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1. (WO2018048644) TILTROTOR PROPULSION SYSTEM FOR AN AIRCRAFT
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Pub. No.: WO/2018/048644 International Application No.: PCT/US2017/048764
Publication Date: 15.03.2018 International Filing Date: 25.08.2017
IPC:
B64C 11/00 (2006.01) ,B64C 11/46 (2006.01) ,B64C 29/00 (2006.01)
B PERFORMING OPERATIONS; TRANSPORTING
64
AIRCRAFT; AVIATION; COSMONAUTICS
C
AEROPLANES; HELICOPTERS
11
Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
B PERFORMING OPERATIONS; TRANSPORTING
64
AIRCRAFT; AVIATION; COSMONAUTICS
C
AEROPLANES; HELICOPTERS
11
Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
46
Arrangements of, or constructional features peculiar to, multiple propellers
B PERFORMING OPERATIONS; TRANSPORTING
64
AIRCRAFT; AVIATION; COSMONAUTICS
C
AEROPLANES; HELICOPTERS
29
Aircraft capable of landing or taking-off vertically
Applicants:
GENERAL ELECTRIC COMPANY [US/US]; 1 River Road Schenectady, NY 12345, US
Inventors:
VONDRELL, Randy, M.; US
POLAKOWSKI, Matthew, Ryan; US
MURROW, Kurt, David; US
CRABTREE, Glenn; US
ZATORSKI, Darek, Tomasz; US
Agent:
MUNNERLYN, William, S.; US
MIDGLEY, Stephen, G.; US
DIMAURO, Peter, T.; US
WINTER, Catherine, J.; US
GNIBUS, Michael, M.; US
Priority Data:
15/259,59608.09.2016US
Title (EN) TILTROTOR PROPULSION SYSTEM FOR AN AIRCRAFT
(FR) SYSTÈME DE PROPULSION À ROTORS BASCULANTS POUR AÉRONEF
Abstract:
(EN) An aircraft includes a fuselage, a forward wing assembly, and aft wing assembly, and a propulsion system. The propulsion system includes a first primary thrust propulsor and a first secondary thrust propulsor, the first primary thrust propulsor being different than the first secondary thrust propulsor. Both the first primary thrust propulsor and the first secondary thrust propulsor are mounted to the same one of: a starboard side of the aft wing assembly, a port side of the aft wing assembly, a starboard side of the forward wing assembly, or a port side of the forward wing assembly.
(FR) L'invention concerne un aéronef comprenant un fuselage, un ensemble aile avant et un ensemble aile arrière, ainsi qu'un système de propulsion. Le système de propulsion comprend un premier propulseur de poussée primaire et un premier propulseur de poussée secondaire, le premier propulseur de poussée primaire étant différent du premier propulseur de poussée secondaire. Le premier propulseur de poussée primaire et le premier propulseur de poussée secondaire sont tous deux montés sur le même côté parmi : un côté tribord de l'ensemble aile arrière, un côté bâbord de l'ensemble aile arrière, un côté tribord de l'ensemble aile avant ou un côté bâbord de l'ensemble aile 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: English (EN)
Filing Language: English (EN)