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 1):
A turbine wheel comprising\n a disk comprising metallic material and arranged around a central axis and formed to include slots that extend radially inward from an outer diameter of the disk toward the central axis, and a plurality of turbine blades comprising ceramic matrix composite materials, the plurality of turbine blades coupled to the disk and extends radially away from the outer diameter, the plurality of turbine blades include a first turbine blade shaped to provide an airfoil configured to interact with hot gasses passing around the plurality of turbine blades, a root received in one of the slots formed in the disk to couple the first turbine blade to the disk, and a platform that extends circumferentially in a single direction from the airfoil to discourage the hot gasses interacting with the airfoil from moving radially inward toward the disk.

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): 0.8031025003255957
- 35 USC 102 Novelty (BERT): 0.5110124793915855
- Combined Prediction Score: 0.7738934982321948
- Mean Citation Score: 381.955332
- Max Citation Score: 447.12985
- Similarity Product: 398.3684584237038

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

Dataset: test