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 17):
The gas turbine engine of  claim 16 , further comprising a plurality of pressure side cooling holes extending through a pressure side of the airfoil in fluid communication with at least one of the plurality of pressure side cooling passages and the plurality of pressure side cooling passages extend in an axial direction.

Metadata:
- Claim Count in Document: 10.0
- Percentile: 86.0
- Lexical Diversity: 2.14286
- Patent Class: 415.0
- Transitional Phrase Type: open
- Component Type: 1
- Foreign Priority: False
- Related Applications: ['14974150', '14892713', '15708603', '14615509', '15433130']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.8287465307065346
- 35 USC 102 Novelty (BERT): 0.476620365423882
- Combined Prediction Score: 0.7935339141782694
- Mean Citation Score: 330.3337860000001
- Max Citation Score: 340.48026
- Similarity Product: 262.15041274012685

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