公开(公告)号：US20230246383A1

公开(公告)日：2023-08-03

申请号：US18161087

申请日：2023-01-29

申请人： Autoflight (Kunshan) Co., Ltd.

发明人： Yu Tian

IPC分类号： B64U50/30 ,  B64U20/65 ,  B64U20/70 ,  B64U30/10

CPC分类号： B64U50/30 ,  B64U20/65 ,  B64U20/70 ,  B64U30/10

摘要： A plug-in assembly structure for a UAV includes a first component (1), a second component (2) and a limit assembly (3). The first component (1) includes a first plug (11) and a positioning sleeve (12), and the positioning sleeve (12) is provided with a first through hole (121). The second component (2) includes a second plug (21), the radial direction of the second plug (21) is provided with a limit hole (2111), the second plug (21) can be electrically connected to the first plug (11), and the limit hole (2111) is facing the first through hole (121). The limit assembly (3) is installed in the limit hole (2111). The limit assembly (3) includes a first elastic element (31) and a limit element (32).

公开(公告)号：US20240353863A1

公开(公告)日：2024-10-24

申请号：US18760905

申请日：2024-07-01

申请人： YANA SOS, INC.

发明人： Fredrick M. Warner, IV ,  Theodore Lavoie ,  Nathan Ernst ,  Vivek Reddy Alla ,  Michael Gorski ,  Casey Alford ,  Tim VanAntwerp ,  Timothy Kent ,  Donald Massey

IPC分类号： G05D1/686 ,  B64C27/39 ,  B64C27/57 ,  B64C27/72 ,  B64D47/02 ,  B64U10/14 ,  B64U20/87 ,  B64U30/29 ,  G01C21/16 ,  G01S19/17 ,  G01S19/18 ,  G05D1/46 ,  G06T7/70 ,  G08G5/00 ,  B64U20/65 ,  B64U101/20

CPC分类号： G05D1/686 ,  B64C27/39 ,  B64C27/57 ,  B64C27/72 ,  B64D47/02 ,  B64U10/14 ,  B64U20/87 ,  B64U30/29 ,  G01C21/16 ,  G01S19/17 ,  G01S19/18 ,  G05D1/46 ,  G06T7/70 ,  G08G5/0073 ,  B64U20/65 ,  B64U2101/20 ,  B64U2201/10 ,  B64U2201/104 ,  B64U2201/20

摘要： Devices and methods for activating a flight-enable beacon configured to provide a light beacon or data signal comprising capability to establish and maintain a fixed set of coordinates. The flight-enabled beacon is configured with a processor, memory, motor, gimbal or swashplate and light emitting source and can be configured to attain and maintain a target altitude and emit a light over a fixed period of time. The flight-enabled beacon is configured to be light and with small form factor for easy portable transport in cases of emergency or to provide a signal easily locatable by parties located a distance from the activated light-enabled beacon.

公开(公告)号：US20240217645A1

公开(公告)日：2024-07-04

申请号：US18557117

申请日：2022-04-26

申请人： Wingcopter GmbH

发明人： Jonathan HESSELBARTH

IPC分类号： B64C1/06 ,  B64C1/00 ,  B64C5/02 ,  B64F5/10 ,  B64U20/65

CPC分类号： B64C1/068 ,  B64C5/02 ,  B64F5/10 ,  B64C2001/0072 ,  B64U20/65

摘要： A main aircraft body is made of fiber-reinforced composite material. The main aircraft body includes a load-bearing structure configured in the form of an elongate fuselage. Two wings are arranged laterally on the elongate fuselage. The wings are configured such that a lifting force is generated for the aircraft. A plurality of receiving devices for receiving drive means are formed on the wings. The main aircraft body is formed from an upper shell and a lower shell. The upper shell and the lower shell are connected to one another along a common connecting surface. An empennage is arranged at a tail of the fuselage. The empennage is formed by a pair of empennage surfaces. Guide surfaces of the pair of empennage surfaces are oriented in a V-shaped manner in relation to one another in a horizontal direction of flight. The upper shell is produced in one piece.

公开(公告)号：US20240124117A1

公开(公告)日：2024-04-18

申请号：US18285692

申请日：2022-04-01

申请人： BAE SYSTEMS PLC

发明人： James Martin MILLER ,  Simon BISHOP ,  James Patrick O'NEILL

IPC分类号： B64C1/06 ,  B64U20/65

CPC分类号： B64C1/061 ,  B64U20/65 ,  B64U2101/00

摘要： In some examples, a structural framework component for an aerial platform comprises a body defining a cavity to receive a support system, and an arm to receive a payload, wherein the arm comprises a conduit to receive cabling linking a support system and a payload.