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 19):
The method as  claim 17  recites, further comprising:\n inducing a yaw motion by varying the speed of at least one of the first and second variable speed rotors; and \n inducing a pitch motion by varying the speed of at least one of the third and fourth variable speed rotors.

Metadata:
- Claim Count in Document: 50.0
- Percentile: 94.0
- Lexical Diversity: 1.7971
- Patent Class: 244.0
- Transitional Phrase Type: open
- Component Type: 1
- Foreign Priority: False
- Related Applications: ['14554892', '13708612', '14738675', '14559529', '15093845']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.8445497653541438
- 35 USC 102 Novelty (BERT): 0.5783874308972273
- Combined Prediction Score: 0.8179335319084522
- Mean Citation Score: 347.205998
- Max Citation Score: 476.07635
- Similarity Product: 460.6824859026939

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