PATENT CLAIM ANALYSIS

Application Number: 16018640
Application Type: Utility
Filing Date: 2018-06
Publication Date: 2018-10
Patent Classification: ["060", "226100"]

Abstract:
A gas turbine engine has a fan section including a fan, a compressor section including a low pressure compressor and a high pressure compressor, a turbine section including a low pressure turbine and a high pressure turbine, and a gear reduction. The low pressure compressor and the low pressure turbine have a number of blades in each of at least one of a plurality of blade rows. The blades are rotatable at least some of the time at a rotational speed in operation. The number of blades in at least one row and the rotational speed are such that the following formula holds true for at least one row of the compressor rotor turbine: (number of blades×rotational speed)/60 s≥5500 Hz, and the rotational speed is in revolutions per minute.

Claim (Index 18):
The gas turbine engine as set forth in  claim 16 , wherein the formula results in a number greater than or equal to 6000 Hz for all of the rows of the low pressure compressor.

Metadata:
- Claim Count in Document: 80.0
- Percentile: 94.0
- Lexical Diversity: 2.38983
- Patent Class: 60.0
- Transitional Phrase Type: none
- Component Type: 0
- Foreign Priority: False
- Related Applications: ['15259232', '14016436', '13630276', '15014363', '14905994']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.7894357266685719
- 35 USC 102 Novelty (BERT): 0.5441023849548607
- Combined Prediction Score: 0.7649023924972008
- Mean Citation Score: 397.95533600000016
- Max Citation Score: 401.15308
- Similarity Product: 321.81093836769344

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

Dataset: test