PATENT CLAIM ANALYSIS

Application Number: 15891423
Application Type: Utility
Filing Date: 2018-02
Publication Date: 2019-08
Patent Classification: ["416", "22300A"]

Abstract:
A blade for a turbine engine comprising a composite core defining a pressure side and a suction side extending axially between a leading edge and a trailing edge defining a chord-wise direction and extending radially between a root and a tip defining a span-wise direction. The composite core is formed from two materials with different compositions.

Claim (Index 11):
The airfoil of  claim 10  wherein the tip cap extends along 100% of the tip.

Metadata:
- Claim Count in Document: 71.0
- Percentile: 88.0
- Lexical Diversity: 1.61111
- Patent Class: 416.0
- Transitional Phrase Type: none
- Component Type: 0
- Foreign Priority: False
- Related Applications: ['13336001', '13330766', '15707133', '12465109', '14596804']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.7795094186445355
- 35 USC 102 Novelty (BERT): 0.4617572100623547
- Combined Prediction Score: 0.7477341977863174
- Mean Citation Score: 230.39147000000003
- Max Citation Score: 270.78067000000004
- Similarity Product: 171.70435237327757

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