PATENT CLAIM ANALYSIS

Application Number: 15863441
Application Type: Utility
Filing Date: 2018-01
Publication Date: 2019-07
Patent Classification: ["416", "09700R"]

Abstract:
An airfoil for a gas turbine engine according to an example of the present disclosure includes a first cavity, a second cavity, and a rib extending from a suction sidewall to a pressure sidewall and separating the first cavity from the second cavity. The rib includes a central portion, a first edge portion extending from the pressure sidewall to the central portion, and a second edge portion extending from the suction sidewall to the central portion. The rib defines one or more communication openings from the first cavity to the second cavity in the first or second edge portion.

Claim (Index 10):
The airfoil for a gas turbine engine as recited in  claim 2 , wherein the first baffle includes a rib-interfacing portion, a first curved portion extending from the rib-interfacing portion, and a second curved portion extending from the rib-interfacing portion.

Metadata:
- Claim Count in Document: 2.0
- Percentile: 86.0
- Lexical Diversity: 2.65
- Patent Class: 416.0
- Transitional Phrase Type: none
- Component Type: 0
- Foreign Priority: False
- Related Applications: ['15863101', '15354172', '15028572', '15433130', '13599226']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.8038731001353987
- 35 USC 102 Novelty (BERT): 0.464320762106053
- Combined Prediction Score: 0.7699178663324642
- Mean Citation Score: 298.938096
- Max Citation Score: 318.2555200000001
- Similarity Product: 253.47011914032944

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