IP Library Granted Patent US 10,586,872
Granted Patent B2
US 10,586,872 · App. 16/026,521 · Granted Mar 10, 2020

Formation of wrap-around-contact to reduce contact resistivity

Inventors: Adra Carr (Albany, NY); Jingyun Zhang (Albany, NY); Choonghyun Lee (Rensselaer, NY); Takashi Ando (Tuckahoe, NY); Pouya Hashemi (White Plains, NY)
Assignee: INTERNATIONAL BUSINESS MACHINES CORPORATION
H01L29/78618H01L21/28568H01L21/76802H01L21/76805H01L21/76864H01L21/76865H01L21/76888H01L21/76895H01L29/0673H01L29/4175H01L29/41733H01L29/41758H01L29/41766H01L29/41783H01L29/41791H01L29/42392H01L29/458H01L29/78696
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Quick Facts
Patent No.
US 10,586,872
App. No.
16/026,521
Granted
Mar 10, 2020
Kind
B2
Abstract

A method of forming a source/drain contact is provided. The method includes forming a sacrificial layer on a source/drain, and depositing an oxidation layer on the sacrificial layer. The method further includes heat treating the oxidation layer and the sacrificial layer to form a modified sacrificial layer. The method further includes forming a protective liner on the modified sacrificial layer, and depositing an interlayer dielectric layer on the protective liner. The method further includes forming a trench in the interlayer dielectric layer that exposes a portion of the protective liner.

Claims (29)

1. A method of forming a source/drain contact, comprising:

forming a sacrificial layer on a source/drain;

depositing an oxidation layer on the sacrificial layer;

heat treating the oxidation layer and the sacrificial layer to form a modified sacrificial layer;

forming a protective liner on the modified sacrificial layer;

depositing an interlayer dielectric layer on the protective liner;

forming a trench in the interlayer dielectric layer that exposes a portion of the protective liner;

depositing a protective liner extension on the exposed sidewalls of the trench; and

removing the modified sacrificial layer to form a channel.

2. The method of claim 1 , further comprising forming a source/drain contact in the channel.

3. The method of claim 2 , wherein the heat treatment is conducted at a temperature in a range of about 400° C. to about 700° C. in a 100% nitrogen (N 2 ) atmosphere.

4. The method of claim 2 , wherein the modified sacrificial layer is silicon dioxide (SiO 2 ).

5. The method of claim 2 , wherein the sacrificial layer is silicon-germanium (SiGe), and the oxidation layer is germanium dioxide (GeO 2 ).

6. The method of claim 5 , wherein the source/drain is silicon germanium (SiGe), and the sacrificial layer is formed by epitaxial growth on the exposed surface of the source/drain.

7. The method of claim 6 , wherein the source/drain has a germanium concentration in a range of 20 atomic percent (at. %) to about 60 at. %.

8. The method of claim 7 , wherein the sacrificial layer has a germanium concentration in a range of 20 atomic percent (at. %) to about 65 at. %.

9. A method of forming a source/drain contact, comprising:

forming a sacrificial layer on a source/drain, wherein the sacrificial layer is silicon-germanium (SiGe);

depositing an oxidation layer on the sacrificial layer, wherein the oxidation layer is germanium dioxide (GeO 2 );

heat treating the oxidation layer and the sacrificial layer to form a modified sacrificial layer, wherein the modified sacrificial layer is silicon dioxide (SiO 2 );

forming a protective liner on the modified sacrificial layer;

depositing an interlayer dielectric layer on the protective liner; and

removing a portion of the interlayer dielectric layer to form a trench that exposes a portion of the protective liner.

10. The method of claim 9 , further comprising depositing a protective liner extension on the exposed sidewalls of the trench, and removing the modified sacrificial layer to form a channel.

11. The method of claim 10 , further comprising forming a source/drain contact in the channel.

12. The method of claim 11 , wherein the source/drain contact is formed of a material selected from the group consisting of titanium (Ti), cobalt (Co), and nickel (Ni).

13. The method of claim 12 , wherein the heat treatment is conducted at a temperature in a range of about 400° C. to about 700° C. in a 100% nitrogen (N 2 ) atmosphere.

14. The method of claim 13 , wherein the sacrificial layer has a thickness in a range of about 1 nanometers (nm) to about 3 nm.

15. The method of claim 13 , wherein the oxidation layer has a thickness in a range of about 2 nm to about 5 nm.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jul 3, 2018
From: CARR, ADRA; ZHANG, JINGYUN; LEE, CHOONGHYUN; ANDO, TAKASHI; HASHEMI, POUYA
To: INTERNATIONAL BUSINESS MACHINES CORPORATION
Reel/Frame 046260/0225 →
Continuity (1)
Related Publication 20200013900A1 · Jan 9, 2020
Cited By (1)
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