PATENT CLAIM ANALYSIS

Application Number: 15864297
Application Type: Utility
Filing Date: 2018-01
Publication Date: 2018-07
Patent Classification: ["060", "262000"]

Abstract:
A method of communicating flow through a gas turbine engine having multiple flow paths according to an exemplary embodiment of the present disclosure includes moving core flow along a core flow path from a compressor section to an exhaust section, selectively communicating a first amount of bypass flow from a bypass flow path defined by a bypass duct to the exhaust section or a second amount of bypass flow from the bypass flow path to the exhaust section, the first amount different than the second amount.

Claim (Index 12):
The method of  claim 10 , wherein the step of communicating the first amount or the second amount of bypass flow radially across the primary bypass duct includes communicating the first amount or the second amount in a flow passage defined between an inlet and an outlet of at least one vane, the at least one vane extending radially from the bypass flow path to the exhaust section.

Metadata:
- Claim Count in Document: 3.0
- Percentile: 86.0
- Lexical Diversity: 2.06977
- Patent Class: 60.0
- Transitional Phrase Type: none
- Component Type: 0
- Foreign Priority: False
- Related Applications: ['14489777', '11290247', '13325034', '14430798', '10982477']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.7683617632937058
- 35 USC 102 Novelty (BERT): 0.5252108546422165
- Combined Prediction Score: 0.7440466724285568
- Mean Citation Score: 296.410746
- Max Citation Score: 380.7624
- Similarity Product: 238.0855050820828

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