PATENT CLAIM ANALYSIS

Application Number: 16034856
Application Type: Utility
Filing Date: 2018-07
Publication Date: 2018-11
Patent Classification: ["701", "002000"]

Abstract:
One example embodiment includes a vertical takeoff and landing (VTOL) unmanned aerial vehicle (UAV). The VTOL UAV includes a flight control system configured to provide avionic control of the VTOL UAV in a hover mode and in a level-flight mode. The VTOL UAV also includes a body encapsulating an engine and the flight control system. The VTOL UAV further includes a propeller disk coupled to the engine and configured to provide vertical thrust in the hover mode and to provide horizontal thrust for flight during the level-flight mode.

Claim (Index 14):
The method of  claim 10 , further comprising:\n changing an orientation of the VTOL UAV from the substantially horizontal orientation to the substantially vertical orientation; decreasing the engine speed to switch from the level-flight mode to the hover mode with a decreasing altitude; retracting the plurality of wings to the body at the first predetermined altitude in the hover mode; and landing the VTOL UAV on a landing pad via landing posts on an aft-section of the body opposite the propeller disk.

Metadata:
- Claim Count in Document: 45.0
- Percentile: 95.0
- Lexical Diversity: 2.18182
- Patent Class: 701.0
- Transitional Phrase Type: open
- Component Type: 1
- Foreign Priority: False
- Related Applications: ['14695693', '15256140', '15827776', '15786793', '12949410']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.5142505273676652
- 35 USC 102 Novelty (BERT): 0.6226988659229111
- Combined Prediction Score: 0.5250953612231898
- Mean Citation Score: 442.48869400000007
- Max Citation Score: 607.39655
- Similarity Product: 543.8366157472551

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