PATENT CLAIM ANALYSIS

Application Number: 16013042
Application Type: Utility
Filing Date: 2018-06
Publication Date: 2018-10
Patent Classification: ["060", "039370"]

Abstract:
A gas turbine engine, in which a compressed gas from a compressor of an axial-flow type is burned in a combustor and an obtained combustion gas drives a turbine, includes: a diffuser of an annular shape connected to an outlet of the compressor, the diffuser including a diffuser inner tube and a diffuser outer tube that are tubular members disposed concentrically with each other; and a plurality of partition members that are disposed in a diffuser flow path, which is an annular space formed between the diffuser inner tube and the diffuser outer tube, and divide the diffuser flow path in a circumferential direction.

Claim (Index 3):
The gas turbine engine as claimed in  claim 1 , wherein an aspect ratio H/W of a height dimension H relative to a width dimension W of a flow-path cross section of each of divided diffuser flow paths which are formed by dividing the diffuser flow path with the partition members is larger at an outlet of the divided diffuser flow path than at an inlet of the divided diffuser flow path, and the aspect ratio of the flow-path cross section at the outlet of the divided diffuser flow path is within a range of 0.3 to 5.

Metadata:
- Claim Count in Document: 9.0
- Percentile: 94.0
- Lexical Diversity: 2.0
- Patent Class: 60.0
- Transitional Phrase Type: none
- Component Type: 0
- Foreign Priority: True
- Related Applications: ['16013396', '14913922', '15521717', '14105313', '13542674']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.7554064432873812
- 35 USC 102 Novelty (BERT): 0.5102828444111176
- Combined Prediction Score: 0.7308940833997548
- Mean Citation Score: 259.02597799999995
- Max Citation Score: 327.20984
- Similarity Product: 243.1185593766594

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