PATENT CLAIM ANALYSIS

Application Number: 15872158
Application Type: Utility
Filing Date: 2018-01
Publication Date: 2018-05
Patent Classification: ["060", "226100"]

Abstract:
A disclosed gas turbine engine includes a fan including a plurality of fan blades rotatable about an axis, a bypass duct, a compressor section and a bypass ratio greater than 10. A combustor in fluid communication with the compressor section and a fan drive turbine in communication with the combustor. A gear system provides a speed reduction between the fan drive turbine and the fan and transfer power input from the fan drive turbine to the fan at an efficiency greater than 98%.

Claim (Index 23):
The gas turbine engine recited in  claim 13 , wherein the compressor section includes a first compressor and a second compressor, the first compressor is a three stage compressor, and wherein the second turbine drives the second compressor through the outer shaft and the inner shaft connects the fan and the first compressor section to the fan drive turbine.

Metadata:
- Claim Count in Document: 80.0
- Percentile: 86.0
- Lexical Diversity: 1.81633
- Patent Class: 60.0
- Transitional Phrase Type: none
- Component Type: 0
- Foreign Priority: False
- Related Applications: ['15379619', '14190159', '13557614', '14034720', '14277472']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.7635560730551116
- 35 USC 102 Novelty (BERT): 0.5270017927420142
- Combined Prediction Score: 0.7399006450238019
- Mean Citation Score: 349.43432
- Max Citation Score: 384.4877
- Similarity Product: 291.1026449958801

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