TLE4922-XIN-F. 1 Product Description

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Transcription:

1 Product Description The TLE4922 is an active mono cell Hall sensor suited to detect motion and position of ferromagnetic and permanent magnet structures. An additional self-calibration module has been implemented to achieve optimum accuracy during normal running operation. 1.1 Target Application The TLE4922 is a speed sensor especially optimized for small engine (2- and 3 wheeler) applications. Crankshaft speed and position sensing Transmission speed on output shaft Speedometer application Excellent sensitivity and accuracy combined with its wide operational temperature range makes the sensor ideally suited for harsh environments. Figure 1-2 Package PG-SSO-4-1 1.2 Key Features and Benefits Twist independent mounting (TIM) enables one sensor fits all Small thin package (PG-SSO-4- Protected against harsh environment due to Short-circuit current protection at the output Over temperature shutdown at the output and Reverse voltage protection Supreme performance due to adaptive symmetrical hysteresis / threshold Independent of back bias magnet polarity due to ±400mT full scale range Enhanced EMC & ESD robustness - ESD : ±3kV HBM Wide operating temperature range - T junction : -40 C - 155 C True zero speed up to 8kHz signal frequency Enabling Low Power Application: Idd = 5mA at Vdd = 9V Large operating voltage range of 4.5V up to 18V Robustness against wheel run outs enables to sense broad range of wheels Figure 1-3 Hall Supply Chopped Hall Probe Pinning, Sensitive Area Analog Supply Tracking ADC Digital Supply D-Core (Min/Max, Offset, Comparator ) Open Drain V DD GND V Q Figure 1-4 Blockdiagram TLE4922 V BA TT V LOAD V BA TT R SERIES 200 Ω C VDD 47 nf IC 1 TLE4922 V DD Q GND V Q I Q C Q 4.7 nf R LOAD 1.2 kω C LOAD 50 pf Figure 1-1 Application circuit TLE4922 Figure 1-5 Wheel with sensor Product Type Marking Ordering Code Package TLE4922-XIN-F 22BAA2 SP001154230 PG-SSO-4-1 Data Sheet 1 V 1.0, 2016-11-21

2 The listed characteristics are ensured over the operating range and lifetime of the integrated circuit. 2.1 Absolute Maximum Ratings Table 2-1 Absolute Maximum Ratings Parameter Symbol Values Unit Note or Test Condition Min. Typ. Max. Supply voltage V S -18 - - V - - 18 V - - 24 V max. 1 hour V SAC - - 30 V max. 1 min with R SERIES = 200Ω Output OFF voltage V Q -1 - - V max. 60 min @ T A = 25 C -0.3-18 V Output ON voltage V Q - - 18 V Junction temperature T J 195 C 3h Overall lifetime 2) T Pol -40-150 C 0.5 years -40-50 C 15 years ESD compliance ESD HBM -3-3 kv HBM according ANSI/ESDA/JEDEC JS-001 In temperature range between operating temperature and absolute maximum temperature no functionality is guaranteed. 2) Maximum exposure time at other junction temperatures shall be calculated based on the values specified using the Arrhenius-model. Note: Stresses above the max. values listed here may cause permanent damage to the device. Exposure to absolute maximum rating conditions for extended periods may affect device reliability. Maximum ratings are absolute ratings; exceeding only one of these values may cause irreversible damage to the integrated circuit. 2.2 Operating Range The following operating conditions must not be exceeded in order to ensure correct operation of the IC. All parameters specified in the following sections refer to these operating conditions unless otherwise mentioned. Table 2-2 Operating Range Parameter Symbol Values Unit Note or Test Condition Min. Typ. Max. Supply voltage V S 4.5-18 V Continuous output ON current I Q - - 8.8 ma Operating junction temperature T J -40-155 C 5000h Frequency range of magnetic f 0 2) - 8000 Hz input signal Typical Rth JA is 170K/W. As soon as back bias magnet is attached or customer mold covers the TLE4922 this value will decrease due to larger surface and mass of the module. Maximum exposure time at other junction temperatures shall be calculated based on the values specified using the Arrhenius-model. 2) Maximum one additional pulse may occur due to temperature variation during stand still. Data Sheet 2 V 1.0, 2016-11-21

2.3 Electrical Characteristics Table 2-3 Electrical Parameters Parameter Symbol Values Unit Note or Test Condition Min. Typ. Max. Supply current I S 3.5 5.3 7.0 ma Output saturation voltage V QSAT - 0.15 0.4 V I Q = 8.8 ma Output leakage current I QLEAK - - 10 μa Current limit for short-circuit I QSHORT 37 44 52 ma protection Junction temperature for output protection Power on time t ON Output fall time 2) t f Output rise time 2) t r Delay time 3) t d T PROT Parameter is characterized by simulation/verification 2) Time between 20% and 80% value of V LOAD 3) Only valid for the falling edge 175 195 215 C Output will shut down (high impedance) when exceeded - 0.7 0.9 ms 2.2 2.8 3.8 μs V LOAD = 5 V, C LOAD =4.7 nf, R LOAD = 1.2 kω 1-20 µs V LOAD = 5 V, C LOAD =4.7 nf, R LOAD = 1.2 kω 12.5 18 23.5 μs V LOAD = 5 V, C LOAD =4.7 nf, R LOAD = 1.2 kω, f=5khz, see Figure 2-1 2.4 Magnetic Characteristics and Self-Calibration Characteristics Table 2-4 Magnetic Characteristics and Self-Calibration Characteristics: 10 Gauss = 1mT Parameter Symbol Values Unit Note / Test Condition Min. Typ. Max. Linear Region B LR -400-400 mt Peak to peak magnetic hysteresis B MIN 2.0 3.0 5.3 mt Full frequency range 2.0 3.0 3.8 mt Up to 3kHz signal frequency Temperature compensation of magnetic hysteresis TC Bmin - -650 - ppm Temperature range from 25 C to 150 C Back Bias Magnet Range B BIAS -400-400 mt At T a =25 C, please notice relation between back bias magnet and linear region as described in user manual Duty Cycle DC 2) 40 50 60 % 30 50 70 % Including EMC (magnetic distortion) Number of falling output edges required to be calibrated n 2)3) Calib - - 3 - At 4 th falling edge full accuracy reached. Relative phase error in calibrated mode Output falling edge repeatability (phase jitter) in calibrated mode ϕ rel 2)4) ϕ jitter 2)4) - ± 0.3 ± 1.5 crank Forward and backward rotational direction. Temperature and airgap included. - 0.05 0.2 crank 99.7 %, 3 pulses out of 1000 above limit. Equivalent to ± 3sigma of a Gaussian distribution. is calculated out of measured sensitivity 2) Parameter is characterized by simulation/verification 3) Maximum one additional pulse may occur due to temperature variation during stand still 4) Performance measured on wheel described in Chapter 2.6 within air gap range 0.5mm to 3.2mm Data Sheet 3 V 1.0, 2016-11-21

Magnetic encoder N S N S N Tooth Gearwheel Magnetic input signal Notch Threshold crossing switching points Delay time t d Threshold crossing switching points Sensor output signal Sensor output signal Delay time t d ᵠjitter 99.7% Figure 2-1 Phase error and delay time definition Phase jitter definition 2.5 Electromagnetic Compatibility (EMC) The TLE4922 is characterized according to the IC level EMC requirements described in the Generic IC EMC Test Version 1.2 from 2007. Additionally, component level EMC characterizations according to ISO 7637-2:2011, ISO 7637-3:2007 and ISO 16750-2:2010 regarding pulse immunity and CISPR 25 (2009-0 Ed. 3.0 regarding conducted emissions are performed. Figure 1-1 on first page outlines all needed external components to operate the DUT under application conditions. They are treated as inherent part of the DUT during component level EMC characterizations. Note: Characterisation of Electro Magnetic Compatibility (EMC) are carried out on sample base of one qualification lot. Not all specification parameters are monitored during EMC exposure. Only key parameters e.g. switching current and duty cycle are monitored. Parameter Symbol Level Class Testpulse 1 V EMC -100 V C Testpulse 2a 100 V A Testpulse 2b 10 V C Testpulse 3a -150 V A Testpulse 3b 100 V A Testpulse 4 2) -7 V C Testpulse 5b 3) 86.5 V A ISO 7637-2 (2004) describes internal resistance = 2Ω 2) According to 7637-2 for test pulse 4 the test voltage shall be 12 V +/- 0.2 V. 3) A central load dump protection of 35V is used. The document is available online at http://www.zvei.org/verband/publikationen/seiten/generic-ic-emctest--english.aspx Data Sheet 4 V 1.0, 2016-11-21

2.6 Reference Target Wheel Table 2-5 Toothed wheel performance Parameter Symbol Values Unit Note or Test Condition Min. Typ. Max. Operational IC air-gap AG 2) - - 3.2 mm Field strength of 300mT at 0.7mm above surface of back-bias magnet (is sensitive area of TLE4922) Air-gap variation over one complete target revolution. Global run-out. AG GLRO Parameter is characterized by verification 2) Measured from surface of package to toothed wheel, explained in Figure 2-2. - - 0.5 mm Difference between min. and max. air-gap over one complete target revolution. Figure 2-2 Infineon reference toothed wheel: dimension in mm Table 2-6 Reference target wheel geometry Parameter Typ value Unit Remarks Material ST37 - Tooth notch ratio 1.00 Data Sheet 5 V 1.0, 2016-11-21

2.7 Performance Graphs Following graphs of typical sensor behavior will help to optimize application performance: 6,5 Supply current @ Vdd=9V 5,5 Supply current 6 5,25 5,5 Tj=25 C [ma] [ma] 5 Tj=100 C 5 4,5 4,75 4-60 -30 0 30 60 90 120 150 180 4,5 3 5 7 9 11 13 15 17 19 Tj[C] Vdd[V] Fall time @ Vout=5V Fall time @ Vout=5V @ Tj=25 C 3,5 3,5 3 3 [us] [us] 2,5 2,5 2-50 0 50 100 150 Tj [ C] 2 4 6 8 10 12 14 16 18 VDD [V] Minimum magnetic field @ f=1khz Minimum magnetic field @ Tj=25 C 4,5 4,5 4 4 [mtpp] 3,5 3 [mtpp] 3,5 3 2,5 2,5 2-50 0 50 100 150 Tj[C] 2 100 1000 10000 Freq[Hz] Duty cycle @ B=10mTpp Duty cycle @ B=10mTpp 60 60 58 58 56 56 54 54 52 52 [%] 50 48 46 44 42 40-50 0 50 100 150 Tj[C] [%] 50 48 46 44 42 40 10 100 1000 10000 Freq[Hz] Figure 2-3 Typical Performance Data Sheet 6 V 1.0, 2016-11-21

2.8 Application Basic functionality The TLE4922 is a mono-cell Hall sensor with analog to digital converter and full digital signal processing for detecting the magnetic field crossing of the threshold levels. A chopped Hall probe is used to mimic the offset and has advantages for 0-Hz feature. Figure 2-1 shows the basic functionality of TLE4922. Unique Feature: Polarity of Pre Induction The back bias magnet can be mounted in both directions to TLE4922 without any difference in performance. One polarity results in switching the output to LOW when passing a tooth and to HIGH when passing a notch, whereas the other polarity of back-bias magnet will switch the output to HIGH when passing a tooth and to LOW when passing a notch. L V S NC GND Q S 0015 4952 S N Air gap from surface of sensor to surface of toothed wheel L V S NC GND Q S 0015 4952 N S Figure 2-4 V Q = LOW in front of tooth of the wheel: Sensor output Signal: Time / angle in rotational direction forward Changing polarity of back bias magnet will change the polarity of TLE4922 output V Q = HIGH in front of tooth of the wheel: Sensor output Signal: Time / angle in rotational direction forward Start-Up and Running Mode In Start-Up-Mode the TLE4922 starts with output at HIGH and stays there until a first minimum in magnetic field is detected after start-up time. Calibrated mode is reached after a maximum of four output transitions (The offset compensation algorithm is considering 4 teeth for averaging). At the 4 th falling edge full accuracy on output signal is reached. These first transitions are determined by the detection of magnetic signal maxima and minima. Output transitions in running phase are determined by the hidden adaptive hysteresis algorithm. Application circuit Figure 1-1 on page one shows an option of an application circuit. The resistor R S is recommended due to reason of EMC. The resistor R L has to be at a value to match the applied V ECU to keep I Q limited to the operating range of maximal 8.8mA. e.g.: V LOAD = 9V: I Q = 9V/1200 Ω = 7.5mA Consideration on Rth JA The Rth is modified by attaching a back-bias magnet or doing molding at the customer. There is dependency on the attached wires: The thicker the attached wire the smaller the value of Rth. It depends on ambient condition: When one end of the module is cooled in oil or through air-flow the Rth JA will decrease. Global run out Due to averaging, global run out is depending on the number of teeth. The wheel in Chapter 2.6 allows a global run out of 0.8mm. Wheels with equal or more than 8 teeth are capable of up to 0.5mm global run out. Data Sheet 7 V 1.0, 2016-11-21

Package Information 3 Package Information Green Product (RoHS compliant) To meet the world-wide customer requirements for environmentally friendly products and to be compliant with government regulations the device is available as a green product. Green products are RoHS-Compliant (i.e Pb-free finish on leads and suitable for Pb-free soldering according to IPC/JEDEC J-STD-020). 3.1 Package Information PG-SSO-4-1 Pure tin covering (green lead plating) is used. The product is RoHS (Restriction of Hazardous Substances) compliant and marked with letter G in front of the data code marking and may contain a data matrix code on the rear side of the package (see also information note 136/03). Please refer to your key account team or regional sales if your need further information. Figure 3-1 Marking pattern Figure 3-2 PG-SSO-4-1 package dimensions, dimensions in mm Data Sheet 8 V 1.0, 2016-11-21

Package Information Figure 3-3 PG-SSO-4-1 packaging, dimensions in mm Data Sheet 9 V 1.0, 2016-11-21

Revision History 4 Revision History Revision Date Changes 1.0 2016-11-21 Initial release Data Sheet 10 V 1.0 2016-11-21

Trademarks of Infineon Technologies AG AURIX, C166, CanPAK, CIPOS, CIPURSE, CoolMOS, CoolSET, CORECONTROL, CROSSAVE, DAVE, DI-POL, EasyPIM, EconoBRIDGE, EconoDUAL, EconoPIM, EconoPACK, EiceDRIVER, eupec, FCOS, HITFET, HybridPACK, I²RF, ISOFACE, IsoPACK, LITIX, MIPAQ, ModSTACK, my-d, NovalithIC, OptiMOS, ORIGA, POWERCODE, PRIMARION, PrimePACK, PrimeSTACK, PRO-SIL, PROFET, RASIC, ReverSave, SatRIC, SIEGET, SINDRION, SIPMOS, SmartLEWIS, SPOC, SOLID FLASH, TEMPFET, thinq!, TRENCHSTOP, TriCore. Other Trademarks Advance Design System (ADS) of Agilent Technologies, AMBA, ARM, MULTI-ICE, KEIL, PRIMECELL, REALVIEW, THUMB, µvision of ARM Limited, UK. AUTOSAR is licensed by AUTOSAR development partnership. Bluetooth of Bluetooth SIG Inc. CAT-iq of DECT Forum. COLOSSUS, FirstGPS of Trimble Navigation Ltd. EMV of EMVCo, LLC (Visa Holdings Inc.). EPCOS of Epcos AG. FLEXGO of Microsoft Corporation. FlexRay is licensed by FlexRay Consortium. HYPERTERMINAL of Hilgraeve Incorporated. IEC of Commission Electrotechnique Internationale. IrDA of Infrared Data Association Corporation. ISO of INTERNATIONAL ORGANIZATION FOR STANDARDIZATION. MATLAB of MathWorks, Inc. MAXIM of Maxim Integrated Products, Inc. MICROTEC, NUCLEUS of Mentor Graphics Corporation. MIPI of MIPI Alliance, Inc. MIPS of MIPS Technologies, Inc., USA. murata of MURATA MANUFACTURING CO., MICROWAVE OFFICE (MWO) of Applied Wave Research Inc., OmniVision of OmniVision Technologies, Inc. Openwave Openwave Systems Inc. RED HAT Red Hat, Inc. RFMD RF Micro Devices, Inc. SIRIUS of Sirius Satellite Radio Inc. SOLARIS of Sun Microsystems, Inc. SPANSION of Spansion LLC Ltd. Symbian of Symbian Software Limited. TAIYO YUDEN of Taiyo Yuden Co. TEAKLITE of CEVA, Inc. TEKTRONIX of Tektronix Inc. TOKO of TOKO KABUSHIKI KAISHA TA. UNIX of X/Open Company Limited. VERILOG, PALLADIUM of Cadence Design Systems, Inc. VLYNQ of Texas Instruments Incorporated. VXWORKS, WIND RIVER of WIND RIVER SYSTEMS, INC. ZETEX of Diodes Zetex Limited. Last Trademarks Update 2011-11-11 www.infineon.com Edition 2016-11-21 Published by Infineon Technologies AG 81726 Munich, Germany 2014 Infineon Technologies AG. All Rights Reserved. Do you have a question about any aspect of this document? Email: erratum@infineon.com Document reference Legal Disclaimer The information given in this document shall in no event be regarded as a guarantee of conditions or characteristics. With respect to any examples or hints given herein, any typical values stated herein and/or any information regarding the application of the device, Infineon Technologies hereby disclaims any and all warranties and liabilities of any kind, including without limitation, warranties of noninfringement of intellectual property rights of any third party. Information For further information on technology, delivery terms and conditions and prices, please contact the nearest Infineon Technologies Office (www.infineon.com). Warnings Due to technical requirements, components may contain dangerous substances. For information on the types in question, please contact the nearest Infineon Technologies Office. Infineon Technologies components may be used in life-support devices or systems only with the express written approval of Infineon Technologies, if a failure of such components can reasonably be expected to cause the failure of that life-support device or system or to affect the safety or effectiveness of that device or system. Life support devices or systems are intended to be implanted in the human body or to support and/or maintain and sustain and/or protect human life. If they fail, it is reasonable to assume that the health of the user or other persons may be endangered.