PATENT CLAIM ANALYSIS

Application Number: 15863172
Application Type: Utility
Filing Date: 2018-01
Publication Date: 2019-07
Patent Classification: ["427", "554000"]

Abstract:
A process for coating a gas turbine blade with an abrasive. The process includes positioning the gas turbine blade in a nest, the gas turbine blade comprising a tip having a top surface; prepositioning a metal powder material on the top surface; fusing the metal powder material to the top surface by use of a laser to form a base layer on the top surface; prepositioning an abrasive composite material on the base layer opposite the top surface; fusing the abrasive composite material to the base layer by use of the laser to form an abrasive coating on the base layer; and removing the gas turbine blade from the nest.

Claim (Index 8):
The process of  claim 1 , further comprising:\n prepositioning an additional predetermined quantity of said metal powder material on said abrasive coating; and fusing said additional predetermined quantity of metal powder material to said abrasive coating by use of said laser to form an encapsulation layer on said abrasive coating.

Metadata:
- Claim Count in Document: 15.0
- Percentile: 86.0
- Lexical Diversity: 2.68182
- Patent Class: 427.0
- Transitional Phrase Type: open
- Component Type: 1
- Foreign Priority: False
- Related Applications: ['15344638', '14706369', '15142247', '12911004', '15142312']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.7923173865588985
- 35 USC 102 Novelty (BERT): 0.4952707943850001
- Combined Prediction Score: 0.7626127273415086
- Mean Citation Score: 199.981054
- Max Citation Score: 210.61429
- Similarity Product: 145.80899308109042

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

Dataset: test