PATENT CLAIM ANALYSIS

Application Number: 15965130
Application Type: Utility
Filing Date: 2018-04
Publication Date: 2019-10
Patent Classification: ["415", "115000"]

Abstract:
A variable vane system for a gas turbine engine includes an airfoil trunnion that extends through a vane platform such that the airfoil is rotatable with respect to the vane platform about an axis, the airfoil trunnion having an inlet configuration into the airfoil and a fixed airflow inlet mask to abut the airfoil trunnion, the fixed airflow inlet mask having a mask inlet configuration that modulates an airflow through the inlet configuration.

Claim (Index 6):
The system as recited in  claim 5 , wherein at least one of a multiple of cavities within the airfoil comprises an airfoil cavity that ejects cooling flow to the gaspath via film cooling.

Metadata:
- Claim Count in Document: 2.0
- Percentile: 91.0
- Lexical Diversity: 2.0
- Patent Class: 415.0
- Transitional Phrase Type: none
- Component Type: 0
- Foreign Priority: False
- Related Applications: ['15034951', '15497757', '13630681', '15852198', '13418451']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.8350754902601593
- 35 USC 102 Novelty (BERT): 0.464415560965872
- Combined Prediction Score: 0.7980094973307306
- Mean Citation Score: 258.562776
- Max Citation Score: 273.24597
- Similarity Product: 195.3306331632632

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

Dataset: test