Process for stabilizing a bonding interface, located within a structure which comprises an oxide layer and structure obtained

09659777 ยท 2017-05-23

Assignee

Inventors

Cpc classification

International classification

Abstract

The invention relates to a process for stabilizing a bonding interface, located within a structure for applications in the fields of electronics, optics and/or optoelectronics and that comprises an oxide layer buried between an active layer and a receiver substrate, the bonding interface having been obtained by molecular adhesion. In accordance with the invention, the process further comprises irradiating this structure with a light energy flux provided by a laser, so that the flux, directed toward the structure, is absorbed by the energy conversion layer and converted to heat in this layer, and in that this heat diffuses into the structure toward the bonding interface, so as to thus stabilize the bonding interface.

Claims

1. A process for stabilizing a bonding interface located within a structure for applications in the field of at least one of electronics, optics and optoelectronics, the process comprising: forming an energy conversion layer on an active layer of the structure, the active layer comprising a semiconductor material, the structure comprising an oxide layer buried between the active layer and a receiver substrate, the structure including a bonding interface between the active layer and the receiver substrate having been obtained by molecular adhesion; and irradiating the structure with a light energy flux provided by a laser, so that this flux, directed toward the structure, passes through the receiver substrate, through the oxide layer, and through the active layer, and is absorbed by the energy conversion layer and converted to heat in the energy conversion layer, the heat diffusing from the energy conversion layer toward the bonding interface through the active layer, and stabilizing the bonding interface by thermally treating the bonding interface without heating the oxide layer beyond a melting point of the oxide layer and without heating the active layer beyond a melting point of the active layer; wherein a fluence of the laser and a material constituting the energy conversion layer are chosen such that the buried oxide layer is heated to a temperature above 1200 C.

2. The process according to claim 1, wherein the buried oxide layer has a thickness less than or equal to 100 nm.

3. The process according to claim 1, wherein the active layer is transparent in the range of wavelengths of the light energy flux, and has a thickness of less than 1 m.

4. The process according to claim 1, wherein the bonding interface extends between two oxide layers together constituting the buried oxide layer.

5. The process according to claim 1, wherein the irradiation of the structure comprises selectively irradiating the structure at a stressed area of the bonding interface.

6. The process according to claim 5, wherein the stressed area of the bonding interface comprises at least one edge of the conversion layer.

7. The process according to claim 6, wherein the bonding interface is between the buried oxide layer and the receiver substrate.

8. The process according to claim 1, wherein the energy conversion layer has a thermal conductivity of less than 20 W/m.Math.K.

9. The process according to claim 8, wherein the energy conversion layer comprises a material selected from the group consisting of silicon oxide (SiO.sub.2), silicon and silicon nitride (Si.sub.3N.sub.4).

10. The process according to claim 1, wherein the irradiation of the structure comprises exposing a free surface of the receiver substrate to the light energy flux, the receiver substrate being transparent in the range of wavelengths of the light energy flux.

11. The process according to claim 10, wherein the receiver substrate comprises a material selected from the group consisting of sapphire, aluminum oxide (Al.sub.2O.sub.3), aluminum nitride (AlN), silicon carbide (SiC) and quartz.

12. The process according to claim 1, wherein the laser is an infrared laser, the wavelength of which is greater than 9 m.

13. The process according to claim 1, wherein the laser is a pulsed CO.sub.2 laser.

14. The process according to claim 1, wherein the semiconductor material is silicon.

15. The process according to claim 1, wherein the buried oxide layer comprises an oxide selected from the group consisting of silicon oxide (SiO.sub.2), aluminum oxide (Al.sub.2O.sub.3) and hafnium oxide (HfO.sub.2).

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) Other features and advantages of the invention will become apparent from the description that will now be given, with reference to the accompanying drawings, which represent therein, by way of example and nonlimitingly, one possible embodiment.

(2) In these drawings:

(3) FIGS. 1 and 2 schematically represent the various successive steps of one embodiment of a process for manufacturing a multilayer structure;

(4) FIGS. 3 and 4 schematically represent the various steps of the process for stabilizing a bonding interface in accordance with the invention, applied to the multilayer structure, in which the bonding interface extends between two oxide layers;

(5) FIG. 5 is a diagram, on an enlarged scale, representing the structure during the application of the stabilization process in accordance with the invention;

(6) FIGS. 6, 7 and 9 schematically represent the various successive steps of another embodiment of a process for manufacturing a multilayer structure; and

(7) FIG. 8 schematically represents the steps of the process for stabilizing a bonding interface in accordance with the invention, applied to the multilayer structure in which the bonding interface extends between an oxide layer and a receiver substrate.

DETAILED DESCRIPTION

(8) One possible embodiment of a multilayer structure, to which the stabilization process in accordance with the invention may be applied, will now be described with reference to FIGS. 1 and 2.

(9) In FIG. 1, a donor substrate 1 can be seen, which has a front face 11 and an opposite back face 12.

(10) Donor substrate 1 is preferably made from a semiconductor material, for example, made of silicon, germanium, silicon/germanium (SiGe) or of gallium nitride (GaN).

(11) It has, in the vicinity of its front face 11, a zone of weakness 13 that delimits, with the front face 11, an active layer 14. The remainder of substrate 1 bears the reference 15.

(12) This zone of weakness 13 is preferably formed by implantation of atomic species through the substrate 1, for example, according to the technique known to a person skilled, in the art under the trademark SMART CUT.

(13) The substrate 1 may be a single-layer or multilayer substrate.

(14) Moreover, its front face 11 is covered with a layer of oxide 16, for example, of silicon oxide (SiO.sub.2), aluminum oxide (Al.sub.2O.sub.3) or hafnium oxide (HfO.sub.2). The layer 16 could also be comprised of a stack of several layers of these oxides, preferably deposited one on top of the other.

(15) In FIG. 1, a receiver substrate 2 may also be seen, which has a front face 21 and an opposite back face 22.

(16) The front face 21 is covered with a layer of oxide 23, for example, of silicon oxide (SiO.sub.2), aluminum oxide (Al.sub.2O.sub.3) or hafnium oxide (HfO.sub.2). The layer 23 could also be comprised of a stack of several layers of these oxides.

(17) It will be noted that the receiver substrate 2 may be a single-layer or multilayer substrate.

(18) The donor substrate 1 and the receiver substrate 2 are then bonded to one another, via molecular adhesion, so that their respective oxide layers 16 and 23 come into contact with one another.

(19) The oxide layers 16 and 23 may be of the same chemical nature (same oxide) or of different nature and may be of the same thicknesses or of different thicknesses.

(20) The bonding interface between the two substrates 1, 2 bears the reference 3.

(21) The remainder 15 of the donor substrate 1 is then detached along the zone of weakness 13, in a manner known to a person skilled in the art, via application of mechanical and/or chemical and/or thermal stresses.

(22) A material-on-insulator structure is then obtained, referenced 4, which successively comprises the receiver substrate 2, two oxide layers 16 and 23 and finally the active layer 14 (see FIG. 2) and even a semiconductor-on-insulator (SeOI) structure 4 is obtained when the active layer 14 is made of a semiconductor material.

(23) The active layer 14 is thus named because it is in this active layer or on this active layer that the electronic, optical or optoelectronic components will be subsequently manufactured.

(24) The two superposed oxide layers 16 and 23 together form a buried oxide layer, which bears the general reference 5.

(25) Structure 4 is then subjected to a process for stabilizing the bonding interface 3 in accordance with the invention, the first step of which is represented in FIG. 3.

(26) This step comprises forming on and/or in the active layer 14 an energy conversion layer 6.

(27) The next step of the process, represented in FIG. 4, comprises irradiating the structure 4, with a light energy flux, provided by a laser 7, so as to stabilize the bonding interface 3.

(28) The phenomenon of stabilizing the bonding interface 3 will now be explained in connection with FIG. 5.

(29) Preferably, the laser 7 is moved so as to sweep the whole of the free surface of the receiver substrate 2, that is to say, its back face 22. The light energy provided by the laser 7 passes through the receiver substrate 2, the buried oxide layer 5, the active layer 14, and is absorbed by the energy conversion layer 6 (the route is marked by the arrow i). The laser 7 passes through the buried oxide layer 5 without being absorbed because the latter is too thin, as will be explained later.

(30) The laser 7 thus makes it possible to obtain strong and rapid heating of the energy conversion layer 6.

(31) Generally, the choice of a laser is dictated by the power to be provided and the nature of the materials constituting the receiver substrate 2, the active layer 14 and the energy conversion layer 6, as is explained below.

(32) The laser 7 is preferably an infrared laser, the wavelength of which is greater than 9 m.

(33) In the case where the receiver substrate 2 is made of silicon, it is preferably a pulsed CO.sub.2 laser.

(34) The pulses used are preferably short. By way of illustrative example, for pulses of less than 1 s, the power density required is of the order of 10.sup.4 to 10.sup.5 W/cm.sup.2. For pulses of less than 1 ns, the power density is of the order of 10.sup.8 W/cm.sup.2.

(35) The material constituting the receiver substrate 2 is, therefore, chosen so as to be transparent in the range of wavelengths of the laser 7. It may be, for example, either silicon as mentioned previously, or sapphire, quartz, aluminum nitride (AlN), aluminum oxide (Al.sub.2O.sub.3) or silicon carbide (SiC).

(36) The material constituting the energy conversion layer 6 is chosen so as to absorb the energy in the range of wavelengths provided by the laser 7 and so as to conduct very little or no heat. In other words, its thermal conductivity is preferably less than 20 W/m.Math.K.

(37) By illuminating the structure 4 via its back face 22, it is the buried part of the energy conversion layer 6 that will be heated to the maximum.

(38) Therefore, the heat diffuses in return into the structure 4 in the direction of the buried oxide layer 5 and of the bonding interface 3 (route marked by the arrows ii).

(39) The energy conversion layer 6 is preferably produced from a material chosen from silicon oxide (SiO.sub.2) and silicon nitride (Si.sub.3N.sub.4).

(40) In the case where the active layer 14 is made of silicon, the energy conversion layer 6 may be formed, for example, by thermal oxidation of this active layer, by annealing in an oxygen-rich atmosphere, for example, at a temperature of the order of 600 C. or more, so as to obtain SiO.sub.2.

(41) In the case where the active layer 14 is made of a material other than silicon, the layer 6 may be formed by a chemical vapor deposition (CVD) technique (deposition of silicon nitride or silicon oxide).

(42) In the case where the layer 6 is made of silicon nitride and the active layer 14 is made of silicon, the layer 6 may be obtained by nitridation of the silicon (annealing at 600 C. in a nitrogen-containing atmosphere) or else by CVD deposition.

(43) In the embodiment, illustrated in FIGS. 1 to 5, the material constituting the active layer 14 must be transparent in the range of wavelengths provided by the laser 7, so as to allow the transfer of light toward the layer 6 (arrow i), must be a good thermal conductor, so as to enable the transfer of heat in return toward the buried oxide layer 5 (arrows ii) and must have a thickness of less than 1 m, more preferably, between a few nanometers and 1 m, for the two aforementioned reasons.

(44) Moreover, the fluence of the laser 7 and the material constituting the energy conversion layer 6 are chosen so as to preferably bring the buried oxide layer 5 to a temperature above 1200 C. and to thus stabilize the bonding interface 3. Preferably, it will be ensured that neither the melting point of the oxide, for example, 1600 C. for SiO.sub.2, 2000 C. for HfO.sub.2 and Al.sub.2O.sub.3, nor the melting point of the active layer 14 are exceeded. Preferably, the fluence is between 0.1 J/m.sup.2 and 10 J/m.sup.2.

(45) It will be noted that the illumination time of the structure is not a fundamental criterion as long as the stabilization temperature is reached. Consequently, although it is possible to use lasers other than a CO.sub.2 laser, it is not essential to use much more expensive lasers, for example, short-pulse lasers. This is one advantage of the invention.

(46) The process in accordance with the invention applies more particularly to structures for which the buried oxide layer 5 has a thickness less than or equal to 100 nm. Indeed, below this thickness, the buried oxide is too thin to absorb a significant power of the laser and it is almost not heated by the light energy flux provided by the laser 7, which passes through it to reach the energy conversion layer 6 (direction of the arrow i).

(47) On the other hand, once the light energy is converted to heat by the layer 6, this heat may be absorbed even by an oxide layer 5 of less than or equal to 100 nm.

(48) The invention may even apply to structures for which the buried oxide layer 5 has a thickness in the vicinity of 50 nm, or even below this value, for example, in the vicinity of 20 nm. Preferably, the buried oxide layer 5 is greater than 1 nm.

(49) Stabilization is a microscopic phenomenon that reflects the establishment of atomic bonds (covalent bonds) between the two faces in contact, this being homogeneous over the whole of the bonding interface 3.

(50) The non-establishment of these bonds, even very locally, may be chemically revealed by etching using a Wright etch solution (as described in publication Margaret Wright Jenkins, Journal of the Electrochemical Society 124, 757-759, 1977), applied for around 10 seconds.

(51) Thus, a stabilized bonding interface inevitably has a strong bonding energy, but the opposite is not true.

(52) Another possible embodiment of a multilayer structure, to which the stabilization process in accordance with the invention may be applied, will now be described with reference to FIGS. 6 to 9. The commons elements with the first embodiment are designated with the same references.

(53) In FIG. 6, a donor substrate 1 can be seen, which has a front face 11 and an opposite back face 12.

(54) This donor substrate 1 is preferably made from a semiconductor material, for example, made of silicon, germanium, silicon/germanium (SiGe) or of gallium nitride (GaN) layer, which is an active layer (14) and, on which are successively disposed, for example, a silicon oxide layer (SiO.sub.2) (24) and a base (25) such as silicon.

(55) Moreover, its front face 11 is covered with a layer of oxide 5, for example, of silicon oxide (SiO.sub.2), aluminum oxide (Al.sub.2O.sub.3) or hafnium oxide (HfO.sub.2). The layer 5 could also be comprised of a stack of several layers of these oxides, preferably deposited one on top of the other.

(56) In FIG. 6, a receiver substrate 2, for example, made of sapphire, may also be seen, which has a front face 21 and an opposite back face 22. It will be noted that the receiver substrate 2 may be a single-layer or multilayer substrate.

(57) The donor substrate 1 and the receiver substrate 2 are then bonded to one another (see FIG. 7) via molecular bonding adhesion, so that the oxide layers 5 and front face 21 come into contact with one another. The bonding interface between the two substrates 1, 2 bears the reference 3.

(58) This structure is then subjected to the process for stabilizing the bonding interface 3 in accordance with the invention (FIG. 8). This process comprises a thermal stabilization step of the bonding interface 3, but because of the different thermal expansion coefficients of the two substrates bonded (1, 2) and in order to limit the stress at the bonding interface 3 during the thermal stabilization step, the structure is irradiated with a light energy flux provided by a laser, but only in a specific location (in this embodiment, on the edges 26 of the structure) so as to stabilize the bonding interface 3.

(59) Ideally, the location that is irradiated is the one where the stress is the more important at the bonding interface 3, the stress location at the bonding interface 3 dependent upon the shape of the substrates to bond. In this embodiment described in FIGS. 6 to 9, it is known that the stress is mainly focused on the edge 26 due to circular shape substrates (1, 2).

(60) The irradiation of only a location, like the edges 26 of the bonding interface 3, enables overcoming the different thermal expansion coefficients (CTEs) problem, and obtaining a strong and stabilized bonding interface 3 by limiting the mechanical stress, the defect and the risks of debonding.

(61) The laser 7 is moved so as to sweep the edges 26 of the receiver substrate 2 back face 22 (FIG. 7). The light energy provided by the laser 7 passes through the receiver substrate 2 and the buried oxide layer 5, and is absorbed by the active layer 14. In this embodiment, the active layer 14 and the energy conversion layer 6 are the same layer, so the light energy is absorbed by the energy conversion layer 6. The laser 7 passes through the buried oxide layer 5 without being absorbed because the latter is too thin.

(62) So, after this stabilizing process (see FIG. 9), the bonding interface 3 is sufficiently strong to ensure good quality of the final layer transfer enabling detachment of the silicon oxide layer (SiO.sub.2) (24) and the base (25) of the donor substrate 1 by grinding, in a manner known to a person skilled in the art, via application of mechanical and/or chemical and/or thermal stresses.

(63) In the remainder of the description and claims, it is considered that a bonding interface is correctly stabilized, as long as, by observation using a scanning electron microscope (SEM) of the bonding interface, after etching using a Wright etch solution, over three fields, each of which extends over the entire diameter of the substrate and over a width of 3 m, a number of defects of less than or equal to one is observed on each field.

(64) A bonding interface that does not have any defect over the three fields will then be considered to be perfectly stabilized.

(65) An interface having one defect per field of 3 m in width will be considered to be weakly stabilized; it will, however, be considered to be sufficiently satisfactory for the invention.

(66) Finally, a bonding interface having more than one defect per field of 3 m in width will be considered to be non-stabilized.

(67) Moreover, the oxide/oxide bonding interface 3 will be considered to be correctly stabilized if it has a resistance to etching using hydrofluoric acid (HF) at a concentration of 10% by volume, of 0.3 m/minute, and if it has a Dit value of less than 2.10.sup.11 cm.sup.2.Math.eV.sup.1, and if the buried oxide layer 5 has a Qbd value of greater than 10 C/cm.sup.2.

(68) As a reminder, it is recalled that Dit denotes the density of traps at the bonding interface, these traps limiting the mobility of electrical carriers in the various layers, in particular, in the active layer 14. A low Dit value (less than 2.10.sup.11 cm.sup.2 eV.sup.1) is associated with a higher mobility of the carriers and, therefore, with better electrical properties of the final structure.

(69) Qbd denotes the charge-to-breakdown measurement (see the standard JESD35-AProcedure for the Wafer-Level Testing of Thin Dielectrics, April 2001).

(70) The invention also applies to the stabilization of a bonding interface between a buried oxide layer and the active layer 14 or of other bonding interfaces.

(71) In the first case, the receiver substrate 2 is covered with an oxide layer 23. The structure 4 treated, therefore, comprises a single oxide layer 23, buried between the active layer 14 and the receiver substrate 2.

(72) The parameters for implementing the stabilization process and the criteria used for a satisfactory stabilization are the same as those described previously for the first embodiment.

(73) The process in accordance with the invention has the advantage of being able to be easily integrated into a process for manufacturing an SeOI or SOI structure, especially when the material constituting the energy conversion layer 6 is oxide. Indeed, these manufacturing processes often integrate a step of sacrificial oxidation among the surface-finishing treatments of these structures, as is described in U.S. Pat. No. 6,403,450.

(74) The stabilization process may, therefore, be inserted between the oxidation that makes it possible to create the energy conversion layer 6 and the removal thereof. Any possible damage caused to the layer 6 during the stabilization is of no consequence since layer 6 is subsequently removed.

(75) Finally, since the two surfaces of the active layer 14 are protected during the illumination, the damaging thereof is not to be feared.