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 3):
The gas turbine engine component of  claim 2 , further comprising a platform supporting the airfoil having a platform cooling passage in fluid communication with at least one of the plurality of suction side cooling passages.

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): 0.828656472259943
- 35 USC 102 Novelty (BERT): 0.4745878582597899
- Combined Prediction Score: 0.7932496108599276
- Mean Citation Score: 330.3337860000001
- Max Citation Score: 340.48026
- Similarity Product: 290.55763200345393

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