WO2023113732A3 - An unmanned aerial vehicle - Google Patents
An unmanned aerial vehicle Download PDFInfo
- Publication number
- WO2023113732A3 WO2023113732A3 PCT/TR2022/051402 TR2022051402W WO2023113732A3 WO 2023113732 A3 WO2023113732 A3 WO 2023113732A3 TR 2022051402 W TR2022051402 W TR 2022051402W WO 2023113732 A3 WO2023113732 A3 WO 2023113732A3
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- wings
- aerial vehicle
- unmanned aerial
- wing body
- destruct
- Prior art date
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U20/00—Constructional aspects of UAVs
- B64U20/50—Foldable or collapsible UAVs
-
- 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
- B64U10/00—Type of UAV
- B64U10/50—Glider-type UAVs, e.g. with parachute, parasail or kite
-
- 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
- B64U30/12—Variable or detachable wings, e.g. wings with adjustable sweep
-
- 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
- B64U30/293—Foldable or collapsible rotors or rotor supports
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
- F42B10/02—Stabilising arrangements
- F42B10/14—Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
- F42B10/02—Stabilising arrangements
- F42B10/14—Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel
- F42B10/146—Fabric fins, i.e. fins comprising at least one spar and a fin cover made of flexible sheet material
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
- F42B10/32—Range-reducing or range-increasing arrangements; Fall-retarding means
- F42B10/38—Range-increasing arrangements
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
- F42B10/60—Steering arrangements
- F42B10/62—Steering by movement of flight surfaces
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
- F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
- F42B12/20—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type
- F42B12/201—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type characterised by target class
- F42B12/202—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type characterised by target class for attacking land area or area targets, e.g. airburst
-
- 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
-
- 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
- B64U2101/30—UAVs specially adapted for particular uses or applications for imaging, photography or videography
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U30/00—Means for producing lift; Empennages; Arrangements thereof
- B64U30/40—Empennages, e.g. V-tails
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U70/00—Launching, take-off or landing arrangements
- B64U70/70—Launching or landing using catapults, tracks or rails
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41F—APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
- F41F3/00—Rocket or torpedo launchers
- F41F3/04—Rocket or torpedo launchers for rockets
- F41F3/042—Rocket or torpedo launchers for rockets the launching apparatus being used also as a transport container for the rocket
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Aviation & Aerospace Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Forklifts And Lifting Vehicles (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
The invention relates to an unmanned aerial vehicle (1) arranged to self-destruct near a target (H), comprising a body (10), foldable wings (20) that comprise wing body (21) connected to the body (10) and flaps (22) partially movably connected to the wing body (21) and are opened after launch, and rear wings (60) and a propeller (30) driven by an engine, and ammunition (40), and it is characterized in that it comprises non-rigid auxiliary wings (70), one side of which is connected to the body (10) and the other to the wings (20), and which become tensioned when the said wings (20) are in the open position and increase the area of the wings (20).
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
TR2021/019857 TR2021019857A1 (en) | 2021-12-14 | AN UNMANNED AERIAL VEHICLE | |
TR2021019857 | 2021-12-14 |
Publications (2)
Publication Number | Publication Date |
---|---|
WO2023113732A2 WO2023113732A2 (en) | 2023-06-22 |
WO2023113732A3 true WO2023113732A3 (en) | 2023-08-31 |
Family
ID=86775368
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/TR2022/051402 WO2023113732A2 (en) | 2021-12-14 | 2022-12-02 | An unmanned aerial vehicle |
Country Status (1)
Country | Link |
---|---|
WO (1) | WO2023113732A2 (en) |
Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3135482A (en) * | 1962-12-26 | 1964-06-02 | Ryan Aeronautical Co | Flexible wing stol assist system for aircraft |
US6119976A (en) * | 1997-01-31 | 2000-09-19 | Rogers; Michael E. | Shoulder launched unmanned reconnaissance system |
US20100282897A1 (en) * | 2005-08-17 | 2010-11-11 | Chang Industry, Inc. | Unmanned Aerial Surveillance Device |
US20110226174A1 (en) * | 2008-06-16 | 2011-09-22 | Aurora Flight Sciences Corporation | Combined submersible vessel and unmanned aerial vehicle |
US9527596B1 (en) * | 2011-03-01 | 2016-12-27 | Richard D. Adams | Remote controlled aerial reconnaissance vehicle |
US20170283035A1 (en) * | 2016-04-05 | 2017-10-05 | Lanping JI | Foldable wing and rotocraft and glider using the same |
US20200284557A1 (en) * | 2016-06-08 | 2020-09-10 | The Boeing Company | Drone deterrence system, method, and assembly |
-
2022
- 2022-12-02 WO PCT/TR2022/051402 patent/WO2023113732A2/en unknown
Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3135482A (en) * | 1962-12-26 | 1964-06-02 | Ryan Aeronautical Co | Flexible wing stol assist system for aircraft |
US6119976A (en) * | 1997-01-31 | 2000-09-19 | Rogers; Michael E. | Shoulder launched unmanned reconnaissance system |
US20100282897A1 (en) * | 2005-08-17 | 2010-11-11 | Chang Industry, Inc. | Unmanned Aerial Surveillance Device |
US20110226174A1 (en) * | 2008-06-16 | 2011-09-22 | Aurora Flight Sciences Corporation | Combined submersible vessel and unmanned aerial vehicle |
US9527596B1 (en) * | 2011-03-01 | 2016-12-27 | Richard D. Adams | Remote controlled aerial reconnaissance vehicle |
US20170283035A1 (en) * | 2016-04-05 | 2017-10-05 | Lanping JI | Foldable wing and rotocraft and glider using the same |
US20200284557A1 (en) * | 2016-06-08 | 2020-09-10 | The Boeing Company | Drone deterrence system, method, and assembly |
Also Published As
Publication number | Publication date |
---|---|
WO2023113732A2 (en) | 2023-06-22 |
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