PATENT CLAIM ANALYSIS

Application Number: 15959906
Application Type: Utility
Filing Date: 2018-04
Publication Date: 2019-10
Patent Classification: ["416", "19300A"]

Abstract:
A turbine wheel for use in a gas turbine engine having a plurality of blades attached to a rotor disk. The blades each fit within slots formed in the rotor disk to couple the blades to the rotor disk. Platform segments are arranged about each of the blades.

Claim (Index 18):
The turbine wheel of  claim 17 , further comprising an annular, full-hoop retention band spaced apart axially from the first turbine blade to locate the first platform segment and the disk axially between the annular, full-hoop retention band and the first turbine blade to block axial movement of the first platform segment.

Metadata:
- Claim Count in Document: 20.0
- Percentile: 91.0
- Lexical Diversity: 1.64516
- Patent Class: 416.0
- Transitional Phrase Type: open
- Component Type: 1
- Foreign Priority: False
- Related Applications: ['15334394', '15348051', '14869580', '15042569', '14968199']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.8072013973486727
- 35 USC 102 Novelty (BERT): 0.4977565217295819
- Combined Prediction Score: 0.7762569097867636
- Mean Citation Score: 381.955332
- Max Citation Score: 447.12985
- Similarity Product: 296.9269098964512

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

Dataset: test