PATENT CLAIM ANALYSIS

Application Number: 16436177
Application Type: Utility
Filing Date: 2019-06
Publication Date: 2020-01
Patent Classification: ["340", "946000"]

Abstract:
In an embodiment, a rotorcraft includes: tail rotor blades; a tail rotor actuator coupled to the tail rotor blades such that the pitch of the tail rotor blades varies according to a current extension of the tail rotor actuator; pilot flight controls electrically coupled to the tail rotor actuator; and a flight control computer electrically coupled to the tail rotor actuator and the pilot flight controls, the flight control computer configured to: determine the current extension of the tail rotor actuator; determine whether the current extension of the tail rotor actuator is within a margin of a maximum extension of the tail rotor actuator; and indicate a first warning to a pilot in response to the current extension of the tail rotor actuator being within the margin of the maximum extension of the tail rotor actuator.

Claim (Index 3):
The rotorcraft of  claim 1 , wherein the flight control computer configured is further configured to determine the commanded position of the tail rotor actuator after providing the commanded position to the tail rotor actuator.

Metadata:
- Claim Count in Document: 3.0
- Percentile: 100.0
- Lexical Diversity: 3.24444
- Patent Class: 340.0
- Transitional Phrase Type: none
- Component Type: 0
- Foreign Priority: False
- Related Applications: ['15708767', '15646894', '15679645', '15484994', '15480152']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.7562425156829574
- 35 USC 102 Novelty (BERT): 0.5988076329637722
- Combined Prediction Score: 0.7404990274110389
- Mean Citation Score: 359.194398
- Max Citation Score: 519.4056
- Similarity Product: 435.7181970511437

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