PATENT CLAIM ANALYSIS

Application Number: 15745932
Application Type: Utility
Filing Date: 2018-01
Publication Date: 2018-08
Patent Classification: ["060", "805000"]

Abstract:
An aircraft comprising a fuselage and a propulsion assembly, the propulsion assembly comprising at least one fan rotor located at the rear of the fuselage in the extension thereof along a longitudinal axis, and a nacelle forming a fairing of the at least one fan rotor into which a flow of air passes. The aircraft also comprises a plurality of radial stator arms mounted upstream of the at least one fan rotor and extending between the fuselage and the nacelle, the radial arms comprising blowing means configured for blowing, into the environment of a trailing edge of the radial arms, an additional air flow adding to the airflow in the extension of the trailing edge.

Claim (Index 4):
The aircraft according to  claim 1 , wherein, with each radial arm comprising two lateral faces extending radially either side of a mean profile, the blowing means comprise orifices arranged on said lateral faces to blow the additional air flow upstream of the trailing edge.

Metadata:
- Claim Count in Document: 53.0
- Percentile: 86.0
- Lexical Diversity: 2.17857
- Patent Class: 60.0
- Transitional Phrase Type: open
- Component Type: 1
- Foreign Priority: True
- Related Applications: ['15745704', '15745661', '15234067', '14904597', '15569639']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.7375088762786016
- 35 USC 102 Novelty (BERT): 0.489257180723324
- Combined Prediction Score: 0.7126837067230738
- Mean Citation Score: 253.986614
- Max Citation Score: 273.51874
- Similarity Product: 211.1290007894778

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