PATENT CLAIM ANALYSIS

Application Number: 15920878
Application Type: Utility
Filing Date: 2018-03
Publication Date: 2019-08
Patent Classification: ["415", "173400"]

Abstract:
A gas turbine engine includes: a turbine section including a casing extending circumferentially about a plurality of turbine blades and having at least one seal member coated with an abradable coating. At least one turbine blade has sides and a tip and at least one seal member is located adjacent to the tip of the at least one turbine blade. The tip of the at least one turbine blade has a wear resistant layer and an abrasive coating disposed on the wear resistant layer. The wear resistant layer has a thickness less than or equal to 10 mils (254 micrometers) and includes metal boride compounds.

Claim (Index 12):
The method of  claim 7 , wherein the blade comprises internal cooling structures.

Metadata:
- Claim Count in Document: 4.0
- Percentile: 90.0
- Lexical Diversity: 1.86667
- Patent Class: 415.0
- Transitional Phrase Type: none
- Component Type: 0
- Foreign Priority: False
- Related Applications: ['15887494', '15638486', '14706369', '14862430', '12910960']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.8315591249952692
- 35 USC 102 Novelty (BERT): 0.4976687697448499
- Combined Prediction Score: 0.7981700894702273
- Mean Citation Score: 300.847898
- Max Citation Score: 417.81485
- Similarity Product: 236.7756180371701

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