PATENT CLAIM ANALYSIS

Application Number: 15745690
Application Type: Utility
Filing Date: 2018-01
Publication Date: 2018-07
Patent Classification: ["415", "160000"]

Abstract:
A stage of variable-pitch vanes for a turbine engine includes a plurality of vanes. Each vane has a blade with a first radially internal frusto-conical surface. The cone angle of the first frusto-conical surface is radially flared inwards and is configured to interact with an internal frusto-conical surface of a first frusto-conical bushing. The vane further includes a second radially external frusto-conical surface with cone angle that is radially flared outwards and is configured to interact with an internal frusto-conical surface of a second substantially frusto-conical bushing.

Claim (Index 7):
A turbine engine for aircraft, comprising at least one stage according to  claim 1 .

Metadata:
- Claim Count in Document: 3.0
- Percentile: 86.0
- Lexical Diversity: 2.21951
- Patent Class: 415.0
- Transitional Phrase Type: open
- Component Type: 1
- Foreign Priority: True
- Related Applications: ['11519056', '14551218', '14163773', '14932028', '10278570']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.7941832280560565
- 35 USC 102 Novelty (BERT): 0.4773915486022993
- Combined Prediction Score: 0.7625040601106807
- Mean Citation Score: 201.964358
- Max Citation Score: 232.14995
- Similarity Product: 104.69205273694692

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