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 8):
A rotor blade arrangement, comprising:\n a first platform portion of a first blade unit, the first platform portion having a first slot portion; a second platform portion of a second blade unit, the second platform portion having a second slot portion and being arranged circumferentially adjacent to the first platform portion; and a sealing part according to  claim 1 , wherein the sealing part is inserted in a slot formed by the first slot portion and the second slot portion, to bridge a platform gap between the two circumferentially adjacent platform portions and to suppress fluid transmission through the gap, wherein the side of the sealing part where the coating is applied faces radially outwards.

Metadata:
- Claim Count in Document: 25.0
- Percentile: 91.0
- Lexical Diversity: 1.41026
- Patent Class: 277.0
- Transitional Phrase Type: open
- Component Type: 1
- Foreign Priority: True
- Related Applications: ['14758236', '14758237', '15338840', '14407867', '10857521']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.8012416957525834
- 35 USC 102 Novelty (BERT): 0.4892931096270578
- Combined Prediction Score: 0.7700468371400309
- Mean Citation Score: 233.358568
- Max Citation Score: 246.57649
- Similarity Product: 184.55234447937903

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