PATENT CLAIM ANALYSIS

Application Number: 16298204
Application Type: Utility
Filing Date: 2019-03
Publication Date: 2019-07
Patent Classification: ["428", "446000"]

Abstract:
A thermal barrier coating for a turbine engine component contains neodymia, optionally alumina, and zirconia. The thermal barrier coating has resistance to CMAS attack and a low thermal conductivity.

Claim (Index 29):
A thermal barrier coating system comprising:\n a substrate; a bond coat on said substrate; a ceramic layer on said bond coat; a first thermal barrier coating layer on said ceramic layer, said first thermal barrier coating layer consisting of neodymia, optionally alumina, and the balance zirconia wherein said first layer consists of from 15-60 mol % neodymia, 2.0-40 mol % alumina, and the balance zirconia; and a second thermal barrier coating layer which consists of an oxide stabilized zirconia and 25 to 99.9 wt % gadolinia.

Metadata:
- Claim Count in Document: 11.0
- Percentile: 99.0
- Lexical Diversity: 1.32
- Patent Class: 428.0
- Transitional Phrase Type: open
- Component Type: 1
- Foreign Priority: False
- Related Applications: ['14762011', '16298217', '10803527', '11611364', '10748516']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.8781183989539622
- 35 USC 102 Novelty (BERT): 0.4899585332966838
- Combined Prediction Score: 0.8393024123882343
- Mean Citation Score: 221.619028
- Max Citation Score: 270.51712000000003
- Similarity Product: 262.69649125686647

Labels:
- Claim Label 101: 1
- Claim Label 102: 1
- Claim Label 103: 1
- Claim Label 112: 0
- Combined Label: 1
- Label 101 Adjusted: 1

Dataset: test