PATENT CLAIM ANALYSIS

Application Number: 16219189
Application Type: Utility
Filing Date: 2018-12
Publication Date: 2019-04
Patent Classification: ["060", "262000"]

Abstract:
A mixer of a bypass turbine aeroengine according to one embodiment, includes circumferential inner and outer flow surfaces in a wavy configuration to form a plurality of lobes of the mixer. The mixer has an upstream end portion of sheet metal with a first thickness and a downstream end portion of sheet metal with a second thickness less than the first thickness.

Claim (Index 5):
The method as defined in  claim 4  further comprising step (e): cutting and blending the upstream end of the complete configuration of the mixer after step (d), for a uniform face ready to be welded to a turbine exhaust case of the aeroengine.

Metadata:
- Claim Count in Document: 15.0
- Percentile: 98.0
- Lexical Diversity: 1.54762
- Patent Class: 60.0
- Transitional Phrase Type: open
- Component Type: 1
- Foreign Priority: False
- Related Applications: ['13621467', '14521888', '15137257', '13773670', '12858313']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.7104429838194162
- 35 USC 102 Novelty (BERT): 0.5276982427755117
- Combined Prediction Score: 0.6921685097150257
- Mean Citation Score: 237.6651
- Max Citation Score: 358.67792000000014
- Similarity Product: 248.15442124837884

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

Dataset: test