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1. (WO2017132804) UNMANNED AERIAL VEHICLE DAMPING DEVICE
Latest bibliographic data on file with the International Bureau

Pub. No.: WO/2017/132804 International Application No.: PCT/CN2016/073089
Publication Date: 10.08.2017 International Filing Date: 01.02.2016
IPC:
B64C 25/60 (2006.01)
B PERFORMING OPERATIONS; TRANSPORTING
64
AIRCRAFT; AVIATION; COSMONAUTICS
C
AEROPLANES; HELICOPTERS
25
Alighting gear
32
characterised by elements which contact the ground or similar surface
58
Arrangements or adaptations of shock-absorbers or springs
60
Oleo legs
Applicants:
张琬彬 ZHANG, Wanbin [CN/CN]; CN
Inventors:
张琬彬 ZHANG, Wanbin; CN
Agent:
深圳市科冠知识产权代理有限公司 SHENZHEN KEGUAN INTELLECTUAL PROPERTY AGENCY CO., LTD; 中国广东省深圳市 南山区南海大道东华园5栋303 Room 303, Building 5 Donghuayuan, Nanhai Road, Nanshan District Shenzhen, Guangdong 518000, CN
Priority Data:
Title (EN) UNMANNED AERIAL VEHICLE DAMPING DEVICE
(FR) DISPOSITIF D'AMORTISSEMENT DE VÉHICULE AÉRIEN SANS PILOTE
(ZH) 一种无人机减震装置
Abstract:
(EN) An unmanned aerial vehicle damping device, comprising two struts (1) and a plate (2) used to mount a UAV. Each strut (1) is provided with at least two corresponding clamps (3) which clamp onto the strut (1). The device further comprises a bracket (4) used to support the clamps (3). The bracket (4) is connected to the bottom surface of the plate (2). A flexible device (5) is provided between the clamps (3) and the plate (2). The UAV has two struts (1), with at least two clamps (3) being provided on the struts (1), and a flexible device (5) being provided between the clamps (3) and the plate (2). When the UAV lands and touches down, multiple locations provide damping, resulting in effective damping. The present device is simple in structure and low in cost.
(FR) La présente invention concerne un dispositif d'amortissement de véhicule aérien sans pilote, comprenant deux jambes de force (1) et une plaque (2) utilisées pour monter un véhicule aérien sans pilote (UAV). Chaque jambe de force (1) est pourvue d'au moins deux brides correspondantes (3) qui se fixent sur la jambe de force (1). Le dispositif comprend en outre un support (4) utilisé pour supporter les brides (3). Le support (4) est relié à la surface inférieure de la plaque (2). Un dispositif souple (5) est prévu entre les brides (3) et la plaque (2). L'UAV comporte deux jambes de force (1), au moins deux brides (3) montées sur les jambes de force (1), et un dispositif souple (5) étant prévu entre les brides (3) et la plaque (2). Lorsque l'UAV atterrit et touche terre, de multiples emplacements offrent un amortissement, ce qui permet un amortissement efficace. Le présent appareil est simple et peu coûteux.
(ZH) 一种无人机减震装置,包括两个脚架(1)和用于安装无人机的面板(2)。每个脚架(1)对应设置有至少两个用于夹紧脚架(1)的夹具(3)进行夹持。该装置还包括用于托起夹具(3)的托架(4)。托架(4)与面板(2)下表面连接设置。夹具(3)与面板(2)之间设置有弹性装置(5)。该无人机设置两个脚架(1),并在脚架(1)上设置至少两个夹具(3),以及在夹具(3)与面板(2)之间设置弹性装置(5)。在无人机降落与地面接触时,多个位置进行减震,减震效果好。该装置整体结构简单,成本低。
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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, DK, DM, DO, DZ, EC, EE, EG, ES, FI, GB, GD, GE, GH, GM, GT, HN, HR, HU, ID, IL, IN, IR, IS, JP, KE, KG, KN, KP, KR, 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 Organization (AM, AZ, BY, KG, KZ, 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, KM, ML, MR, NE, SN, TD, TG)
Publication Language: Chinese (ZH)
Filing Language: Chinese (ZH)