(19)
(11) EP 3 604 132 A8

(12) CORRECTED EUROPEAN PATENT APPLICATION
Note: Bibliography reflects the latest situation

(15) Correction information:
Corrected version no 1 (W1 A1)

(48) Corrigendum issued on:
29.04.2020 Bulletin 2020/18

(43) Date of publication:
05.02.2020 Bulletin 2020/06

(21) Application number: 19185660.8

(22) Date of filing: 11.07.2019
(51) International Patent Classification (IPC): 
B64C 39/02(2006.01)
B64C 39/12(2006.01)
 B64C 39/04(2006.01)
(84) Designated Contracting States:
AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR
Designated Extension States:
BA ME
Designated Validation States:
KH MA MD TN

(30) Priority: 30.07.2018 US 201816049629

(71) Applicant: Shanghai Autoflight Co., Ltd.
Jinshan District Shanghai 201500 (CN)

(72) Inventor:
  • TIAN, Yu
    Causeway Bay (HK)

(74) Representative: MERH-IP Matias Erny Reichl Hoffmann Patentanwälte PartG mbB 
Paul-Heyse-Strasse 29
80336 München
80336 München (DE)

   


(54) HYBRID VERTICAL TAKE-OFF AND LANDING (VTOL) FIXED-WING DRONE


(57) A long-distance drone 100 is disclosed having a canard body style with a main body 110, a left main wing 113, a right main wing 114, a left forewing 111, and a right forewing 112. The left forewing 111 is attached to the main body 110 forward of the left main wing 113, and the right forewing 112 is attached to the main body 110 forward of the right main wing 114. There is a left linear support 120 connecting the left forewing 111 to the left main wing 113, and a right linear support 121 connecting the right forewing 112 to the right main wing 114. A plurality of propellers 131, 132, 133, 134, 135, 136 are disposed on the left and the right linear supports 120, 121.