COMPOSITE MICROELECTRONIC DIELECTRIC LAYER WITH INHIBITED CRACK SUSCEPTIBILITY
First Claim
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1. A method for fabricating a microelectronic fabrication comprising:
- providing a substrate;
forming upon the substrate a pair of horizontally spaced topographic features;
forming upon exposed portions of the substrate and the pair of horizontally spaced topographic features a conformal silicon oxide liner layer formed employing a chemical vapor deposition method selected from the group consisting of low pressure thermal chemical vapor deposition methods and plasma enhanced chemical vapor deposition methods;
forming over the conformal silicon oxide liner layer a gap filling silicon oxide layer formed employing a method selected from the group consisting of sub-atmospheric chemical vapor deposition methods, atmospheric pressure chemical vapor deposition methods and spin-on methods;
forming over the gap filling silicon oxide layer a capping silicon oxide layer formed employing a chemical vapor deposition method selected from the group consisting of low pressure thermal chemical vapor deposition methods and plasma enhanced chemical vapor deposition methods; and
forming at least either;
(1) interposed between the conformal silicon oxide liner layer and the gap filling silicon oxide layer;
(2) interposed between the gap filling silicon oxide layer and the capping silicon oxide layer; and
(3) upon the capping silicon oxide layer, at least one stress reducing layer, wherein the at least one stress reducing layer is formed of a silicon and nitrogen containing dielectric material.
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Abstract
Within each of a pair of methods for forming each of a pair of microelectronic fabrications with reduced cracking within each of a pair of silicon oxide dielectric layers there is employed at least one stress reducing layer. The at least one stress reducing layer is formed of a silicon and nitrogen containing dielectric material, such as a silicon nitride dielectric material or a silicon oxynitride dielectric material.
398 Citations
12 Claims
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1. A method for fabricating a microelectronic fabrication comprising:
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providing a substrate;
forming upon the substrate a pair of horizontally spaced topographic features;
forming upon exposed portions of the substrate and the pair of horizontally spaced topographic features a conformal silicon oxide liner layer formed employing a chemical vapor deposition method selected from the group consisting of low pressure thermal chemical vapor deposition methods and plasma enhanced chemical vapor deposition methods;
forming over the conformal silicon oxide liner layer a gap filling silicon oxide layer formed employing a method selected from the group consisting of sub-atmospheric chemical vapor deposition methods, atmospheric pressure chemical vapor deposition methods and spin-on methods;
forming over the gap filling silicon oxide layer a capping silicon oxide layer formed employing a chemical vapor deposition method selected from the group consisting of low pressure thermal chemical vapor deposition methods and plasma enhanced chemical vapor deposition methods; and
forming at least either;
(1) interposed between the conformal silicon oxide liner layer and the gap filling silicon oxide layer;
(2) interposed between the gap filling silicon oxide layer and the capping silicon oxide layer; and
(3) upon the capping silicon oxide layer, at least one stress reducing layer, wherein the at least one stress reducing layer is formed of a silicon and nitrogen containing dielectric material. - View Dependent Claims (2, 3, 4, 5, 6)
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7. A method for fabricating a microelectronic fabrication comprising:
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providing a substrate;
forming upon the substrate a pair of horizontally spaced topographic features;
forming upon exposed portions of the substrate and the pair of horizontally spaced topographic features a silicon oxide passivation layer formed employing a high density plasma chemical vapor deposition method; and
forming upon the silicon oxide passivation layer a stress reducing layer formed of a silicon and nitrogen containing dielectric material. - View Dependent Claims (8, 9, 10, 11, 12)
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Specification