PATENT CLAIM ANALYSIS

Application Number: 15903824
Application Type: Utility
Filing Date: 2018-02
Publication Date: 2019-08
Patent Classification: ["415", "173100"]

Abstract:
A turbine shroud or other assembly adapted for use in a gas turbine engine is disclosed in this paper. In illustrative embodiments, a metallic carrier included in the assembly is configured to be manufactured by casting or additive layer manufacturing.

Claim (Index 1):
A turbine shroud adapted mount outward of blades included in a turbine wheel assembly and block gasses from passing over the blades without interacting with the blades, the turbine shroud comprising\n a blade track segment comprising ceramic matrix composite materials, the blade track segment including a runner that extends partway around a central axis to face a primary gas path of the gas turbine engine and an attachment feature that extends radially outward from the runner away from the central axis, and a carrier segment comprising metallic materials and configured to be mounted to other metallic components within the gas turbine engine, the carrier segment shaped to form a relief of a portion of a radially-outwardly facing side of the blade track segment such that a constant gap is formed between a portion of the runner and the attachment feature.

Metadata:
- Claim Count in Document: 36.0
- Percentile: 88.0
- Lexical Diversity: 1.22857
- Patent Class: 415.0
- Transitional Phrase Type: open
- Component Type: 1
- Foreign Priority: False
- Related Applications: ['15004436', '14970748', '14950794', '15097343', '15264280']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.8432838186737746
- 35 USC 102 Novelty (BERT): 0.4811786523347598
- Combined Prediction Score: 0.807073302039873
- Mean Citation Score: 341.71587
- Max Citation Score: 350.35904
- Similarity Product: 308.41982570129386

Labels:
- Claim Label 101: 1
- Claim Label 102: 0
- Claim Label 103: 1
- Claim Label 112: 1
- Combined Label: 0
- Label 101 Adjusted: 1

Dataset: test