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1. (WO2019029387) AERIAL VEHICLE AND ARM ASSEMBLY AND FRAME THEREOF
Latest bibliographic data on file with the International BureauSubmit observation

Pub. No.: WO/2019/029387 International Application No.: PCT/CN2018/097520
Publication Date: 14.02.2019 International Filing Date: 27.07.2018
IPC:
B64C 1/00 (2006.01) ,B64C 27/32 (2006.01)
B PERFORMING OPERATIONS; TRANSPORTING
64
AIRCRAFT; AVIATION; COSMONAUTICS
C
AEROPLANES; HELICOPTERS
1
Fuselages; Constructional features common to fuselages, wings, stabilising surfaces, or the like
B PERFORMING OPERATIONS; TRANSPORTING
64
AIRCRAFT; AVIATION; COSMONAUTICS
C
AEROPLANES; HELICOPTERS
27
Rotorcraft; Rotors peculiar thereto
32
Rotors
Applicants:
深圳市道通智能航空技术有限公司 AUTEL ROBOTICS CO., LTD. [CN/CN]; 中国广东省深圳市 南山区西丽街道学苑大道1001号智园B1栋9层 9th Floor, Building B1, Zhiyuan No. 1001, Xueyuan Road, Xili Street, Nanshan Shenzhen, Guangdong 518055, CN
Inventors:
余春 YU, Chun; CN
Agent:
北京安信方达知识产权代理有限公司 AFD CHINA INTELLECTUAL PROPERTY LAW OFFICE; 中国北京市 海淀区学清路8号B座1601A Suite B 1601A, 8 Xue Qing Rd., Haidian Beijing 100192, CN
Priority Data:
201721008359.910.08.2017CN
Title (EN) AERIAL VEHICLE AND ARM ASSEMBLY AND FRAME THEREOF
(FR) AÉRONEF ET ENSEMBLE BRAS ET CADRE DE CELUI-CI
(ZH) 飞行器及其机臂组件和机架
Abstract:
(EN) An aircraft and an arm assembly (10) and frame thereof, the arm assembly (10) comprising: an elastic locking member (100), a fixing seat (200) and an arm (300); the arm (300) is rotatably connected to the fixing seat (200) such that the arm (300) may rotate relative to the fixing seat (200) between a folding position and an unfolding position; the elastic locking member (100) is connected to the fixing seat (200), being used for locking the arm (300) when the arm (300) is in the folding position or unfolding position. By means of the foregoing manner, stable folding and rapid unfolding of the arm may be achieved, thus reducing the volume of an unused unmanned aerial vehicle.
(FR) Un aéronef, un ensemble bras (10) et un cadre de celui-ci, l'ensemble bras (10) comprenant : un élément de verrouillage élastique (100), un siège de fixation (200) et un bras (300) ; le bras (300) est relié de manière rotative au siège de fixation (200) de telle sorte que le bras (300) peut tourner par rapport au siège de fixation (200) entre une position de pliage et une position de dépliage ; l'élément de verrouillage élastique (100) est relié au siège de fixation (200), étant utilisé pour verrouiller le bras (300) lorsque le bras (300) est dans la position de pliage ou la position de dépliage. Au moyen de la manière qui précède, un pliage stable et un dépliage rapide du bras peuvent être obtenus, réduisant ainsi le volume d'un aéronef sans pilote inutilisé.
(ZH) 一种飞行器及其机臂组件(10)和机架,所述机臂组件(10)包括:弹性锁紧件(100)、固定座(200)以及机臂(300);机臂(300)与固定座(200)转动连接,以使机臂(300)可相对固定座(200)在折叠位置与展开位置之间旋转;弹性锁紧件(100)与固定座(200)连接,用于在机臂(300)处于折叠位置或展开位置时锁紧机臂(300)。通过上述方式,能够实现机臂的稳固折叠和快速展开,减小无人飞行器在非使用状态下的体积。
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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 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)