PATENT CLAIM ANALYSIS

Application Number: 15924525
Application Type: Utility
Filing Date: 2018-03
Publication Date: 2019-09
Patent Classification: ["423", "245300"]

Abstract:
An aircraft inert gas generating system includes a fuel source configured to supply fuel, a stream of reaction air having a first temperature, an air-fuel mixing unit configured to receive an amount of the fuel and an amount of the reaction air stream to create an air-fuel mixture, and a catalytic oxidation unit configured to receive and react the air-fuel mixture. The stream of reaction air includes an amount of mixing air from a mixing air source, and the mixing air source includes a primary heat exchanger of an aircraft ram circuit and a cooling air extraction element proximate the heat exchanger. The mixing air can alternatively include cool air from a heat sink air source.

Claim (Index 19):
The method of  claim 14 , wherein the fluid line is an environmental control system outlet.

Metadata:
- Claim Count in Document: 16.0
- Percentile: 90.0
- Lexical Diversity: 2.41176
- Patent Class: 423.0
- Transitional Phrase Type: none
- Component Type: 0
- Foreign Priority: False
- Related Applications: ['15673012', '15883244', '15010675', '15238287', '14310531']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.7932457516295599
- 35 USC 102 Novelty (BERT): 0.5142024677165551
- Combined Prediction Score: 0.7653414232382594
- Mean Citation Score: 234.022746
- Max Citation Score: 247.7734
- Similarity Product: 143.0001993768215

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

Dataset: test