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 16):
The method of  claim 12 , wherein the outlet is tilted circumferentially relative to the engine longitudinal axis to introduce flow to the exhaust section in a direction having a circumferential component.

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): 0.7670950074620767
- 35 USC 102 Novelty (BERT): 0.5262209415816906
- Combined Prediction Score: 0.7430076008740382
- Mean Citation Score: 296.410746
- Max Citation Score: 380.7624
- Similarity Product: 294.16556730823515

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