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 12):
The aircraft fuel tank inerting system as claimed in  claim 1 , wherein the vent for discharging oxygen from the inerting system comprises an ejector.

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): 0.6573349749383889
- 35 USC 102 Novelty (BERT): 0.4933150990538907
- Combined Prediction Score: 0.6409329873499391
- Mean Citation Score: 239.213664
- Max Citation Score: 254.38757
- Similarity Product: 191.4606860367656

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