WO2014156782A1 - 中空構造体の製造方法 - Google Patents
中空構造体の製造方法 Download PDFInfo
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- WO2014156782A1 WO2014156782A1 PCT/JP2014/057182 JP2014057182W WO2014156782A1 WO 2014156782 A1 WO2014156782 A1 WO 2014156782A1 JP 2014057182 W JP2014057182 W JP 2014057182W WO 2014156782 A1 WO2014156782 A1 WO 2014156782A1
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- sacrificial film
- forming
- film
- hollow structure
- hollow
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B81—MICROSTRUCTURAL TECHNOLOGY
- B81C—PROCESSES OR APPARATUS SPECIALLY ADAPTED FOR THE MANUFACTURE OR TREATMENT OF MICROSTRUCTURAL DEVICES OR SYSTEMS
- B81C1/00—Manufacture or treatment of devices or systems in or on a substrate
- B81C1/00015—Manufacture or treatment of devices or systems in or on a substrate for manufacturing microsystems
- B81C1/00023—Manufacture or treatment of devices or systems in or on a substrate for manufacturing microsystems without movable or flexible elements
- B81C1/00047—Cavities
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B81—MICROSTRUCTURAL TECHNOLOGY
- B81C—PROCESSES OR APPARATUS SPECIALLY ADAPTED FOR THE MANUFACTURE OR TREATMENT OF MICROSTRUCTURAL DEVICES OR SYSTEMS
- B81C2201/00—Manufacture or treatment of microstructural devices or systems
- B81C2201/01—Manufacture or treatment of microstructural devices or systems in or on a substrate
- B81C2201/0101—Shaping material; Structuring the bulk substrate or layers on the substrate; Film patterning
- B81C2201/0102—Surface micromachining
- B81C2201/0104—Chemical-mechanical polishing [CMP]
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B81—MICROSTRUCTURAL TECHNOLOGY
- B81C—PROCESSES OR APPARATUS SPECIALLY ADAPTED FOR THE MANUFACTURE OR TREATMENT OF MICROSTRUCTURAL DEVICES OR SYSTEMS
- B81C2201/00—Manufacture or treatment of microstructural devices or systems
- B81C2201/01—Manufacture or treatment of microstructural devices or systems in or on a substrate
- B81C2201/0101—Shaping material; Structuring the bulk substrate or layers on the substrate; Film patterning
- B81C2201/0102—Surface micromachining
- B81C2201/0105—Sacrificial layer
- B81C2201/0108—Sacrificial polymer, ashing of organics
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B81—MICROSTRUCTURAL TECHNOLOGY
- B81C—PROCESSES OR APPARATUS SPECIALLY ADAPTED FOR THE MANUFACTURE OR TREATMENT OF MICROSTRUCTURAL DEVICES OR SYSTEMS
- B81C2201/00—Manufacture or treatment of microstructural devices or systems
- B81C2201/01—Manufacture or treatment of microstructural devices or systems in or on a substrate
- B81C2201/0101—Shaping material; Structuring the bulk substrate or layers on the substrate; Film patterning
- B81C2201/0128—Processes for removing material
- B81C2201/013—Etching
- B81C2201/0132—Dry etching, i.e. plasma etching, barrel etching, reactive ion etching [RIE], sputter etching or ion milling
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B82—NANOTECHNOLOGY
- B82Y—SPECIFIC USES OR APPLICATIONS OF NANOSTRUCTURES; MEASUREMENT OR ANALYSIS OF NANOSTRUCTURES; MANUFACTURE OR TREATMENT OF NANOSTRUCTURES
- B82Y40/00—Manufacture or treatment of nanostructures
Definitions
- the present invention relates to a method for manufacturing a hollow structure.
- Patent Documents 1 and 2 Conventionally, a semiconductor device having a structure in which a hollow air gap is formed and a hollow structure such as a MEMS device are known (for example, see Patent Documents 1 and 2).
- a sacrificial film process is generally used. Specifically, first, a sacrificial film made of polyimide or the like is embedded on a lower structure having a groove or the like, and an upper structure is formed on the sacrificial film. Next, an air gap is formed by removing the sacrificial film.
- a polyamic acid that is a precursor of polyimide is dissolved in an organic solvent to form a polyamic acid solution. Then, a polyamic acid solution is applied onto the lower structure and heated to, for example, about 350 ° C. to form a sacrificial film made of polyimide.
- the shape pattern of the grooves and the like formed in the lower structure is minute.
- the polyamide solution does not spread to the minute grooves or the like in coating, and a minute structure air gap is formed. Difficult to do.
- the embodiment of the present invention provides a method for manufacturing a hollow structure that can form an air gap with high accuracy by using a sacrificial film forming process having a low stress and high embedding property.
- a lower structure including a hollow shape is prepared, A sacrificial film made of an organic film is deposited on the lower structure by vapor deposition polymerization, and the recess shape is filled with the sacrificial film.
- FIG. 1A is a diagram illustrating an example of a lower structure preparation process.
- FIG. 1B is a diagram illustrating an example of a sacrificial film forming process.
- FIG. 1C is a diagram illustrating an example of the unnecessary portion removing process.
- FIG. 1D is a diagram showing an example of the upper structure forming process.
- FIG. 1E is a diagram illustrating an example of a sacrificial film removal process. It is the figure which showed an example of the sacrificial film formation process using the vapor deposition polymerization method of the manufacturing method of the hollow structure which concerns on Embodiment 1 of this invention.
- FIG. 1A is a diagram illustrating an example of a lower structure preparation process.
- FIG. 1B is a diagram illustrating an example of a sacrificial film forming process.
- FIG. 1C is a diagram illustrating an example of the unnecessary portion removing process.
- FIG. 1D is a diagram showing an example of the upper structure forming
- FIG. 2A is a diagram illustrating an example of a film formation apparatus that forms a resin film using a vapor deposition polymerization method.
- FIG. 2B is a diagram showing an example of monomers as raw materials and their reactions. It is the figure which showed the state which embedded the hollow shape by the vapor deposition polymerization method. It is the figure which showed an example of the manufacturing method of the hollow structure which concerns on Embodiment 2 of this invention.
- FIG. 4A is a diagram showing an example of the lower structure preparation process.
- FIG. 4B shows an example of a sacrificial film forming process.
- FIG. 4C is a diagram illustrating an example of the unnecessary portion removing process.
- FIG. 4D is a diagram showing an example of the sacrificial film after the unnecessary portion removing process is completed.
- FIG. 4E is a diagram showing an example of the upper structure forming process.
- FIG. 4F illustrates an example of the sacrificial film removal process. It is the figure which showed an example of the manufacturing method of the hollow structure which concerns on Embodiment 3 of this invention.
- FIG. 5A is a diagram showing an example of the lower structure preparation process.
- FIG. 5B is a diagram illustrating an example of a sacrificial film formation step and a planarization step.
- FIG. 5C is a diagram showing an example of the first upper structure forming process.
- FIG. 5D is a diagram illustrating an example of a second upper structure forming process.
- FIG. 5E shows an example of the sacrificial film removal process.
- FIG. 1 is a diagram showing an example of a method for manufacturing a hollow structure according to Embodiment 1 of the present invention.
- FIG. 1A is a diagram illustrating an example of a lower structure preparation process.
- the lower structure preparation step the lower structure 30 having the concavo-convex pattern 20 is prepared.
- the protrusions 21 are formed on the substrate 10 with a predetermined interval, and the recess-shaped part 22 is formed between the protrusions 21 to form the uneven pattern 20.
- the substrate 10 constitutes a bottom surface of the lower structure 30 and serves as a reference surface of the lower structure 30.
- the substrate 10 may be composed of various materials including a semiconductor material, but may be a silicon substrate composed of silicon, for example. Further, if necessary, an SOI (Silicon on Insulator) substrate or the like may be used as the substrate 10.
- SOI Silicon on Insulator
- the concavo-convex pattern 20 is a concavo-convex pattern formed on the surface of the substrate 10, and includes a protruding portion 21 and a recessed portion 22.
- the concavo-convex pattern 20 may be configured in various shapes depending on the use of the hollow structure.
- the recessed portion 22 is formed on the side surface of the protruding portion 21.
- the protruding portion 21 is a protruding structure provided to form the concavo-convex pattern 20 on the surface of the substrate 10.
- the protrusion 21 may be made of various materials depending on the application as long as the predetermined uneven pattern 20 can be formed on the surface of the substrate 10.
- the protrusion 21 may be made of a metal material such as copper (Cu) or tungsten (W), or may be made of a semiconductor material such as Si or an insulating material such as SiO 2 .
- the material used for the protrusion 21 may be selected including the electrical properties, chemical properties, mechanical strength, etc. in addition to the shape.
- the protruding portion 21 when it is desired to configure the protruding portion 21 with a conductor, a metal material such as Cu or W may be used, and when it is desired to configure with an insulator, an insulating material such as SiO 2 may be used.
- a metal material such as Cu or W
- an insulating material such as SiO 2
- the protruding portion 21 By forming the protruding portion 21, the portion where the protruding portion 21 is not formed inevitably becomes the recessed shape portion 22, so that the shape of the protruding portion 21 is appropriately determined in relation to the recessed shape portion 22. You can do it.
- the depth of the hollow of the hollow shape part 22 can be adjusted by changing the height of the protrusion part 21.
- the upper surface of the protruding portion 21 forms a horizontal surface
- the side surface forms a vertical surface.
- these shapes may be appropriately changed according to the application.
- the side surface may be an inclined surface
- the recessed portion 22 may be configured to form a tapered groove or hole.
- the hollow portion 22 may be a groove or a hole such as a through hole.
- a groove (trench) and a hole (via) are mainly formed as a recessed portion 22.
- MEMS Micro Electro Mechanical Systems
- the hollow shape portion 22 is configured in various shapes according to applications.
- the hollow shape part 22 may be comprised by various shapes according to the use of a hollow structure.
- FIG. 1A shows a state in which the lower structure 30 in which the concavo-convex pattern 20 is formed in advance is prepared, but the lower structure 30 is prepared by performing the above-described etching process. It may be.
- the lower structure preparation step may be called a lower structure formation step.
- the lower structure 30 forms the concavo-convex pattern 20 including the recessed portion 22 by forming the protruding portion 21 on the substrate 10, but if there is a processing technique, Alternatively, the lower structure 30 may be formed using only the material constituting the protrusion 22.
- the lower structure 30 can be prepared by various methods as long as a desired shape can be realized as a whole.
- FIG. 1B is a diagram showing an example of a sacrificial film forming process.
- a sacrificial film 40 made of an organic film is deposited on the surface of the lower structure 30 by vapor deposition polymerization.
- the recess-shaped portion 22 is embedded with the sacrificial film 40, and further, the sacrificial film 40 is formed on the upper surface of the protruding portion 22, and the concavo-convex pattern 20 is covered with the sacrificial film 40.
- an organic film is used as the sacrificial film 40, and the sacrificial film 40 is formed by vapor deposition polymerization.
- the sacrificial film 40 may be various polymer films, but may be a polyimide film, for example.
- a polyamic acid solution is applied onto the surface of the lower structure 30 and heated at a temperature of about 350 ° C. to imidize to form a polyimide film.
- the polyimide film contracts and stress is generated in the polyimide film itself.
- the width of the hollow portion 22 is several tens of micrometers, and the depth is on the order of several micrometers, such as several hundreds of micrometers.
- a level on the order of nm such as the width of the recessed portion 22 is several tens of nm and the depth is several hundred nm.
- the polyamic acid solution does not sufficiently enter the depression-shaped portion 22 in the application to the depression-shaped portion 22 of such nm order level.
- the sacrificial film forming step is performed by a vapor deposition polymerization method.
- FIG. 2 is a diagram showing an example of a sacrificial film forming process using the vapor deposition polymerization method of the hollow structure manufacturing method according to Embodiment 1 of the present invention.
- FIG. 2A is a view showing an example of a film forming apparatus for forming a resin film using vapor deposition polymerization
- FIG. 2B is an example of monomers as raw materials and their reactions.
- FIG. 2A shows a state where two substrates 10 are placed in the chamber 70.
- the chamber 70 includes a premixing chamber 71 and a processing chamber 72, both of which are partitioned by a partition wall 73 in which an opening 74 is formed.
- a supply port 76 communicating with the monomer supply units 80 and 81 is formed in the side wall 75 opposite to the partition wall 73 of the premixing chamber 71.
- the monomer supply units 80 and 81 are small chambers for evaporating the monomer and supplying the monomer to the premixing chamber 71, and have a carrier gas supply port 82 on the opposite side of the supply port 76.
- An exhaust port 78 is formed in the side wall 77 on the opposite side of the partition wall 73 of the processing chamber 72.
- the chamber 70 and the monomer supply units 80 and 81 are entirely covered with the heater 90 except for the exhaust port 78 and the carrier gas supply port 82, and are configured by a hot wall system.
- one monomer supply unit 80 is supplied with pyromellitic anhydride (PMDA), and the other monomer supply unit 81 is supplied with oxydianiline (ODA) as a monomer.
- PMDA pyromellitic anhydride
- ODA oxydianiline
- PMDA is heated by the heater 90 and evaporated in the monomer supply unit 80, and is carried by the N 2 carrier gas supplied from the carrier gas supply port 82. Steam is supplied into the premixing chamber 71 through the supply port 76.
- ODA is also heated by the heater 90 in the monomer supply unit 81 and evaporated, and is transported by the N 2 carrier gas supplied from the carrier gas supply port 82, and is supplied into the premixing chamber 71 through the supply port 76. Supplied in the state of steam.
- the PMDA molecule 100 and the ODA molecule 101 supplied to the premixing chamber 71 are mixed in the premixing chamber 71 and moved into the processing chamber 72 from the opening 74 formed in the partition wall 73.
- PMDA molecules 100 and ODA molecules 101 supplied into the processing chamber 72 adhere to the surface of the substrate 10. Then, a molecular level reaction is performed on the surface of the substrate 10 to generate a polyamic acid (polyamic acid) by polymerization, and then dehydrated and bonded with polyimide to form a polyimide film.
- dehydration occurs whenever the PMDA molecule 100 and the ODA molecule 101 react, so that the dehydration remains at the molecular level until tired. And since it dehydrates and accumulates on the surface of the substrate 10 in a state where a molecular layer of the polyimide film is generated, the film formation is performed in a state where the stress generated in the polyimide film is extremely low.
- the vapor deposition polymerization method is a dry film formation in a vacuum, unlike a film formation method in which a polyamic acid solution is applied to the whole and heated to perform a large amount of dehydration at a stretch, a low stress film formation is performed. It can be performed.
- the chamber including the premixing chamber 71 and the processing chamber 72 is heated to a temperature suitable for performing the vapor deposition reaction by the heater 90. Further, the processing chamber 72 is exhausted from the exhaust port 78 by a vacuum pump or the like, and the inside is kept in a vacuum.
- FIG. 2 shows an example in which the sacrificial film forming step is performed by placing two substrates 10 on the processing chamber 71.
- the sacrificial film forming step may be performed by single wafer processing with one substrate 10 or, conversely, batch processing in which several tens of substrates 10 are processed at once using a vertical heat treatment furnace. It may be done at.
- a film forming method various methods may be used as long as a vapor deposition polymerization method can be used.
- the sacrificial film forming step can be performed by various film forming methods and film forming apparatuses by using the vapor deposition polymerization method.
- FIG. 3 is a view showing a state in which a hollow shape is embedded by vapor deposition polymerization.
- the hollow shape shown in FIG. 3 is a minute hollow shape having an opening width of about 20 nm and a depth of about 200 nm.
- FIG. 3 shows that there is no void or the like, and the depression is embedded with very good coverage.
- the sacrificial film 40 is embedded in the hollow portion 22, but as described with reference to FIGS. 2 and 3, the sacrificial film 40 is deposited using the vapor deposition polymerization method, thereby reducing the stress.
- the sacrificial film 40 can be formed.
- the recess-shaped portion 22 has an opening width and depth on the order of nanometers. For example, even if the opening width is on the order of 10 to 100 nm and the depth is on the order of 1 to 999 nm, the sacrificial film 40 is embedded with good coverage. It can be performed.
- FIG. 1C is a diagram showing an example of an unnecessary portion removing process.
- the unnecessary process removing process an unnecessary part of the sacrificial film 40 formed on the uneven pattern 20 of the lower structure 30 is removed.
- an area protruding above the highest part of the protruding portion 21 is an unnecessary portion, and the protruding portion is removed to form a flat surface having the same height as the outer protruding portion 21. Yes.
- the unnecessary portion may be removed by an appropriate method such as chemical mechanical polishing (CMP) or dry etching.
- CMP chemical mechanical polishing
- dry etching dry etching
- FIG. 1D is a diagram showing an example of the upper structure forming process.
- the upper structure 50 is formed on the lower structure 30 from which unnecessary portions of the sacrificial film 40 are removed.
- the upper structure 50 is formed, for example, by depositing a cover layer.
- an upper structure 50 is formed as a cover layer covering the flat surface on the flat surface formed by the upper surface of the protruding portion 21 and the upper surface of the sacrificial film 40 filled in the hollow shape portion 22. Is formed.
- the upper structure 50 may be composed of various materials, but may be composed of, for example, a silicon oxide film (SiO 2 ) or a polysilicon film.
- the upper structure 50 can be formed using a film forming process of a general semiconductor manufacturing process.
- An opening 51 may be formed in a part of the upper structure 50.
- the sacrificial film 40 is exposed from the opening 51.
- a medium for removing the sacrificial film 40 can be supplied to the sacrificial film 40.
- the opening 51 may be formed by various methods. For example, a resist pattern may be formed on the upper structure 50 and a part of the upper structure 50 may be removed by etching to form the opening 51.
- FIG. 1E is a diagram illustrating an example of a sacrificial film removal process.
- a medium for removing the sacrificial film 40 is supplied from the opening 51, and the sacrificial film 40 is removed.
- the sacrificial film 40 may be removed by, for example, ashing using an oxygen gas (O 2 ) that is an ashing gas, or dissolving and removing using a solution (remover).
- O 2 oxygen gas
- oxygen gas is supplied from the opening 51, and the sacrificial film 40 is burned to be ashed.
- the remover is supplied from the opening 51 to dissolve and remove the sacrificial film 40.
- a hollow structure As shown in FIG. 1E, by removing the sacrificial film 40, a gap is formed between the lower structure 30 and the upper structure 50, and a hollow structure is formed.
- a hollow structure can be manufactured with high precision by forming the sacrificial film 40 using the vapor deposition polymerization method.
- FIG. 4 is a diagram showing an example of a method for manufacturing a hollow structure according to Embodiment 2 of the present invention.
- symbol is attached
- FIG. 4A is a diagram showing an example of the lower structure preparation process. Since the lower structure preparation step is the same as that in FIG. 1A of the method for manufacturing the hollow structure according to the first embodiment, the same reference numerals are given to the respective constituent elements and the description thereof is omitted.
- FIG. 4B shows an example of the sacrificial film forming process. Since the sacrificial film forming step is also the same as that in FIG. 1B of the method for manufacturing the hollow structure according to the first embodiment, the same reference numerals are assigned to the respective constituent elements and the description thereof is omitted.
- FIG. 4C is a diagram showing an example of the unnecessary part removing step.
- a photoresist film 60 is formed on the sacrificial film 40 formed by vapor deposition polymerization, and the photoresist film 60 is patterned by exposure to form an opening 61.
- the sacrificial film 40 is etched using the patterned photoresist film 60 as a mask, and an opening 41 is formed.
- FIG. 4D is a diagram showing an example of the sacrificial film after the unnecessary portion removing process is completed. Openings 41 are formed at both ends of the sacrificial film 40, and a part of the upper surface of the protruding portion 21 at both ends is exposed to form a concavo-convex pattern.
- the unnecessary portion removing step it is possible to pattern the sacrificial film 40 by removing an unnecessary portion as a pattern of the sacrificial film 40 as well as merely flattening. Thereby, an air gap can be comprised in various shapes.
- FIG. 4E is a diagram showing an example of the upper structure forming process.
- the upper structure 52 is formed on the surface of the lower structure 30 including the concavo-convex pattern of the sacrificial film 40 formed in the unnecessary portion removing step.
- the upper structure 52 may be formed as a cover layer that covers the lower structure 30 including the sacrificial film 40.
- the lower surface is configured in a shape corresponding to the concavo-convex pattern. That is, in the first embodiment, the lower surface of the upper structure 50 is a flat surface, but in the second embodiment, the lower surface of the upper structure 50 is configured to embed the opening 41.
- the upper structure forming step in the second embodiment is the same as that in the first embodiment except that the upper structure 52 may be a film used in the semiconductor manufacturing process of a SiO 2 film or a polysilicon film. is there. Therefore, the description is omitted.
- an opening 53 for exposing the sacrificial film 40 is formed in a part of the upper structure 52. Since this point is the same as that of the first embodiment, the description thereof is omitted.
- FIG. 4F shows an example of the sacrificial film removal process.
- the sacrificial film removal step the sacrificial film 40 is removed, and a gap (air gap) is formed between the upper structure 52 and the lower structure 30.
- the shape of the air gap is such that the upper structure 52 is formed further upward, and the air gap 23 is larger than that reflecting the hollow shape portion 22 of the first embodiment.
- the sacrificial film 40 is patterned in the unnecessary portion removing process of the sacrificial film 40, thereby changing the shape of the air gap 23 to various shapes. be able to.
- the sacrificial film 40 has been described with reference to an example in which the sacrificial film 40 is configured as a pattern having openings 41 at both ends.
- various patterns can be configured according to applications.
- FIG. 5 is a diagram showing an example of a method for manufacturing a hollow structure according to Embodiment 3 of the present invention.
- the method for manufacturing a hollow structure according to the third embodiment an example of manufacturing a hollow structure having a more complicated shape than those of the first and second embodiments will be described.
- FIG. 5A is a diagram showing an example of the lower structure preparation process.
- FIG. 5A shows a state in which a lower structure 31 configured by forming an uneven pattern 25 on a substrate 15 is prepared.
- the substrate 15 is composed of three layers: a silicon substrate 16, a metal wiring layer 17, and an insulating layer 18.
- a concavo-convex pattern 25 including a protruding portion 26 and a recessed portion 27 is formed on the surface of the substrate 15, that is, on the surface of the insulating layer 18.
- the protrusion part 26 may be comprised from metal materials, such as gold
- the protruding portion 26 may be formed by plating.
- the lower structure preparation process in FIG. 5A may be referred to as a plating process.
- FIG. 5B is a diagram showing an example of a sacrificial film formation step and a planarization step.
- a sacrificial film 45 is formed on the lower structure 31 so as to embed the concave / convex pattern 25 including the recessed portion 27, and the surface of the sacrificial film 45 is further flattened.
- FIG. 5B shows the lower structure 31 and the sacrificial film 45 that have passed through FIGS. 1B and 1C of the first embodiment.
- the sacrificial film 45 is formed by a vapor deposition polymerization method. Thereby, the sacrificial film 45 with low stress and good coverage can be formed. As the sacrificial film 45, various organic films that can be formed by vapor deposition polymerization are applied.
- the sacrificial film 45 may be a polyimide film.
- FIG. 5C is a diagram showing an example of the first upper structure forming process.
- the first upper structure 55 is formed so as to connect the two inner protrusions 26 to each other.
- the first upper structure 55 is made of a metal material such as gold, like the protruding portion 26.
- the first upper structure 55 has the height of the protrusion 26 and the sacrificial film 45 by repeating the plating process, the sacrificial film forming process and the planarization process shown in FIGS. 5A and 5B a plurality of times.
- plating is performed on the entire surface, and a pattern is formed by etching.
- the aspect ratio of the hollow portion 27 is increased.
- the sacrificial film 45 is formed using the vapor deposition polymerization method. Therefore, the sacrificial film 45 can be deposited with high embedding without forming voids on the side and bottom surfaces.
- FIG. 5D is a diagram showing an example of the second upper structure forming process.
- sacrifice is performed to fill the protrusions 26 at both ends and the recess-shaped part 27 by the plating process, the sacrificial film forming process, and the planarization process shown in FIGS.
- the entire surface is plated and the second upper structure 56 is patterned by etching.
- the second upper structure 56 is different from the first upper structure 55 in that an opening 57 is formed. This is because the upper structure 56 can be patterned into an arbitrary shape, so that the upper structure 56 can have various shapes depending on the application.
- a double side wall and an upper surface are formed by the second upper structure forming step.
- FIG. 5E shows an example of the sacrificial film removal process.
- oxygen gas, a solution, or the like for removing the sacrificial film 45 is supplied from the opening 57, and the sacrificial film 45 is removed by decomposition and / or dissolution.
- the air gap 28 is formed between the lower structure 31 and the first and second upper structures 55 and 56.
- 5C to 5E no opening is shown in the upper structure 55.
- the sacrificial film 45 between the upper structure 55 and the lower structure 31 is also formed in the opening 57 in the sacrificial film removing step.
- the removal medium can be removed at a time by supplying the removal medium.
- the air gap can be formed with high accuracy according to the method for manufacturing a hollow structure according to this embodiment.
- the substrate 15 can be appropriately selected depending on the application, and may be, for example, the substrate 15 made of only the silicon substrate 16.
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Abstract
Description
蒸着重合法により、前記下部構造体上に有機膜からなる犠牲膜が堆積され、前記窪み形状が前記犠牲膜で埋め込まれる。
不要部分が除去された前記犠牲膜上に上部構造体が形成される。
20、25 凹凸形状パターン
21、26 突出部
22、27 窪み形状部
30、31 下部構造体
40、45 犠牲膜
41、51、53、57 開口部
50、52、55、56 上部構造体
図1は、本発明の実施形態1に係る中空構造体の製造方法の一例を示した図である。図1(A)は、下部構造体用意工程の一例を示した図である。下部構造体用意工程においては、凹凸形状パターン20を有する下部構造体30が用意される。下部構造体30は、基板10上に突出部21が所定間隔を有して形成され、突出部21の間に窪み形状部22が形成されて凹凸形状パターン20が形成される。
図4は、本発明の実施形態2に係る中空構造体の製造方法の一例を示した図である。なお、実施形態2に係る中空構造体の製造方法において、実施形態1で説明したのと同様の構成要素については、同一の符号を付し、その説明を省略する。
図5は、本発明の実施形態3に係る中空構造体の製造方法の一例を示した図である。実施形態3に係る中空構造体の製造方法においては、実施形態1、2よりも複雑な形状の中空構造体を製造する例について説明する。
Claims (11)
- 窪み形状を含む下部構造体を用意し、
蒸着重合法により、前記下部構造体上に有機膜からなる犠牲膜を堆積させ、前記窪み形状を前記犠牲膜で埋め込み、
前記犠牲膜の不要部分を除去し、
不要部分が除去された前記犠牲膜上に上部構造体を形成し、
前記犠牲膜を除去し、前記下部構造体と前記上部構造体との間に空隙を形成する工程、を含む中空構造体の製造方法。 - 前記犠牲膜として、ポリイミド膜を用いて前記窪み形状を埋め込む請求項1に記載の中空構造体の製造方法。
- 前記犠牲膜の不要部分を除去する工程は、前記窪み形状よりも上方に堆積した前記犠牲膜を除去して平坦面を形成する工程を含む請求項1に記載の中空構造体の製造方法。
- 前記平坦面を形成する工程は、化学機械研磨又はドライエッチングにより行われる請求項3に記載の中空構造体の製造方法。
- 前記上部構造体を形成する工程は、前記平坦面上にカバー層を形成する工程を含む請求項3に記載の中空構造体の製造方法。
- 前記犠牲膜の不要部分を除去する工程は、前記犠牲膜上にレジストパターンを形成して不要部分を除去し、前記犠牲膜をパターニングする工程を含む請求項1に記載の中空構造体の製造方法。
- 前記上部構造体を形成する工程は、パターニングされた前記犠牲膜上にカバー層を形成する工程を含む請求項6に記載の中空構造体の製造方法。
- 前記空隙を形成する工程における前記犠牲膜の除去は、アッシング又は溶解液の供給により行われる請求項1に記載の中空構造体の製造方法。
- 前記上部構造体を形成する工程は、前記カバー層の一部に、前記犠牲層の上面を露出させる開口を形成する工程を更に含み、
前記空隙を形成する工程における前記犠牲膜の除去は、前記開口からアッシング用ガス又は溶解液を供給することにより行われる請求項5に記載の中空構造体の製造方法。 - 前記窪み形状は、ナノメールオーダーの開口幅と深さを有して加工されている請求項1に記載の中空構造体の製造方法。
- 前記開口幅は、10~100nmの範囲に加工され、
前記深さは、1~999nmの範囲に加工されている請求項10に記載の中空構造体の製造方法。
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JP2014188656A (ja) | 2014-10-06 |
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US20160280536A1 (en) | 2016-09-29 |
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