PATENT CLAIM ANALYSIS

Application Number: 15880717
Application Type: Utility
Filing Date: 2018-01
Publication Date: 2018-06
Patent Classification: ["060", "226300"]

Abstract:
A method of designing an engine according to an exemplary aspect of the present disclosure includes, among other things, designing an engine and a nacelle assembly together in an interactive process, the engine including a turbine section that drives a fan section and a compressor section. The step of designing the compressor section includes the step of designing a first compressor and a second compressor, with an overall pressure ratio being greater than or equal to about 35. The step of designing the nacelle assembly includes the step of designing the fan section to include a fan nacelle arranged at least partially about a fan, with the fan section having a fan pressure ratio of less than about 1.7. The step of designing the fan section includes configuring the fan section to deliver a portion of air into the compressor section, and a portion of air into a bypass duct, and with a bypass ratio equal to or greater than about 5.

Claim (Index 4):
The method as recited in  claim 3 , wherein the nacelle assembly includes a fan case made of an organic matrix composite.

Metadata:
- Claim Count in Document: 50.0
- Percentile: 86.0
- Lexical Diversity: 2.66154
- Patent Class: 60.0
- Transitional Phrase Type: none
- Component Type: 0
- Foreign Priority: False
- Related Applications: ['14615484', '14684503', '15173288', '15292405', '15292472']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.7431248506866671
- 35 USC 102 Novelty (BERT): 0.5652600212898469
- Combined Prediction Score: 0.7253383677469851
- Mean Citation Score: 353.960242
- Max Citation Score: 496.67075
- Similarity Product: 348.9611365217417

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

Dataset: test