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1. (WO2018038909) AIR INTAKE SYSTEMS AND METHODS OF ASSEMBLY THEREOF
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Pub. No.: WO/2018/038909 International Application No.: PCT/US2017/045881
Publication Date: 01.03.2018 International Filing Date: 08.08.2017
IPC:
B64D 11/00 (2006.01) ,B64D 27/10 (2006.01) ,B64D 27/18 (2006.01) ,B64D 27/16 (2006.01) ,B64D 33/02 (2006.01) ,B64D 33/08 (2006.01)
B PERFORMING OPERATIONS; TRANSPORTING
64
AIRCRAFT; AVIATION; COSMONAUTICS
D
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS
11
Passenger or crew accommodation; Flight-deck installations not otherwise provided for
B PERFORMING OPERATIONS; TRANSPORTING
64
AIRCRAFT; AVIATION; COSMONAUTICS
D
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS
27
Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
02
Aircraft characterised by the type or position of power plant
10
of gas-turbine type
B PERFORMING OPERATIONS; TRANSPORTING
64
AIRCRAFT; AVIATION; COSMONAUTICS
D
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS
27
Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
02
Aircraft characterised by the type or position of power plant
16
of jet type
18
within, or attached to, wing
B PERFORMING OPERATIONS; TRANSPORTING
64
AIRCRAFT; AVIATION; COSMONAUTICS
D
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS
27
Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
02
Aircraft characterised by the type or position of power plant
16
of jet type
B PERFORMING OPERATIONS; TRANSPORTING
64
AIRCRAFT; AVIATION; COSMONAUTICS
D
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS
33
Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
02
of combustion air intakes
B PERFORMING OPERATIONS; TRANSPORTING
64
AIRCRAFT; AVIATION; COSMONAUTICS
D
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS
33
Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
08
of power plant cooling systems
Applicants:
GENERAL ELECTRIC COMPANY [US/US]; 1 River Road Schenectady, NY 12345, US
Inventors:
DIAZ, Carlos, Enrique; DE
HERNANDEZ, Alvaro, Enrique; US
BALADI, Mehdi, Milani; IT
KIMBALL, David, William; US
Agent:
KACHUR, Pamela A.; US
GNIBUS, Michael, M.; US
KACHUR, Pamela, A.; US
MIDGLEY, Stephen, G.; US
WINTER, Catherine, J.; US
Priority Data:
10201600008651122.08.2016IT
Title (EN) AIR INTAKE SYSTEMS AND METHODS OF ASSEMBLY THEREOF
(FR) SYSTÈMES D'ENTRÉE D'AIR ET LEURS PROCÉDÉS DE MONTAGE
Abstract:
(EN) An air intake system includes an exterior housing for a vehicle, the exterior housing including an outer surface including a recessed portion defined therein. The recessed portion includes an angled bottom member having a first end and a second end that is coupled to the outer surface. The recessed portion further includes a first sidewall, a second sidewall opposing the first sidewall, and an inlet opening defined within the recessed portion. The inlet opening is bounded by the first sidewall, the second sidewall, and the second end, and the inlet opening is configured to receive a fluid stream therethrough. The air intake system further includes an actuation component coupled to the angled bottom member. The actuation component includes a shape memory alloy, and the actuation component is responsive to a change in a thermal condition and configured to move the second end, thereby regulating the inlet opening.
(FR) L'invention porte sur un système d'entrée d'air comprenant un carter extérieur pour un véhicule, le carter extérieur comprenant une surface extérieure comprenant une partie encastrée définie ici. La partie encastrée comprend un élément inférieur incurvé ayant une première extrémité, ainsi qu'une seconde extrémité accouplée à la surface extérieure. La partie encastrée comprend aussi une première paroi latérale, une seconde paroi latérale opposée à la première paroi latérale, ainsi qu'un orifice d'entrée délimité dans la partie encastrée. L'orifice d'entrée est bordé par la première paroi latérale, par la seconde paroi latérale et par la seconde extrémité, et l'orifice d'entrée est configuré afin de recevoir un courant de fluide à travers cette dernière. Le système d'entrée d'air comprend en outre un élément de déclenchement accouplé à l'élément inférieur incurvé. L'élément de déclenchement comprend un alliage à mémoire de forme, et l'élément de déclenchement est sensible à un changement dans un état thermique et est configuré pour déplacer la seconde extrémité, ce qui permet de réguler l'orifice d'entrée.
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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)