SE547852C2 - A kit for providing an unmanned aerial vehicle and an unmanned aerial system - Google Patents
A kit for providing an unmanned aerial vehicle and an unmanned aerial systemInfo
- Publication number
- SE547852C2 SE547852C2 SE2350595A SE2350595A SE547852C2 SE 547852 C2 SE547852 C2 SE 547852C2 SE 2350595 A SE2350595 A SE 2350595A SE 2350595 A SE2350595 A SE 2350595A SE 547852 C2 SE547852 C2 SE 547852C2
- Authority
- SE
- Sweden
- Prior art keywords
- unmanned aerial
- kit
- aerial vehicle
- providing
- vehicle
- Prior art date
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/22—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft
- B64C27/26—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft characterised by provision of fixed wings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
- B64U10/13—Flying platforms
- B64U10/14—Flying platforms with four distinct rotor axes, e.g. quadcopters
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
- B64C29/02—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis vertical when grounded
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/20—Vertical take-off and landing [VTOL] aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/25—Fixed-wing aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U30/00—Means for producing lift; Empennages; Arrangements thereof
- B64U30/10—Wings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U30/00—Means for producing lift; Empennages; Arrangements thereof
- B64U30/20—Rotors; Rotor supports
- B64U30/21—Rotary wings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U30/00—Means for producing lift; Empennages; Arrangements thereof
- B64U30/20—Rotors; Rotor supports
- B64U30/29—Constructional aspects of rotors or rotor supports; Arrangements thereof
- B64U30/295—Rotors arranged in the wings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
- B64U2101/15—UAVs specially adapted for particular uses or applications for conventional or electronic warfare
- B64U2101/18—UAVs specially adapted for particular uses or applications for conventional or electronic warfare for dropping bombs; for firing ammunition
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Toys (AREA)
- Forklifts And Lifting Vehicles (AREA)
Abstract
The present disclosure is related to a kit 11 comprising an unmanned aerial vehicle 1. The vehicle 1 of the kit 11, comprises at least three rotors 3, 4, 5, and also a fixed wing 2. The unmanned aerial vehicle 1 of the kit 11 may attain two different flying configurations, the first flying configuration A where the wing 2 provides the lift, and a second flying configuration B where the rotors 3, 4, 5 provide the lift.
Priority Applications (6)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| SE2350595A SE547852C2 (en) | 2023-05-16 | 2023-05-16 | A kit for providing an unmanned aerial vehicle and an unmanned aerial system |
| CN202480032855.4A CN121127419A (en) | 2023-05-16 | 2024-05-16 | Unmanned aerial vehicles, unmanned flight systems and kits |
| EP24729111.5A EP4713257A1 (en) | 2023-05-16 | 2024-05-16 | Unmanned aerial vehicle, unmanned aerial system, and a kit |
| AU2024274011A AU2024274011A1 (en) | 2023-05-16 | 2024-05-16 | Unmanned aerial vehicle, unmanned aerial system, and a kit |
| PCT/SE2024/050474 WO2024237848A1 (en) | 2023-05-16 | 2024-05-16 | Unmanned aerial vehicle, unmanned aerial system, and a kit |
| IL324689A IL324689A (en) | 2023-05-16 | 2024-05-16 | Unmanned aerial vehicle, unmanned aerial system, and a kit |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| SE2350595A SE547852C2 (en) | 2023-05-16 | 2023-05-16 | A kit for providing an unmanned aerial vehicle and an unmanned aerial system |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| SE2350595A1 SE2350595A1 (en) | 2024-11-17 |
| SE547852C2 true SE547852C2 (en) | 2025-12-09 |
Family
ID=91276935
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| SE2350595A SE547852C2 (en) | 2023-05-16 | 2023-05-16 | A kit for providing an unmanned aerial vehicle and an unmanned aerial system |
Country Status (6)
| Country | Link |
|---|---|
| EP (1) | EP4713257A1 (en) |
| CN (1) | CN121127419A (en) |
| AU (1) | AU2024274011A1 (en) |
| IL (1) | IL324689A (en) |
| SE (1) | SE547852C2 (en) |
| WO (1) | WO2024237848A1 (en) |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP2760739B1 (en) * | 2011-09-27 | 2017-11-22 | Singapore Technologies Aerospace Ltd | Control of an unmanned aerial vehicle |
| EP3172130B1 (en) * | 2014-07-24 | 2018-10-03 | Atmos Uav B.V. | Aircraft with wing-borne flight mode and hover flight mode |
| US20200277069A1 (en) * | 2019-03-01 | 2020-09-03 | Bell Helicopter Textron Inc. | Fuel cell powered line-replaceable thrust module |
| US11643207B1 (en) * | 2021-12-07 | 2023-05-09 | Textron Innovations Inc. | Aircraft for transporting and deploying UAVs |
Family Cites Families (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US10561956B2 (en) * | 2014-07-25 | 2020-02-18 | University Of Kansas | Moveable member bearing aerial vehicles and methods of use |
| US10189565B2 (en) * | 2016-12-02 | 2019-01-29 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Modular unmanned aerial system with multi-mode propulsion |
| US20190389573A1 (en) * | 2018-06-26 | 2019-12-26 | Honeywell International Inc. | Vertical take-off and landing unmanned aerial vehicle |
| IT201800007202A1 (en) * | 2018-07-13 | 2020-01-13 | Unmanned aircraft, control method, associated platform and high-altitude turbine | |
| US20200140079A1 (en) * | 2018-11-02 | 2020-05-07 | Textron Innovations Inc. | Vertical takeoff and landing dual-wing aerial vehicle |
| US12091149B2 (en) | 2021-04-08 | 2024-09-17 | Abbott Aerospace Canada Ltd. | Aerial vehicle for carrying a payload |
-
2023
- 2023-05-16 SE SE2350595A patent/SE547852C2/en unknown
-
2024
- 2024-05-16 AU AU2024274011A patent/AU2024274011A1/en active Pending
- 2024-05-16 IL IL324689A patent/IL324689A/en unknown
- 2024-05-16 CN CN202480032855.4A patent/CN121127419A/en active Pending
- 2024-05-16 EP EP24729111.5A patent/EP4713257A1/en active Pending
- 2024-05-16 WO PCT/SE2024/050474 patent/WO2024237848A1/en not_active Ceased
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP2760739B1 (en) * | 2011-09-27 | 2017-11-22 | Singapore Technologies Aerospace Ltd | Control of an unmanned aerial vehicle |
| EP3172130B1 (en) * | 2014-07-24 | 2018-10-03 | Atmos Uav B.V. | Aircraft with wing-borne flight mode and hover flight mode |
| US20200277069A1 (en) * | 2019-03-01 | 2020-09-03 | Bell Helicopter Textron Inc. | Fuel cell powered line-replaceable thrust module |
| US11643207B1 (en) * | 2021-12-07 | 2023-05-09 | Textron Innovations Inc. | Aircraft for transporting and deploying UAVs |
Non-Patent Citations (1)
| Title |
|---|
| 'Swan K1 PRO Base Combo Vertical Takeoff Wing Long Range Drone by HEQ', www.urbandrones.com/products/alpha-vertical-take-off-wing (archived 2022-05-24 on WayBack Machine: https://web.archive.org/web/20220524223234/https://www.urbandrones.com/products/alpha-vertical-take-off-wing) * |
Also Published As
| Publication number | Publication date |
|---|---|
| CN121127419A (en) | 2025-12-12 |
| WO2024237848A1 (en) | 2024-11-21 |
| AU2024274011A1 (en) | 2026-01-08 |
| SE2350595A1 (en) | 2024-11-17 |
| IL324689A (en) | 2026-01-01 |
| EP4713257A1 (en) | 2026-03-25 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| WO2020247148A3 (en) | Electrically powered vtol aircraft for providing transportation | |
| WO2020056311A3 (en) | Uav facility | |
| WO2024172875A3 (en) | Dual engine vertical take off and landing collapsible fixed wing aircraft | |
| WO2019082043A3 (en) | Vertical take-off and landing aircraft and transformation gear sets for same | |
| DE69402312D1 (en) | AERODYNAMIC AUXILIARY STRUCTURES OF AN UNMANNED AIRCRAFT WITH RECESSED, COAXIAL, REVERSE ROTORS | |
| NO20092700L (en) | System and method for providing runway conditions for landing aircraft | |
| WO2021011045A3 (en) | Ground support equipment for a high altitude long endurance aircraft | |
| AU2001234677A1 (en) | Improved aerobatic aircraft | |
| WO2022249176A3 (en) | Drone with a charging platform | |
| WO2021124211A8 (en) | Convertiplane and associated folding method | |
| EP4411501A3 (en) | Method and system for controlling interval management of an aircraft | |
| NL2026721B1 (en) | An amphibious flight vehicle | |
| BR112023026139A2 (en) | UNMANNED AERIAL VEHICLE SYSTEM AND AUTONOMOUS VTOL UAV | |
| EP4434897A3 (en) | An unmanned aerial vehicle | |
| WO2024226441A3 (en) | Vortex drone | |
| GB515562A (en) | Improvements in or relating to the structure of aircraft | |
| GB2614228A8 (en) | A VTOL aerial vehicle | |
| GB1124929A (en) | A folding multi-blade airscrew | |
| AU2491888A (en) | An engine, particularly for ultralight aircraft | |
| AU2025902194A0 (en) | System for generating power through the use of soaring unmanned aerial vehicles | |
| AU2024901396A0 (en) | System for generating power through the use of soaring unmanned aerial vehicles | |
| CN109018427A (en) | A kind of unmanned plane fault processing system | |
| CN205239898U (en) | Unmanned aerial vehicle of multiple encryption control | |
| WO2025184696A8 (en) | Aircraft and electric power systems for aircraft | |
| JP1775924S (en) | Modular Mobility System |