PATENT CLAIM ANALYSIS

Application Number: 16043954
Application Type: Utility
Filing Date: 2018-07
Publication Date: 2018-11
Patent Classification: ["375", "257000"]

Abstract:
A system for data transfer in a rotorcraft includes a power bus extending from a power source in a main fuselage of the rotorcraft to provide electrical power to electrical loads located in a tail boom section of the rotorcraft, a first power line communication node on the power bus in the tail boom section of the rotorcraft, a second power line communication node on the power bus in the main fuselage of the rotorcraft, and a digital sensor bus connected to the first power line communication node. Information from the digital sensor bus is transmitted to the first power line communication node and across the power bus to the second power line communication node.

Claim (Index 16):
The system of  claim 13 , and further comprising a processor connected to the digital sensor bus and the first power line communication node in the extremity of the aircraft, wherein the information from the digital sensor bus is analyzed, compressed, and processed at the processor before it is sent to the main fuselage.

Metadata:
- Claim Count in Document: 48.0
- Percentile: 95.0
- Lexical Diversity: 2.85714
- Patent Class: 375.0
- Transitional Phrase Type: open
- Component Type: 1
- Foreign Priority: False
- Related Applications: ['15490687', '14060833', '14605097', '14528300', '15424801']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.4672242072322801
- 35 USC 102 Novelty (BERT): 0.5372073085007999
- Combined Prediction Score: 0.4742225173591321
- Mean Citation Score: 216.560066
- Max Citation Score: 381.53302
- Similarity Product: 308.2094213809908

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