PATENT CLAIM ANALYSIS

Application Number: 16127640
Application Type: Utility
Filing Date: 2018-09
Publication Date: 2019-01
Patent Classification: ["244", "00700R"]

Abstract:
Systems, methods, and devices provide a vehicle, such as an aircraft, with rotors configured to function as a tri-copter for vertical takeoff and landing (“VTOL”) and a fixed-wing vehicle for forward flight. One rotor may be mounted at a front of the vehicle fuselage on a hinged structure controlled by an actuator to tilt from horizontal to vertical positions. Two additional rotors may be mounted on the horizontal surface of the vehicle tail structure with rotor axes oriented vertically to the fuselage. For forward flight of the vehicle, the front rotor may be rotated down such that the front rotor axis may be oriented horizontally along the fuselage and the front rotor may act as a propeller. For vertical flight, the front rotor may be rotated up such that the front rotor axis may be oriented vertically to the fuselage, while the tail rotors may be activated.

Claim (Index 14):
The tri-rotor vehicle of  claim 5 , wherein the wing is swept.

Metadata:
- Claim Count in Document: 1.0
- Percentile: 97.0
- Lexical Diversity: 2.32857
- Patent Class: 244.0
- Transitional Phrase Type: none
- Component Type: 0
- Foreign Priority: False
- Related Applications: ['15080167', '15332391', '14121001', '15494780', '13708612']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.8996506432617071
- 35 USC 102 Novelty (BERT): 0.6337289926803332
- Combined Prediction Score: 0.8730584782035697
- Mean Citation Score: 479.86585
- Max Citation Score: 700.92676
- Similarity Product: 559.2830545863009

Labels:
- Claim Label 101: 1
- Claim Label 102: 0
- Claim Label 103: 1
- Claim Label 112: 1
- Combined Label: 0
- Label 101 Adjusted: 1

Dataset: test