EP2979296A1 - Procede de fabrication d'une structure composite - Google Patents
Procede de fabrication d'une structure compositeInfo
- Publication number
- EP2979296A1 EP2979296A1 EP14718659.7A EP14718659A EP2979296A1 EP 2979296 A1 EP2979296 A1 EP 2979296A1 EP 14718659 A EP14718659 A EP 14718659A EP 2979296 A1 EP2979296 A1 EP 2979296A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- layer
- dielectric layer
- dielectric
- useful
- composite structure
- 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- Withdrawn
Links
Classifications
-
- H—ELECTRICITY
- H10—SEMICONDUCTOR DEVICES; ELECTRIC SOLID-STATE DEVICES NOT OTHERWISE PROVIDED FOR
- H10P—GENERIC PROCESSES OR APPARATUS FOR THE MANUFACTURE OR TREATMENT OF DEVICES COVERED BY CLASS H10
- H10P95/00—Generic processes or apparatus for manufacture or treatments not covered by the other groups of this subclass
-
- H—ELECTRICITY
- H10—SEMICONDUCTOR DEVICES; ELECTRIC SOLID-STATE DEVICES NOT OTHERWISE PROVIDED FOR
- H10P—GENERIC PROCESSES OR APPARATUS FOR THE MANUFACTURE OR TREATMENT OF DEVICES COVERED BY CLASS H10
- H10P90/00—Preparation of wafers not covered by a single main group of this subclass, e.g. wafer reinforcement
- H10P90/19—Preparing inhomogeneous wafers
- H10P90/1904—Preparing vertically inhomogeneous wafers
- H10P90/1906—Preparing SOI wafers
- H10P90/1914—Preparing SOI wafers using bonding
- H10P90/1916—Preparing SOI wafers using bonding with separation or delamination along an ion implanted layer, e.g. Smart-cut
-
- H—ELECTRICITY
- H10—SEMICONDUCTOR DEVICES; ELECTRIC SOLID-STATE DEVICES NOT OTHERWISE PROVIDED FOR
- H10D—INORGANIC ELECTRIC SEMICONDUCTOR DEVICES
- H10D62/00—Semiconductor bodies, or regions thereof, of devices having potential barriers
- H10D62/10—Shapes, relative sizes or dispositions of the regions of the semiconductor bodies; Shapes of the semiconductor bodies
- H10D62/113—Isolations within a component, i.e. internal isolations
- H10D62/115—Dielectric isolations, e.g. air gaps
-
- H—ELECTRICITY
- H10—SEMICONDUCTOR DEVICES; ELECTRIC SOLID-STATE DEVICES NOT OTHERWISE PROVIDED FOR
- H10D—INORGANIC ELECTRIC SEMICONDUCTOR DEVICES
- H10D86/00—Integrated devices formed in or on insulating or conducting substrates, e.g. formed in silicon-on-insulator [SOI] substrates or on stainless steel or glass substrates
-
- H—ELECTRICITY
- H10—SEMICONDUCTOR DEVICES; ELECTRIC SOLID-STATE DEVICES NOT OTHERWISE PROVIDED FOR
- H10P—GENERIC PROCESSES OR APPARATUS FOR THE MANUFACTURE OR TREATMENT OF DEVICES COVERED BY CLASS H10
- H10P14/00—Formation of materials, e.g. in the shape of layers or pillars
- H10P14/60—Formation of materials, e.g. in the shape of layers or pillars of insulating materials
- H10P14/69—Inorganic materials
- H10P14/692—Inorganic materials composed of oxides, glassy oxides or oxide-based glasses
- H10P14/6921—Inorganic materials composed of oxides, glassy oxides or oxide-based glasses containing silicon
- H10P14/69215—Inorganic materials composed of oxides, glassy oxides or oxide-based glasses containing silicon the material being a silicon oxide, e.g. SiO2
-
- H—ELECTRICITY
- H10—SEMICONDUCTOR DEVICES; ELECTRIC SOLID-STATE DEVICES NOT OTHERWISE PROVIDED FOR
- H10P—GENERIC PROCESSES OR APPARATUS FOR THE MANUFACTURE OR TREATMENT OF DEVICES COVERED BY CLASS H10
- H10P14/00—Formation of materials, e.g. in the shape of layers or pillars
- H10P14/60—Formation of materials, e.g. in the shape of layers or pillars of insulating materials
- H10P14/69—Inorganic materials
- H10P14/694—Inorganic materials composed of nitrides
- H10P14/6943—Inorganic materials composed of nitrides containing silicon
- H10P14/69433—Inorganic materials composed of nitrides containing silicon the material being a silicon nitride not containing oxygen, e.g. SixNy or SixByNz
-
- H—ELECTRICITY
- H10—SEMICONDUCTOR DEVICES; ELECTRIC SOLID-STATE DEVICES NOT OTHERWISE PROVIDED FOR
- H10W—GENERIC PACKAGES, INTERCONNECTIONS, CONNECTORS OR OTHER CONSTRUCTIONAL DETAILS OF DEVICES COVERED BY CLASS H10
- H10W10/00—Isolation regions in semiconductor bodies between components of integrated devices
- H10W10/10—Isolation regions comprising dielectric materials
- H10W10/181—Semiconductor-on-insulator [SOI] isolation regions, e.g. buried oxide regions of SOI wafers
Definitions
- the present invention relates to a method of manufacturing a composite structure.
- the invention also relates to a composite structure.
- a manufacturing method, illustrated in FIG. 1, of a composite structure comprising from its rear face towards its front face a support substrate 1, a covering layer 2, at least one dielectric layer 3 and a useful layer 4, and known of the state of the art (see, for example, EP1780794), comprises the following steps:
- the dielectric layer 3 has a contour Cz
- the assembly formed by the useful layer 4, the dielectric layer 3 and the covering layer 2 will be referred to as the stack of layers 8.
- step f the stack of layers is transferred onto the support substrate 1 to form the composite structure.
- the composite structure has a peripheral ring 9.
- This peripheral ring 9 is located in a peripheral zone of the support substrate 1, and in which, in the absence of sufficient adhesion between the support substrate 1 and the donor substrate 5, the transfer of the stack of layers 8 has no effect. no place.
- the blanks of the cover layer 2 and the dielectric layer 3 are exposed at the step and therefore not protected from possible chemical attacks.
- etching can generate particles via delamination of the useful layer 4.
- a creep of the useful layer 4 is generally performed so as to cover or encapsulate the dielectric layer 3 at the step.
- FIG. 3 thus shows the steps obtained on such a substrate after step f) of fracture.
- the fracture step does not lead to a single step, but instead to several steps.
- the main disadvantage of this manufacturing process is that it leads to an atypical fracture at the edge of the substrate.
- the composite structure comprises from its rear face towards its front face a silicon substrate, a silicon dioxide layer, a silicon nitride layer, a silicon dioxide layer and a silicon layer.
- An object of the invention is therefore to propose a method of manufacturing a composite substrate that makes it possible to carry out a creep step of the useful layer 4 so as to cover the exposed surface of the cover layer 2 and the layer dielectric 3 at the step.
- the present invention aims to overcome the aforementioned drawbacks, and relates to a method of manufacturing a composite structure comprising from its rear face to its front face a support substrate, a cover layer, at least one dielectric layer and a useful layer, said process comprising the following steps:
- the dielectric layer has an outline
- steps b) and e) are performed so that the contour of the dielectric layer is inscribed in the contour of the contact surface, and step c) is performed so that the covering layer covers the peripheral surface of the dielectric layer.
- the stack of layers is transferred onto the support substrate.
- the stack of transferred layers comprises a central portion and a peripheral portion.
- the central portion of the stack comprises the useful layer, the dielectric layer and the cover layer.
- the peripheral portion comprises only the useful layer and the covering layer.
- the peripheral portion corresponds to the transfer of a stack comprising a single intermediate layer.
- the fracture step leads to a single step at the peripheral ring.
- the support substrate comprises:
- steps b) and e) are executed so that the contour of the dielectric layer and the peripheral zone of the support substrate delimit a substantially annular surface with a width of between 105 and 150%, preferably between 1 and 140%, even more preferably between 1 and 15%.
- the dielectric layer is formed in two steps b1) and b2):
- the dielectric layer comprises silicon nitride with a thickness of between 10 and 80 nm.
- the cover layer comprises silicon dioxide with a thickness greater than 80 nm.
- the donor substrate comprises at least one of the following materials: silicon, germanium, germanium silicon alloy.
- step f) is followed by a heat treatment step for encapsulating the cover layer and the dielectric layer with the useful layer.
- the donor substrate comprises an additional layer, the additional layer being in contact with the dielectric layer, the additional layer having the same chemical composition as the covering layer.
- the donor substrate comprises silicon
- the additional layer comprises silicon dioxide
- the dielectric layer comprises silicon nitride
- the covering layer comprises silicon dioxide.
- the invention also relates to a composite structure comprising from its rear face towards its front face a support substrate, a covering layer, at least one dielectric layer and a useful layer, the dielectric layer having:
- said composite structure being remarkable in that the covering layer covers in its entirety the peripheral surface of the dielectric layer, so that the useful layer and the covering layer encapsulate the dielectric layer.
- the transferred layer stack comprises a central portion and a peripheral portion.
- the central portion of the stack comprises the useful layer, the dielectric layer and the cover layer.
- the peripheral portion comprises only the useful layer and the covering layer.
- peripheral portion corresponds to a stack comprising a single intermediate layer.
- the composite structure obtained allows the creep of the useful layer, for example by carrying out a heat treatment, so as to encapsulate the covering layer at the level of the single step.
- the useful layer comprises at least one of the following materials: silicon, germanium, germanium silicon alloy. According to one embodiment, the useful layer comprises a monocrystalline material.
- the covering layer comprises silicon dioxide.
- the dielectric layer comprises silicon nitride.
- the covering layer has: a first surface in contact with the support substrate,
- the useful layer covering the peripheral surface of the covering layer.
- an additional layer is interposed between the useful layer and the dielectric layer, the additional layer having the same chemical composition as the covering layer.
- the useful layer comprises monocrystalline silicon
- the additional layer comprises thermal silicon dioxide
- the dielectric layer comprises silicon nitride
- the covering layer comprises silicon dioxide
- FIG. 1 is a schematic representation of a manufacturing method according to the known techniques of the prior art
- FIG. 2 is a view of the front face of a composite structure obtained by a manufacturing method according to the techniques known from the prior art
- FIG. 3 is a sectional view of a substrate used in a manufacturing method according to the techniques known from the prior art
- FIGS. 4a and 4b are a schematic representation of a first embodiment of the invention.
- FIG. 5 is a cross-sectional view of a composite structure obtained by a manufacturing method according to the invention and having undergone an encapsulation treatment;
- FIG. 6a and 6b are a schematic representation of a second embodiment of the invention.
- the method is a method of manufacturing a composite structure comprising from its rear face towards its front face a support substrate 10, a covering layer 20, at least one dielectric layer 30 and a useful layer 40, said method comprising the following steps:
- the dielectric layer 30 has a contour Cz
- steps b) and e) are carried out so that the contour Cz of the dielectric layer 30 is inscribed in the contour Cs of the contact surface 70, and step c ) is executed so that the cover layer 20 covers the peripheral surface of the dielectric layer 30.
- a step of determining the contour Cs of the contact surface can be performed prior to the implementation of the manufacturing method according to the invention.
- This determination step is particularly advantageous when it comes to implementing the method for manufacturing a plurality of composite structures.
- a plurality of donor substrates 50 and a plurality of support substrates 10 are chosen so that the contour Cs of the contact surface is substantially equivalent, or even identical, a composite structure to another.
- the donor substrates 50 of the plurality of donor substrates 50 are then chosen so as to have substantially equivalent or equal geometric characteristics.
- the support substrates 10 of the plurality of support substrates 10 are then chosen so as to have substantially equivalent or equal geometric characteristics.
- geometric characteristics of a substrate is meant, without limitation, its thickness at any point on its surface, its thickness variation, its shape. Thus, it is sufficient to determine the contour Cs for the manufacture of a structure and apply the result to the manufacture of a plurality of composite structures.
- the determination of the contour Cs can comprise the following steps:
- Another solution would be to perform the method of manufacturing a composite structure by omitting the formation of the dielectric layer 30, and measure at all points of the edge of the support substrate the width of the peripheral ring.
- the appearance of the peripheral ring on the composite structure is delimited by the edge of the support substrate and the contour Cs of the contact surface 70. The determination of the contour Cs is then direct.
- the Applicant has found that the manufacture of a composite structure having a cover layer 20 leads to the formation of a peripheral ring with a width of 0.8 mm.
- the support substrate (10) comprises:
- the contour (Cs) of the contact surface (70) and the peripheral zone of the support substrate (10) define a substantially annular surface of width L, and steps b) and e) are executed so that the contour (Cz) of the dielectric layer (30) and the peripheral area of the support substrate (10) delimit a substantially annular surface having a width of between 105 and 150%, preferably between 1 10 and 140%, even more preferably between 1 and 130%, of the width L.
- the plurality of donor substrates 50 and the plurality of support substrates 10 may exhibit some dispersion of their geometric characteristics.
- the donor substrate 10 provided in step a) may comprise one of the materials chosen from: silicon, silicon germanium, germanium.
- the support substrate 30 provided in step a) may consist of all the materials commonly used in the microelectronics, optics, optoelectronics and photovoltaics industry.
- the support substrate 10 comprises at least one of the materials selected from the following group: silicon, silicon carbide, silicon germanium, glass, a ceramic, a metal alloy.
- At least one dielectric layer 30 is formed on the donor substrate.
- a cover layer 20 is formed in overlap of the dielectric layer 30.
- a step d) of forming a weakening zone 60 in the donor substrate 50 is performed.
- the weakening zone 60 delimits, in the donor substrate 50, a useful layer 40, the useful layer being in contact with the dielectric layer 30.
- the useful layer 40 is intended to be transferred onto the support substrate 10.
- the weakening zone 60 can be created by implantation of atomic species in the donor substrate 50.
- atomic species we mean atomic, molecular or ionic species.
- Introduced species may include at least one of the following species: hydrogen, helium.
- the hydrogen can be introduced with an energy of between 10 and 210 keV, and a dose of between 7x10 15 and 1 x 10 17 at / cm 2 .
- the assembly step e) may be a molecular bonding step.
- the fracture step f) may advantageously be thermal annealing carried out at a temperature of between 300 and 600 ° C.
- step f the composite structure is obtained.
- the composite structure comprises from its front face towards its rear face the useful layer 40, the dielectric layer 30, the covering layer 20, and the support substrate 10.
- the first embodiment is illustrated in Figures 4a and 4b.
- the dielectric layer 30 can be formed in two steps:
- Step b1) may be a vapor phase deposition technique, low pressure vapor phase deposition, or plasma assisted vapor phase deposition on the donor substrate 50. It may also be a technique heat treatment in a chosen atmosphere (nitriding, oxidation, ).
- the thickness of the layer of dielectric material may be between 10 nm and 80 nm, for example 50 nm.
- Step b1) is then followed by a step b2) which comprises a partial removal of the layer of dielectric material. The partial shrinkage is performed so that the remaining or residual dielectric material layer portion constitutes the dielectric layer 30.
- the partial removal of the layer of dielectric material is performed on a peripheral surface of the donor substrate 50 delimited by the edge of the donor substrate 50 and the contour Cz.
- the layer portion of residual dielectric material forms the dielectric layer 30.
- the peripheral surface of the donor substrate 50 may be in the form of an annular surface.
- Step b2) can advantageously be performed by a chemical etching solution.
- dielectric layers 30 may be formed successively.
- a dielectric layer 30 comprising silicon nitride, and another dielectric layer 30 comprising silicon dioxide.
- the chemical etching solution may be a solution of phosphoric acid (H 3 PO 4 ) heated at a temperature above 50 ° C.
- the chemical etching solution may be distributed by a nozzle on the edge of the donor substrate 50 in rotation, so as to etch the dielectric layer 30 only on the peripheral surface of the donor substrate 50 delimited by the edge of the donor substrate 10 and the contour cz.
- the cover layer 30 may be formed by a vapor deposition technique, low pressure vapor deposition, or plasma assisted vapor deposition.
- the covering layer covers in their entirety the second surface and the peripheral surface of the dielectric layer 30.
- the cover layer 20 may comprise a material, different from the materials of the dielectric layer 30, selected from among the following materials: silicon oxide, silicon nitride or oxynitride, aluminum nitride, aluminum oxide, polyc stallin silicon, amorphous silicon.
- the cover layer 20 comprises silicon oxide and its thickness is greater than 80 nm, for example 100 nm.
- step f the composite structure is obtained.
- the composite structure comprises from its rear face towards its front face a support substrate 10, a covering layer 20, at least one dielectric layer 30 and a useful layer 40, the dielectric layer 30 having:
- the covering layer 20 completely covers the peripheral surface of the dielectric layer 30, so that the useful layer 40 and the covering layer 20 encapsulate the dielectric layer 30.
- the dielectric layer of contour Cz is located above a central surface 80 of contour Cp of the support substrate.
- the surface delimited by the contour Cs of the contact surface 70 and the contour Cp of the central surface 80 is opposite a stack of layers comprising only the useful layer 40 and the covering layer 20.
- the central surface 80 of the support substrate 10 is opposite a stack of layers comprising the useful layer 40, the dielectric layer 30 and the covering layer 20. Thus, a single step is observed at the edge of the substrate.
- the cover layer 20 is made of polycrystalline silicon or amorphous silicon, and its thickness is between a few nm and a few millers of nm, for example 2000 nm.
- the dielectric layer 30 is made of silicon oxide, and the useful layer 40 is made of silicon.
- a silicon-on-insulator composite structure having a buried layer of polycrystalline silicon or amorphous silicon under the insulator layer is formed. This type of composite structure is particularly suitable for the manufacture of semiconductor devices having applications in the field of radio frequencies.
- the second embodiment differs from the first embodiment in that the donor substrate 50 comprises an additional layer 90, the additional layer 90 being in contact with the dielectric layer 30, the additional layer 90 having the same chemical composition as the covering layer 20.
- the additional layer 90 and the cover layer 20 comprise silicon oxide.
- the additional layer 90 is formed directly on the donor substrate 50, before the dielectric layer 30.
- the additional layer 90 may comprise a material, different from the materials of the dielectric layer 30, selected from the following materials: silicon oxide, silicon nitride or oxynitride, aluminum nitride, aluminum oxide, polycrystalline silicon, amorphous silicon.
- the additional layer 90 is made of silicon oxide and its thickness is between 2 and 20 nm, for example 7 nm.
- the additional silicon oxide layer 90 can be obtained by thermal oxidation of this donor substrate, and thus form an additional layer 90 of thermal silicon dioxide.
- step f the composite structure is obtained.
- the composite structure comprises from its front face towards its rear face a useful layer 40, an additional layer 90, a dielectric layer 30, a cover layer 20 and a support substrate 10.
- the dielectric layer 30 of contour Cz is located above a central surface 80 and of contour Cp of the support substrate 10.
- the surface delimited by the contour Cs of the contact surface 70 and the contour Cp of the central surface 80 is opposite a stack of layers comprising only the useful layer 40, the additional layer 90, and the covering layer 20.
- the central surface 80 of the support substrate 10 is opposite a stack of layers comprising the useful layer 40, the dielectric layer 30 and the covering layer 20.
- the covering layer 20 and the additional layer 90 having the same chemical composition, their stack is then associated with a single layer of dielectric material.
- a single step is observed at the edge of the substrate. Consequently, the observation of a single step makes it possible to encapsulate the covering layer 20, the dielectric layer 30, and the additional layer 90 with the useful layer 40.
- the encapsulation is carried out by a heat treatment, without observing any dewetting of the useful layer 40.
- the additional layer 90 advantageously comprises silicon dioxide.
- SOI ONO silicon on silicon dioxide, on silicon nitride, and on silicon dioxide
- the invention is advantageously used for the production of SOI ONO composite substrates or for the production of SOI substrates for radiofrequency applications.
Landscapes
- Micromachines (AREA)
- Recrystallisation Techniques (AREA)
- Thin Film Transistor (AREA)
Abstract
Description
Claims
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR1300738A FR3003997B1 (fr) | 2013-03-29 | 2013-03-29 | Procede de fabrication d'une structure composite |
| PCT/FR2014/050666 WO2014154978A1 (fr) | 2013-03-29 | 2014-03-21 | Procede de fabrication d'une structure composite |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| EP2979296A1 true EP2979296A1 (fr) | 2016-02-03 |
Family
ID=48856695
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP14718659.7A Withdrawn EP2979296A1 (fr) | 2013-03-29 | 2014-03-21 | Procede de fabrication d'une structure composite |
Country Status (9)
| Country | Link |
|---|---|
| US (1) | US9799549B2 (fr) |
| EP (1) | EP2979296A1 (fr) |
| JP (1) | JP6306684B2 (fr) |
| KR (1) | KR20150140313A (fr) |
| CN (1) | CN105074895A (fr) |
| FR (1) | FR3003997B1 (fr) |
| RU (1) | RU2645895C2 (fr) |
| SG (1) | SG11201507963QA (fr) |
| WO (1) | WO2014154978A1 (fr) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE3326818C2 (de) * | 1983-07-26 | 1986-11-06 | Rudolf 8729 Zeil Weigmann | Krückenpaar für Steh- und Gehbehinderte mit einer Sitzfläche |
| US20180175008A1 (en) * | 2015-01-09 | 2018-06-21 | Silicon Genesis Corporation | Three dimensional integrated circuit |
Family Cites Families (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2003224247A (ja) * | 2002-01-29 | 2003-08-08 | Shin Etsu Handotai Co Ltd | Soiウエーハ及びsoiウエーハの製造方法 |
| FR2852143B1 (fr) * | 2003-03-04 | 2005-10-14 | Soitec Silicon On Insulator | Procede de traitement preventif de la couronne d'une tranche multicouche |
| JP4854917B2 (ja) * | 2003-03-18 | 2012-01-18 | 信越半導体株式会社 | Soiウェーハ及びその製造方法 |
| JP4730581B2 (ja) * | 2004-06-17 | 2011-07-20 | 信越半導体株式会社 | 貼り合わせウェーハの製造方法 |
| JP2006173354A (ja) * | 2004-12-15 | 2006-06-29 | Canon Inc | Soi基板の製造方法 |
| US7781309B2 (en) * | 2005-12-22 | 2010-08-24 | Sumco Corporation | Method for manufacturing direct bonded SOI wafer and direct bonded SOI wafer manufactured by the method |
| CN101669193B (zh) * | 2007-04-27 | 2012-02-15 | 株式会社半导体能源研究所 | Soi衬底及其制造方法和半导体器件 |
| US7875532B2 (en) | 2007-06-15 | 2011-01-25 | Semiconductor Energy Laboratory Co., Ltd. | Substrate for manufacturing semiconductor device and manufacturing method thereof |
| JP5498670B2 (ja) * | 2007-07-13 | 2014-05-21 | 株式会社半導体エネルギー研究所 | 半導体基板の作製方法 |
| TWI493609B (zh) | 2007-10-23 | 2015-07-21 | 半導體能源研究所股份有限公司 | 半導體基板、顯示面板及顯示裝置的製造方法 |
| US8357974B2 (en) * | 2010-06-30 | 2013-01-22 | Corning Incorporated | Semiconductor on glass substrate with stiffening layer and process of making the same |
| FR2967295B1 (fr) | 2010-11-05 | 2013-01-11 | Soitec Silicon On Insulator | Procédé de traitement d'une structure multicouche |
| RU2469433C1 (ru) * | 2011-07-13 | 2012-12-10 | Юрий Георгиевич Шретер | Способ лазерного отделения эпитаксиальной пленки или слоя эпитаксиальной пленки от ростовой подложки эпитаксиальной полупроводниковой структуры (варианты) |
-
2013
- 2013-03-29 FR FR1300738A patent/FR3003997B1/fr not_active Expired - Fee Related
-
2014
- 2014-03-21 RU RU2015141124A patent/RU2645895C2/ru not_active IP Right Cessation
- 2014-03-21 WO PCT/FR2014/050666 patent/WO2014154978A1/fr not_active Ceased
- 2014-03-21 US US14/780,467 patent/US9799549B2/en not_active Expired - Fee Related
- 2014-03-21 JP JP2016504722A patent/JP6306684B2/ja not_active Expired - Fee Related
- 2014-03-21 CN CN201480018752.9A patent/CN105074895A/zh active Pending
- 2014-03-21 KR KR1020157030956A patent/KR20150140313A/ko not_active Withdrawn
- 2014-03-21 SG SG11201507963QA patent/SG11201507963QA/en unknown
- 2014-03-21 EP EP14718659.7A patent/EP2979296A1/fr not_active Withdrawn
Non-Patent Citations (2)
| Title |
|---|
| None * |
| See also references of WO2014154978A1 * |
Also Published As
| Publication number | Publication date |
|---|---|
| KR20150140313A (ko) | 2015-12-15 |
| RU2015141124A (ru) | 2017-05-04 |
| US20160042989A1 (en) | 2016-02-11 |
| RU2645895C2 (ru) | 2018-02-28 |
| JP6306684B2 (ja) | 2018-04-04 |
| FR3003997B1 (fr) | 2015-03-20 |
| CN105074895A (zh) | 2015-11-18 |
| JP2016519431A (ja) | 2016-06-30 |
| FR3003997A1 (fr) | 2014-10-03 |
| US9799549B2 (en) | 2017-10-24 |
| WO2014154978A1 (fr) | 2014-10-02 |
| SG11201507963QA (en) | 2015-10-29 |
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Legal Events
| Date | Code | Title | Description |
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| PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
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| 17P | Request for examination filed |
Effective date: 20150921 |
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