PATENT CLAIM ANALYSIS

Application Number: 15883633
Application Type: Utility
Filing Date: 2018-01
Publication Date: 2018-06
Patent Classification: ["423", "245300"]

Abstract:
Fuel tank inerting systems and methods for an aircraft. 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 heating duct thermally connected to the catalytic reactor and arranged in thermal communication with the first source to provide heat to the first source to generate the first reactant.

Claim (Index 16):
The method of  claim 14 , further comprising supplying discharge air from an environmental control system of the aircraft to the heat exchanger to enable cooling of the output from the catalytic reactor.

Metadata:
- Claim Count in Document: 20.0
- Percentile: 86.0
- Lexical Diversity: 2.55319
- Patent Class: 423.0
- Transitional Phrase Type: open
- Component Type: 1
- Foreign Priority: False
- Related Applications: ['15883244', '15849151', '15849274', '11560290', '13464043']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.8044770504852454
- 35 USC 102 Novelty (BERT): 0.5626644614780955
- Combined Prediction Score: 0.7802957915845304
- Mean Citation Score: 359.79058
- Max Citation Score: 451.13425
- Similarity Product: 383.6188465707898

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