PATENT CLAIM ANALYSIS

Application Number: 15863289
Application Type: Utility
Filing Date: 2018-01
Publication Date: 2019-07
Patent Classification: ["415", "115000"]

Abstract:
A gas turbine engine component includes an airfoil that includes a trailing edge feed cavity. A baffle is located in the trailing edge feed cavity and includes a plurality of pressure side cooling openings in fluid communication with a corresponding one of a plurality of pressure side cooling passages. A plurality of suction side cooling openings are in fluid communication with a corresponding one of a plurality of suction side cooling passages.

Claim (Index 9):
The gas turbine engine component of  claim 1 , wherein the plurality of suction side cooling passages extend in an axial direction having an inlet to the suction side cooling passage upstream of an outlet to the suction side cooling passage.

Metadata:
- Claim Count in Document: 10.0
- Percentile: 86.0
- Lexical Diversity: 2.14286
- Patent Class: 415.0
- Transitional Phrase Type: none
- Component Type: 0
- Foreign Priority: False
- Related Applications: ['14974150', '14892713', '15708603', '14615509', '15433130']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.8449630370920682
- 35 USC 102 Novelty (BERT): 0.4788391265637132
- Combined Prediction Score: 0.8083506460392327
- Mean Citation Score: 330.3337860000001
- Max Citation Score: 340.48026
- Similarity Product: 263.19205339761254

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