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1. (WO2018197772) RHOMBOHEDRAL-WING AIRCRAFT FOR VERTICAL TAKE-OFF AND/OR LANDING
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Pub. No.: WO/2018/197772 International Application No.: PCT/FR2018/050881
Publication Date: 01.11.2018 International Filing Date: 09.04.2018
IPC:
B64C 29/00 (2006.01) ,B64C 39/06 (2006.01) ,B64C 3/10 (2006.01) ,B64C 25/06 (2006.01) ,B64C 25/04 (2006.01)
B PERFORMING OPERATIONS; TRANSPORTING
64
AIRCRAFT; AVIATION; COSMONAUTICS
C
AEROPLANES; HELICOPTERS
29
Aircraft capable of landing or taking-off vertically
B PERFORMING OPERATIONS; TRANSPORTING
64
AIRCRAFT; AVIATION; COSMONAUTICS
C
AEROPLANES; HELICOPTERS
39
Aircraft not otherwise provided for
06
having disc- or ring-shaped wings
B PERFORMING OPERATIONS; TRANSPORTING
64
AIRCRAFT; AVIATION; COSMONAUTICS
C
AEROPLANES; HELICOPTERS
3
Wings
10
Shape of wings
B PERFORMING OPERATIONS; TRANSPORTING
64
AIRCRAFT; AVIATION; COSMONAUTICS
C
AEROPLANES; HELICOPTERS
25
Alighting gear
02
Undercarriages
06
fixed
B PERFORMING OPERATIONS; TRANSPORTING
64
AIRCRAFT; AVIATION; COSMONAUTICS
C
AEROPLANES; HELICOPTERS
25
Alighting gear
02
Undercarriages
04
Arrangement or disposition on aircraft
Applicants:
FLY-R [FR/FR]; 7 bis, rue Henri Cornu Base ULM de Cambaie 97460 SAINT-PAUL, FR
Inventors:
VARIGAS, François; FR
Agent:
CASSIOPI; 230 Avenue de l'Aube Rouge 34170 CASTELNAU LE LEZ, FR
Priority Data:
175351324.04.2017FR
Title (EN) RHOMBOHEDRAL-WING AIRCRAFT FOR VERTICAL TAKE-OFF AND/OR LANDING
(FR) AÉRONEF À VOILURE RHOMBOÉDRIQUE À DÉCOLLAGE ET/OU ATTERRISSAGE VERTICAL
Abstract:
(EN) The aircraft (10) comprises a fuselage (11) and a rhombohedral wing structure (12) comprising front wings (13, 14) mounted on a front wing-root support (17) and rear wings (15, 16) mounted on a rear wing-root support (18). At least two wings (13, 14) support an engine (24, 26) provided with a propeller (25, 27). The rear end of the fuselage supports an engine (21) provided with a propeller (22). The aircraft comprises means (28 to 35) for tilting said engines, the rotary shaft of each of the propellers being tilted between an orientation parallel to the main axis of the fuselage and an orientation perpendicular to the main axis of the fuselage and to an axis extending through the ends of the front wings.
(FR) L'aéronef (10) comporte un fuselage (11) et une voilure rhomboédrique (12) comportant des ailes avant (13, 14) montées sur un support d'emplanture avant (17) et des ailes arrière (15, 16) montées sur un support d'emplanture arrière(18). Au moins deux ailes (13, 14) portent un moteur (24, 26) muni d'une hélice(25, 27). L'extrémité arrière du fuselage porte un moteur (21) muni d'une hélice (22). L'aéronef comporte des moyens (28 à 35) de basculement de ces moteurs, l'arbre de rotation de chacune des hélices basculant entre une orientation parallèle à l'axe principal du fuselage et une orientation perpendiculaire à l'axe principal du fuselage et à un axe passant par les extrémités des ailes avant.
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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: French (FR)
Filing Language: French (FR)