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 19):
The gas turbine engine as recited in  claim 18 , comprising\n a rotor section axially spaced from the vane section with respect to an engine central longitudinal axis, wherein the support includes an orifice configured to provide fluid communication between the platform cavity and a pressurized cavity provided at least partially by the rotor section.

Metadata:
- Claim Count in Document: 11.0
- Percentile: 86.0
- Lexical Diversity: 2.31034
- Patent Class: 415.0
- Transitional Phrase Type: open
- Component Type: 1
- Foreign Priority: False
- Related Applications: ['15884473', '13585274', '15252874', '14618035', '15810279']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.7952117100797201
- 35 USC 102 Novelty (BERT): 0.4501735213302923
- Combined Prediction Score: 0.7607078912047774
- Mean Citation Score: 221.89896
- Max Citation Score: 270.07062
- Similarity Product: 226.5905987610913

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