PATENT CLAIM ANALYSIS

Application Number: 16006680
Application Type: Utility
Filing Date: 2018-06
Publication Date: 2018-10
Patent Classification: ["307", "091000"]

Abstract:
An aircraft jet propulsion system is disclosed. The aircraft jet propulsion system may comprise a thermoelectric generator array (“TEG” array) coupled to a portion of the aircraft jet propulsion system, wherein the TEG array converts heat energy to electrical energy, and supplies power to the aircraft jet propulsion system, wherein the electrical energy is supplied to a power supply. The aircraft jet propulsion system may comprise an alternator that generates less energy than is required to power the aircraft jet propulsion system. The TEG array may supplement the energy generated by the alternator. The energy generated by the TEG array and the energy generated by the alternator may be sufficient to power the aircraft jet propulsion system and/or the electrical energy generated by the TEG array may be sufficient to power to aircraft jet propulsion system.

Claim (Index 7):
The aircraft jet propulsion system of  claim 6 , wherein the exhaust portion is an exhaust nozzle.

Metadata:
- Claim Count in Document: 4.0
- Percentile: 94.0
- Lexical Diversity: 3.02041
- Patent Class: 307.0
- Transitional Phrase Type: none
- Component Type: 0
- Foreign Priority: False
- Related Applications: ['14946151', '15030317', '15977588', '14969640', '14077795']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.819266007032998
- 35 USC 102 Novelty (BERT): 0.5662676389288657
- Combined Prediction Score: 0.7939661702225848
- Mean Citation Score: 259.520456
- Max Citation Score: 444.34216
- Similarity Product: 435.99715247159

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

Dataset: test