Finfet device and method of forming and monitoring quality of the same
US-2017110567-A1 · Apr 20, 2017 · US
US2017194430A1 · US · A1
| Field | Value |
|---|---|
| Publication number | US-2017194430-A1 |
| Application number | US-201615395928-A |
| Country | US |
| Kind code | A1 |
| Filing date | Dec 30, 2016 |
| Priority date | Jan 5, 2016 |
| Publication date | Jul 6, 2017 |
| Grant date | — |
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The present disclosure provides methods for forming nanowire spacers for nanowire structures with desired materials in horizontal gate-all-around (hGAA) structures for semiconductor chips. In one example, a method of forming nanowire spaces for nanowire structures on a substrate includes performing a lateral etching process on a substrate having a multi-material layer disposed thereon, wherein the multi-material layer including repeating pairs of a first layer and a second layer, the first and second layers each having a first sidewall and a second sidewall respectively exposed in the multi-material layer, wherein the lateral etching process predominately etches the second layer through the second layer forming a recess in the second layer, filling the recess with a dielectric material, and removing the dielectric layer over filled from the recess.
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1 . A method of forming nanowire spaces for nanowire structures on a substrate comprising: performing a lateral etching process on a substrate having a multi-material layer disposed thereon, wherein the multi-material layer including repeating pairs of a first layer and a second layer, the first and second layers each having a first sidewall and a second sidewall respectively exposed in the multi-material layer, wherein the lateral etching process predominately etches the second layer through the second layer forming a recess in the second layer; filling the recess with a dielectric material; and removing the dielectric layer extending out of the recess. 2 . The method of claim 1 , further comprising: forming a liner layer in the recess prior to filling the dielectric material in the recess. 3 . The method of claim 2 , further comprising: removing the liner layer formed on the first sidewall of the first layer prior to filling the dielectric layer in the recess. 4 . The method of claim 2 , where the liner layer includes more than one layer. 5 . The method of claim 2 , wherein the liner layer is silicon nitride, silicon oxynitride, silicon oxycarbide, silicon carbonitride or silicon oxycarbonitride or silicon materials with dopants. 6 . The method of claim 2 , wherein the liner layer is fabricated by an ALD process. 7 . The method of claim 2 , wherein the liner layer has a thickness between about 0.5 nm and about 5 nm. 8 . The method of claim 1 , wherein the first layer of the multi-material layer is an intrinsic silicon layer and the second layer of the multi-material layer is a SiGe layer while the substrate is a silicon substrate. 9 . The method of claim 1 , further comprising: forming the dielectric layer in the recess as an nanowire spacer in horizontal gate-all-around (hGAA) structures. 10 . The method of claim 1 , wherein the dielectric layer is selected from a group consisting of silicon nitride, silicon oxide, silicon oxynitride, silicon carbide, silicon oxycarbide, silicon carbide nitride and doped silicon layer. 11 . The method of claim 1 , wherein filling the recess with the dielectric material comprises: filling an amorphous carbon from the substrate. 12 . The method of claim 1 , wherein removing the dielectric layer further comprises: etching the dielectric layer filled over the recess by an isotropic etching process or by an anisotropic etching process. 13 . The method of claim 3 , further comprising: forming an epi-silicon layer from the first sidewall of the first layer in the multi-material layer. 14 . The method of claim 13 , further comprising: forming an air gap in the recess. 15 . The method of claim 14 , further comprising: forming the air gap in the recess as an nanowire air gap spacer in horizontal gate-all-around (hGAA) structures. 16 . The method of claim 3 , further comprising: performing an oxide treatment process on the liner layer to form an oxidation modification layer predominately formed on the first sidewall of the first layer. 17 . The method of claim 16 , further comprising: maintaining the liner layer within the recess unchanged from the oxide treatment process. 18 . The method of claim 17 , further comprising: selectively removing the oxidation modification layer from the first sidewall of the first layer while maintaining the liner layer remained in the recess. 19 . The method of claim 18 , further comprising forming an epi-silicon layer from the first sidewall of the first layer in the multi-material layer. 20 . The method of claim 19 , further comprising: forming an air gap in the recess.
the material being a silicon nitride not containing oxygen, e.g. SixNy or SixByNz · CPC title
the material being a silicon oxynitride, e.g. SiON or SiON:H · CPC title
the material containing Si, O and at least one of H, N, C, F or other non-metal elements, e.g. SiOC, SiOC:H or SiONC · CPC title
Silicon, silicon germanium or germanium · CPC title
using chemical vapour deposition [CVD] · CPC title
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