PATENT CLAIM ANALYSIS

Application Number: 15755669
Application Type: Utility
Filing Date: 2018-02
Publication Date: 2019-01
Patent Classification: ["244", "049000"]

Abstract:
An unmanned air vehicle (UAV) having a fuselage, a foldable propulsion means to generate thrust leading to the UAV movement, a driving means to drive the propulsion means and a plurality of flight control surfaces actuators are further included. The UAV further includes at least one pair of foldable wings where the rear portion of the wings is pivotally attached to the fuselage. The wings having at least one roll control surface hinged to at least one of the foldable wings. At least a pair of tail stabilizers having ruddervators flight control surfaces hinged to the tail stabilizers. In a fully extended position or in ready to fly state position, each of the foldable wings are deployed perpendicular to one another and perpendicular to the fuselage to form an offset-x shaped wings, and in a stowed position, each of the wings are positioned parallel to one another and positioned parallel to the fuselage.

Claim (Index 1):
An unmanned air vehicle (UAV) having a fuselage comprising:\n a plurality of flight control surfaces actuators; at least one pair of foldable wings where the rear portion of said wings are pivotally attached to said fuselage, said wings having at least one roll flight control surface hinged to said at least one of said foldable wing; at least pair of tail stabilizers having ruddervators flight control surfaces hinged to said tail stabilizers; wherein, in a fully extended position or in ready to fly state position, each of said foldable wings are deployed perpendicular to one another and perpendicular to said fuselage to form an offset-x shaped wings, and when said UAV is in a stowed position, each of said wings are positioned parallel to one another and lie stowed parallel to said fuselage; wherein, in particular when the width of said foldable wings are wider than the width or diameter of said fuselage, said UAV further comprising a coupling mechanisms means having an axial pins combined with springs and latching means, wherein, said coupling mechanisms are attached to said fuselage and to each of said wings in a stowed position and in a fully deployed position, wherein in said stowed position said pins extend outwardly from said fuselage, thereby causing said wings to decouple from said fuselage to about the extended pin distance, and wherein, in said fully deployed position said pins return back to a non-extended position and said wings are coupled to said fuselage, thereby reducing wind gust about any axis of said UAV when said UAV is in a flight state.

Metadata:
- Claim Count in Document: 1.0
- Percentile: 88.0
- Lexical Diversity: 2.26027
- Patent Class: 244.0
- Transitional Phrase Type: open
- Component Type: 1
- Foreign Priority: True
- Related Applications: ['12230638', '14179697', '11803720', '15198946', '14260889']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.8486794291445181
- 35 USC 102 Novelty (BERT): 0.5085039242341716
- Combined Prediction Score: 0.8146618786534835
- Mean Citation Score: 303.126492
- Max Citation Score: 314.7743200000001
- Similarity Product: 256.9888817406703

Labels:
- Claim Label 101: 1
- Claim Label 102: 1
- Claim Label 103: 1
- Claim Label 112: 0
- Combined Label: 1
- Label 101 Adjusted: 1

Dataset: test