PATENT CLAIM ANALYSIS

Application Number: 16125179
Application Type: Utility
Filing Date: 2018-09
Publication Date: 2020-01
Patent Classification: ["415", "122100"]

Abstract:
A gas turbine engine includes a fan shaft that drives a fan that has fan blades. A fan shaft support that supports the fan shaft defines a fan shaft support transverse stiffness. A gear system is connected to the fan shaft and includes a gear mesh that defines a gear mesh transverse stiffness. A flexible support supports the gear system and defines a flexible support transverse stiffness. The flexible support transverse stiffness is less than 11% of the fan shaft support transverse stiffness and less than 8% of the gear mesh transverse stiffness.

Claim (Index 9):
The gas turbine engine of  claim 8 , wherein said gear system includes a reduction ratio greater than 2.3.

Metadata:
- Claim Count in Document: 80.0
- Percentile: 97.0
- Lexical Diversity: 2.94118
- Patent Class: 415.0
- Transitional Phrase Type: none
- Component Type: 0
- Foreign Priority: False
- Related Applications: ['15606494', '14859381', '14604811', '15484441', '15185292']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.8433083225506034
- 35 USC 102 Novelty (BERT): 0.5694626898028815
- Combined Prediction Score: 0.8159237592758313
- Mean Citation Score: 542.4575
- Max Citation Score: 572.0665
- Similarity Product: 481.11008639234313

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