A compound wing unmanned aerial vehicle vertical takeoff fixed wing

Abstract

The utility model provides a kind of composite wing unmanned plane vertical fixed wing, belong to unmanned plane equipment technical field, including the fixed wing being symmetrically arranged on composite wing unmanned plane fuselage, one vertical power frame is arranged on each fixed wing, the bottom of the middle of each fixed wing is provided with a connecting piece, connecting piece is installed close to the middle axis of composite wing unmanned plane fuselage, the bottom of each connecting piece is provided with a delivery device, the bottom of composite wing unmanned plane fuselage is symmetrically provided with a pair of landing gear along fuselage axis direction, the utility model is placed by opening storehouse door to give the emergency rescue articles in throwing box, then when needing throwing, by unlocking electronic mortise lock first, and then make the bottom of throwing door lose support, and then open throwing door plate, so that emergency articles can be put into emergency rescue area, prevent the situation that throwing articles and landing gear collide when throwing articles again, also facilitate subsequent maintenance of unmanned plane.

Description

Technical Field

[0001] This utility model relates to the field of unmanned aerial vehicle (UAV) equipment technology, specifically to a composite wing UAV with a vertical take-off and landing fixed wing. Background Technology

[0002] In layman's terms, drones are a general term for unmanned aerial vehicles. From a professional perspective, they refer to unmanned aerial vehicles that fly autonomously or remotely using radio remote control equipment or the aircraft's own flight control system. Through these technologies, drones can perform various types of tasks and are characterized by being retrievable and reusable.

[0003] In related technologies, compound-wing UAVs can perform tasks such as environmental monitoring, remote sensing, disaster area search and rescue, and emergency rescue in the civilian field. Currently, most compound-wing UAVs are driven by vertical propellers to rise to the ground. They are versatile and can take off in a variety of environments. Compared with ordinary UAVs, they are more practical and have a longer flight endurance.

[0004] However, most compound-wing drones have their throwing devices installed at the bottom of the fuselage. When throwing items, the items may collide with the landing gear. In addition, the bottom of most drones is where batteries and sensors are installed, making subsequent maintenance of the drone inconvenient. To solve the above problems, a compound-wing drone with a vertical fixed wing is proposed. Utility Model Content

[0005] In view of this, the present invention provides a vertical take-off and landing fixed wing for a compound wing UAV. The present invention allows emergency rescue items to be placed in the drop box by opening the compartment door. When it is necessary to drop items, the electronic lock is first unlocked, which causes the bottom of the drop box to lose support and open the drop box door, so that the emergency items can be dropped into the emergency rescue area. This prevents the dropped items from colliding with the landing gear when dropping items, and also facilitates the subsequent maintenance of the UAV.

[0006] To solve the above-mentioned technical problems, this utility model provides a vertical take-off fixed wing for a compound wing UAV, including fixed wings symmetrically arranged on the fuselage of the compound wing UAV, each fixed wing being provided with a vertical power frame, and a connector being provided at the bottom center of each fixed wing. The connector is installed close to the central axis of the fuselage of the compound wing UAV, and a deployment device is provided at the bottom of each connector. A pair of landing gears are symmetrically arranged along the fuselage axis at the bottom of the compound wing UAV fuselage.

[0007] Each connector includes a vertical plate that is connected to the fixed wing on the same side. The vertical plate is used to connect the flat plate to the fixed wing. A flat plate is provided at the bottom of the vertical plate, which is used to connect the vertical plate to the adjusting positioning rod.

[0008] Each plate has an adjustable positioning rod fixed at its bottom. The adjustable positioning rod is used to install throwing boxes of different lengths and widths. Each adjustable positioning rod has multiple positioning holes for installing bolts.

[0009] Each delivery device includes a clamp that mates with the adjusting positioning rod on the same side. The clamp is used to connect the delivery box to the adjusting positioning rod. Each clamp consists of two clamping plates, each with multiple mounting holes. The mounting holes are used to mate with the positioning holes for bolt connection. The mounting holes are also used to install bolts. The clamp and the adjusting positioning rod are connected by bolts after the mounting holes align with the positioning holes, thereby connecting the delivery box to the adjusting positioning rod, with the mounting holes and positioning holes mate.

[0010] The delivery device also includes a delivery box at the bottom of the clamp, which is used to deliver emergency rescue supplies. Inside the delivery box, a pair of delivery doors are rotatably installed at the bottom. The delivery doors are used to open the delivery box from the bottom. Each delivery door includes an upper door and a lower door. The upper door and the lower door are tenon-and-mortise fitted together. Multiple electronic locks are installed at the gap at the bottom of the upper door and the lower door to prevent the delivery doors from opening automatically.

[0011] One end of the electronic bolt lock is connected to the bottom of the upper door panel, and the other end is connected to the lower door panel.

[0012] The drop box has an openable door on the side away from the nose of the compound wing UAV. The door is used to place emergency supplies inside the drop box. The bottom of the door is hinged to the drop box, which makes it easy to open. The top of the door is equipped with a door lock to fix the door. The other end of the door lock is connected to the outer wall of the drop box.

[0013] The landing gear is in an inverted Y-shape, with several ventilation holes on each landing gear. These ventilation holes reduce wind resistance during flight and also dampen the compound-wing UAV during landing, reducing the impact force from the ground that could damage the electronic components of the compound-wing UAV. A shock absorber is fixedly installed at the bottom of each landing gear, further reducing the vibration experienced by the landing gear during landing, thereby protecting the internal electronic components of the compound-wing UAV and extending their service life. The shock absorber adopts a gas flow guiding design.

[0014] In summary, compared with the prior art, this application includes at least one of the following beneficial technical effects: 1. By opening the cargo door, emergency rescue items can be placed in the drop box. When it is necessary to drop items again, the electronic lock is unlocked first, which causes the bottom of the drop door to lose support and open the drop door, so that the emergency items can be dropped into the emergency rescue area. This prevents the dropped items from colliding with the landing gear when dropping items, and also facilitates the subsequent maintenance of the drone.

[0015] 2. The connector should be installed close to the centerline of the drone fuselage to reduce the impact on flight attitude after the throwing device is loaded with emergency items, and also to reduce the stress on the fixed wings.

[0016] 3. Ventilation holes are used to reduce wind resistance during flight. Ventilation openings are also used to dampen vibrations when the compound wing UAV lands, thereby reducing the impact force from the ground that could damage the electronic components of the compound wing UAV during landing. Shock-absorbing plates are used to further reduce the vibration experienced by the landing gear during landing, thereby protecting the electronic components inside the compound wing UAV and improving the service life of the components. Attached Figure Description

[0017] Figure 1 This is a schematic diagram of the main structure of this utility model; Figure 2 This is a schematic diagram of the lower view assembly structure of this utility model; Figure 3 This utility model Figure 3 A magnified view of part A; Figure 4 This is a schematic diagram of the rear view structure of this utility model; Figure 5 This utility model Figure 4 A magnified view of part B; Figure 6 This is a front sectional view of the present invention; Figure 7 This utility model Figure 6 A magnified view of part C.

[0018] Explanation of reference numerals in the attached drawings: 100, Compound-wing UAV; 101, Fixed wing; 102, Vertical power frame; 103, Connector; 104, Vertical plate; 105, Flat plate; 200, Drop device; 201, Clamp; 202, Clamping plate; 203, Mounting hole; 204, Drop door panel; 205, Upper door panel; 206, Lower door panel; 207, Electronic latch; 208, Door; 209, Door lock; 210, Hinge; 211, Drop box; 300, Adjustable positioning rod; 301, Positioning hole; 400, Landing gear; 401, Ventilation hole; 402, Shock absorber. Detailed Implementation

[0019] To make the objectives, technical solutions, and advantages of the embodiments of this utility model clearer, the following will be described in conjunction with the accompanying drawings of the embodiments of this utility model. Figure 1-7 The technical solutions of the embodiments of this utility model are clearly and completely described below. Obviously, the described embodiments are only some, not all, of the embodiments of this utility model. All other embodiments obtained by those skilled in the art based on the described embodiments of this utility model are within the protection scope of this utility model.

[0020] like Figure 1-7 As shown: This embodiment provides a vertical take-off and landing fixed wing for a compound-wing UAV, including fixed wings 101 symmetrically arranged on the fuselage of the compound-wing UAV 100. The fixed wings 101 are laterally mounted on the fuselage of the compound-wing UAV 100 and can be welded or riveted to the UAV fuselage. Each fixed wing 101 is provided with a vertical power frame 102, and each vertical power frame 102 is provided with a pair of vertical propellers. A connector 103 is provided at the bottom center of each fixed wing 101. The connector 103 is installed close to the center of the UAV fuselage. The axis is used to reduce the impact on flight attitude after the throwing device is loaded with emergency items, and also to reduce the stress on the fixed wing 101. The connector 103 is used to connect the fixed wing 101 to the throwing device. Each connector 103 has a throwing device 200 at its bottom. The throwing device 200 is used to throw items from the bottom of the vertical power frame 102. A pair of landing gears 400 are symmetrically arranged along the fuselage axis at the bottom of the compound wing UAV 100. The landing gears 400 are used to reduce the recoil force when the compound wing UAV 100 lands on the ground, thereby protecting the internal components of the UAV.

[0021] When in use, emergency rescue items are placed in the drop box 211 by opening the door 208. When it is necessary to drop items, the electronic lock 207 is unlocked first, which causes the bottom of the drop door 204 to lose support, thereby opening the drop door 204 and allowing the emergency items to be dropped into the emergency rescue area. This prevents the dropped items from colliding with the landing gear 400 when dropping items, and also facilitates the subsequent maintenance of the drone.

[0022] This embodiment provides a vertical take-off and landing fixed wing for a compound-wing unmanned aerial vehicle (UAV). like Figure 1 , 2As shown in Figure 3: Each connector 103 includes a vertical plate 104 connected to the fixed wing 101 on the same side. The vertical plate 104 and the fixed wing 101 can be fixed together by rivets. The vertical plate 104 is used to connect the flat plate 105 to the fixed wing 101. A flat plate 105 is provided at the bottom of the vertical plate 104. The flat plate 105 and the vertical plate 104 can be connected integrally. The flat plate 105 is used to connect the vertical plate 104 to the adjusting positioning rod 300. An adjusting positioning rod 300 is fixedly provided at the bottom of each flat plate 105. The adjusting positioning rod 300 and the flat plate 105 can be fixed together by bolts. The adjusting positioning rod 300 is long and narrow. The adjusting positioning rod 300 is used to install throwing boxes 211 of different lengths and widths. Each adjusting positioning rod 300 is provided with multiple positioning holes 301. The positioning holes 301 are threaded and used to install bolts.

[0023] Its effects are as follows: the vertical plate 104 is used to connect the flat plate 105 to the fixed wing 101, the flat plate 105 is used to connect the vertical plate 104 to the adjusting positioning rod 300, the adjusting positioning rod 300 is used to install throwing boxes 211 of different lengths and widths, and the positioning hole 301 is used to install bolts.

[0024] like Figure 2 , 3 As shown in Figures 4, 5, 6, and 7: Each dispensing device 200 includes a clamp 201 adapted to the adjusting positioning rod 300 on the same side. The clamp 201 is used to connect the throwing box 211 to the adjusting positioning rod 300. Each clamp 201 consists of two clamping plates 202, which are heat-fused to the throwing box 211. Each clamping plate 202 is provided with multiple mounting holes 203. The mounting holes 203 are threaded for installing positioning bolts. The mounting holes 203 are adapted to the positioning holes 301 and are fixed by bolt connection. The clamp 201 and the adjusting positioning rod 300 are connected by bolts after the mounting holes 203 correspond to the positioning holes 301, thereby connecting the throwing box 211 to the adjusting positioning rod 300, and the mounting holes 203 and positioning holes 301 are adapted.

[0025] Its effect is as follows: the chuck 201 is used to connect the throwing box 211 with the adjusting positioning rod 300, and the mounting hole 203 is also used to install bolts. The chuck 201 and the adjusting positioning rod 300 are connected by bolts after the mounting hole 203 corresponds to the positioning hole 301, thereby connecting the throwing box 211 with the adjusting positioning rod 300.

[0026] like Figure 2 , 3As shown in Figures 4 and 5: The delivery device 200 also includes a delivery box 211 at the bottom of the clamp 201. The delivery box 211 is a hollow box with a gas guide design on the windward side. The box wall of the delivery box 211 is also made of hollow material to reduce its weight. The delivery box 211 is used to deliver emergency rescue supplies. A pair of delivery door panels 204 are rotatably installed at the bottom of the delivery box 211. The delivery door panels 204 are used to open the delivery box 211 from the bottom. Each delivery door panel 204 includes an upper door panel 205 and a lower door panel 206. The upper door panel 205 and the lower door panel 206 are tenon-and-mortise engaged. Multiple electronic locks 207 are provided in the gap at the bottom of the upper door panel 205 and the lower door panel 206. The electronic locks 207 include a slot and an electric bolt. The electric slot is compatible with the electric latch. The slot is fixed to the bottom of the lower door panel 206 by bolts. The electric latch is fixed to the bottom of the upper door panel by bolts. The pin in the electric latch is used to support the gap of the throwing door panel 204. The electronic latch 207 is used to prevent the throwing door panel 204 from opening automatically. One end of the electronic latch 207 is connected to the bottom of the upper door panel 205, and the other end of the electronic latch 207 is connected to the lower door panel 206. The upper door panel 205 is rotatably connected to one side of the throwing box 211 through a rotating shaft. One end of the rotating shaft is equipped with a gear set and a limiting device. The lower door panel 206 is rotatably connected to the other side of the throwing box 211 through a rotating shaft. One end of the rotating shaft is equipped with a gear set and a limiting device. The limiting device is used to control the rotation angle of the throwing door panel 204.

[0027] Its functions are as follows: the throwing box 211 is used to throw emergency rescue supplies, the pin in the electric latch is used to support the gap of the throwing door panel 204, and the electronic latch 207 is used to prevent the throwing door panel 204 from opening automatically.

[0028] like Figure 2 , 3 As shown in Figures 4, 5, and 6: The drop box 211 has a closable door 208 on the side away from the nose of the compound-wing UAV 100. The door 208 is used to place emergency items inside the drop box 211. The bottom of the door 208 is hinged to the drop box 211 via a hinge 210, which facilitates opening the door 208. The top of the door 208 is equipped with a lock 209. The lock 209 includes a plug that connects to the door 208, with a threaded hole at the top of the plug and a slot that is fixed to the wall of the drop box 211. The slot has a threaded hole and a bolt. The bolt connects the slot to the plug, thereby connecting the door 208 to the drop box 211. The lock 209 is used to fix the door 208. The other end of the lock 209 is connected to the outer wall of the drop box 211.

[0029] Its effect is:

[0030] like Figure 1 , 2As shown: The landing gear 400 is in an inverted Y-shape. The landing gear 400 can be heat-fused to the fuselage of the compound wing UAV 100 or fixed by bolts. Each landing gear 400 is provided with several ventilation holes 401. The ventilation holes 401 are used to reduce wind resistance during flight. The ventilation holes are also used to dampen the compound wing UAV 100 when landing, thereby reducing the impact force of the ground action during landing and reducing damage to the electronic components of the compound wing UAV 100. A shock-absorbing plate 402 is fixedly installed at the bottom of each landing gear 400. The shock-absorbing plate 402 is fixed to the landing gear 400 by bolts. The shock-absorbing plate 402 is used to further reduce the vibration of the landing gear 400 during landing, thereby protecting the electronic components inside the compound wing UAV 100 and improving the service life of the components. The shock-absorbing plate 402 adopts a gas guiding design.

[0031] Its effects are as follows: the ventilation hole 401 is used to reduce wind resistance during flight, and the ventilation port is also used to dampen the composite wing UAV 100 when it lands, thereby reducing the impact force of the ground action during landing and reducing damage to the electronic components of the composite wing UAV 100. The damping plate 402 is used to further reduce the vibration of the landing gear 400 during landing, thereby protecting the electronic components inside the composite wing UAV 100 and improving the service life of the components.

[0032] Working principle: Emergency rescue items are placed in the drop box 211 by opening the door 208. When it is necessary to drop items again, the electronic lock 207 is unlocked first, which causes the bottom of the drop door 204 to lose support and open the drop door 204, so that the emergency items can be dropped into the emergency rescue area. This prevents the dropped items from colliding with the landing gear 400 when dropping items again, and also facilitates the subsequent maintenance of the drone.

[0033] Furthermore, it should be noted that, in the description of this utility model, unless otherwise explicitly specified and limited, the terms "installation," "connection," and "joining" should be interpreted broadly. For example, they can refer to a fixed connection, a detachable connection, or an integral connection; they can refer to a mechanical connection or an electrical connection; they can refer to a direct connection or an indirect connection through an intermediate medium; and they can refer to the internal connection of two components. Those skilled in the art can understand the specific meaning of the above terms in this utility model according to the specific circumstances.

[0034] The above description is the preferred embodiment of this utility model. It should be noted that for those skilled in the art, several improvements and modifications can be made without departing from the principle of this utility model, and these improvements and modifications should also be considered within the protection scope of this utility model.

Claims

1. A vertical take-off fixed wing for a compound-wing unmanned aerial vehicle (UAV), comprising fixed wings (101) symmetrically arranged on the fuselage of a compound-wing UAV (100), each fixed wing (101) being provided with a vertical power frame (102), characterized in that: Each of the fixed wings (101) has a connector (103) at its central bottom. The connector (103) is installed close to the central axis of the fuselage of the compound wing UAV (100). Each connector (103) has a delivery device (200) at its bottom. A pair of landing gears (400) are symmetrically arranged along the fuselage axis at the bottom of the fuselage of the compound wing UAV (100).

2. The vertical take-off fixed wing of a compound wing UAV as described in claim 1, characterized in that: Each of the connectors (103) includes a vertical plate (104) connected to the fixed wing (101) on the same side thereon, and a flat plate (105) is provided at the bottom of the vertical plate (104).

3. A composite-wing unmanned aerial vehicle with a vertical take-off and landing fixed wing as described in claim 2, characterized in that: Each of the flat plates (105) has an adjustment positioning rod (300) fixedly installed at its bottom, and each of the adjustment positioning rods (300) has multiple positioning holes (301).

4. A composite-wing unmanned aerial vehicle with a vertical take-off and landing fixed wing as described in claim 3, characterized in that: Each of the dispensing devices (200) includes a clamp (201) adapted to the adjusting positioning rod (300) on the same side therewith. Each clamp (201) consists of two clamping plates (202), and each clamping plate (202) is provided with a plurality of mounting holes (203), which are adapted to the positioning holes (301).

5. A composite wing UAV with a vertical take-off and landing fixed wing as described in claim 4, characterized in that: The delivery device (200) also includes a delivery box (211) at the bottom of the clamp (201). A pair of delivery gates (204) are rotatably provided at the bottom of the delivery box (211). Each delivery gate (204) includes an upper gate (205) and a lower gate (206). Multiple electronic locks (207) are provided at the gap between the bottom of the upper gate (205) and the lower gate (206).

6. A composite-wing unmanned aerial vehicle with a vertical take-off and landing fixed wing as described in claim 5, characterized in that: One end of the electronic lock (207) is connected to the bottom of the upper door panel (205), and the other end of the electronic lock (207) is connected to the lower door panel (206).

7. A composite-wing unmanned aerial vehicle with a vertical take-off and landing fixed wing as described in claim 6, characterized in that: The drop box (211) is provided with a door (208) on the side away from the nose of the compound wing UAV (100). The bottom of the door (208) is hinged to the drop box (211) via a hinge (210). The top of the door (208) is provided with a door lock (209), and the other end of the door lock (209) is connected to the outer wall of the drop box (211).

8. A composite-wing unmanned aerial vehicle with a vertical take-off and landing fixed wing as described in claim 7, characterized in that: The landing gear (400) is in the shape of an inverted Y. Each landing gear (400) is provided with several ventilation holes (401). A shock-absorbing plate (402) is fixedly provided at the bottom of each landing gear (400). The shock-absorbing plate (402) adopts a gas flow guiding design.

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