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 13):
The method of  claim 12 , wherein the at least one vane is an array of vanes including a first set of vanes and a second set of vanes, and further comprising communicating flow from the bypass flow path to the core flow path with the first set of vanes, and communicating flow from the fan discharge bypass flow path to the core flow path with the second set of vanes.

Metadata:
- Claim Count in Document: 3.0
- Percentile: 86.0
- Lexical Diversity: 2.06977
- Patent Class: 60.0
- Transitional Phrase Type: open
- Component Type: 1
- Foreign Priority: False
- Related Applications: ['14489777', '11290247', '13325034', '14430798', '10982477']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.7462007296439046
- 35 USC 102 Novelty (BERT): 0.5231672430037593
- Combined Prediction Score: 0.7238973809798901
- Mean Citation Score: 296.410746
- Max Citation Score: 380.7624
- Similarity Product: 251.89896588048936

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