PATENT CLAIM ANALYSIS

Application Number: 15966049
Application Type: Utility
Filing Date: 2018-04
Publication Date: 2018-08
Patent Classification: ["415", "115000"]

Abstract:
A turbine blade according to an example of the present disclosure includes, among other things, a platform extending from a root section, an airfoil section extending radially from the platform to an airfoil tip, a plurality of cooling passages defined in an external wall of the airfoil tip, the plurality of cooling passages extending radially between the airfoil tip and a cavity in the airfoil section bounded by the external wall, and each of the plurality of cooling passages defining an inlet port along the cavity and an exit port adjacent the airfoil tip, and at least one internal feature within each of the plurality of cooling passages that meter flow to the respective exit port.

Claim (Index 9):
The turbine blade of  claim 2 , wherein the at least one internal feature is radially spaced a distance equal to or greater than 1.0 hydraulic diameters from the exit port, the hydraulic diameters defined relative to a minimum cross-sectional flow area and a wetted perimeter of a respective one of the plurality of cooling passages.

Metadata:
- Claim Count in Document: 10.0
- Percentile: 91.0
- Lexical Diversity: 2.25455
- Patent Class: 415.0
- Transitional Phrase Type: none
- Component Type: 0
- Foreign Priority: False
- Related Applications: ['14619343', '14618912', '14942025', '15679442', '14820786']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.8180895847799652
- 35 USC 102 Novelty (BERT): 0.5211598812466143
- Combined Prediction Score: 0.7883966144266301
- Mean Citation Score: 354.400014
- Max Citation Score: 443.74374000000006
- Similarity Product: 354.8573821647049

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

Dataset: test