PATENT CLAIM ANALYSIS

Application Number: 15923878
Application Type: Utility
Filing Date: 2018-03
Publication Date: 2018-07
Patent Classification: ["244", "022000"]

Abstract:
Heavier-than-air, aircraft having flapping wings, e.g., ornithopters, where angular orientation control is effected by variable differential sweep angles of deflection of the flappable wings in the course of sweep angles of travel and/or the control of variable wing membrane tension.

Claim (Index 9):
The air vehicle of  claim 8 , wherein the processor and the at least one drive motor are further configured to:\n drive the first and second flapping wings to flap horizontally about a fuselage, wherein the first and second flapping wings have a first and second variable differential sweep angles of deflection, respectively; and provide vertical and horizontal air vehicle orientation control in response to the horizontal flapping.

Metadata:
- Claim Count in Document: 2.0
- Percentile: 90.0
- Lexical Diversity: 1.45161
- Patent Class: 244.0
- Transitional Phrase Type: none
- Component Type: 0
- Foreign Priority: False
- Related Applications: ['14198418', '12795539', '13023772', '14247062', '13969258']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.9113824127941296
- 35 USC 102 Novelty (BERT): 0.6490098453522808
- Combined Prediction Score: 0.8851451560499446
- Mean Citation Score: 636.0661759999998
- Max Citation Score: 768.1531
- Similarity Product: 578.7778008240102

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