USPatent applicationPatented

Method of fabricating fin structure

Granted 8 May 2018 · no office action yet

Assignee: United Microelectronics Corporation

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Inventors: Chih-Hsun Lin, Li-Chieh Hsu, Kun-Ju Li, Hsin-Jung Liu +2 · Examiner: Nadine Norton · AU 1713 · TC 1700

Application· this page
15/587,228
filed 4 May 2017
Publication
Not published
not published
Patent
US 9,966,263
granted 8 May 2018

Life of the application

5 dated events
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Abstract

A method of fabricating fin structure is provided. A patterned catalyst layer and a patterned passivation layer extending along a first direction are formed on a substrate. The patterned passivation layer is located on the patterned catalyst layer. A carbon layer is formed on at least one side of the patterned catalyst layer and includes hollow carbon tubes arranged along the first direction. Each hollow carbon tube extends along a second direction. A removal process is performed to remove the top and a portion of the bottom of each hollow carbon tube closest to the substrate, so that remnants are left and serve as a mask layer. Two adjacent remnants form a stripe pattern extending along the second direction. The patterned passivation layer and the patterned catalyst layer are removed. The pattern of the mask layer is transferred to the substrate to form fin structures. The mask layer is removed.

Description

11 parts
›CROSS-REFERENCE TO RELATED APPLICATION

This application claims the priority benefit of China application serial no. 201710236563.4, filed on Apr. 12, 2017. The entirety of the above-mentioned patent application is hereby incorporated by reference herein and made a part of this specification.

BACKGROUND OF THE INVENTION
›Field of the Invention

The invention relates to a method of fabricating a fin structure.

›Description of Related Art

As semiconductor components continuously decrease in sizes, three-dimensional multi-gate structures such as fin field-effect transistor (FinFET) have been developed to replace complementary metal-oxide-semiconductor (CMOS) components. The structural feature of FinFETs lies in a silicon-based fin structure that extends upwards from a surface of a semiconductor substrate in a direction perpendicular to the surface of the semiconductor substrate. According to the conventional FinFET technology, however, it is difficult to control the dimensional accuracy of the fin structures, and spaces between the fin structures are also subject to certain limitations. As semiconductor components have been developed to achieve high integration, how to accurately control the dimensions of the fin structures and reduce the spaces between the fin structures have become an issue that needs to be solved.

›SUMMARY OF THE INVENTION

The invention provides a method of fabricating a fin structure to accurately control dimensions of the fin structure and obtain the fin structures with smaller spaces.

The invention provides a method of fabricating a fin structure, and the method includes a step of forming a patterned catalyst layer and a patterned passivation layer on a substrate. The patterned catalyst layer and the patterned passivation layer extend along a first direction. The patterned passivation layer is located on the patterned catalyst layer. A carbon layer is formed on at least one side of the patterned catalyst layer. The carbon layer includes a plurality of hollow carbon tubes arranged along the first direction, and each of the hollow carbon tubes extends along a second direction. A removal process is performed to remove a top of each of the hollow carbon tubes and a portion of a bottom of each of the hollow carbon tubes closest to the substrate, such that a plurality of remnants are left and serve as a mask layer. Two adjacent remnants of the remnants form a stripe pattern extending along the second direction. The patterned passivation layer and the patterned catalyst layer are removed. A pattern of the mask layer is transferred to the substrate to form a plurality of fin structures. The mask layer is removed.

In an embodiment of the invention, the patterned catalyst layer includes a first catalyst pattern and a second catalyst pattern. The carbon layer is formed between the first catalyst pattern and the second catalyst pattern.

In an embodiment of the invention, the patterned passivation layer further covers a second side of the first catalyst pattern and a second side of the second catalyst pattern, such that the hollow carbon tubes grow along the second direction from a first side of the first catalyst pattern to the second side of the second catalyst pattern.

In an embodiment of the invention, the patterned catalyst layer further includes a third catalyst pattern located between the first catalyst pattern and the second catalyst pattern. The patterned passivation layer further covers the second side of the first catalyst pattern and a first side of the second catalyst pattern.

In an embodiment of the invention, the hollow carbon tubes are connected by growing along the second direction from the first side of the first catalyst pattern and growing along a negative second direction from a second side of the third catalyst pattern, and connected by growing along the second direction from a first side of the third catalyst pattern and growing along the negative second direction from the second side of the second catalyst pattern.

In an embodiment of the invention, the method further includes a step of forming a hard mask layer on the substrate before the patterned catalyst layer is formed.

In an embodiment of the invention, the method further includes a step of patterning the hard mask layer with use of the mask layer as a mask before the pattern of the mask layer is transferred to the substrate, so as to form a patterned hard mask layer. The patterned hard mask layer is removed after the fin structures are formed.

In an embodiment of the invention, a material of the patterned hard mask layer is different from a material of the patterned passivation layer.

In an embodiment of the invention, a method of removing the patterned passivation layer includes performing an isotropic etching process, an anisotropic etching process, or a combination thereof.

In an embodiment of the invention, the hard mask layer includes a conductive material, a dielectric material, or a combination thereof.

In an embodiment of the invention, the hard mask layer includes platinum, silicon oxide, silicon nitride, titanium oxide, aluminum oxide, copper oxide, silicon oxynitride, silicon carbonitride, or silicon oxycarbonitride.

In an embodiment of the invention, the patterned passivation layer includes a conductive material, a dielectric material, or a combination thereof.

In an embodiment of the invention, the patterned passivation layer includes platinum, silicon oxide, silicon nitride, silicon oxynitride, silicon carbonitride, or silicon oxycarbonitride.

In an embodiment of the invention, the patterned catalyst layer includes metal or a metal alloy.

In an embodiment of the invention, the patterned catalyst layer includes iron, cobalt, nickel, copper, or an alloy thereof.

In an embodiment of the invention, the method further includes a step of performing an annealing process to the mask layer after the patterned passivation layer and the patterned catalyst layer are removed but before the pattern of the mask layer is transferred to the substrate.

In view of the above, according to the method of fabricating the fin structure provided herein, the fin structure is formed by patterning the substrate with use of the hollow carbon tubes as the mask layer, so as to accurately control the dimensions of the fin structure and obtain the fin structures with smaller spaces.

To make the aforementioned and other features and advantages of the invention more comprehensible, several embodiments accompanied with drawings are described in detail as follows.

›BRIEF DESCRIPTION OF THE DRAWINGS

The accompanying drawings are included to provide a further understanding of the invention, and are incorporated in and constitute a part of this specification. The drawings illustrate exemplary embodiments of the invention and, together with the description, serve to explain the principles of the invention.

FIG. 1 to FIG. 3 and FIGS. 4A / 4 B/ 4 C to FIGS. 8A / 8 B/ 8 C are schematic flow charts of a method of fabricating a fin structure according to a first embodiment of the invention, wherein

FIG. 4A to FIG. 8A are top views of a process of fabricating the fin structure;

FIG. 4B to FIG. 8B are front views of the process of fabricating the fin structure;

FIG. 4C to FIG. 8C are side views of the process of fabricating the fin structure.

FIG. 9 to FIG. 11 and FIGS. 12A / 12 B/ 12 C to FIGS. 16A / 16 B/ 16 C are schematic flow charts of a method of fabricating a fin structure according to a second embodiment of the invention, wherein

FIG. 12A to FIG. 16A are top views of a process of fabricating the fin structure;

FIG. 12B to FIG. 16B are front views of the process of fabricating the fin structure;

FIG. 12C to FIG. 16C are side views of the process of fabricating the fin structure.

FIG. 17 to FIG. 19 and FIGS. 20A / 20 B/ 20 C to FIGS. 25A / 25 B/ 25 C are schematic flow charts of a method of fabricating a fin structure according to a third embodiment of the invention, wherein

FIG. 20A to FIG. 25A are top views of a process of fabricating the fin structure;

FIG. 20B to FIG. 25B are front views of the process of fabricating the fin structure;

FIG. 20C to FIG. 25C are side views of the process of fabricating the fin structure.

FIG. 26 to FIG. 28 and FIGS. 29A / 29 B/ 29 C to FIGS. 34A / 34 B/ 34 C are schematic flow charts of a method of fabricating a fin structure according to a fourth embodiment of the invention, wherein

FIG. 29A to FIG. 34A are top views of a process of fabricating the fin structure;

FIG. 29B to FIG. 34B are front views of the process of fabricating the fin structure;

FIG. 29C to FIG. 34C are side views of the process of fabricating the fin structure.

›DESCRIPTION OF THE EMBODIMENTS · 1 of 5

Detailed embodiments of the invention are hereby provided for reference. Descriptions on the embodiments are provided in drawings. In the different embodiments provided below, same component numerals are used to show identical components in both the drawings and the descriptions. To keep the descriptions brief, descriptions of materials, forming methods, and so on are not repeated. In FIG. 4A to FIG. 8A , FIG. 12A to FIG. 16A , FIG. 20A to FIG. 25A , and FIG. 29A to FIG. 34A , a first direction D 1 may be, for example, a column direction, and a second direction D 2 may be, for example, a row direction. Nevertheless, the invention is not limited to the above.

FIG. 1 to FIG. 3 and FIGS. 4A / 4 B/ 4 C to FIGS. 8A / 8 B/ 8 C are schematic flow charts of a method of fabricating a fin structure according to a first embodiment of the invention.

Referring to FIG. 1 , a substrate 10 is provided. The substrate 10 may be a semiconductor substrate, a doped silicon substrate, an undoped silicon substrate, or a silicon-on-insulator (SOI) substrate. A dopant of the doped silicon may be a p-type dopant, an n-type dopant, or a combination thereof. A catalyst layer 11 is then formed on the substrate 10 . A material of the catalyst layer 11 includes metal or a metal alloy, such as iron, cobalt, nickel, copper, or a metal alloy thereof. A method of forming the catalyst layer 11 is, for example, a chemical vapor deposition or a physical vapor deposition. Afterwards, a patterned mask layer 12 is formed on the catalyst layer 11 . The patterned mask layer 12 exposes a portion of the catalyst layer 11 . A material of the patterned mask layer 12 is, for example, photoresist. The patterned mask layer 12 is formed by, for example, forming a photoresist layer on the catalyst layer 11 and then performing an exposure process and a development process on the photoresist layer.

Referring to FIG. 1 and FIG. 2 , the catalyst layer 11 is patterned through etching with use of the patterned mask layer 12 as a mask, for example, so as to form a patterned catalyst layer 11 e . The patterned catalyst layer 11 e includes a first catalyst pattern 11 a and a second catalyst pattern 11 b . The first catalyst pattern 11 a and the second catalyst pattern 11 b both have a first side 8 a and a second side 8 b . The first side 8 a of the first catalyst pattern 11 a is adjacent to the second side 8 b of the second catalyst pattern 11 b . The patterned mask layer 12 is removed afterwards.

A passivation layer 13 is formed on the substrate 10 to cover the patterned catalyst layer 11 e and the substrate 10 . A material of the passivation layer 13 includes a conductive material, a dielectric material, or a combination thereof. The conductive material is, for example, metal, a metal alloy, metal oxide, or a combination thereof. The dielectric material is, for example, oxide, nitride, oxynitride, carbonitride, or a combination thereof. A material of the passivation layer 13 is, for example, platinum, silicon oxide, silicon nitride, silicon oxynitride, silicon carbonitride, silicon oxycarbonitride, or a combination thereof. A method of forming the passivation layer 13 is, for example, a physical vapor deposition, a chemical vapor deposition, or a spin coating.

A patterned mask layer 14 is formed on the passivation layer 13 . A material of the patterned mask layer 14 is, for example, photoresist. The patterned mask layer 14 is formed by, for example, forming a photoresist layer on the passivation layer 13 and then performing an exposure process and a development process on the photoresist layer. The patterned mask layer 14 covers a portion of the passivation layer 13 above the patterned catalyst layer 11 e . An area of the portion of the passivation layer 13 covered by the patterned mask layer 14 is greater than an area of the patterned catalyst layer 11 e.

Referring to FIG. 2 and FIG. 3 , the passivation layer 13 is patterned by etching with use of the patterned mask layer 14 as a mask, for instance, so as to form a patterned passivation layer 13 a . The patterned passivation layer 13 a covers surfaces and the second sides 8 b of the first catalyst pattern 11 a and the second catalyst pattern 11 b and exposes the first sides 8 a of the first catalyst pattern 11 a and the second catalyst pattern 11 b . The patterned mask layer 14 is then removed.

Referring to FIG. 4A to FIG. 4C , the patterned catalyst layer 11 e and the patterned passivation layer 13 extend along the first direction D 1 . The second sides 8 b of the first catalyst pattern 11 a and the second catalyst pattern 11 b of the patterned catalyst layer 11 e are both covered by the patterned passivation layer 13 a . A carbon layer 15 is formed on the exposed first sides 8 a of the first catalyst pattern 11 a and the second catalyst pattern 11 b . In some embodiments, the carbon layer 15 is connected to the first side 8 a of the first catalyst pattern 11 a and separated from the second side 8 b of the second catalyst pattern 11 b by a space 20 . In some other embodiments, the carbon layer 15 is connected to the second side 8 b of the second catalyst pattern 11 b without any space between the carbon layer 150 and the second side 8 b . In some embodiments, the carbon layer 15 is attached to the substrate 10 due to a van der waal's force between the carbon layer 15 and the substrate 10 .

In some embodiments of the invention, the carbon layer 15 includes a plurality of hollow carbon tubes 16 . In some embodiments, the hollow carbon tubes 16 are cylindrical carbon nanotubes (CNT) and are formed by, for example, a chemical vapor deposition. The chemical vapor deposition includes a low pressure chemical vapor deposition (LPCVD. In some exemplary embodiments, the hollow carbon tubes 16 are formed by self-aligning and growing along a second direction D 2 from the first side 8 a of the first catalyst pattern 11 a to the second side 8 b of the second catalyst pattern 11 b through the LPCVD with use of a gas mixture of acetylene (C 2 H 2 ) and argon (Ar) under the circumstances where a pressure is lower than 500 torr and a temperature is lower than 500° C. The hollow carbon tubes 16 extend along the second direction D 2 and are arranged along the first direction D 1 . In some embodiments, the hollow carbon tubes 16 are arranged in an array. A space 25 exists between two adjacent hollow carbon tubes 16 and the substrate 10 . A cross-section of the space 25 is, for example, in a shape of a triangle, a fish tail, an inverted T, or a hanger. In some embodiments, an outer diameter D o of the hollow carbon tubes 16 ranges from 1 nm to 15 nm, a wall thickness t of the hollow carbon tubes 16 ranges from 0.3 nm to 5 nm, and a length L of the hollow carbon tubes 16 ranges from 10 nm to 100 nm.

›DESCRIPTION OF THE EMBODIMENTS · 2 of 5

Referring to FIG. 4A to 4C , FIG. 5A to 5C , a removal process is performed to remove a top 16 d and a portion 16 c of a bottom of each of the hollow carbon tubes 16 closest to the substrate 10 , and remnants 16 a and 16 b are left. The removal process is performed through carrying out a proper etching process, for instance. Two remnants 16 a and 16 b are left in each of the hollow carbon tubes 16 after the etching process is performed on the hollow carbon tubes 16 . An opening 21 is formed between the remnants 16 a and 16 b left in the same hollow carbon tube 16 , and a portion of the substrate 10 is exposed. In some embodiments, the cross-sections of remnants 16 a and 16 b are in a shape of a fan, a triangle, or a combination thereof. Surfaces of each of two remnants 16 a and 16 b in the same hollow carbon tube 16 are substantially same level and connected, and thus a stripe pattern 16 e extending along a second direction D 2 is formed. In other words, the remnant 16 a left in each of the hollow carbon tubes 16 is connected to the remnant 16 b left in an adjacent hollow carbon tube 16 , and thus the stripe pattern 16 e is formed. The remnant 16 b left in each of the hollow carbon tubes 16 is connected to the remnant 16 a left in an adjacent hollow carbon tube 16 , and thus the stripe pattern 16 e is formed. Since the remnant 16 a and the remnant 16 b respectively located on two ends do not have the adjacent remnant 16 b and the adjacent remnant 16 a , the remnants 16 a and 16 b located on the two ends respectively form an independent stripe pattern 16 e extending along the second direction D 2 . In other words, the stripe patterns 16 e formed by the remnants 16 a or/and the remnants 16 b extend along the second direction D 2 and are arranged along the first direction D 1 , and an opening 21 exists between two adjacent stripe patterns 16 e in the same row. In some embodiments of the invention, a plurality of stripe patterns 16 e form a mask layer 26 .

Referring to FIG. 5A to FIG. 5C and FIG. 6A to FIG. 6C , the patterned passivation layer 13 a , the first catalyst pattern 11 a , and the second catalyst pattern 11 b are removed to form an opening 23 between the remnants 16 a / 16 b in two adjacent columns, and a portion of the substrate 10 is exposed. A method of said removal is, for example, an etching process. The etching process includes an isotropic etching process, an anisotropic etching process, or a combination thereof. The mask layer 26 has the opening 21 and the opening 23 that expose a portion of the substrate 10 .

An annealing process is performed on the mask layer 26 to enhance properties of the mask layer 26 , such as bond energy of a C—C bond in the mask layer 26 and a C—Si van der waal's force existing between the mask layer 26 and the substrate 10 . The annealing process includes a rapid temperature process (RTP).

Referring to FIG. 7A to FIG. 7C and FIG. 8A to FIG. 8C , a portion of the substrate 10 exposed by the opening 21 located between two adjacent stripe patterns 16 e in the same column is removed by etching with use of the mask layer 26 as a mask, for example, so as to form a trench 22 in the substrate 10 . The substrate 10 exposed by the opening 23 located between two columns of the stripe patterns 16 is simultaneously removed to form a trench 24 in the substrate 10 . A fin structure 17 is formed on the substrate 10 located between two adjacent trenches 22 in the same column. The fin structures 17 extend along the second direction D 2 and are arranged along the first direction D 1 . Two adjacent columns of the fin structures 17 are separated by the trench 24 . The mask layer 26 is then removed through etching, for instance.

FIG. 9 to FIG. 11 and FIGS. 12A / 12 B/ 12 C to FIGS. 16A / 16 B/ 16 C are schematic flow charts of a method of fabricating a fin structure according to a second embodiment of the invention. A difference between this embodiment and the first embodiment of the invention lies in that a patterned catalyst layer 11 e provided in the present embodiment has three catalyst patterns ( 11 a / 11 b / 11 c ). Detailed descriptions are as follows.

Referring to FIG. 9 and FIG. 10 , a catalyst layer 11 and a patterned mask layer 12 are formed on a substrate 10 . The catalyst layer 11 is patterned by using the patterned mask layer 12 as a mask to form a patterned catalyst layer 11 e . The patterned catalyst layer 11 e includes a first catalyst pattern 11 a , a second catalyst pattern 11 b , and a third catalyst pattern 11 c . The third catalyst pattern 11 c is located between the first catalyst pattern 11 a and the second catalyst pattern 11 b . Each of the catalyst patterns 11 a , 11 b , and 11 c has a first side 8 a and a second side 8 b . The patterned mask layer 12 is then removed.

Referring to FIG. 10 and FIG. 11 , a passivation layer 13 is formed to cover the patterned catalyst layer 11 e and the substrate 10 . A patterned mask layer 14 is then formed on the passivation layer 13 . The passivation layer 13 is patterned by using the patterned mask layer 14 as a mask to form a patterned passivation layer 13 a . The patterned mask layer 14 is removed afterwards.

Referring to FIG. 11 , the patterned passivation layer 13 a covers surfaces of the first catalyst pattern 11 a , the second catalyst pattern 11 b , and the third catalyst pattern 11 c . The patterned passivation layer 13 a also covers the second side 8 b of the first catalyst pattern 11 a and the first side 8 a of the second catalyst pattern 11 b . The first side 8 a of the first catalyst pattern 11 a , the second side 8 b of the second catalyst pattern 11 b , and the first side 8 a and the second side 8 b of the third catalyst pattern 11 c are exposed.

Referring to FIG. 12A to FIG. 12C , a carbon layer 15 is formed between the first catalyst pattern 11 a and the third catalyst pattern 11 c and between the second catalyst pattern 11 b and the third catalyst pattern 11 c . The carbon layer 15 includes a plurality of hollow carbon tubes 16 . The carbon layer 15 is connected to the first side 8 a of the first catalyst pattern 11 a and the second side 8 b of the third catalyst pattern 11 c . The carbon layer 15 is also connected to the first side 8 a of the third catalyst pattern 11 c and the second side 8 b of the second catalyst pattern 11 b.

›DESCRIPTION OF THE EMBODIMENTS · 3 of 5

Specifically, in this embodiment of the invention, the hollow carbon tubes 16 located between the first catalyst pattern 11 a and the third catalyst pattern 11 c are connected by growing along the second direction D 2 from the first side 8 a of the first catalyst pattern 11 a and growing along a negative second direction D 2 from the second side 8 b of the third catalyst pattern 11 c . The hollow carbon tubes 16 located between the third catalyst pattern 11 c and the second catalyst pattern 11 b are connected by growing along the second direction D 2 from the first side 8 a of the third catalyst pattern 11 c and growing along the negative second direction D 2 from the second side 8 b of the second catalyst pattern 11 b.

A distance between the first catalyst pattern 11 a and the third catalyst pattern 11 c and/or a distance between the third catalyst pattern 11 c and the second catalyst pattern 11 b may be adjusted according to practical demands. For example, in some other embodiments where said distances are greater than those in the present embodiment, the hollow carbon tubes 16 located between the first catalyst pattern 11 a and the third catalyst pattern 11 c grow along the second direction D 2 from the first side 8 a of the first catalyst pattern 11 a and grows along the negative second direction D 2 from the second side 8 b of the third catalyst pattern 11 c . However, the hollow carbon tubes 16 are not connected, and spaces exist between the hollow carbon tubes 16 . The hollow carbon tubes 16 located between the third catalyst pattern 11 c and the second catalyst pattern 11 b grow along the second direction D 2 from the first side 8 a of the third catalyst pattern 11 c and grow along the negative second direction D 2 from the second side 8 b of the second catalyst pattern 11 b . The hollow carbon tubes 16 are not connected, and other spaces exist between the hollow carbon tubes.

A process similar to the process described in the first embodiment is then performed to form a fin structure 17 .

Referring to FIG. 13A to FIG. 13 c and FIG. 14A to FIG. 14C , atop 16 d and a portion 16 c of a bottom of each of the hollow carbon tubes 16 closest to the substrate 10 are removed, and a plurality of remnants 16 a and 16 b are left. An opening 21 exists between two remnants 16 a and 16 b left in the same hollow carbon tube 16 . In some embodiments of the invention, shapes of each of the remnants 16 a / 16 b , arrangements of the remnants 16 a / 16 b and adjacent remnants, and arrangements of the stripe pattern 16 e formed by the remnants are substantially the same as those provided in the first embodiment. To keep the descriptions brief, no further explanation will be provided hereinafter.

Referring to FIG. 14A to FIG. 14C , the patterned passivation layer 13 a and the patterned catalyst layer 11 e are removed to form an opening 23 between two adjacent columns of remnants 16 a / 16 b . A plurality of remnants 16 a or/and 16 b constitute a stripe pattern 16 e . A plurality of stripe patterns 16 e constitute a mask layer 26 . The mask layer 26 has an opening 21 and an opening 23 that expose a portion of the substrate 10 . An annealing process is performed to the mask layer 26 to enhance properties of the mask layer 26 .

Referring to FIG. 15A to FIG. 15C and FIG. 16A to FIG. 16C , the portion of the substrate 10 exposed by the opening 21 and the opening 23 are removed by using the mask layer 26 as a mask, so as to respectively form trenches 22 and 24 in the substrate 10 . A fin structure 17 is formed on the substrate 10 located between two adjacent trenches 22 in the same column. The fin structures 17 in two adjacent columns are separated by a trench 24 . The mask layer 26 is removed afterwards.

FIG. 17 to FIG. 19 and FIGS. 20A / 20 B/ 20 C to FIGS. 25A / 25 B/ 25 C are schematic flow charts of a method of fabricating a fin structure according to a third embodiment of the invention. This embodiment is similar to the first embodiment. A difference between this embodiment and the first embodiment lies in that a hard mask layer 18 is formed before the catalyst layer 11 is formed in this embodiment. Subsequent processes are then performed, and detailed descriptions are as follows.

Referring to FIG. 17 , the hard mask layer 18 is formed on the substrate 10 . A material of the hard mask layer 18 includes a conductive material, a dielectric material, or a combination thereof. The conductive material is, for example, metal, a metal alloy, a metal oxide, or a combination thereof. The dielectric material is, for example, oxide, nitride, oxynitride, carbonitride, or a combination thereof. The hard mask layer 18 is, for example, platinum, titanium oxide, aluminum oxide, copper oxide, silicon oxide, silicon nitride, silicon oxynitride, silicon carbonitride, silicon oxycarbonitride, or a combination thereof. A method of forming the hard mask layer 18 is, for example, a chemical vapor deposition. A catalyst layer 11 and a patterned mask layer 12 are then formed on the hard mask layer 18 .

Referring to FIG. 17 and FIG. 18 , the catalyst layer 11 is patterned by using the patterned mask layer 12 as a mask, so as to form a patterned catalyst layer 11 e . The patterned catalyst layer 11 e includes a first catalyst pattern 11 a and a second catalyst pattern 11 b . The patterned mask layer 12 is removed afterwards.

A passivation layer 13 is formed on the substrate 10 to cover the patterned catalyst layer 11 e and the substrate 10 . In some embodiments of the invention, a material of a passivation layer 13 is different from a material of a hard mask layer 18 . In some other embodiments of the invention, a material of a passivation layer 13 is identical to a material of a hard mask layer 18 . A patterned mask layer 14 is then formed on the passivation layer 13 .

Referring to FIG. 18 and FIG. 19 , the passivation layer 13 is patterned by using the patterned mask layer 14 as a mask to form a patterned passivation layer 13 a . The patterned passivation layer 13 a covers the surfaces and the second sides 8 b of the first catalyst pattern 11 a and the second catalyst pattern 11 b and exposes the first sides 8 a of the first catalyst pattern 11 a and the second catalyst pattern 11 b . Afterwards, the patterned mask layer 14 is removed.

›DESCRIPTION OF THE EMBODIMENTS · 4 of 5

Referring to FIG. 20A to FIG. 20C , as provided in the first embodiment of the invention, the carbon layer 15 including a plurality of hollow carbon tubes 16 is formed on the first sides 8 a of the first catalyst pattern 11 a and the second catalyst pattern 11 b . In some embodiments, the carbon layer 15 is connected to the first side 8 a of the first catalyst pattern 11 a and is separated from the second side 8 b of the second catalyst pattern 11 b by a space 20 . In some other embodiments, the carbon layer 15 is connected to the second side 8 b of the second catalyst pattern 11 b , and no space exists between the carbon layer 15 and the second side 8 b of the second catalyst pattern 11 b.

Referring to FIG. 21A to FIG. 21C and FIG. 22A to FIG. 22C , a top 16 d and a portion 16 c of a bottom of each of the hollow carbon tubes 16 closest to the substrate 10 are removed, such that a plurality of remnants 16 a and/or 16 b are left, and that a stripe pattern 16 e is formed. A plurality of the stripe patterns 16 e constitute a mask layer 26 . An opening 21 exists between two remnants 16 a and 16 b left in the same hollow carbon tube 16 . The patterned passivation layer 13 a and the patterned catalyst layer 11 e are then removed to form an opening 23 between two adjacent columns of remnants 16 a / 16 b . In other words, the mask layer 26 has the opening 21 and the opening 23 that expose a portion of the hard mask layer 18 . An annealing process is then performed on the mask layer 15 to enhance properties of the mask layer 26 .

Referring to FIG. 23A to FIG. 23C , the portion of the hard mask layer 18 exposed by the opening 21 and the opening 23 is removed to form a patterned hard mask layer 18 a . A method of said removal is, for example, an etching process. The etching process includes an anisotropic etching process. The patterned hard mask layer 18 a has an opening 27 and an opening 28 that expose a portion of the substrate 10 . The opening 27 and the opening 28 respectively correspond to the opening 21 and the opening 23 .

Referring to FIG. 24A to FIG. 24C and FIG. 25A to FIG. 25C , the portion of the substrate 10 exposed by the opening 27 and the opening 28 is removed by using the mask layer 26 and the patterned hard mask layer 18 a as a mask to respectively form trenches 22 and 24 . A fin structure 17 is formed on the substrate 10 located between two adjacent trenches 22 in the same column. Two adjacent columns of fin structures 17 are separated by the trench 24 . The mask layer 26 and the hard mask layer 18 are then removed. A method of said removal is, for example, an etching process, e.g., an isotropic etching process or an anisotropic etching process.

FIG. 26 to FIG. 28 and FIGS. 29A / 29 B/ 29 C to FIGS. 34A / 34 B/ 34 C are schematic flow charts of a method of fabricating a fin structure according to a fourth embodiment of the invention. This embodiment is similar to the second embodiment of the invention. A difference between this embodiment and the second embodiment lies in that a hard mask layer 18 is formed before a catalyst layer 11 is formed in this embodiment. Sequential processes are performed afterwards, and detailed descriptions are as follows.

Referring to FIG. 26 and FIG. 27 , the hard mask layer 18 , the catalyst layer 11 , and the patterned mask layer 12 are sequentially formed on the substrate 10 . The catalyst layer 11 is patterned by using the patterned mask layer 12 as a mask to form a patterned catalyst layer 11 e . The patterned catalyst layer 11 e includes a first catalyst pattern 11 a , a second catalyst pattern 11 b , and a third catalyst pattern 11 c . The patterned mask layer 12 is then removed.

Referring to FIG. 27 and FIG. 28 , a passivation layer 13 and a patterned mask layer 14 are formed. The passivation layer 13 is patterned by using the patterned mask layer 14 as a mask to form a patterned passivation layer 13 a . The patterned mask layer 14 is then removed.

Referring to FIG. 28 , as provided in the second embodiment of the invention, the patterned passivation layer 13 a covers the surface of the patterned catalyst layer 11 e . The patterned passivation layer 13 a also covers the second side 8 b of the first catalyst pattern 11 a and the first side 8 a of the second catalyst pattern 11 b . The first side 8 a of the first catalyst pattern 11 a , the second side 8 b of the second catalyst pattern 11 b , and the first side 8 a and the second side 8 b of the third catalyst pattern 11 c are exposed.

Referring to FIG. 29A to FIG. 29C , a carbon layer 15 is formed between the first catalyst pattern 11 a and the third catalyst pattern 11 c and between the second catalyst pattern 11 b and the third catalyst pattern 11 c . The carbon layer 15 includes a plurality of hollow carbon tubes 16 .

Referring to FIG. 30A to FIG. 30C , a top 16 d and a portion 16 c of a bottom of each of the hollow carbon tubes 16 closest to the substrate 10 are removed, such that a plurality of remnants 16 a and/or 16 b are left, and that a stripe pattern 16 e is formed. A plurality of the stripe patterns 16 e constitute a mask layer 26 . An opening 21 exists between two remnants 16 a and 16 b left in the same hollow carbon tube 16 .

Referring to FIG. 31A to FIG. 31C , the patterned passivation layer 13 a and the patterned catalyst layer 11 e are removed to form an opening 23 between two adjacent rows of remnants 16 a / 16 b . In other words, the mask layer 26 has the opening 21 and the opening 23 that expose a portion of the hard mask layer 18 . An annealing process is then performed to the mask layer 26 .

Referring to FIG. 32A to FIG. 32C , a portion of the hard mask layer 18 exposed by the opening 21 and the opening 23 is removed to form a patterned hard mask layer 18 a . The patterned hard mask layer 18 a has an opening 27 and an opening 28 that expose a portion of the substrate 10 . The opening 27 and the opening 28 respectively correspond to the opening 21 and the opening 23 .

Referring to FIG. 33A to FIG. 33C and FIG. 34A to FIG. 34C , the portion of the substrate 10 exposed by the opening 27 and the opening 28 is removed by using the mask layer 26 and the patterned hard mask layer 18 as a mask, so as to respectively form trenches 22 and 24 . A fin structure 17 is formed on the substrate 10 located between two adjacent trenches 22 in the same column. The fin structures 17 in two adjacent columns are separated by the trench 24 . The mask layer 26 and the hard mask layer 18 are then removed.

›DESCRIPTION OF THE EMBODIMENTS · 5 of 5

To sum up, according to the method of fabricating the fin structure provided herein, while the fin structure is being fabricated, the remnants formed by the hollow carbon tubes serve as the mask layer, or the remnants and the underlying the patterned hard mask layer together act as a mask. Thereby, the dimensional accuracy of the fin structures may be improved, and the fin structures with smaller spaces may be obtained.

Although the invention has been described with reference to the above embodiments, it will be apparent to one of ordinary skill in the art that modifications to the described embodiments may be made without departing from the spirit of the invention. Accordingly, the scope of the invention is defined by the attached claims not by the above detailed descriptions.

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Classifications

1 codes
IPC · International Patent Classification
Section H — Electricity
  • H10P76/40

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⤢ drag to zoomApr 2017Jul 2017Oct 2017Jan 2018Apr 2018Jul 2018USPTOApplicantNotice of allowance
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Pendency
1.0 y
369 days filing → grant
Office actions
0
none on record
Examiner
Nadine Norton
art unit 1713 · TC 1700
Citations: 8 back · 2 forward

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⤢ drag to zoom20182020202220242026202820302032203420362038Owner 1
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