PATENT CLAIM ANALYSIS

Application Number: 15878126
Application Type: Utility
Filing Date: 2018-01
Publication Date: 2018-08
Patent Classification: ["307", "031000"]

Abstract:
The invention relates to a power communication architecture ( 100 ) for an aircraft comprising: a power electronics module management unit ( 103 ) that is capable of receiving input signals ( 104 ) and of delivering a current setpoint ( 106 ); at least one power electronics module ( 107 ) that is capable of receiving said current setpoint ( 106 ); at least one load ( 105 ) that is controlled by the at least one power electronics module ( 107 ); the power electronics module management unit ( 103 ) storing control laws ( 108 ) for controlling the one or more loads ( 105 ) allowing a current setpoint ( 106 ) to be transmitted according to the input signals ( 104 ) and said control laws ( 108 ).   The invention also relates to an electrical distribution device for an aircraft comprising at least one such architecture.

Claim (Index 3):
The power communication architecture according to  claim 2 , comprising a contactor matrix that is configured by the electrical network management unit, said contactor matrix being capable of communicating with each power electronics module and each load.

Metadata:
- Claim Count in Document: 7.0
- Percentile: 86.0
- Lexical Diversity: 2.50794
- Patent Class: 307.0
- Transitional Phrase Type: open
- Component Type: 1
- Foreign Priority: True
- Related Applications: ['12559192', '12148771', '14361345', '15657709', '14064144']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.7750235049879418
- 35 USC 102 Novelty (BERT): 0.4589172517744017
- Combined Prediction Score: 0.7434128796665879
- Mean Citation Score: 115.480602
- Max Citation Score: 121.78204
- Similarity Product: 86.49530437508581

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

Dataset: test