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1. (WO2017037698) FOLDABLE WINGS FOR AN UNMANNED AIR VEHICLE
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Pub. No.: WO/2017/037698 International Application No.: PCT/IL2016/050935
Publication Date: 09.03.2017 International Filing Date: 25.08.2016
IPC:
F42B 10/14 (2006.01) ,B64C 3/56 (2006.01)
F MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
42
AMMUNITION; BLASTING
B
EXPLOSIVE CHARGES, e.g. FOR BLASTING; FIREWORKS; AMMUNITION
10
Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
02
Stabilising arrangements
14
using fins spread or deployed after launch, e.g. after leaving the barrel
B PERFORMING OPERATIONS; TRANSPORTING
64
AIRCRAFT; AVIATION; COSMONAUTICS
C
AEROPLANES; HELICOPTERS
3
Wings
38
Adjustment of complete wings or parts thereof
56
Folding or collapsing to reduce overall dimensions of aircraft
Applicants:
UVISION AIR LTD [IL/IL]; 4, Bazelet St., Industrial park, 4486200 Zur Igal, IL
Inventors:
KAHLON, Moshe; IL
MORAG, Amit; IL
Agent:
GIGI, Eli; IL
Priority Data:
24120106.09.2015IL
Title (EN) FOLDABLE WINGS FOR AN UNMANNED AIR VEHICLE
(FR) AILES PLIABLES POUR VÉHICULE AÉRIEN SANS PILOTE
Abstract:
(EN) 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.
(FR) L'invention concerne un véhicule aérien sans pilote (UAV) comprenant un fuselage, un moyen de propulsion pliable pour générer une poussée entraînant le mouvement d'UAV, un moyen d'entraînement pour entraîner le moyen de propulsion, et une pluralité d'actionneurs de surfaces de commande de vol. L'UAV comprend en outre au moins une paire d'ailes pliables, la partie arrière des ailes étant fixée de façon pivotante au fuselage. Les ailes comportant au moins une surface de commande de roulement articulée à au moins l'une des ailes pliables. Au moins une paire de stabilisateurs de queue comportant des surfaces de commande de vol d'empennage papillon articulées aux stabilisateurs de queue. Dans une position entièrement étendue ou une position d'état de vol, les ailes pliables sont déployées perpendiculairement l'une à l'autre et perpendiculairement au fuselage pour former des ailes en forme de décalage en x et, dans une position rangée, les ailes sont positionnées parallèlement l'une à l'autre et positionnées parallèlement au fuselage.
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Designated States: AE, AG, AL, AM, AO, AT, AU, AZ, BA, BB, BG, BH, BN, BR, BW, BY, BZ, CA, CH, CL, CN, CO, CR, CU, CZ, DE, DK, DM, DO, DZ, EC, EE, EG, ES, FI, GB, GD, GE, GH, GM, GT, HN, HR, HU, ID, IL, IN, IR, IS, JP, KE, KG, KN, KP, KR, KZ, LA, LC, LK, LR, LS, LU, LY, MA, MD, ME, MG, MK, MN, MW, MX, MY, MZ, NA, NG, NI, NO, NZ, OM, PA, PE, PG, PH, PL, PT, QA, RO, RS, RU, RW, SA, SC, SD, SE, SG, SK, SL, SM, ST, SV, SY, TH, TJ, TM, TN, TR, TT, TZ, UA, UG, US, UZ, VC, VN, ZA, ZM, ZW
African Regional Intellectual Property Organization (ARIPO) (BW, GH, GM, KE, LR, LS, MW, MZ, NA, RW, SD, SL, ST, SZ, TZ, UG, ZM, ZW)
Eurasian Patent Office (AM, AZ, BY, KG, KZ, RU, TJ, TM)
European Patent Office (EPO) (AL, AT, BE, BG, CH, CY, CZ, DE, DK, EE, ES, FI, FR, GB, GR, HR, HU, IE, IS, IT, LT, LU, LV, MC, MK, MT, NL, NO, PL, PT, RO, RS, SE, SI, SK, SM, TR)
African Intellectual Property Organization (BF, BJ, CF, CG, CI, CM, GA, GN, GQ, GW, KM, ML, MR, NE, SN, TD, TG)
Publication Language: English (EN)
Filing Language: English (EN)