PATENT CLAIM ANALYSIS

Application Number: 16108540
Application Type: Utility
Filing Date: 2018-08
Publication Date: 2018-12
Patent Classification: ["060", "039080"]

Abstract:
A gas turbine engine has a fan drive turbine for driving a gear reduction. The gear reduction drives a fan rotor. A lubrication system supplies oil to the gear reduction, and includes a lubricant pump to supply an air/oil mixture to an inlet of a deaerator. The deaerator includes a separator for separating oil and air, delivering separated air to an air outlet, and delivering separated oil back into an oil tank. The separated oil is first delivered into a pipe outwardly of the oil tank, and then into a location beneath a minimum oil level in the tank. Air within the oil tank moves outwardly through an air exit into the deaerator. A method of designing a gas turbine engine is also disclosed.

Claim (Index 17):
The method as set forth in  claim 16 , wherein an inlet velocity to the deaerator is less than or equal to 14 feet/second.

Metadata:
- Claim Count in Document: 12.0
- Percentile: 96.0
- Lexical Diversity: 2.14286
- Patent Class: 60.0
- Transitional Phrase Type: none
- Component Type: 0
- Foreign Priority: False
- Related Applications: ['14794866', '14737670', '14595255', '15112869', '13362094']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.7834026319573179
- 35 USC 102 Novelty (BERT): 0.5446195487559411
- Combined Prediction Score: 0.7595243236371803
- Mean Citation Score: 337.655026
- Max Citation Score: 448.16153
- Similarity Product: 310.1031105060757

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

Dataset: test