PATENT CLAIM ANALYSIS

Application Number: 16031340
Application Type: Utility
Filing Date: 2018-07
Publication Date: 2019-01
Patent Classification: ["416", "22300A"]

Abstract:
The invention relates to a rotor of a turbomachine, which has a plurality of rotor blades, which each have a blade leading edge and a tip, the rotor blades forming a first group and at least one further group of rotor blades of different construction. It is provided that the rotor blades of the first group are nominal rotor blades, the rotor blades of the at least one further group each have a material cutout in the transition from the blade leading edge to the tip, said material cutout not being present in the case of the rotor blades of the first group, and the rotor blades of the first group and of the at least one further group form a non-periodic sequence in the circumferential direction.

Claim (Index 15):
The rotor according to  claim 1 , wherein the rotor is formed with a BLISK design.

Metadata:
- Claim Count in Document: 23.0
- Percentile: 95.0
- Lexical Diversity: 2.59615
- Patent Class: 416.0
- Transitional Phrase Type: none
- Component Type: 0
- Foreign Priority: True
- Related Applications: ['15018072', '15163990', '15326505', '12494595', '12078608']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.7731988288299506
- 35 USC 102 Novelty (BERT): 0.4540577288790037
- Combined Prediction Score: 0.7412847188348559
- Mean Citation Score: 217.209948
- Max Citation Score: 218.45244
- Similarity Product: 135.05791123960017

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