 of the position sensor unit 200 detects a change in the magnetic force according to the position change of the magnet 270 and outputs a change value of the magnetic force through the terminal 241.
본 발명에 의하면, 터보차저 상태를 검출하기 위한 구성이 마그네트와 홀센서만으로 이루어짐으로, 구성부품의 단순화를 통한 제조원가 절감과 제품의 오동작율을 줄일 수 있는 효과가 있다. According to the present invention, since the configuration for detecting the turbocharger is composed only of the magnet and the hall sensor, there is an effect that can reduce the manufacturing cost and the malfunction rate of the product by simplifying the components.
또한, 검출하기 위한 센서부가 제품의 구성부품 내에 일체로 오버 몰딩됨으로써, 진동이나 수분 유입에 의한 오작동을 방지하여 내구성을 향상시킬 수 있는 효과가 있다. In addition, since the sensor unit for detection is integrally overmolded in the component parts of the product, it is possible to prevent malfunction due to vibration or moisture inflow and to improve durability.
또한, 포지션 센서부를 구성하는 홀센서를 구성부품에 일체로 성형시 보호캡을 씌운 상태로 성형함으로써, 제품의 사출 성형시 고온에 의하여 센서부의 기능이 상실되는 것을 방지하여 제품의 성능을 향상시킬 수 있는 효과가 있다. In addition, by forming the Hall sensor constituting the position sensor unit integrally to the component parts with a protective cap when molding, it prevents the sensor from losing its function due to high temperature during injection molding, thereby improving the performance of the product. It has an effect.
또한, 포지션 센서부의 구성부품 중 홀센서가 구비되는 터미널 앗세이를 부품에 별도로 결합함으로써, 제품의 사출 성형시 센서부의 기능이 상실되는 것을 방지하여 제품의 성능을 향상실 수 있는 효과가 있다. In addition, by separately combining the terminal assembly having a Hall sensor among the components of the position sensor unit to the component, it is possible to prevent the sensor unit from losing its function during injection molding, thereby improving the performance of the product.

Claims (11)

  1. 엔진 상태에 따라 왕복 운동하는 피스톤 로드를 구비하는 액츄에이터부;An actuator unit having a piston rod reciprocating according to an engine state;
    상기 피스톤 로드를 센싱하기 위한 포지션 센서부를 포함하는 것으로,Including a position sensor for sensing the piston rod,
    상기 포지션 센서부는 상기 액츄에이터부의 상측에 장착되는 커버바디와,The position sensor unit and the cover body mounted on the upper side of the actuator unit;
    상기 커버바디에 일체로 성형되고 관통홀이 형성되는 인서트 바디와, An insert body formed integrally with the cover body and having a through hole formed therein;
    상기 관통홀에 왕복 이동 가능하게 설치되는 샤프트와, A shaft installed in the through hole so as to be reciprocated;
    상기 샤프트의 내측에 구비되는 마그네트와,A magnet provided inside the shaft,
    상기 마그네트의 자력에 반응하는 홀센서를 갖는 터미널 앗세이를 포함하여 구성되며, It comprises a terminal assembly having a Hall sensor in response to the magnetic force of the magnet,
    상기 커버바디의 하측에 상기 액츄에이터부가 일체로 구성되는 것을 특징으로 하는 터보차저 액츄에이터. Turbocharger actuator, characterized in that the actuator unit is integrally formed on the lower side of the cover body.
  2. 청구항 1항에 있어서,The method according to claim 1,
    상기 포지션 센서부에는 상기 인서트 바디에 구비되어 상기 샤프트의 왕복 운동시 상기 인서트 바디의 내측과 상기 샤프트 사이에 발생되는 마찰을 저감시키기 위한 마찰저감부가 더 구비되는 것을 특징으로 하는 터보차저 액츄에이터. The position sensor unit may further include a friction reducing unit provided in the insert body to reduce friction generated between the inner side of the insert body and the shaft during the reciprocating movement of the shaft.
  3. 청구항 2항에 있어서, The method according to claim 2,
    상기 마찰저감부는 상기 인서트 바디의 관통홀에 구비되는 베어링인 것을 특징으로 하는 터보차저 액츄에이터. The friction reducing unit is a turbocharger actuator, characterized in that the bearing provided in the through-hole of the insert body.
  4. 청구항 3항에 있어서, The method according to claim 3,
    상기 베어링은 상기 인서트 바디의 사출 성형시 인서트 성형에 의하여 상기 인서트 바디에 일체로 구성되는 것을 특징으로 하는 터보차저 액츄에이터. The bearing is a turbocharger actuator, characterized in that integrally configured to the insert body by insert molding during the injection molding of the insert body.
  5. 청구항 1항에 있어서, The method according to claim 1,
    상기 인서트 바디와 샤프트에는 상기 관통홀에서 상기 샤프트가 왕복 운동할 때 편심되는 것을 방지하기 위하여 가이드하는 가이드부가 구비되는 것을 특징으로 하는 터보차저 액츄에이터. The insert body and the shaft is a turbocharger actuator, characterized in that the guide portion for guiding to prevent the eccentricity when the shaft reciprocates in the through hole.
  6. 청구항 5항에 있어서, The method according to claim 5,
    상기 가이드부는 상기 샤프트의 외주에 일정높이로 형성되는 돌출부에 형성되는 하나 이상의 가이드 리브와, The guide portion and one or more guide ribs formed on the protrusion formed at a predetermined height on the outer circumference of the shaft,
    상기 가이드 리브에 대응되며 상기 관통홀 내주에 형성되는 하나이상의 가이드홈을 포함하는 것을 특징으로 하는 터보차저 액츄에이터. And at least one guide groove corresponding to the guide rib and formed in the inner circumference of the through hole.
  7. 청구항 1항에 있어서, The method according to claim 1,
    상기 터미널 앗세이는 리드프레임과, 상기 리드프레임의 상단에 고정되는 터미널과, 상기 리드프레임의 하단에 고정되는 홀센서를 포함하는 것으로, The terminal assembly includes a lead frame, a terminal fixed to an upper end of the lead frame, and a hall sensor fixed to a lower end of the lead frame.
    상기 터미널 앗세이는 상기 인서트 바디의 사출 성형시 일체로 성형되는 것을 특징으로 하는 터보차저 액츄에이터. The terminal assembly may be integrally molded during injection molding of the insert body.
  8. 청구항 7항에 있어서, The method of claim 7, wherein
    상기 터미널 앗세이는 상기 인서트 바디에 상기 터미널 앗세이가 일체로 사출 성형될 때, 상기 홀센서에 끼워져 보호하는 보호캡을 더 구비하는 것을 특징으로 하는 터보차저 액츄에이터. The terminal assembly may further include a protective cap fitted to the hall sensor to protect the terminal assembly when the terminal assembly is injection molded integrally with the insert body.
  9. 청구항 7항에 있어서, The method of claim 7, wherein
    상기 인서트 바디에 상기 터미널 앗세이를 일체로 성형 할 때, 상기 인서트 바디에 노출부가 형성되되, 상기 노출부로 상기 홀센서가 돌출되도록 성형되고, When the terminal assembly is integrally formed on the insert body, an exposed part is formed in the insert body, and the hall sensor is formed to protrude into the exposed part.
    상기 홀센서에 보호캡이 끼워져 고정되는 것을 특징으로 하는 터보차저 액츄에이터. Turbocharger actuator, characterized in that the protective cap is fitted to the Hall sensor.
  10. 청구항 8항 또는 청구항 9항에 있어서, The method according to claim 8 or 9,
    상기 보호캡은 에폭시(EPOSY)나 ABS 수지로 이루어지는 것을 특징으로 하는 터보차저 액츄에이터.The protective cap is a turbocharger, characterized in that consisting of epoxy (EPOSY) or ABS resin.
  11. 청구항 1항에 있어서, The method according to claim 1,
    상기 인서트 바디의 관통홀 일측에 결합홈이 형성되고, 상기 결합홈에 상기 터미널 앗세이가 끼워져 결합되는 것을 특징으로 하는 터보차저 액츄에이터. A coupling groove is formed at one side of the through hole of the insert body, and the terminal assembly is inserted into and coupled to the coupling groove.
PCT/KR2010/008785 2010-02-05 2010-12-09 Turbocharger actuator WO2011096640A2 (en)

Applications Claiming Priority (8)

Application Number Priority Date Filing Date Title
KR10-2010-0010704 2010-02-05
KR1020100010704A KR20110091067A (en) 2010-02-05 2010-02-05 Turbo charger actuator positon sensor
KR1020100101432A KR101160073B1 (en) 2010-10-18 2010-10-18 Actuator structure of turbocharger
KR1020100101426A KR101160072B1 (en) 2010-10-18 2010-10-18 Actuator structure of turbocharger
KR10-2010-0101432 2010-10-18
KR10-2010-0101426 2010-10-18
KR10-2010-0107475 2010-11-01
KR1020100107475A KR101205707B1 (en) 2010-11-01 2010-11-01 Actuator structure of turbocharger

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WO2011096640A2 true WO2011096640A2 (en) 2011-08-11
WO2011096640A3 WO2011096640A3 (en) 2011-11-03

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Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP3514606B2 (en) * 1997-06-03 2004-03-31 三菱電機株式会社 Turbocharger control device
JP2004150400A (en) * 2002-11-01 2004-05-27 Hino Motors Ltd Continuously operating device for apparatus for engine
JP2004251203A (en) * 2003-02-20 2004-09-09 Jidosha Denki Kogyo Co Ltd Nozzle vane driving control device for variable nozzle type turbo charger
JP2005180456A (en) * 2005-03-04 2005-07-07 Hitachi Ltd Variable displacement turbocharger of automobile internal combustion engine with moving blade type turbine
KR20080090696A (en) * 2007-04-05 2008-10-09 삼성전자주식회사 Device for detecting position of antenna

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP3514606B2 (en) * 1997-06-03 2004-03-31 三菱電機株式会社 Turbocharger control device
JP2004150400A (en) * 2002-11-01 2004-05-27 Hino Motors Ltd Continuously operating device for apparatus for engine
JP2004251203A (en) * 2003-02-20 2004-09-09 Jidosha Denki Kogyo Co Ltd Nozzle vane driving control device for variable nozzle type turbo charger
JP2005180456A (en) * 2005-03-04 2005-07-07 Hitachi Ltd Variable displacement turbocharger of automobile internal combustion engine with moving blade type turbine
KR20080090696A (en) * 2007-04-05 2008-10-09 삼성전자주식회사 Device for detecting position of antenna

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