PATENT CLAIM ANALYSIS

Application Number: 15953751
Application Type: Utility
Filing Date: 2018-04
Publication Date: 2018-08
Patent Classification: ["096", "109000"]

Abstract:
An aircraft fuel tank inerting system includes an inlet, an oxygen absorption unit, and a vent to discharge oxygen from the system. The inlet may be configured to be in fluid communication with a ullage of a fuel tank. In embodiments, the oxygen absorption unit is in communication with the inlet and includes a chamber, a temperature reversible oxygen absorption medium within said chamber, and a temperature controller for selectively heating or cooling the medium. The reversible oxygen absorption medium may be a medium which absorbs oxygen by chemisorption.

Claim (Index 11):
The aircraft fuel tank inerting system as claimed in  claim 10 , wherein the inerting system comprises a plurality of oxygen absorption units and the oxygen absorption units are configured or controlled such that at least one unit is in the first, oxygen absorption, configuration when another unit is in the second, oxygen desorption, configuration, such that continuous oxygen absorption is available.

Metadata:
- Claim Count in Document: 1.0
- Percentile: 91.0
- Lexical Diversity: 1.96
- Patent Class: 96.0
- Transitional Phrase Type: none
- Component Type: 0
- Foreign Priority: True
- Related Applications: ['10454826', '14526425', '10463764', '10708110', '15849151']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.6564853529474477
- 35 USC 102 Novelty (BERT): 0.4976592182312938
- Combined Prediction Score: 0.6406027394758322
- Mean Citation Score: 239.213664
- Max Citation Score: 254.38757
- Similarity Product: 179.3564392993784

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