PATENT CLAIM ANALYSIS

Application Number: 15776920
Application Type: Utility
Filing Date: 2018-05
Publication Date: 2018-11
Patent Classification: ["416", "24100R"]

Abstract:
A turbine blade with a ceramic thermal barrier coating system has a substrate designed as a blade platform and as a blade airfoil. On the substrate is a first ceramic layer as a thermal barrier coating, which protects the substrate in the exposed high temperature region and there is locally an increase of the thermal barrier coating for locally reinforcing the thermal barrier. The increase includes a material that is different from the material of the first ceramic layer. The local reinforcement is arranged over the first ceramic layer, without the first ceramic layer having a reduced layer thickness. The local reinforcement is provided at most on 30% of the area of the blade airfoil and is arranged close to a platform extending over the entire pressure side in the direction of flow and with an extent thereto in the radial direction of the blade airfoil is at most 30%.

Claim (Index 16):
The turbine blade as claimed in  claim 13 ,\n in which the material of the local reinforcement comprises fully stabilized zirconia.

Metadata:
- Claim Count in Document: 23.0
- Percentile: 93.0
- Lexical Diversity: 2.27143
- Patent Class: 416.0
- Transitional Phrase Type: none
- Component Type: 0
- Foreign Priority: True
- Related Applications: ['11306125', '12978676', '12978679', '11895259', '12917114']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.7593265015510252
- 35 USC 102 Novelty (BERT): 0.4342550977983164
- Combined Prediction Score: 0.7268193611757543
- Mean Citation Score: 130.72636599999998
- Max Citation Score: 133.08243000000002
- Similarity Product: 83.36755307665409

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

Dataset: test