EP2984494A1 - Verfahren zur untersuchung der temperaturzuverlässigkeit eines elektronischen bauelements - Google Patents

Verfahren zur untersuchung der temperaturzuverlässigkeit eines elektronischen bauelements

Info

Publication number
EP2984494A1
EP2984494A1 EP14712244.4A EP14712244A EP2984494A1 EP 2984494 A1 EP2984494 A1 EP 2984494A1 EP 14712244 A EP14712244 A EP 14712244A EP 2984494 A1 EP2984494 A1 EP 2984494A1
Authority
EP
European Patent Office
Prior art keywords
electronic
laser source
coupling member
interest
wavelength
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Withdrawn
Application number
EP14712244.4A
Other languages
English (en)
French (fr)
Inventor
Florent Miller
Sébastien MORAND
Florian Moliere
Thomas Santini
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus SAS
Original Assignee
Airbus Group SAS
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 Airbus Group SAS filed Critical Airbus Group SAS
Publication of EP2984494A1 publication Critical patent/EP2984494A1/de
Withdrawn legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01RMEASURING ELECTRIC VARIABLES; MEASURING MAGNETIC VARIABLES
    • G01R31/00Arrangements for testing electric properties; Arrangements for locating electric faults; Arrangements for electrical testing characterised by what is being tested not provided for elsewhere
    • G01R31/28Testing of electronic circuits, e.g. by signal tracer
    • G01R31/2851Testing of integrated circuits [IC]
    • G01R31/2855Environmental, reliability or burn-in testing
    • G01R31/2856Internal circuit aspects, e.g. built-in test features; Test chips; Measuring material aspects, e.g. electro migration [EM]
    • G01R31/2858Measuring of material aspects, e.g. electro-migration [EM], hot carrier injection
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01RMEASURING ELECTRIC VARIABLES; MEASURING MAGNETIC VARIABLES
    • G01R31/00Arrangements for testing electric properties; Arrangements for locating electric faults; Arrangements for electrical testing characterised by what is being tested not provided for elsewhere
    • G01R31/28Testing of electronic circuits, e.g. by signal tracer
    • G01R31/2851Testing of integrated circuits [IC]
    • G01R31/2855Environmental, reliability or burn-in testing
    • G01R31/2872Environmental, reliability or burn-in testing related to electrical or environmental aspects, e.g. temperature, humidity, vibration, nuclear radiation
    • G01R31/2874Environmental, reliability or burn-in testing related to electrical or environmental aspects, e.g. temperature, humidity, vibration, nuclear radiation related to temperature
    • G01R31/2875Environmental, reliability or burn-in testing related to electrical or environmental aspects, e.g. temperature, humidity, vibration, nuclear radiation related to temperature related to heating
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01RMEASURING ELECTRIC VARIABLES; MEASURING MAGNETIC VARIABLES
    • G01R31/00Arrangements for testing electric properties; Arrangements for locating electric faults; Arrangements for electrical testing characterised by what is being tested not provided for elsewhere
    • G01R31/28Testing of electronic circuits, e.g. by signal tracer
    • G01R31/302Contactless testing
    • G01R31/308Contactless testing using non-ionising electromagnetic radiation, e.g. optical radiation
    • G01R31/311Contactless testing using non-ionising electromagnetic radiation, e.g. optical radiation of integrated circuits

Definitions

  • the present invention belongs to the field of the analysis of electronic components, and more particularly to the procedures for analyzing the operation of electronic components subjected to thermal stresses.
  • the electronic components before their implementation, are generally subjected to analysis procedures during which these components are notably subject to constraints representative of the operational constraints, that is to say the constraints to which they are susceptible of to be confronted in their final environment.
  • These analysis procedures are especially important, especially for components that are required to operate in highly constrained environments, such as components to be used in space and / or military missions, aircraft, power plants, energy, etc.
  • State of the art are especially important, especially for components that are required to operate in highly constrained environments, such as components to be used in space and / or military missions, aircraft, power plants, energy, etc.
  • a thermal stress which corresponds, for example, to an operational thermal stress (it is then referred to as a functional test) or a thermal stress applied to accelerate the aging of said integrated circuit (it is called aging test).
  • the aging tests make it possible to reveal the failure mechanisms such as the breakdown of the gate oxide of the transistors, the instability of the threshold voltage in temperature as well as the phenomenon of electromigration present at the level of the metallizations. These tests aging also make it possible to anticipate the thermomechanical fatigue of the component present at the level of the connectors, the metallizations and the barrier layer between the etching and oxide layers of a component.
  • one method consists of carrying out tests in a climatic chamber or under a packing bell.
  • the component and its support are solicited, statically or by cycle, in temperature.
  • these tests require a large number of elements such as the component chip, the housing, the solders, the connection pins, the connection wires, thus limiting the possibilities of interpretation of the failure mechanisms.
  • the present invention intends to overcome the drawbacks of the prior art by proposing a solution which makes it possible to locate thermal stresses on an electronic component by means of a laser beam coupled to a cooling device of the component.
  • the present invention relates, in its most general sense, to a method for analyzing the temperature reliability of an electronic component comprising an electronic chip mounted in a housing, said electronic chip being composed of several layers of materials. said method comprising the following steps:
  • the invention makes it possible to implement, for example, the thermally induced voltage modification (TIVA) method or the thermally induced resistance modification method "OBIRCH” (for "Optical induced voltage alteration”). beam induced resistance change ").
  • TIVA thermally induced voltage modification
  • OBIRCH thermally induced resistance modification method
  • the method for modifying the thermally induced resistance "OBIRCH” it is in particular to identify degradations in the metallizations of the electronic component.
  • This method is based on a local modification of the properties (resistivity for example) of the metallization depending on whether the impacted area is degraded or not.
  • the temperature variations generated by the laser beam are however in this case adjusted (in energy, frequency or duration) so as not to contribute to degrade or age the component.
  • the temperature variations produced are typically of the order of ten degrees.
  • the invention thus makes it possible to simulate, on the basis of the physical laser heating mechanisms, much larger temperature ranges making it possible to reproduce, in a localized manner (at the scale of one or a few elementary structures in the component) the constraints environmental and / or functional aspects of an electronic component.
  • the invention makes it possible, for example, to impose temperatures varying between -55 ° C. and + 125 ° C., depending on the characteristics of the laser source and the regulation source.
  • the wavelength is determined so that the energy of the photons of the laser beam is less than the energy of the forbidden band of the electronic chip. This implementation prevents the photoelectric interactions in the component. In the case of a silicon component, the wavelength must thus be less than 1, 1 ⁇ .
  • said method comprises two recurrent steps: a first step of activating the laser source and a second step of deactivating the laser source.
  • This implementation creates a cycle phenomenon in the component that accelerates its aging.
  • said method comprises a step of adapting the laser source to an area of interest of the electronic component.
  • This implementation makes it possible to target an area of interest whose size is adjustable according to the needs.
  • said method comprises a step of focusing or adjusting the size of a collimated beam of the laser source on one or more structures of interest of the electronic component.
  • This implementation makes it possible, for example, to target with a high precision, through the use of a high-magnitude objective, a transistor or a logical function of a component for which a sensitive mechanism can intervene, or if the beam is less focused and / or collimated, to solicit a component in whole.
  • the thermal coupling member is a passive cooling device.
  • a passive cooling device includes climatic chambers, cryostats and natural convection devices. It keeps the component at a substantially constant temperature.
  • the thermal coupling member is an active cooling device.
  • An active cooling device includes thermoelectric modules, water cooling devices and forced convention devices. It maintains, more effectively than a passive device, the component at a substantially constant temperature.
  • said electronic component comprises a front face and a rear face and the coupling member may be applied on the same face as the thermal stressing or on opposite faces.
  • the method comprises a radiation stressing step of the electronic chip through an opening, previously formed in the housing, the coupling member preserving optical access to said opening.
  • said method further comprises:
  • a second step of thermally stressing the zone of interest by means of a laser source emitting the predetermined wavelength This implementation makes it possible to solicit the electronic component by two laser sources simultaneously having the effect of increasing the possibilities of energy transfer.
  • a first Laser source is directed to one side while the other source is directed to the other side.
  • FIG. 1 illustrates a device for analyzing the temperature reliability of an electronic component according to a first embodiment, in which the laser beam and the coupling member are directed on the front face;
  • FIG. 2 illustrates an analysis device according to a second embodiment, in which the laser beam is collimated on the front face and the coupling member is in contact with the rear face;
  • FIG. 3 illustrates an analysis device according to a third embodiment, in which the laser beam is focused on the rear face and the coupling member is in contact with the rear face;
  • FIG. 4 illustrates an analysis device according to a fourth embodiment, in which the laser beam is focused on the front face and the coupling member corresponds to a climatic chamber;
  • FIG. 5 illustrates an analysis device according to a fifth embodiment, in which the laser beam is collimated on the front face and the coupling member corresponds to a climatic chamber;
  • FIG. 6 illustrates an analysis device according to a sixth embodiment, in which the laser beam is focused on a large surface of the front face and the coupling member corresponds to a climatic chamber;
  • FIG. 7 illustrates the evolution of the absorption coefficient per centimeter in boron-doped silicon as a function of photons of different energies;
  • FIG. 8 illustrates the evolution of the absorption rate of several materials as a function of the wavelength of the laser.
  • Figure 9 illustrates the evolution of the temperature in the component as a function of the distance to the area of interest.
  • FIG. 1 illustrates a device for analyzing the temperature reliability of an electronic component 10.
  • Said component 10 is composed of a housing 11 surrounding a chip 12, the chip 12 is composed of several layers 13-15 of materials .
  • the chip 12 of FIG. 1 may be composed of an aluminum metallization layer 13, a silicon substrate 14 and a copper lower layer 15.
  • the chip 12 has two opposite faces 17-18, a rear face 18 and a front face 17.
  • the term "housing" 1 1 any element preventing mechanical access to the electronic chip 12.
  • 1 1 housing may for example be formed by a protective shell, an encapsulation resin ...
  • the device imposes a thermal stressing by means of a laser beam 33 emanating from a laser source 32 and a thermal regulation by means of a thermal coupling member 25.
  • the thermal coupling member 25 comprises a source 24 of thermal stress, which can be of any known type.
  • the source 24 of thermal stress comprises a thermoelectric module 29, such as a Peltier module.
  • a Peltier module generally has two opposite faces. When it is supplied with current, one of its faces, called “hot face”, will warm up, while the other face, called “cold face”, will cool down.
  • the source 24 of thermal stress also comprises a thermoregulator module 23, which can be of any known type. This is for example a module thermoregulator circulating heat transfer fluid (water, oil, etc.), implemented to regulate the temperature of a face of the Peltier module, the cold face if it is desired to apply a heat stress to the electronic component 10.
  • the Coupling member 25 also has an end 26 to be thermally coupled to source 24 of thermal stress.
  • the end 26 of the coupling member 25 is wholly or partly made of thermally conductive material, for example copper or copper alloy, aluminum or aluminum alloy, etc.
  • the end 26 of the coupling member 25 is adapted, by its geometry, to be introduced into an opening 19 previously formed in the housing 1 1 of the electronic component 10.
  • geometric of the end 26 is meant its external volume, that is, its shape and dimensions.
  • the opening 19 previously formed in the housing 1 1 provides mechanical access to all or part of the front face 17 of the electronic chip 12, with which a coupling face of the end 26 is thermally coupled at the time of entry. stress of the electronic component 10.
  • the coupling member 25 comprises an optical window 30 allowing the laser beam 33 to pass to reach the front face 17 of the electronic chip 12.
  • the optical window 30 can take any known shape such as a cylindrical recess.
  • Figures 2 to 4 show other embodiments of the device for analyzing the temperature reliability of an electronic component 10.
  • the thermal coupling member 25 may take different forms other than that of Figures 1 and 3 comprising a thermoelectric module.
  • FIG. 2 shows a forced convection system in which the coupling member 25 is in contact on the entire rear face 18 of the electronic chip 12.
  • the coupling member 25 can thus be traversed by a hydraulic circuit whose temperature of the water is adjustable.
  • Figures 4, 5 and 6 illustrate a coupling member 25 formed by a climatic chamber 37 whose temperature is fully regulated.
  • the laser beam 33 enters the climatic chamber by an optical access window having a glazed surface.
  • the coupling member 25 has the effect of limiting as much as possible the thermal stress experienced by the whole of the electronic component 10 to the zone of interest 20.
  • the localized stress can be effective only if localized heating is coupled to a dissipation phase to evacuate the heat generated locally or if a second source is used to force a thermal gradient in the area of interest.
  • the coupling member 25 can be positioned on the opposite side to the laser excitation (in the case of FIG. 2) or on the same side (in the case of FIGS. 1 and 3) or can encompass the electronic component 10 (as in FIG. 4). .
  • the function of the coupling member 25 is to amplify the thermal stresses and to constrain the electronic component 10 more locally.
  • the laser beam 33 makes it possible to create a localized heating in a precise layer 13-15 of the electronic chip 12.
  • the energy of the laser source 30 is adjusted so that the temperature at the surface of the aluminum layer 13 is +200 ° C.
  • the copper layer 15 serves as an interface with the coupling member 25 imposing a temperature of -20 ° C.
  • the presence of active cooling makes it possible to greatly reduce the temperature at the silicon layer 14 of the electronic chip 12 while maintaining a high level of temperature at the level of the aluminum layer 13 on which the area of interest is placed.
  • the laser beam 33 can also be focused by means of optical lenses 34 of different magnitudes as shown in FIGS.
  • the focused laser beam 33 allows, according to the objective used, to urge one or more elementary structures of the electronic component 10 or an entire component. In the case of Figure 6, the focused laser beam can solicit a component in whole. In contrast, the laser beam 33 may also be collimated, as shown in Figures 2 and 5, to adjust the size of the thermally biased area of interest. Moreover, the device can implement several laser beams 33 to increase the stress. For example, two laser beams 33 may be arranged on either side of the electronic component 10 to bias an elementary structure independently of the position of the coupling member 25. A first laser source is then arranged to bias the component 10 by the front face 17 and a second laser source is arranged to bias the component 10 by the rear face 18. The two laser sources must emit beams of different wavelengths determined according to the layers 13-15 of materials that the laser beams must cross to solicit the same area of interest 20.
  • the laser source 32 When the laser source 32 emits, it very locally heats the material. Due to the small heated surface, very rapidly, when the laser source 32 no longer emits, the zone of interest 20 returns to ambient temperature or to the operating temperature.
  • the laser beam 33 can thus be used to simulate aging of the electronic component 10 by alternating laser excitation phases and non-excitation phases.
  • the laser source 32 may also emit a pulsed or non-pulsed laser beam 33.
  • the wavelength ⁇ of the laser source 32 is determined according to three criteria:
  • the energy of the photons must be less than the forbidden band energy of the chip 12 to prevent photoelectric interactions in the materials.
  • the wavelength ⁇ should be greater than 1, 1 ⁇ if the beam is to cross this area before reaching the area of interest.
  • Figure 7 illustrates the absorption rate ⁇ (in cm-1) in a layer of boron-doped silicon material (the dopings are given in 1 e18 / cm3) as a function of different photon energies ⁇ and for different amounts of doping.
  • the energy ⁇ of the photons is directly connected to the wavelength ⁇ by the Planck constant and the celerity of the light.
  • the photon energy ⁇ has a decay phase followed by a growth phase.
  • the absorption rate ⁇ changes between 30 and 10 then between 10 and 300 whereas for a doping of 120e18 / cm3, the absorption rate ⁇ changes between 1800 and 800 then between 800 and 2000.
  • the minimum energy ⁇ differs depending on the amount of doping, this minimum is substantially located to 1 .12 electronvolts (eV) at 300 K.
  • a length a wavelength ⁇ close to a value greater than 1 .1 ⁇ corresponding to an energy ⁇ of 1 .12 eV is preferably used, the silicon being transparent for these wavelengths with respect to the linear absorption mechanisms.
  • This analysis differs according to the material of the layer or layers to be crossed.
  • FIG. 8 illustrates the absorption rate T of the laser for different materials as a function of the wavelength ⁇ of the laser source 30.
  • the materials represented are aluminum (Al), silver (Ag ), copper (Cu), gold (Au), molybdenum (Mo) and iron (Fe). Except for aluminum, for all the other materials presented, the absorption rate ⁇ decreases the longer the wavelength ⁇ increases. As regards aluminum, the absorption rate ⁇ decreases to a wavelength ⁇ of 0.5 ⁇ and then has a resonance peak.
  • a wavelength ⁇ between 800 nm and 1 .5 ⁇ can be advantageously used.
  • the choice is preferably made on a wavelength ⁇ of 1 .3 ⁇ or 1 .5 ⁇ .
  • FIG. 9 represents the evolution of the temperature (in Kelvin) in the thickness (in ⁇ ) of a chip 12, comprising an aluminum layer 13, a silicon layer 14 and a copper layer 15, solicited at the of the aluminum layer 13.
  • the temperature at the aluminum layer 13 is about 400 K and then it decreases rapidly in the thickness of the silicon layer 14 between 390 K and 345 K.
  • the temperature decreases still in the thickness of the copper layer 15 between 310 K and 260 K.
  • the laser beam 33 thus effectively heats the aluminum layer 13 while the coupling member 25 allows a rapid dissipation of heat to reduce the thermal stress of the other layers 14-15.
  • the invention makes it possible to solicit an electronic component 10 in a localized manner and on large temperature variations.
  • the invention can be applicable to any type of electronic components (digital, linear, power) and technologies (modulo an adjustment of the wavelength ⁇ of the laser).
  • the invention can also be used on any physical system (solid, liquid) requiring localized stressing.

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  • Engineering & Computer Science (AREA)
  • Environmental & Geological Engineering (AREA)
  • Computer Hardware Design (AREA)
  • Microelectronics & Electronic Packaging (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Health & Medical Sciences (AREA)
  • Toxicology (AREA)
  • Cooling Or The Like Of Semiconductors Or Solid State Devices (AREA)
EP14712244.4A 2013-04-09 2014-03-17 Verfahren zur untersuchung der temperaturzuverlässigkeit eines elektronischen bauelements Withdrawn EP2984494A1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1353184A FR3004262B1 (fr) 2013-04-09 2013-04-09 Procede d'etude de la fiabilite en temperature d'un composant electronique
PCT/EP2014/055257 WO2014166701A1 (fr) 2013-04-09 2014-03-17 Procede d'etude de la fiabilite en temperature d'un composant electronique

Publications (1)

Publication Number Publication Date
EP2984494A1 true EP2984494A1 (de) 2016-02-17

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EP14712244.4A Withdrawn EP2984494A1 (de) 2013-04-09 2014-03-17 Verfahren zur untersuchung der temperaturzuverlässigkeit eines elektronischen bauelements

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EP (1) EP2984494A1 (de)
FR (1) FR3004262B1 (de)
WO (1) WO2014166701A1 (de)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114152863B (zh) * 2021-11-27 2023-12-08 北京工业大学 一种智能可控温的GaN功率循环实验装置

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6078183A (en) * 1998-03-03 2000-06-20 Sandia Corporation Thermally-induced voltage alteration for integrated circuit analysis

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6483326B1 (en) * 1999-08-10 2002-11-19 Advanced Micro Devices, Inc. Localized heating for defect isolation during die operation
FR2959018B1 (fr) * 2010-04-20 2012-08-31 European Aeronautic Defence & Space Co Eads France Procedes et dispositifs de mise sous contrainte d'un circuit integre

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6078183A (en) * 1998-03-03 2000-06-20 Sandia Corporation Thermally-induced voltage alteration for integrated circuit analysis

Non-Patent Citations (3)

* Cited by examiner, † Cited by third party
Title
GLOWACKI A M ET AL: "Systematic Characterization of Integrated Circuit Standard Components as Stimulated by Scanning Laser Beam", IEEE TRANSACTIONS ON DEVICE AND MATERIALS RELIABILITY, IEEE SERVICE CENTER, PISCATAWAY, NJ, US, vol. 7, no. 1, 1 March 2007 (2007-03-01), pages 31 - 49, XP011187285, ISSN: 1530-4388, DOI: 10.1109/TDMR.2007.900056 *
LELLOUCHI D ET AL: "MEMS failure analysis case studies using the IR-OBIRCH method - Short circuit localization in a MEMS pressure sensor", PHYSICAL AND FAILURE ANALYSIS OF INTEGRATED CIRCUITS, 2009. IPFA 2009. 16TH IEEE INTERNATIONAL SYMPOSIUM ON THE, IEEE, PISCATAWAY, NJ, USA, 6 July 2009 (2009-07-06), pages 827 - 831, XP031526469, ISBN: 978-1-4244-3911-9 *
See also references of WO2014166701A1 *

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Publication number Publication date
FR3004262B1 (fr) 2015-05-15
WO2014166701A1 (fr) 2014-10-16
FR3004262A1 (fr) 2014-10-10

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