PATENT CLAIM ANALYSIS

Application Number: 15876579
Application Type: Utility
Filing Date: 2018-01
Publication Date: 2019-07
Patent Classification: ["416", "09700R"]

Abstract:
Components for gas turbine engines are provided. The components include a hot external wall that is exposed to hot gaspath air when installed within a gas turbine engine, and an interior impingement wall, wherein the interior impingement wall defines a feed cavity and at least one impingement cavity is defined between the impingement wall and the external wall. The impingement wall includes a plurality of impingement holes that fluidly connect the feed cavity to the at least one impingement cavity, the external wall includes a plurality of film holes that fluidly connect the at least one impingement cavity to an exterior surface of the external wall, and wherein the only source of cooling air within the at least one impingement cavity is the feed cavity.

Claim (Index 16):
The gas turbine engine of  claim 12 , further comprising a divider rib located within the feed cavity and arranged to divide the feed cavity into two or more feed sub-cavities.

Metadata:
- Claim Count in Document: 50.0
- Percentile: 86.0
- Lexical Diversity: 2.53846
- Patent Class: 416.0
- Transitional Phrase Type: open
- Component Type: 1
- Foreign Priority: False
- Related Applications: ['15791464', '15874070', '15723446', '15723473', '15723512']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.7922561724851545
- 35 USC 102 Novelty (BERT): 0.4681294427894623
- Combined Prediction Score: 0.7598434995155853
- Mean Citation Score: 318.343254
- Max Citation Score: 330.18033
- Similarity Product: 238.7325770581073

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