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 15):
The air vehicle of  claim 9 , wherein the processor and the at least one drive motor are further configured to:\n induce a backward pitching moment in the air vehicle in response to:\n a deflection of first and second flapping wings during a first portion of a forward stroke of the flapping more than during a second portion of the forward stroke of the 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): 0.9136148690331704
- 35 USC 102 Novelty (BERT): 0.6309391986125044
- Combined Prediction Score: 0.8853473019911039
- Mean Citation Score: 636.0661759999998
- Max Citation Score: 768.1531
- Similarity Product: 529.8438229772329

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