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 3):
The method of  claim 1 , further comprising:\n disengaging and reengaging the first shaft via the phase adjustor; wherein the disengaging and reengaging the first shaft causes the first rotor assembly to offset from the second rotor assembly, thereby creating the phase angle between the two 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): 0.7270730263792292
- 35 USC 102 Novelty (BERT): 0.424358753209287
- Combined Prediction Score: 0.696801599062235
- Mean Citation Score: 131.388212
- Max Citation Score: 199.69374
- Similarity Product: 158.44014164355042

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