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 13):
The gas turbine engine recited in  claim 12 , wherein the load limiter constraining radial loads and torsional loads within defined limits.

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): 0.763866729387233
- 35 USC 102 Novelty (BERT): 0.5266791985617444
- Combined Prediction Score: 0.7401479763046842
- Mean Citation Score: 349.43432
- Max Citation Score: 384.4877
- Similarity Product: 278.3696360138416

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