PATENT CLAIM ANALYSIS

Application Number: 16141741
Application Type: Utility
Filing Date: 2018-09
Publication Date: 2019-08
Patent Classification: ["244", "172300"]

Abstract:
In some embodiments, a rotor assembly for an aerial vehicle includes a main body; and four or more rotors having blades mounted relative to the main body for rotation about respective axes configured to provide thrust predominantly in a common direction. Respective blade trajectories of rotors of at least one pair of adjacent rotors of the four or more rotors rotate in different planes. The blade trajectories of the at least one pair of adjacent rotors partially overlap when viewed along a line containing the common direction.

Claim (Index 25):
The vertical take-off and landing aerial vehicle of  claim 14 , wherein the main body includes a fuselage.

Metadata:
- Claim Count in Document: 63.0
- Percentile: 97.0
- Lexical Diversity: 1.58621
- Patent Class: 244.0
- Transitional Phrase Type: none
- Component Type: 0
- Foreign Priority: False
- Related Applications: ['15328352', '15033788', '15095011', '12740005', '14855448']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.8369535454698668
- 35 USC 102 Novelty (BERT): 0.4925442325998534
- Combined Prediction Score: 0.8025126141828655
- Mean Citation Score: 200.770224
- Max Citation Score: 203.80978
- Similarity Product: 134.7451629942727

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