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 1):
An air vehicle apparatus, comprising:\n first and second flapping control surfaces; wherein the first and second flapping control surfaces are capable of providing hovering and control moments without the benefit of additional control surfaces; and wherein the hovering and control moments are selected from at least one of: variable differential sweep angles of deflection of the first and second flappable wings in the course of respective sweep angles of travel, variable differential luffing of the respective first and second flapping wings, and variable and differential angular velocity of the respective first and second flapping wings.

Metadata:
- Claim Count in Document: 2.0
- Percentile: 90.0
- Lexical Diversity: 1.45161
- Patent Class: 244.0
- Transitional Phrase Type: open
- Component Type: 1
- Foreign Priority: False
- Related Applications: ['14198418', '12795539', '13023772', '14247062', '13969258']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.9017699914210656
- 35 USC 102 Novelty (BERT): 0.6435104016548989
- Combined Prediction Score: 0.8759440324444489
- Mean Citation Score: 636.0661759999998
- Max Citation Score: 768.1531
- Similarity Product: 569.5046360683978

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