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 2):
The vehicle of  claim 1 , further comprising a first control flap and a second control flap that are each coupled to the body and are respectively offset equally and oppositely with respect to a central axis of the body and substantially entirely within a propeller wash of the propeller disk that is defined by a diameter of the propeller disk, the first and second control flaps being controlled by the flight control system to provide rotation and lateral motion control of the VTOL UAV during the hover mode.

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): 0.5073900706277611
- 35 USC 102 Novelty (BERT): 0.6395940206808737
- Combined Prediction Score: 0.5206104656330723
- Mean Citation Score: 442.48869400000007
- Max Citation Score: 607.39655
- Similarity Product: 604.0815260712802

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