PATENT CLAIM ANALYSIS

Application Number: 15878631
Application Type: Utility
Filing Date: 2018-01
Publication Date: 2018-05
Patent Classification: ["423", "245300"]

Abstract:
Fuel tank inerting systems and methods for aircraft are provided. The systems include a fuel tank, a first reactant source fluidly connected to the fuel tank, the first source arranged to receive fuel from the fuel tank, a second reactant source, a catalytic reactor arranged to receive a first reactant from the first source and a second reactant from the second source to generate an inert gas that is supplied to the fuel tank to fill a ullage space of the fuel tank, and a cool air source arranged to supply cool air to the catalytic reactor to provide thermal control of a reaction within the catalytic reactor, wherein the cool air is discharged from at least one of a cabin of the aircraft and an environmental control system of the aircraft.

Claim (Index 6):
The system of  claim 1 , further comprising an injector pump arranged to receive the first reactant and the second reactant and to supply a mixture of the first reactant and the second reactant to the catalytic reactor.

Metadata:
- Claim Count in Document: 18.0
- Percentile: 86.0
- Lexical Diversity: 2.5
- Patent Class: 423.0
- Transitional Phrase Type: open
- Component Type: 1
- Foreign Priority: False
- Related Applications: ['15849151', '15849274', '11560290', '13464043', '12579021']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.7680108710038818
- 35 USC 102 Novelty (BERT): 0.5418775075591726
- Combined Prediction Score: 0.7453975346594109
- Mean Citation Score: 325.9891120000001
- Max Citation Score: 378.66974
- Similarity Product: 298.7438498406434

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