CA1123920A - Laser soldering apparatus - Google Patents
Laser soldering apparatusInfo
- Publication number
- CA1123920A CA1123920A CA331,825A CA331825A CA1123920A CA 1123920 A CA1123920 A CA 1123920A CA 331825 A CA331825 A CA 331825A CA 1123920 A CA1123920 A CA 1123920A
- Authority
- CA
- Canada
- Prior art keywords
- solder
- chip
- component
- soldering
- energy
- 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.)
- Expired
Links
Classifications
-
- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05K—PRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
- H05K3/00—Apparatus or processes for manufacturing printed circuits
- H05K3/30—Assembling printed circuits with electric components, e.g. with resistor
- H05K3/32—Assembling printed circuits with electric components, e.g. with resistor electrically connecting electric components or wires to printed circuits
- H05K3/34—Assembling printed circuits with electric components, e.g. with resistor electrically connecting electric components or wires to printed circuits by soldering
- H05K3/341—Surface mounted components
- H05K3/3431—Leadless components
- H05K3/3442—Leadless components having edge contacts, e.g. leadless chip capacitors, chip carriers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K1/00—Soldering, e.g. brazing, or unsoldering
- B23K1/005—Soldering by means of radiant energy
- B23K1/0056—Soldering by means of radiant energy soldering by means of beams, e.g. lasers, E.B.
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K26/00—Working by laser beam, e.g. welding, cutting or boring
- B23K26/02—Positioning or observing the workpiece, e.g. with respect to the point of impact; Aligning, aiming or focusing the laser beam
- B23K26/06—Shaping the laser beam, e.g. by masks or multi-focusing
- B23K26/0604—Shaping the laser beam, e.g. by masks or multi-focusing by a combination of beams
- B23K26/0619—Shaping the laser beam, e.g. by masks or multi-focusing by a combination of beams with spots located on opposed surfaces of the workpiece
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K26/00—Working by laser beam, e.g. welding, cutting or boring
- B23K26/02—Positioning or observing the workpiece, e.g. with respect to the point of impact; Aligning, aiming or focusing the laser beam
- B23K26/06—Shaping the laser beam, e.g. by masks or multi-focusing
- B23K26/064—Shaping the laser beam, e.g. by masks or multi-focusing by means of optical elements, e.g. lenses, mirrors or prisms
- B23K26/0652—Shaping the laser beam, e.g. by masks or multi-focusing by means of optical elements, e.g. lenses, mirrors or prisms comprising prisms
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K26/00—Working by laser beam, e.g. welding, cutting or boring
- B23K26/02—Positioning or observing the workpiece, e.g. with respect to the point of impact; Aligning, aiming or focusing the laser beam
- B23K26/06—Shaping the laser beam, e.g. by masks or multi-focusing
- B23K26/067—Dividing the beam into multiple beams, e.g. multifocusing
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K2101/00—Articles made by soldering, welding or cutting
- B23K2101/36—Electric or electronic devices
- B23K2101/42—Printed circuits
-
- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05K—PRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
- H05K2201/00—Indexing scheme relating to printed circuits covered by H05K1/00
- H05K2201/10—Details of components or other objects attached to or integrated in a printed circuit board
- H05K2201/10613—Details of electrical connections of non-printed components, e.g. special leads
- H05K2201/10621—Components characterised by their electrical contacts
- H05K2201/10636—Leadless chip, e.g. chip capacitor or resistor
-
- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05K—PRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
- H05K2203/00—Indexing scheme relating to apparatus or processes for manufacturing printed circuits covered by H05K3/00
- H05K2203/10—Using electric, magnetic and electromagnetic fields; Using laser light
- H05K2203/107—Using laser light
-
- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05K—PRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
- H05K3/00—Apparatus or processes for manufacturing printed circuits
- H05K3/30—Assembling printed circuits with electric components, e.g. with resistor
- H05K3/32—Assembling printed circuits with electric components, e.g. with resistor electrically connecting electric components or wires to printed circuits
- H05K3/34—Assembling printed circuits with electric components, e.g. with resistor electrically connecting electric components or wires to printed circuits by soldering
- H05K3/3494—Heating methods for reflowing of solder
-
- Y—GENERAL 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
- Y02P70/00—Climate change mitigation technologies in the production process for final industrial or consumer products
- Y02P70/50—Manufacturing or production processes characterised by the final manufactured product
Landscapes
- Physics & Mathematics (AREA)
- Optics & Photonics (AREA)
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Plasma & Fusion (AREA)
- Manufacturing & Machinery (AREA)
- Microelectronics & Electronic Packaging (AREA)
- Electric Connection Of Electric Components To Printed Circuits (AREA)
- Laser Beam Processing (AREA)
- Fixed Capacitors And Capacitor Manufacturing Machines (AREA)
Abstract
LASER SOLDERING APPARATUS
Abstract of the Disclosure A laser soldering apparatus and method for soldering chip components to circuit modules. Optical means are provided to simultaneously focus coherent laser beams toward solder at opposing ends of a chip component. The energy thus provided reflows the solder and two joints are simultaneously formed when the solder cools.
Abstract of the Disclosure A laser soldering apparatus and method for soldering chip components to circuit modules. Optical means are provided to simultaneously focus coherent laser beams toward solder at opposing ends of a chip component. The energy thus provided reflows the solder and two joints are simultaneously formed when the solder cools.
Description
~ 3 ~ 2 ~
Background o the Invention Ceramic chip capacitors are widely used in hybrid and printed circuit modules because theyoffer ruggedness, volumetric efficiency J wide available range and attractive cost. Generally, the chips are fabricated by interleaving rectangular electrode plates and dielectric layers, alter-nately attaching the plates to two termination bands on the opposing ends of the chip. A substantial percentage of cermic chip capacitors are fabricated using barium titanate ceramic as the dielectric material with a typical thickness of 1 mil. Palladium silver is frequently used or the plates and thicknesses in the order of 0.1 mil are typical. It is common practice to use solder joints to connect the termination bands to the circuit of the module.
The primary means of soldering chip capacitors and chip components in general, is with a hand soldering iron which can damage not only the component but also the module. For example, if heat is permitted to conduct into the component, internal pressure may develop from trapped gas molecules within the component that are not able to escape as rapidly as they expand.
Also, if the adjoining layers of the component have a mismatch in coeficients of thermal expansion, shear stresses develop within the component. Further~ even if the component materials are selected to have similar coe~ficients o thermal expansion, they likely will exhibit different thermal conductivities such that a temperature gradient will exist between the layers and cause shear stresses of expansion. Also, stress can be created in the solder joints substantially caused by two conditions.
First, during the heating process, the chip is free to expand but the module area is hindered from expansion by the mechanical ~ ~ ~ 3 ~ Z ~
restraint provided by the cooler surrounding material of the module; compr0ssive stress occurs in the local area of the module but no expansion. Then, upon cooling to room temperature, the chîp and solder joints are in a state of tensile stress as the chip is partially restrained from decreasing to its original length by the solidified solder. SecondJ if the joints are soldered one at a time, substantial stresses occur in the joints and the chip caused by even minimal contact with the chip during the formation of the second solder joint.
The internal component stresses heretofore described can cause component failures and thereby substantially reduce the reliability of a module. Examples of structural defects caused by stress are delaminations, material crumpling, voids, and cracks. The effects may, for example, be short and open circuits or changes in capacitive properties. Also, stress on the soldering joints m~y result in a poor connection. The prior art includes various techniques for soldering chip capacitors, the most common of which is the use of hand soldering iron.
Other methods utilize flame, hot air, or focused radlant energy.
However, a need still exists for a means and method for soldering chip capacitors to modules so as to minimize the internal component stresses and the stress on the solder joints.
3~
Summary of the Invention Electromagnetic radiation having a wavelength in the range from one millimeter to one nanometer is separated into a plurality of beams which are directed at spaced impingement areas on a support means for supporting materials to be bonded.
More specifically, the radiation preferably comprises pulsed coherent laser energy having pulse wid-ths less than 10 milli-seconds, a pulse repetition rate less than 10 pulses per second, and a pulse train duration of less than 1 second. It is also preferahle that these pulse parameters be selectable so as to be optimized for various applications.
The apparatus so described may be used for soldering.
More specifically, it is preferable to use the apparatus for the soldering of chip components onto circuit modules. In this application, it is preferable that the radiation have a wave-length of 1.06 micrometers and pulse widths of 4 to 6 milli-seconds. It may also be preferable to support the module on a X-Y table which may be controlled by a microprocessor and which is used to precisely position the module while soldering chip components to it.
In accordance with the present invention, there is provided a method of soldering an electronic chip component having solder on opposing encls to two supporting conductor pads connected to a substrate, comprising the steps oE: providing pulsed coherent laser radiation having pulse widths of less than 10 milliseconds with a repetition rate of less than 10 pulses per second, the pulse train duration of said radiation being less than one second; separating said radiation inko two simul-taneous spatially separate heams having substantially equal energy; directing said beams inward toward said opposing ends of said electronic chip component to reflow said solder; and .. ~J
-~ ~Z3~2C~
removing said beams to substantially simultaneously form solder joints bet~een said component and said pads.
- 3a -~39;~
Description of the Drawings The invention will be described in more detail by refe~ence to the drawings in which: .
FIG. 1 is a mechanical ~chema~ic diagram depicting the operation of the apparatus ~mbodying the invention, FIG. 2 is a pictoral view of the outward appearance of a laser soldering apparatus;
FIG, 3 is an elevation view with partial section showing a chip capacitor soldered to a module circuit;
FIGS. 4A and 4B are diagrams demonstrating the relation-ship of the creep ang~le for two different solder thicknesses tl and t2, for a given creep distance ~; and FIG. 5 shows a graph of chip tensile stress plotted as a function of temperature for two different solder thicknesses.
~ 3~ Z ~
Descri~tion of the Preferred Embodiment Referring to Figure 1, an illustration is shown which demonstrates the operation of the apparatus embodying the invention. Two laser beams 2 and 4 are formed by directing a coherent beam 6 of laser radiation at a double slotted aperture disc 8. Preferably, the disc may be selected from a plurality of discs so that the length and width of the slots can be varied for different applications. Any con-ventlonal pulse laser such as, for example, laser model SS-380 supplied by Raytheon Company may be used as the source of laser radiation. Preferably, laser radiation with a wavelength of approximately 1.06 micrometers is used for reasons herein-after described. Also, the preferable pulse widths, pulse repetition rate, and total energy requirements will be described later. The total energy of the two formed beams is monitored by directing the beams through a beam splitting mirror 10, well known in the art, that reflects 1~ o the incident energy to a conventional energy monitor 12 as shown in Figure 1. The remaining 99~ of the incident energy of two beams is transmitted through the beam splitting mirror to reflecting prism 14, the f~mction of which is to provide a spacing between the two beams which is sufficien~ly large so that the beams may be simultaneously directed at two opposing ends of a component 16 as shown in Figure 1. Next, each beam passes through a conventional cylinder lens 18 and 20 to ocus the energy to a size and shape, the preerential specifications o~ which will hereinater be described. Each focused beam then impinges on a beam power splitting mirror 22 and 24 which has a characteristic property at the frequency of the energy of reflecting 99~ of the beam toward ~he soldering plane 32 ~2392~
where solder is to be reflowed. The mirrors 22 and 24 transmit the remaining 1% of the energy through to energy monitors 26 and 28. The position of mirror 24 may be adjusted as illus-trated in Figure 1 so that the beams may be directed to be incident on the soldering plane at different distances apart to facilitate the simultaneous soldering of both ends of dif-ferent sized components. Additional adjustment is urther attained through step changes in -the position of mirror 22 in a like manner to the adjustment of mirror 24. Also, as shown in Figure 1, 100~ reflecting mirrors 34 and 36 direct the images of visible light 38 and 40 from the soldering plane to te~evision cameras 4? and 44 for aligning the position of a component 16 relative to the sight lines where the two laser beams are directed when activated. Visible light may be trans-mitted to the soldering area by the use of fiber optics ~not shown). The hardware heretofore ~.escribed is well-known to one skilled in the art.
In operation, referring to Figure 2, a protective shroud 46 is opened by the operator to expose a conventional X-Y
table (not shown). Typically, a printed circuit module 70, as shown in Figure 3, is rigidly affixed to the X-Y table by any means and a chip component 16 is placed across the conductor pads 74 which are part of the printed circuit module and to which the chip component is to be soldered. After the pro-tective shroud is closed, the X-Y table control panel 48 which has both coarse and fine adjustments for both axes is used to position the module so that when the laser 50 is activated, the two beams as described with reference to Pigure 1 will simultaneously impinge at the bases of the opposing ends of the chip component. The proper positioning of the X-Y table ~ ~ ~ 3~ ~ ~
may be accomplished with the television monitors 52 and 54 connected to the television cameras in Figure 1 and which have transparent overlays 56 and 57 to indicate the area and location of laser radiation when activated. After the laser firing parameters, l~hich are discussed hereinafter, are selected using the laser control panel 58, the laser lS acti-vated. The laser radiation energy absorbed by the solder on the pad and the solder on the chip component is converted to thermal energy which reflo~s the solder. When the energy is removed and the solder cools, a solder joint is formed at each end of the chip component connecting it to the circuit of the module. The energy ln joules at the total energy monitor and the individual beam monitors is displayed on the laser control panel.
In an alternate embodiment, a microprocessor ~not shown) is used to control the position of the X-Y table and the exci-tation of the laser such that a plurality of chip components can be sequentially soldered to a single module without operator intervention. Whether in automatic or manual mode, the X and Y
coordinates of the X-Y table are displayed on digital readouts 59 on the X-Y control panel.
The soldering apparatus heretofore described provides for a soldering technique that has substantial improvements over the prior art. The improvements substantially result from the simultaneous reflow of solder at both ends of the chip and the operator o the apparatus havin~ very precise control over the soldering parameters.
With re~erence to the background and Figure 3, chip capa-citors are fabricated by interleaving rectangular electrode plates 60 and dielectric layers 62 alternately attaching the ~ ~ ~ 3 ~ 2 ~
pla~es to two termination bands 64 at opposing ends of the chip.
For example, the elec~rode plates may be fabrica~ed of palladium silver while the dielectric is a ceramic material. A chip may be dipped into solder 66 during fabrication. It has been found that when two strips of materials having different coeficients o thermal expansion are bonded along an interface and heated isothermally, the composite will bow concave to the material having the lower coefficient of expansion. ~ neutral region is established within each material which comprises a locus o unstressed points which define a boundary between compressive a~d tensile stresses; the maximum compressive and tensile stresses generally exist on the surfaces of the materials. In the case of a chip capaci~or where the bending moments are counterpoised by successi~e layers of ceramic and electrode plates such that the interfaces are maintained planar, the stresses are at a minimum~at the center of each layer and maximum at the boundaries. Also, in the case of a chip capa-citor, even though the adjacent layer may have a similar coefficient of thermal expansion, the materials typicalIy have different thermal diffusivities such that stresses result from d~fferent expansions caused by different temperatures rather than different coefficients of expansion. Thermal diffusivity of a material is defined as its thermal conduc-tivity divided by the product of its specific heat and density.
Accordingly, to prevent damage to a ch:ip capacitor or a chip component, it is, in general, important to minimize the heat permitted to transfer into the chip during the soldering process.
The laser solder apparatus h~retofore described provides very precise control over the amount and profile of energy transerred to the solder and thereby provides a means of ~L~23~3~
minimizing the heat transferred to the chip. Por example, the basic equation for the energy required to melt a substanee is given by the equation E~ /V = ~C~T + Hs) where EM is the required melting energy in joules, V is the volume to be melted in cubic centimeters, ~ is the material density in grams per cubic centimeter, C is the material specific heat in calories per gram per degree centigrade, ~T is the melting tempera~ure minus the initial material temperature in degrees centigrade, and Hs is the heat of fusion in calories per gram. Generally, solder should be approximately 30 to 50 above its mel~ing point to achieve good wetting. Therefore, the total energy required to reflow is approximately given by the equation Er/V ~(C~Tl + Hs) ~ 6(C~T2) where ~T2 is the desired reflow temperature minus the melting temperature Assuming an "A" size (.035 x .055 x .65 inches} chip capacitor including an end termination of 0.2 mils of silver and 1.5 mils of copper followed by a 1.5 mil 63 Sn/37 Pb solder dip, and all three materials reachlng the temperature of 215C or 32C above the 63/37 solder eutectic temperature, - a total energy of .434 joules is required to re~low each solder joint. Further~ assuming a reflection factor at the solder of 50% and a 90% optics transmission factor, approximately 0.964 joules would preferably be delivered in each beam for the specified conditions. Similarly~ for example, 3.7 joules would preferably be d~livered in each beam to solder an "F" size ~.235 x .075 x .210 inches) chip capacitor. A series of tests ~ ~ 2 ~
were made with the apparatus and energy monitor data was taken for ~arious combinations of double slotted discs and laser parameters. The precise amount of energy as theoretically calculated above with any deviations arising from practical considerations can be delivered by the apparatus with a high degree of repeatability and consistency.
The laser model SS-380 is a Neodymium Yttrium Aluminum Garnet (Nd-YAG) type that operates at a wavelength of ~.06 micrometers. The pulse width is variable from two to ten milliseconds with the pulse repetition rate selectable to 6, 4, Z and 1 pulse per second and manual single shot~ There is a maximum power of 40 watts. In the preferred embodiment, the SS-380 laser system was modified to provide even greater flexibili~y. Pulse widths to 30 milliseconds in 0.1 milli second increments are a~ailable. l~lso, 30 joules per pulse protected at 50 watts may be delivered. Further, a burst mode is provided which operates above 10 pulses per second.
The use of 1.06 micrometer wavelength minimizes light reflection from solder as compared to a 10.6 micrometer Carbon Dioxide laser. I~ith the increased energy absorption by the solder, a smaller percentage re-flects ~oward the chip to result in increased stress within the chip. Also, because the energy is coherent, ~he cylindrlcal lens can be desi~ned to precisely focus substantially all the energy so that the incidence of energy directly onto the chip is substantially eliminated.
Furthermore, the preferred laser energy profile comprises a train of pulses with relatively narrow pulse widths. l~or example, to solder an "~" size chip capacitor, it has been determined to be preferable to deliver six pulses at a pulse repe~ition ~ ~ ~ 3 ~ 2 ~
rate of six pulses per second, each pulse having a pulse width of four to six milliseconds. The double slotted aperture disc used is one which provides a beam having a depth dimension approximately equal to the depth (.0~5 inches) dimension as viewed on Figure 3. Also, the laser amplitude is set at 20%
of maximum. It is preferable not to vary the amplitude when changing from one component size to another; rather, the double slotted aperture is changed and the pulse repetition rate, pulse width, and duration are varied to optimize for the particular application.
The narrow pulse ~rain energy profile described in the previous paragraph provides significant protection against component damage during and immediately af~er the soldering process. First, the emissivity of liquid solder is substantially greater than in the solid state. Accordingly, a relatively large percentage of heat added to the solder af~er it becomes liquid is conducted to the component. It follows that if the energy that is added to the solder is precisely controlled in small increments so that the solder passes into the liquid state for only a very brief period of time such as milliseconds, the amount of heat conducted to the component is minimized.
Second, for any given point within a chip capacitor, the stress is maximized when the diference in temperature between the electrodes and dielectric layers is also maximum. Further, studies have shownthat a maximum diference occurs at approximately three time constants where one time constant is defined as the time for a point to rise to 63% of its total temperature rise caused by the addition of heat to the material. This is Iogical because if the temperature is raised very gradually over a relatively long period of time, ~he different diffusivities ~23~32~3 of the layers have very little e~fect and the dierence in temperature between the two layers is very small. Provided their coefficients of thermal expansion are well matched~ the stress t Up to a limit, will become smaller as the number of time constants is increased. Also, if ~Lhe number of time constants is reduced from three time constants, the material has insuicient time to react. In most industrial applications the production rate is important such that it is not easible to expend considerable time to raise the ~emperature o components slowly. Therefore, in order ~o minimize stress, it is important to trans~er heat to the solder very rapidly.
The four to six millisecond pulses provide an introduction of heat into the sol~er in a time subs~antially less than one time constant.
The simultaneous soldering of both ends of a chip capacitor by the use of two beams of laser radiation provides substantial improvements in stress relief over prior art methods. More specifically, after coollng down there is less stress in the solder joints and accordingly less stress applied to the chip. The simultaneous re1Ow at both ends of the component without external contact permits the component to float on the liquid solder. This provides a sufficient thickness of solder between the component and the printed circuit board.
More speciically, it is preferable that not less than .0025 inches of solder solidiy under the chip to limit stress in the chip and plastic atigue in the 5O1der.
Reerring to Figures 4A and 4B, it is illustrated that given ~, the creep distance at each end of the component required to compensate or the component expansion during soldering being greater than the printed circuit module, the ~ 3 ~ 2 ~
creep angle ~ gets smaller as the thickness of the solder is increased. More specifically, 32 is smaller than 01 because t2 is greater than tl. Figure 5 plots emperical data that demonstrates that the tensile stress applied to the component after cooling down is reduced when the thickness is increased from .003 inches to .OlO inches. Also, the simultaneous reflow substantially eliminates the vertical stress applied to the chip when soldering one end after the other end has already been soldered.
Although the in~ention has been described with a preferred embodiment, it will be appreciated to those skilled in the art that various modifications can be made without departing from its scope. For example, although the discussion is primarily directed at chip components and chip capacitor in particular, the general soldering technique would be applicable to a variety of applications. It is therefore intendad that the invention not be limited except as defined by the claims.
Background o the Invention Ceramic chip capacitors are widely used in hybrid and printed circuit modules because theyoffer ruggedness, volumetric efficiency J wide available range and attractive cost. Generally, the chips are fabricated by interleaving rectangular electrode plates and dielectric layers, alter-nately attaching the plates to two termination bands on the opposing ends of the chip. A substantial percentage of cermic chip capacitors are fabricated using barium titanate ceramic as the dielectric material with a typical thickness of 1 mil. Palladium silver is frequently used or the plates and thicknesses in the order of 0.1 mil are typical. It is common practice to use solder joints to connect the termination bands to the circuit of the module.
The primary means of soldering chip capacitors and chip components in general, is with a hand soldering iron which can damage not only the component but also the module. For example, if heat is permitted to conduct into the component, internal pressure may develop from trapped gas molecules within the component that are not able to escape as rapidly as they expand.
Also, if the adjoining layers of the component have a mismatch in coeficients of thermal expansion, shear stresses develop within the component. Further~ even if the component materials are selected to have similar coe~ficients o thermal expansion, they likely will exhibit different thermal conductivities such that a temperature gradient will exist between the layers and cause shear stresses of expansion. Also, stress can be created in the solder joints substantially caused by two conditions.
First, during the heating process, the chip is free to expand but the module area is hindered from expansion by the mechanical ~ ~ ~ 3 ~ Z ~
restraint provided by the cooler surrounding material of the module; compr0ssive stress occurs in the local area of the module but no expansion. Then, upon cooling to room temperature, the chîp and solder joints are in a state of tensile stress as the chip is partially restrained from decreasing to its original length by the solidified solder. SecondJ if the joints are soldered one at a time, substantial stresses occur in the joints and the chip caused by even minimal contact with the chip during the formation of the second solder joint.
The internal component stresses heretofore described can cause component failures and thereby substantially reduce the reliability of a module. Examples of structural defects caused by stress are delaminations, material crumpling, voids, and cracks. The effects may, for example, be short and open circuits or changes in capacitive properties. Also, stress on the soldering joints m~y result in a poor connection. The prior art includes various techniques for soldering chip capacitors, the most common of which is the use of hand soldering iron.
Other methods utilize flame, hot air, or focused radlant energy.
However, a need still exists for a means and method for soldering chip capacitors to modules so as to minimize the internal component stresses and the stress on the solder joints.
3~
Summary of the Invention Electromagnetic radiation having a wavelength in the range from one millimeter to one nanometer is separated into a plurality of beams which are directed at spaced impingement areas on a support means for supporting materials to be bonded.
More specifically, the radiation preferably comprises pulsed coherent laser energy having pulse wid-ths less than 10 milli-seconds, a pulse repetition rate less than 10 pulses per second, and a pulse train duration of less than 1 second. It is also preferahle that these pulse parameters be selectable so as to be optimized for various applications.
The apparatus so described may be used for soldering.
More specifically, it is preferable to use the apparatus for the soldering of chip components onto circuit modules. In this application, it is preferable that the radiation have a wave-length of 1.06 micrometers and pulse widths of 4 to 6 milli-seconds. It may also be preferable to support the module on a X-Y table which may be controlled by a microprocessor and which is used to precisely position the module while soldering chip components to it.
In accordance with the present invention, there is provided a method of soldering an electronic chip component having solder on opposing encls to two supporting conductor pads connected to a substrate, comprising the steps oE: providing pulsed coherent laser radiation having pulse widths of less than 10 milliseconds with a repetition rate of less than 10 pulses per second, the pulse train duration of said radiation being less than one second; separating said radiation inko two simul-taneous spatially separate heams having substantially equal energy; directing said beams inward toward said opposing ends of said electronic chip component to reflow said solder; and .. ~J
-~ ~Z3~2C~
removing said beams to substantially simultaneously form solder joints bet~een said component and said pads.
- 3a -~39;~
Description of the Drawings The invention will be described in more detail by refe~ence to the drawings in which: .
FIG. 1 is a mechanical ~chema~ic diagram depicting the operation of the apparatus ~mbodying the invention, FIG. 2 is a pictoral view of the outward appearance of a laser soldering apparatus;
FIG, 3 is an elevation view with partial section showing a chip capacitor soldered to a module circuit;
FIGS. 4A and 4B are diagrams demonstrating the relation-ship of the creep ang~le for two different solder thicknesses tl and t2, for a given creep distance ~; and FIG. 5 shows a graph of chip tensile stress plotted as a function of temperature for two different solder thicknesses.
~ 3~ Z ~
Descri~tion of the Preferred Embodiment Referring to Figure 1, an illustration is shown which demonstrates the operation of the apparatus embodying the invention. Two laser beams 2 and 4 are formed by directing a coherent beam 6 of laser radiation at a double slotted aperture disc 8. Preferably, the disc may be selected from a plurality of discs so that the length and width of the slots can be varied for different applications. Any con-ventlonal pulse laser such as, for example, laser model SS-380 supplied by Raytheon Company may be used as the source of laser radiation. Preferably, laser radiation with a wavelength of approximately 1.06 micrometers is used for reasons herein-after described. Also, the preferable pulse widths, pulse repetition rate, and total energy requirements will be described later. The total energy of the two formed beams is monitored by directing the beams through a beam splitting mirror 10, well known in the art, that reflects 1~ o the incident energy to a conventional energy monitor 12 as shown in Figure 1. The remaining 99~ of the incident energy of two beams is transmitted through the beam splitting mirror to reflecting prism 14, the f~mction of which is to provide a spacing between the two beams which is sufficien~ly large so that the beams may be simultaneously directed at two opposing ends of a component 16 as shown in Figure 1. Next, each beam passes through a conventional cylinder lens 18 and 20 to ocus the energy to a size and shape, the preerential specifications o~ which will hereinater be described. Each focused beam then impinges on a beam power splitting mirror 22 and 24 which has a characteristic property at the frequency of the energy of reflecting 99~ of the beam toward ~he soldering plane 32 ~2392~
where solder is to be reflowed. The mirrors 22 and 24 transmit the remaining 1% of the energy through to energy monitors 26 and 28. The position of mirror 24 may be adjusted as illus-trated in Figure 1 so that the beams may be directed to be incident on the soldering plane at different distances apart to facilitate the simultaneous soldering of both ends of dif-ferent sized components. Additional adjustment is urther attained through step changes in -the position of mirror 22 in a like manner to the adjustment of mirror 24. Also, as shown in Figure 1, 100~ reflecting mirrors 34 and 36 direct the images of visible light 38 and 40 from the soldering plane to te~evision cameras 4? and 44 for aligning the position of a component 16 relative to the sight lines where the two laser beams are directed when activated. Visible light may be trans-mitted to the soldering area by the use of fiber optics ~not shown). The hardware heretofore ~.escribed is well-known to one skilled in the art.
In operation, referring to Figure 2, a protective shroud 46 is opened by the operator to expose a conventional X-Y
table (not shown). Typically, a printed circuit module 70, as shown in Figure 3, is rigidly affixed to the X-Y table by any means and a chip component 16 is placed across the conductor pads 74 which are part of the printed circuit module and to which the chip component is to be soldered. After the pro-tective shroud is closed, the X-Y table control panel 48 which has both coarse and fine adjustments for both axes is used to position the module so that when the laser 50 is activated, the two beams as described with reference to Pigure 1 will simultaneously impinge at the bases of the opposing ends of the chip component. The proper positioning of the X-Y table ~ ~ ~ 3~ ~ ~
may be accomplished with the television monitors 52 and 54 connected to the television cameras in Figure 1 and which have transparent overlays 56 and 57 to indicate the area and location of laser radiation when activated. After the laser firing parameters, l~hich are discussed hereinafter, are selected using the laser control panel 58, the laser lS acti-vated. The laser radiation energy absorbed by the solder on the pad and the solder on the chip component is converted to thermal energy which reflo~s the solder. When the energy is removed and the solder cools, a solder joint is formed at each end of the chip component connecting it to the circuit of the module. The energy ln joules at the total energy monitor and the individual beam monitors is displayed on the laser control panel.
In an alternate embodiment, a microprocessor ~not shown) is used to control the position of the X-Y table and the exci-tation of the laser such that a plurality of chip components can be sequentially soldered to a single module without operator intervention. Whether in automatic or manual mode, the X and Y
coordinates of the X-Y table are displayed on digital readouts 59 on the X-Y control panel.
The soldering apparatus heretofore described provides for a soldering technique that has substantial improvements over the prior art. The improvements substantially result from the simultaneous reflow of solder at both ends of the chip and the operator o the apparatus havin~ very precise control over the soldering parameters.
With re~erence to the background and Figure 3, chip capa-citors are fabricated by interleaving rectangular electrode plates 60 and dielectric layers 62 alternately attaching the ~ ~ ~ 3 ~ 2 ~
pla~es to two termination bands 64 at opposing ends of the chip.
For example, the elec~rode plates may be fabrica~ed of palladium silver while the dielectric is a ceramic material. A chip may be dipped into solder 66 during fabrication. It has been found that when two strips of materials having different coeficients o thermal expansion are bonded along an interface and heated isothermally, the composite will bow concave to the material having the lower coefficient of expansion. ~ neutral region is established within each material which comprises a locus o unstressed points which define a boundary between compressive a~d tensile stresses; the maximum compressive and tensile stresses generally exist on the surfaces of the materials. In the case of a chip capaci~or where the bending moments are counterpoised by successi~e layers of ceramic and electrode plates such that the interfaces are maintained planar, the stresses are at a minimum~at the center of each layer and maximum at the boundaries. Also, in the case of a chip capa-citor, even though the adjacent layer may have a similar coefficient of thermal expansion, the materials typicalIy have different thermal diffusivities such that stresses result from d~fferent expansions caused by different temperatures rather than different coefficients of expansion. Thermal diffusivity of a material is defined as its thermal conduc-tivity divided by the product of its specific heat and density.
Accordingly, to prevent damage to a ch:ip capacitor or a chip component, it is, in general, important to minimize the heat permitted to transfer into the chip during the soldering process.
The laser solder apparatus h~retofore described provides very precise control over the amount and profile of energy transerred to the solder and thereby provides a means of ~L~23~3~
minimizing the heat transferred to the chip. Por example, the basic equation for the energy required to melt a substanee is given by the equation E~ /V = ~C~T + Hs) where EM is the required melting energy in joules, V is the volume to be melted in cubic centimeters, ~ is the material density in grams per cubic centimeter, C is the material specific heat in calories per gram per degree centigrade, ~T is the melting tempera~ure minus the initial material temperature in degrees centigrade, and Hs is the heat of fusion in calories per gram. Generally, solder should be approximately 30 to 50 above its mel~ing point to achieve good wetting. Therefore, the total energy required to reflow is approximately given by the equation Er/V ~(C~Tl + Hs) ~ 6(C~T2) where ~T2 is the desired reflow temperature minus the melting temperature Assuming an "A" size (.035 x .055 x .65 inches} chip capacitor including an end termination of 0.2 mils of silver and 1.5 mils of copper followed by a 1.5 mil 63 Sn/37 Pb solder dip, and all three materials reachlng the temperature of 215C or 32C above the 63/37 solder eutectic temperature, - a total energy of .434 joules is required to re~low each solder joint. Further~ assuming a reflection factor at the solder of 50% and a 90% optics transmission factor, approximately 0.964 joules would preferably be delivered in each beam for the specified conditions. Similarly~ for example, 3.7 joules would preferably be d~livered in each beam to solder an "F" size ~.235 x .075 x .210 inches) chip capacitor. A series of tests ~ ~ 2 ~
were made with the apparatus and energy monitor data was taken for ~arious combinations of double slotted discs and laser parameters. The precise amount of energy as theoretically calculated above with any deviations arising from practical considerations can be delivered by the apparatus with a high degree of repeatability and consistency.
The laser model SS-380 is a Neodymium Yttrium Aluminum Garnet (Nd-YAG) type that operates at a wavelength of ~.06 micrometers. The pulse width is variable from two to ten milliseconds with the pulse repetition rate selectable to 6, 4, Z and 1 pulse per second and manual single shot~ There is a maximum power of 40 watts. In the preferred embodiment, the SS-380 laser system was modified to provide even greater flexibili~y. Pulse widths to 30 milliseconds in 0.1 milli second increments are a~ailable. l~lso, 30 joules per pulse protected at 50 watts may be delivered. Further, a burst mode is provided which operates above 10 pulses per second.
The use of 1.06 micrometer wavelength minimizes light reflection from solder as compared to a 10.6 micrometer Carbon Dioxide laser. I~ith the increased energy absorption by the solder, a smaller percentage re-flects ~oward the chip to result in increased stress within the chip. Also, because the energy is coherent, ~he cylindrlcal lens can be desi~ned to precisely focus substantially all the energy so that the incidence of energy directly onto the chip is substantially eliminated.
Furthermore, the preferred laser energy profile comprises a train of pulses with relatively narrow pulse widths. l~or example, to solder an "~" size chip capacitor, it has been determined to be preferable to deliver six pulses at a pulse repe~ition ~ ~ ~ 3 ~ 2 ~
rate of six pulses per second, each pulse having a pulse width of four to six milliseconds. The double slotted aperture disc used is one which provides a beam having a depth dimension approximately equal to the depth (.0~5 inches) dimension as viewed on Figure 3. Also, the laser amplitude is set at 20%
of maximum. It is preferable not to vary the amplitude when changing from one component size to another; rather, the double slotted aperture is changed and the pulse repetition rate, pulse width, and duration are varied to optimize for the particular application.
The narrow pulse ~rain energy profile described in the previous paragraph provides significant protection against component damage during and immediately af~er the soldering process. First, the emissivity of liquid solder is substantially greater than in the solid state. Accordingly, a relatively large percentage of heat added to the solder af~er it becomes liquid is conducted to the component. It follows that if the energy that is added to the solder is precisely controlled in small increments so that the solder passes into the liquid state for only a very brief period of time such as milliseconds, the amount of heat conducted to the component is minimized.
Second, for any given point within a chip capacitor, the stress is maximized when the diference in temperature between the electrodes and dielectric layers is also maximum. Further, studies have shownthat a maximum diference occurs at approximately three time constants where one time constant is defined as the time for a point to rise to 63% of its total temperature rise caused by the addition of heat to the material. This is Iogical because if the temperature is raised very gradually over a relatively long period of time, ~he different diffusivities ~23~32~3 of the layers have very little e~fect and the dierence in temperature between the two layers is very small. Provided their coefficients of thermal expansion are well matched~ the stress t Up to a limit, will become smaller as the number of time constants is increased. Also, if ~Lhe number of time constants is reduced from three time constants, the material has insuicient time to react. In most industrial applications the production rate is important such that it is not easible to expend considerable time to raise the ~emperature o components slowly. Therefore, in order ~o minimize stress, it is important to trans~er heat to the solder very rapidly.
The four to six millisecond pulses provide an introduction of heat into the sol~er in a time subs~antially less than one time constant.
The simultaneous soldering of both ends of a chip capacitor by the use of two beams of laser radiation provides substantial improvements in stress relief over prior art methods. More specifically, after coollng down there is less stress in the solder joints and accordingly less stress applied to the chip. The simultaneous re1Ow at both ends of the component without external contact permits the component to float on the liquid solder. This provides a sufficient thickness of solder between the component and the printed circuit board.
More speciically, it is preferable that not less than .0025 inches of solder solidiy under the chip to limit stress in the chip and plastic atigue in the 5O1der.
Reerring to Figures 4A and 4B, it is illustrated that given ~, the creep distance at each end of the component required to compensate or the component expansion during soldering being greater than the printed circuit module, the ~ 3 ~ 2 ~
creep angle ~ gets smaller as the thickness of the solder is increased. More specifically, 32 is smaller than 01 because t2 is greater than tl. Figure 5 plots emperical data that demonstrates that the tensile stress applied to the component after cooling down is reduced when the thickness is increased from .003 inches to .OlO inches. Also, the simultaneous reflow substantially eliminates the vertical stress applied to the chip when soldering one end after the other end has already been soldered.
Although the in~ention has been described with a preferred embodiment, it will be appreciated to those skilled in the art that various modifications can be made without departing from its scope. For example, although the discussion is primarily directed at chip components and chip capacitor in particular, the general soldering technique would be applicable to a variety of applications. It is therefore intendad that the invention not be limited except as defined by the claims.
2~
Claims (4)
Case No. 31648
1. A method of soldering an electronic chip component having solder on opposing ends to two supporting conductor pads connected to a substrate, comprising the steps of:
providing pulsed coherent laser radiation having pulse widths of less than 10 milliseconds with a repetition rate of less than 10 pulses per second, the pulse train duration of said radiation being less than one second;
separating said radiation into two simultaneous spatially separate beams having substantially equal energy;
directing said beams inward toward said opposing ends of said electronic chip component to reflow said solder; and removing said beams to substantially simultaneously form solder joints between said component and said pads.
providing pulsed coherent laser radiation having pulse widths of less than 10 milliseconds with a repetition rate of less than 10 pulses per second, the pulse train duration of said radiation being less than one second;
separating said radiation into two simultaneous spatially separate beams having substantially equal energy;
directing said beams inward toward said opposing ends of said electronic chip component to reflow said solder; and removing said beams to substantially simultaneously form solder joints between said component and said pads.
2. The method recited in claim 1 wherein said pulse widths are in the range from 4 to 6 milliseconds.
3. The method recited in Claim 2 wherein said pulse train comprises 6 pulses.
4. The method recited in claim 1 wherein the wavelength of said radiation is 1.06 micrometers.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US93667178A | 1978-08-24 | 1978-08-24 | |
US936,671 | 1978-08-24 |
Publications (1)
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CA1123920A true CA1123920A (en) | 1982-05-18 |
Family
ID=25468940
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CA331,825A Expired CA1123920A (en) | 1978-08-24 | 1979-07-13 | Laser soldering apparatus |
Country Status (7)
Country | Link |
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JP (1) | JPS5530895A (en) |
CA (1) | CA1123920A (en) |
DE (1) | DE2934407A1 (en) |
FR (1) | FR2434002A1 (en) |
GB (1) | GB2038220B (en) |
IT (1) | IT1120489B (en) |
NL (1) | NL7906042A (en) |
Families Citing this family (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0085278A1 (en) * | 1982-01-28 | 1983-08-10 | Battelle Development Corporation | Split beam method of altering material properties |
JPH0347730Y2 (en) * | 1985-04-18 | 1991-10-11 | ||
DE3539933A1 (en) * | 1985-11-11 | 1987-05-14 | Nixdorf Computer Ag | DEVICE FOR SOLELING ELECTRONIC COMPONENTS ON A CIRCUIT BOARD |
JPH0677811B2 (en) * | 1986-01-20 | 1994-10-05 | 株式会社ハイベツク | Automatic soldering equipment |
JPH0783036B2 (en) * | 1987-12-11 | 1995-09-06 | 三菱電機株式会社 | Carrier tape |
JPH02138066U (en) * | 1989-04-17 | 1990-11-19 | ||
US5060288A (en) * | 1990-08-27 | 1991-10-22 | Sierra Research And Technology, Inc. | Infrared heater array for IC soldering |
US5309545A (en) * | 1990-08-27 | 1994-05-03 | Sierra Research And Technology, Inc. | Combined radiative and convective rework system |
DE19833368C1 (en) * | 1998-07-24 | 2000-02-17 | Schott Glas | Method and device for processing components made of brittle materials |
JP2005347415A (en) * | 2004-06-01 | 2005-12-15 | Miyachi Technos Corp | Electric part mounting method |
WO2006037370A1 (en) * | 2004-10-06 | 2006-04-13 | Hentze-Lissotschenko Patentverwaltungs Gmbh & Co. Kg | Laser array |
JP5420172B2 (en) | 2004-10-06 | 2014-02-19 | リモ パテントフェルヴァルトゥング ゲーエムベーハー ウント コー.カーゲー | Laser equipment |
CN110948079B (en) * | 2019-12-24 | 2023-10-10 | 武汉嘉铭激光股份有限公司 | Double-laser tin soldering combined device and welding method thereof |
CN114682948B (en) * | 2022-03-04 | 2023-10-31 | 广东风华高新科技股份有限公司 | Method, device and system for testing weldability of chip component |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1565832A1 (en) * | 1966-09-06 | 1970-02-12 | Siemens Ag | Optical arrangement for laser beams |
US3524046A (en) * | 1968-04-26 | 1970-08-11 | Aluminum Co Of America | Apparatus and method for piercing holes in elastomeric articles |
GB1371624A (en) * | 1971-03-26 | 1974-10-23 | Atomic Energy Authority Uk | Optical processing of materials |
JPS5539434B2 (en) * | 1972-08-25 | 1980-10-11 | ||
JPS5310937B2 (en) * | 1973-05-18 | 1978-04-18 | ||
JPS5148917B2 (en) * | 1973-10-26 | 1976-12-23 | ||
GB1510899A (en) * | 1975-11-21 | 1978-05-17 | Boc Ltd | Laser machining |
JPS5297696U (en) * | 1976-01-21 | 1977-07-22 | ||
US4083629A (en) * | 1976-11-29 | 1978-04-11 | Gte Laboratories Incorporated | Beam splitting system for a welding laser |
-
1979
- 1979-07-13 CA CA331,825A patent/CA1123920A/en not_active Expired
- 1979-07-20 GB GB7925327A patent/GB2038220B/en not_active Expired
- 1979-07-31 FR FR7919725A patent/FR2434002A1/en active Granted
- 1979-08-07 NL NL7906042A patent/NL7906042A/en not_active Application Discontinuation
- 1979-08-07 IT IT49988/79A patent/IT1120489B/en active
- 1979-08-24 JP JP10805979A patent/JPS5530895A/en active Granted
- 1979-08-24 DE DE19792934407 patent/DE2934407A1/en not_active Withdrawn
Also Published As
Publication number | Publication date |
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FR2434002A1 (en) | 1980-03-21 |
GB2038220B (en) | 1982-10-20 |
IT1120489B (en) | 1986-03-26 |
GB2038220A (en) | 1980-07-23 |
JPS5530895A (en) | 1980-03-04 |
NL7906042A (en) | 1980-02-26 |
DE2934407A1 (en) | 1980-03-06 |
FR2434002B1 (en) | 1983-08-12 |
JPS6349594B2 (en) | 1988-10-05 |
IT7949988A0 (en) | 1979-08-07 |
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