PATENT CLAIM ANALYSIS

Application Number: 15953421
Application Type: Utility
Filing Date: 2018-04
Publication Date: 2018-10
Patent Classification: ["244", "002000"]

Abstract:
A personal air vehicle may feature an air module that may be attached to a ground module. The air module may be equipped with exit vanes or vectored engine exhaust to provide redundant control effectors to the cyclic or collective pitch of at least one rotary wing under the control of a control system.

Claim (Index 6):
The personal air vehicle of  claim 5  wherein said monocyclic pitch is non-differential monocyclic pitch, said non-differential monocyclic pitch and said vanes providing said redundant control authority for aircraft pitch control when said rotary wings and said circular ducts are in said side-by-side configuration.

Metadata:
- Claim Count in Document: 1.0
- Percentile: 91.0
- Lexical Diversity: 1.4
- Patent Class: 244.0
- Transitional Phrase Type: none
- Component Type: 0
- Foreign Priority: False
- Related Applications: ['14684995', '13068601', '15205162', '15476612', '12549872']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.9186708873777164
- 35 USC 102 Novelty (BERT): 0.554135697599019
- Combined Prediction Score: 0.8822173683998467
- Mean Citation Score: 469.95584
- Max Citation Score: 542.4033
- Similarity Product: 327.32824021722075

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