PATENT CLAIM ANALYSIS

Application Number: 15766050
Application Type: Utility
Filing Date: 2018-04
Publication Date: 2018-10
Patent Classification: ["277", "650000"]

Abstract:
A sealing part for a turbine section of a gas turbine to seal a gap between two circumferentially adjacent rotor blades includes a body, and a coating applied on a surface of the body. The coating includes a soft heat resisting material that deforms under centrifugal force of the rotating rotor blades.

Claim (Index 10):
The rotor blade arrangement according to  claim 8 ,\n wherein the first slot portion comprises as limiting border for the sealing part a first radially inner surface, wherein during rotation of the first platform portion the coated side of the sealing part is pressed due to centrifugal force towards the first radially inner surface.

Metadata:
- Claim Count in Document: 25.0
- Percentile: 91.0
- Lexical Diversity: 1.41026
- Patent Class: 277.0
- Transitional Phrase Type: none
- Component Type: 0
- Foreign Priority: True
- Related Applications: ['14758236', '14758237', '15338840', '14407867', '10857521']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.8186351933102238
- 35 USC 102 Novelty (BERT): 0.4981045967237171
- Combined Prediction Score: 0.7865821336515733
- Mean Citation Score: 233.358568
- Max Citation Score: 246.57649
- Similarity Product: 168.05394860780598

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

Dataset: test