PATENT CLAIM ANALYSIS

Application Number: 15873496
Application Type: Utility
Filing Date: 2018-01
Publication Date: 2019-07
Patent Classification: ["415", "173100"]

Abstract:
An assembly for use in a turbine section of a gas turbine engine, the assembly including: a blade outer air seal having a forward end and opposite aft end and a pair of opposing sides extending between the forward end and the opposite aft end; a blade outer air seal support, the blade outer air seal support having a rail with at least one scalloped opening, the rail engaging a hook located at the forward end of the blade outer air seal when the blade outer air seal is secured to the blade outer air seal support, wherein two points of contact are made between the hook and the rail of the blade outer air seal support when the blade outer air seal is secured to the blade outer air seal support; and a vane platform, that receives and supports a rail of the blade outer air seal, the rail being located at the aft end of the blade outer air seal and the rail extends continuously between the pair of opposing sides of the blade outer air seal, wherein a single point of contact is made between the rail of the blade outer air seal and the vane platform when the blade outer air seal is secured to the vane platform.

Claim (Index 19):
A method of supporting a blade outer air seal of a gas turbine engine, the method comprising:\n supporting a forward end of the blade outer air seal with a blade outer air seal support, the blade outer air seal support having a rail with at least one scalloped opening and the rail engages a hook located at the forward end of the blade outer air seal when the blade outer air seal is secured to the blade outer air seal support, wherein two points of contact are made between the hook of the blade outer air seal and the rail of the blade outer air seal support when the blade outer air seal is secured to the blade outer air seal support; and supporting an opposite aft end of the blade outer air seal with a vane platform, wherein the vane platform receives and supports a rail of the blade outer air seal, the rail being located on an aft end of the blade outer air seal and extends continuously between a pair of opposing sides of the blade outer air seal, wherein a single point contact is made between the rail of the blade outer air seal and the vane platform when the blade outer air seal is secured to the vane platform.

Metadata:
- Claim Count in Document: 2.0
- Percentile: 86.0
- Lexical Diversity: 3.53968
- Patent Class: 415.0
- Transitional Phrase Type: open
- Component Type: 1
- Foreign Priority: False
- Related Applications: ['15813083', '15339581', '15017798', '15806830', '13731154']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.8265243469188962
- 35 USC 102 Novelty (BERT): 0.480742018130205
- Combined Prediction Score: 0.791946114040027
- Mean Citation Score: 327.021462
- Max Citation Score: 353.88153
- Similarity Product: 280.99658381224395

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