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Machine translation
1. (WO2012099300) FLIGHT CONTROL SURFACE-DRIVING DEVICE OF AIRCRAFT
Latest bibliographic data on file with the International Bureau   

Pub. No.:    WO/2012/099300    International Application No.:    PCT/KR2011/003261
Publication Date: 26.07.2012 International Filing Date: 02.05.2011
IPC:
B64C 13/28 (2006.01), B64C 13/36 (2006.01)
Applicants: HANWHA CORPORATION [KR/KR]; Hanwha Building, 1, Janggyo-dong, Jung-gu Seoul 100-797 (KR) (For All Designated States Except US).
YOON, Gi-Jun [KR/KR]; (KR) (For US Only).
KIM, Sang-Seok [KR/KR]; (KR) (For US Only).
PARK, Chang-Yong [KR/KR]; (KR) (For US Only).
KIM, Dae-Hyun [KR/KR]; (KR) (For US Only).
KIM, Sang-Beom [KR/KR]; (KR) (For US Only).
JANG, Ki-Won [KR/KR]; (KR) (For US Only).
LEE, Sung-Taick [KR/KR]; (KR) (For US Only)
Inventors: YOON, Gi-Jun; (KR).
KIM, Sang-Seok; (KR).
PARK, Chang-Yong; (KR).
KIM, Dae-Hyun; (KR).
KIM, Sang-Beom; (KR).
JANG, Ki-Won; (KR).
LEE, Sung-Taick; (KR)
Agent: HANYANG PATENT FIRM; Hanyang Building, 412-1 Dogok-dong, Gangnam-gu Seoul 135-854 (KR)
Priority Data:
10-2011-0006379 21.01.2011 KR
Title (EN) FLIGHT CONTROL SURFACE-DRIVING DEVICE OF AIRCRAFT
(FR) DISPOSITIF D'ENTRAÎNEMENT D'UNE SURFACE DE COMMANDE DE VOL D'UN AVION
(KO) 항공기의 비행조종면 구동장치
Abstract: front page image
(EN)The present invention relates to a flight control surface-driving device of an aircraft, in which an actuator is installed on a wing frame and power transmitted by said actuator drives a flight control surface, wherein the invention is structured such that: said actuator is installed on the outside of the wing frame in a direction of being laid on said wing frame; and the power generated from said actuator is converted, through a direction converting means, in the direction in which the actuator is erected on said wing frame whereby the power is delivered to said flight control surface. The invention efficiently uses a fuel storage space formed in the wing frame, and reduces the weight of gas.
(FR)La présente invention se rapporte à un dispositif d'entraînement d'une surface de commande de vol d'un avion, dans lequel un actionneur est installé sur un cadre d'aile et l'énergie transmise par ledit actionneur entraîne une surface de commande de vol. L'invention est structurée de sorte que : ledit actionneur soit installé sur l'extérieur du cadre d'aile dans une direction où il repose sur ledit cadre d'aile ; et l'énergie produite à partir dudit actionneur soit convertie, par l'intermédiaire d'un moyen de conversion de direction, dans la direction dans laquelle l'actionneur se dresse sur ledit cadre d'aile, l'énergie étant distribuée à ladite surface de commande de vol. L'invention utilise efficacement un espace de stockage formé dans le cadre d'aile, et réduit le poids de gaz.
(KO)본 발명은 항공기의 비행조종면 구동장치에 관한 것으로 날개 프레임에 액츄에이터가 설치되고 상기 액츄에이터에 의해 전달되는 동력이 비행조종면을 구동하는 항공기의 비행조종면 구동장치에 있어서, 상기 액츄에이터를 상기 날개 프레임에 대해 눕혀지는 방향으로 날개 프레임의 외부에 설치하고, 상기 액츄에이터에서 발생하는 동력을 방향전환수단을 통해 상기 날개 프레임에 대해 세워지는 방향으로 전환시켜 상기 비행조종면에 전달하는 구조로 된 것이다. 본 발명은 날개 프레임에 형성되는 연료저장공간을 효율적으로 활용하고 기체의 중량을 절감할 수 있다는 효과가 있다.
Designated States: AE, AG, AL, AM, AO, AT, AU, AZ, BA, BB, BG, BH, 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, IS, JP, KE, KG, KM, KN, KP, KZ, LA, LC, LK, LR, LS, LT, LU, LY, MA, MD, ME, MG, MK, MN, MW, MX, MY, MZ, NA, NG, NI, NO, NZ, OM, PE, PG, PH, PL, PT, RO, RS, RU, 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 (BW, GH, GM, KE, LR, LS, MW, MZ, NA, SD, SL, SZ, TZ, UG, ZM, ZW)
Eurasian Patent Organization (AM, AZ, BY, KG, KZ, MD, RU, TJ, TM)
European Patent Office (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, ML, MR, NE, SN, TD, TG).
Publication Language: Korean (KO)
Filing Language: Korean (KO)