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 4):
The gas turbine rotor according to  claim 1 , wherein\n the second rotor includes a sleeve surrounding the inner hollow space and an outer cylinder surrounding the sleeve, the sleeve includes a protruding portion protruding from the outer cylinder, and the protruding portion is in contact with 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): 0.6337648593405757
- 35 USC 102 Novelty (BERT): 0.4846105215338033
- Combined Prediction Score: 0.6188494255598985
- Mean Citation Score: 179.69098799999998
- Max Citation Score: 185.98508
- Similarity Product: 130.1341813376236

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