PATENT CLAIM ANALYSIS

Application Number: 16269227
Application Type: Utility
Filing Date: 2019-02
Publication Date: 2019-06
Patent Classification: ["244", "02300C"]

Abstract:
A manned or unmanned aircraft has a main body with a circular shape and a circular outer periphery. One or more rotor blades extend substantially horizontally outward from the main body at or about the circular outer periphery. In addition, one or more counter-rotation blades extend substantially horizontally outward from said main body at or about the circular outer periphery, but vertically offset from the main rotor blades.

Claim (Index 2):
The aircraft of  claim 1 , wherein the thrust pushes downward on said one or more flaps in the second position to tilt the aircraft downward at said one or more flaps in the second position.

Metadata:
- Claim Count in Document: 30.0
- Percentile: 99.0
- Lexical Diversity: 1.97297
- Patent Class: 244.0
- Transitional Phrase Type: none
- Component Type: 0
- Foreign Priority: False
- Related Applications: ['15600296', '15883781', '15058708', '14712062', '10672003']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.8785604947881287
- 35 USC 102 Novelty (BERT): 0.5018256764601909
- Combined Prediction Score: 0.840887012955335
- Mean Citation Score: 240.08223400000003
- Max Citation Score: 257.56122
- Similarity Product: 159.61245725430962

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