PATENT CLAIM ANALYSIS

Application Number: 15889065
Application Type: Utility
Filing Date: 2018-02
Publication Date: 2018-08
Patent Classification: ["415", "116000"]

Abstract:
A gas turbine ring segment for a gas turbine. The gas turbine ring segment includes an impingement target wall having an impingement target surface formed in one side, in a direction of a main cavity, and a hot side surface formed on the other side, in which the main cavity is located in a central portion in an axial direction. Cooling holes allowing an inside to communicate with an outside are arranged along the outer circumferential surface at predetermined distances from each other, each of the cooling holes having a straight structure communicating with the main cavity located in the central portion in the axial direction. This configuration consequently omits the structure comprised of a plurality of cooling holes, which has been necessary in the related art, such that the ceramic core that has been necessarily used during machining is unnecessary, thereby significantly reducing machining time and costs.

Claim (Index 8):
The gas turbine ring segment according to  claim 1 , wherein each of the cooling holes comprises different-diameter cooling holes communicating with each other.

Metadata:
- Claim Count in Document: 39.0
- Percentile: 88.0
- Lexical Diversity: 1.91566
- Patent Class: 415.0
- Transitional Phrase Type: none
- Component Type: 0
- Foreign Priority: True
- Related Applications: ['12840671', '12861339', '12763723', '14264552', '12839481']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.8132718475494466
- 35 USC 102 Novelty (BERT): 0.4456762131934089
- Combined Prediction Score: 0.7765122841138429
- Mean Citation Score: 209.549128
- Max Citation Score: 216.29974
- Similarity Product: 157.16265433611397

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