PATENT CLAIM ANALYSIS

Application Number: 16025094
Application Type: Utility
Filing Date: 2018-07
Publication Date: 2019-02
Patent Classification: ["060", "226100"]

Abstract:
A turbofan engine according to an example of the present disclosure includes, among other things, an engine case and a gaspath through the engine case. A fan has a circumferential array of fan blades. The engine further has a compressor, a combustor, a gas generating turbine, and a low pressure turbine section. A speed reduction mechanism couples the low pressure turbine section to the fan. A bypass area ratio is greater than about 6.0. The low pressure turbine section airfoil count to bypass area ratio is below about 170.

Claim (Index 15):
The turbofan engine as recited in  claim 14 , wherein the abradable seals include honeycomb.

Metadata:
- Claim Count in Document: 80.0
- Percentile: 95.0
- Lexical Diversity: 1.88679
- Patent Class: 60.0
- Transitional Phrase Type: none
- Component Type: 0
- Foreign Priority: False
- Related Applications: ['15292472', '15292405', '14692090', '13475252', '13599175']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.7404729687103806
- 35 USC 102 Novelty (BERT): 0.4968443962950252
- Combined Prediction Score: 0.7161101114688451
- Mean Citation Score: 333.2221100000001
- Max Citation Score: 362.86703
- Similarity Product: 348.45198379159086

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

Dataset: test