PATENT CLAIM ANALYSIS

Application Number: 16072540
Application Type: Utility
Filing Date: 2018-07
Publication Date: 2019-02
Patent Classification: ["415", "132000"]

Abstract:
A gas turbine having an axially adjustable rotor, has the following components: at least one external compressor air bleed for bleeding compressor air; a control valve for adjusting the amount of compressor air bled via the at least one external compressor air bleed; an axial thrust piston that can be supplied with the compressor bleed air via a supply line in such a way that a different axial compensation thrust is applied to same when the amount of compressor bleed air is adjusted; and a radial bearing which cooperates with the axial thrust piston for bearing purposes, and which can also be directly or indirectly supplied with the compressor bleed air via the supply line.

Claim (Index 3):
The gas turbine as claimed in  claim 1 ,\n wherein the axial thrust piston and the radial bearing are interconnected in parallel with regard to the supply with compressor air.

Metadata:
- Claim Count in Document: 17.0
- Percentile: 95.0
- Lexical Diversity: 1.90625
- Patent Class: 415.0
- Transitional Phrase Type: none
- Component Type: 0
- Foreign Priority: True
- Related Applications: ['12073980', '15399457', '10546883', '11007817', '12167800']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.8083477679766453
- 35 USC 102 Novelty (BERT): 0.443067658306255
- Combined Prediction Score: 0.7718197570096064
- Mean Citation Score: 200.648474
- Max Citation Score: 205.1367
- Similarity Product: 148.56251903547047

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

Dataset: test