PATENT CLAIM ANALYSIS

Application Number: 15884494
Application Type: Utility
Filing Date: 2018-01
Publication Date: 2019-08
Patent Classification: ["415", "115000"]

Abstract:
A vane section of a gas turbine engine according to an example of the present disclosure includes a platform and an airfoil extending outwardly from the platform and having an internal channel communicating with an opening in the platform. A rail extends inwardly from the platform, such that a surface of the platform opposite the airfoil and the rail at least partially define a platform cavity. A flow diverter extends inwardly of the platform within the platform cavity and defines a diverter cavity, an inlet configured to receive fluid flowing in a first direction from the opening in the platform to the diverter cavity, and an outlet configured to expel fluid from the diverter cavity to the platform cavity in a second direction different from the first direction.

Claim (Index 16):
The gas turbine engine as recited in  claim 12 , wherein the first direction has a major component in a radially inward direction from the internal channel to the platform cavity, and the second direction has a major component in a circumferential direction between a pressure side surface of the platform and a suction side surface of the platform.

Metadata:
- Claim Count in Document: 11.0
- Percentile: 86.0
- Lexical Diversity: 2.31034
- Patent Class: 415.0
- Transitional Phrase Type: none
- Component Type: 0
- Foreign Priority: False
- Related Applications: ['15884473', '13585274', '15252874', '14618035', '15810279']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.8138727931724669
- 35 USC 102 Novelty (BERT): 0.4526236603612171
- Combined Prediction Score: 0.777747879891342
- Mean Citation Score: 221.89896
- Max Citation Score: 270.07062
- Similarity Product: 225.99117751760605

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