PATENT CLAIM ANALYSIS

Application Number: 15863101
Application Type: Utility
Filing Date: 2018-01
Publication Date: 2019-07
Patent Classification: ["415", "115000"]

Abstract:
An airfoil for a gas turbine engine includes a cavity including an internal surface of an outer wall. A baffle is disposed within the cavity and spaced apart from the internal surface. A partition is disposed between the baffle and the internal surface to divide a space between the baffle and the internal surface into at least a first passage and a second passage. A gas turbine engine is also disclosed.

Claim (Index 9):
The airfoil as recited in  claim 1 , wherein the partition comprises a first partition and a second partition dividing space between the baffle and the internal surface into the first passage and the second passage and a third passage.

Metadata:
- Claim Count in Document: 1.0
- Percentile: 86.0
- Lexical Diversity: 1.875
- Patent Class: 415.0
- Transitional Phrase Type: none
- Component Type: 0
- Foreign Priority: False
- Related Applications: ['15028572', '13599226', '14911148', '15114196', '12413649']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.8412750038217213
- 35 USC 102 Novelty (BERT): 0.4717102318232385
- Combined Prediction Score: 0.8043185266218731
- Mean Citation Score: 281.781092
- Max Citation Score: 319.1912
- Similarity Product: 251.2634232034684

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

Dataset: test