PATENT CLAIM ANALYSIS

Application Number: 16004924
Application Type: Utility
Filing Date: 2018-06
Publication Date: 2018-10
Patent Classification: ["244", "006000"]

Abstract:
This disclosure is generally directed to a High Speed vertical takeoff and landing (VTOL) aircraft that includes fixed wing flight capabilities. The High Speed VTOL aircraft may include at least two thrust producing rotors located equidistant from a longitudinal axis of the aircraft on a main wing, and at least two thrust producing rotors located equidistant from a longitudinal axis of the aircraft on a vertical wing. The rotors may be driven by electric motors. However, other power sources may be used such as combustion or hybrid engines. By adjusting the speed and/or the pitch of the rotors, the aircraft can transition from a vertical flight configuration to a horizontal flight configuration and back.

Claim (Index 9):
The aircraft as  claim 1  recites, wherein the thrust control from at least one of the first propulsion system or second propulsion system adjusts at least one of the pitch, roll, and yaw of the aircraft.

Metadata:
- Claim Count in Document: 50.0
- Percentile: 94.0
- Lexical Diversity: 1.7971
- Patent Class: 244.0
- Transitional Phrase Type: none
- Component Type: 0
- Foreign Priority: False
- Related Applications: ['14554892', '13708612', '14738675', '14559529', '15093845']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.8621532503269997
- 35 USC 102 Novelty (BERT): 0.5686082150521687
- Combined Prediction Score: 0.8327987467995167
- Mean Citation Score: 347.205998
- Max Citation Score: 476.07635
- Similarity Product: 388.36155398350365

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

Dataset: test