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Machine translation
1. (WO2009142790) VIBRATION ISOLATION DEVICES AND ASSOCIATED SYSTEMS AND METHODS
Latest bibliographic data on file with the International Bureau   

Pub. No.:    WO/2009/142790    International Application No.:    PCT/US2009/035320
Publication Date: 26.11.2009 International Filing Date: 26.02.2009
IPC:
B64C 1/00 (2006.01)
Applicants: INSITU, INC. [US/US]; 118 East Columbia River Way Bingen, WA 98605 (US) (For All Designated States Except US).
VON FLOTOW, Andreas, H. [CA/US]; (US) (For US Only).
HORTON, Tyler, Patrick [US/US]; (US) (For US Only)
Inventors: VON FLOTOW, Andreas, H.; (US).
HORTON, Tyler, Patrick; (US)
Agent: POLEDNA, Aaron, J.; (US)
Priority Data:
61/032,858 29.02.2008 US
12/390,301 20.02.2009 US
Title (EN) VIBRATION ISOLATION DEVICES AND ASSOCIATED SYSTEMS AND METHODS
(FR) DISPOSITIFS D’ISOLATION CONTRE LES VIBRATIONS ET SYSTÈMES ET PROCÉDÉS ASSOCIÉS
Abstract: front page image
(EN)Vibration isolation devices and associated systems and methods are disclosed herein. In one embodiment, for example, an unmanned aircraft can include a fuselage having a first fuselage section and a second fuselage section adjacent to and at least approximately longitudinally aligned with the first fuselage section. The aircraft can also include at least one vibration isolation device coupling the first fuselage section to the second fuselage section. The vibration isolation device is translationally stiffer along a longitudinal axis than it is along a lateral and a vertical axis, and rotationally stiffer about a pitch and a yaw axis than it is about a roll axis.
(FR)L’invention concerne des dispositifs d'isolation contre les vibrations et des systèmes et procédés associés. Dans un mode de réalisation, par exemple, un avion sans pilote peut inclure un fuselage ayant une première section de fuselage et une seconde section de fuselage adjacente et au moins approximativement longitudinalement alignée avec la première section de fuselage. L’avion peut également inclure au moins un dispositif d’isolation contre les vibrations reliant la première section de fuselage à la seconde section de fuselage. Le dispositif d’isolation contre les vibrations est plus rigide d’un point de vue translationnel le long d’un axe longitudinal que le long d’un axe latéral et vertical, et plus rigide en rotation autour d’un axe de tangage et de lacet qu’autour d’un axe de roulis.
Designated States: AE, AG, AL, AM, AO, AT, AU, AZ, BA, BB, BG, BH, BR, BW, BY, BZ, CA, CH, 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, KR, 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, PG, PH, PL, PT, RO, RS, RU, SC, SD, SE, SG, SK, SL, SM, ST, SV, SY, TJ, TM, TN, TR, TT, TZ, UA, UG, US, UZ, VC, VN, ZA, ZM, ZW.
African Regional Intellectual Property Organization (BW, GH, GM, KE, 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 (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, SE, SI, SK, TR)
African Intellectual Property Organization (BF, BJ, CF, CG, CI, CM, GA, GN, GQ, GW, ML, MR, NE, SN, TD, TG).
Publication Language: English (EN)
Filing Language: English (EN)