PATENT CLAIM ANALYSIS

Application Number: 16032093
Application Type: Utility
Filing Date: 2018-07
Publication Date: 2019-01
Patent Classification: ["290", "052000"]

Abstract:
A gas turbine rotor includes a first rotor and a second rotor. The first rotor includes a compressor impeller, a turbine wheel, and a shaft. The turbine wheel has a common rotational axis with the compressor impellor. The shaft connects the compressor impeller to the turbine wheel. The second rotor is an electric generator rotor and defines an inner hollow space. The shaft includes an insertable portion disposed in the inner hollow space of the second rotor.

Claim (Index 5):
The gas turbine rotor according to  claim 1 , wherein\n the compressor impeller and the turbine wheel define a first gap therebetween, the first gap has a distal end in radial directions, the radial directions being perpendicular to axial directions, the axial directions indicating directions in which the common rotational axis extends, and the distal end has a length in the axial directions equal to or shorter than 25% of a diameter of the compressor impeller.

Metadata:
- Claim Count in Document: 1.0
- Percentile: 95.0
- Lexical Diversity: 2.23684
- Patent Class: 290.0
- Transitional Phrase Type: none
- Component Type: 0
- Foreign Priority: True
- Related Applications: ['10747386', '10862136', '14229677', '12300726', '14588529']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.6352511320524141
- 35 USC 102 Novelty (BERT): 0.4783732211706891
- Combined Prediction Score: 0.6195633409642417
- Mean Citation Score: 179.69098799999998
- Max Citation Score: 185.98508
- Similarity Product: 138.1762779641724

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