PATENT CLAIM ANALYSIS

Application Number: 16248580
Application Type: Utility
Filing Date: 2019-01
Publication Date: 2019-07
Patent Classification: ["073", "863510"]

Abstract:
A system for converting propelling thrust to produce a continuous flow is provided. The system can be integrated and/or retrofitted to the body of an aircraft. The system includes a pressure-lowering device and a sample chamber. The pressure-lowering device is used produce a low-pressure, continuous flow from a high-velocity propelling thrust source. Moreover, the pressure-lowering device is a passive flow generator that does not require a power source in order to produce a continuous flow from a propelling thrust. The design of the pressure-lowering device produces a flow rate that is independent of the aircraft motion. The sample chamber is used to measure and analyze ambient gases which are pulled through the sample chamber by the pressure-lowering device, as a result of the high-velocity air stream produced by the propelling thrust source.

Claim (Index 4):
The system for transferring propelling thrust to produce a continuous flow as claimed in  claim 1 , wherein a diameter of the scoop inlet is larger than a diameter of the scoop outlet.

Metadata:
- Claim Count in Document: 50.0
- Percentile: 99.0
- Lexical Diversity: 2.15152
- Patent Class: 73.0
- Transitional Phrase Type: none
- Component Type: 0
- Foreign Priority: False
- Related Applications: ['15060573', '15412179', '11297698', '12052923', '14977018']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.7066656406729821
- 35 USC 102 Novelty (BERT): 0.4863505240506897
- Combined Prediction Score: 0.6846341290107528
- Mean Citation Score: 142.04657400000005
- Max Citation Score: 143.80354
- Similarity Product: 89.71403954025627

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