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1. (WO2019028071) UNMANNED AIRCRAFT SYSTEM WITH SWAPPABLE COMPONENTS
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Pub. No.: WO/2019/028071 International Application No.: PCT/US2018/044690
Publication Date: 07.02.2019 International Filing Date: 31.07.2018
IPC:
B64C 39/02 (2006.01)
B PERFORMING OPERATIONS; TRANSPORTING
64
AIRCRAFT; AVIATION; COSMONAUTICS
C
AEROPLANES; HELICOPTERS
39
Aircraft not otherwise provided for
02
characterised by special use
Applicants:
PERRY, Paul [US/US]; US
LASZLO, Zoltan [US/US]; US
PARKER, Scott [US/US]; US
GOLDSBERRY, Nathan [US/US]; US
WADE, Bryan [US/US]; US
WYROBEK, Keenan [US/US]; US
BOOMGAARD, Brian [US/US]; US
LI, Zhefei [US/US]; US
BLASER, Sven [US/US]; US
Inventors:
PERRY, Paul; US
LASZLO, Zoltan; US
PARKER, Scott; US
GOLDSBERRY, Nathan; US
WADE, Bryan; US
WYROBEK, Keenan; US
BOOMGAARD, Brian; US
LI, Zhefei; US
BLASER, Sven; US
Agent:
NAGLE, Peter J.; US
HEMENWAY, S. Craig; US
ASARO, Elissa; US
ATKINSON, David S.; US
SCHULTE, Timothy R.; US
GUGGENHEIMER, Benno M.; US
OSTERLOTH, Gregory W.; US
PRENDERGAST, Paul J.; US
JARVIS, Peter M.; US
JONAS, Tamala R.; US
TREECE, Randolph E.; US
Priority Data:
62/540,00001.08.2017US
Title (EN) UNMANNED AIRCRAFT SYSTEM WITH SWAPPABLE COMPONENTS
(FR) SYSTÈME D'AÉRONEF SANS PILOTE AVEC COMPOSANTS POUVANT ÊTRE INTERCHANGÉS
Abstract:
(EN) An unmanned aerial vehicle may include a fuselage and an anchor structure coupled to the fuselage and including a wing retention structure and a power module retention structure. The unmanned aerial vehicle may also include a wing releasably coupled to the wing retention structure, thereby coupling the wing to the fuselage, and a power module releasably coupled to the power module retention structure, thereby coupling the power module to the fuselage.
(FR) L'invention concerne un véhicule aérien sans pilote, lequel véhicule peut comprendre un fuselage et une structure d'ancrage couplée au fuselage et comprenant une structure de maintien d'aile et une structure de maintien de module de puissance. Le véhicule aérien sans pilote peut également comprendre une aile couplée de manière libérable à la structure de maintien d'aile, de façon à coupler ainsi l'aile au fuselage, et un module de puissance couplé de manière libérable à la structure de maintien de module de puissance, de façon à coupler ainsi le module de puissance 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, DJ, DK, DM, DO, DZ, EC, EE, EG, ES, FI, GB, GD, GE, GH, GM, GT, HN, HR, HU, ID, IL, IN, IR, IS, JO, JP, KE, KG, KH, KN, KP, KR, KW, 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)