PATENT CLAIM ANALYSIS

Application Number: 15895589
Application Type: Utility
Filing Date: 2018-02
Publication Date: 2020-01
Patent Classification: ["416", "001000"]

Abstract:
An aircraft includes a first rotor assembly, a second rotor assembly, and a rotor phase angle control system. The system includes a phase adjustor operably associated with the first rotor assembly and the second rotor assembly. The method includes sensing vibrations exerted on the aircraft and offsetting a phase angle of the first rotor assembly and the second rotor assembly to minimize the vibrations.

Claim (Index 2):
The method of  claim 1 , further comprising:\n relaying the sensed vibration to a control system operably associated with the phase adjustor; and commanding the phase adjustor via the control system to adjust the phase angle of the two or more rotor assemblies.

Metadata:
- Claim Count in Document: 1.0
- Percentile: 88.0
- Lexical Diversity: 2.3
- Patent Class: 416.0
- Transitional Phrase Type: open
- Component Type: 1
- Foreign Priority: False
- Related Applications: ['14174004', '14494036', '14533276', '15606197', '15820129']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.7273956330268432
- 35 USC 102 Novelty (BERT): 0.4227775586416872
- Combined Prediction Score: 0.6969338255883276
- Mean Citation Score: 131.388212
- Max Citation Score: 199.69374
- Similarity Product: 160.85658689963938

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