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 9):
The rotor blade arrangement according to  claim 8 ,\n wherein the first slot portion, the second slot portion and the sealing part are dimensioned such that the sealing part can move to some degree in the circumferential direction and the radial direction.

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): 0.8191546408836029
- 35 USC 102 Novelty (BERT): 0.4941892558326914
- Combined Prediction Score: 0.7866581023785117
- Mean Citation Score: 233.358568
- Max Citation Score: 246.57649
- Similarity Product: 177.96946746328354

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