PATENT CLAIM ANALYSIS

Application Number: 15977588
Application Type: Utility
Filing Date: 2018-05
Publication Date: 2018-09
Patent Classification: ["244", "058000"]

Abstract:
In one aspect the present subject matter is directed to a gas-electric propulsion system for an aircraft. The system may include a turbofan jet engine, an electric powered boundary layer ingestion fan that is coupled to a fuselage portion of the aircraft aft of the turbofan jet engine, and an electric generator that is electronically coupled to the turbofan jet engine and to the boundary layer ingestion fan. The electric generator converts rotational energy from the turbofan jet engine to electrical energy and provides at least a portion of the electrical energy to the boundary layer ingestion fan. In another aspect of the present subject matter, a method for propelling an aircraft via the gas-electric propulsion system is disclosed.

Claim (Index 17):
The system as in  claim 12 , further comprising an energy management system.

Metadata:
- Claim Count in Document: 50.0
- Percentile: 93.0
- Lexical Diversity: 2.37736
- Patent Class: 244.0
- Transitional Phrase Type: open
- Component Type: 1
- Foreign Priority: False
- Related Applications: ['14969640', '15132298', '14879217', '15132304', '14859514']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.8639702755593032
- 35 USC 102 Novelty (BERT): 0.5540233441237159
- Combined Prediction Score: 0.8329755824157445
- Mean Citation Score: 390.320648
- Max Citation Score: 476.97058
- Similarity Product: 320.10139107592585

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