PATENT CLAIM ANALYSIS

Application Number: 15953209
Application Type: Utility
Filing Date: 2018-04
Publication Date: 2018-10
Patent Classification: ["244", "055000"]

Abstract:
An unmanned aircraft includes a propulsion system having a diesel or kerosene internal combustion engine and a charger device for engine charging. The propulsion system can be a hybrid propulsion system or a parallel hybrid propulsion system.

Claim (Index 23):
The unmanned aircraft of  claim 16 , wherein the controller is configured to control switching on and off of a first or second stage of the engine charging or the switching on and off of the electric motor, in accordance with at least one of the parameters of altitude, angle of a takeoff or landing flight to the vertical, desired velocity, allowable heat output, allowable operating noise level, or temperature.

Metadata:
- Claim Count in Document: 29.0
- Percentile: 91.0
- Lexical Diversity: 1.56
- Patent Class: 244.0
- Transitional Phrase Type: none
- Component Type: 0
- Foreign Priority: True
- Related Applications: ['15597597', '13867628', '14999343', '12334098', '14247608']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.8501551945090329
- 35 USC 102 Novelty (BERT): 0.5050100571689281
- Combined Prediction Score: 0.8156406807750225
- Mean Citation Score: 252.630814
- Max Citation Score: 267.051
- Similarity Product: 183.22326295799016

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