Unmanned aerial vehicle parachute landing protection device

Abstract

The utility model discloses an unmanned aerial vehicle parachute landing protection device, and relates to the technical field of unmanned aerial vehicle parachute landing. The unmanned aerial vehicle comprises an unmanned aerial vehicle body, an unmanned support connected with the side face of the unmanned aerial vehicle body and an unmanned aerial vehicle paddle connected with the top of the unmanned support, and further comprises a parachute landing function bin attached to the top of the unmanned aerial vehicle body, a parachute landing filling bin is arranged on one side of the parachute landing function bin, and a detonating bin is fixedly arranged at the front end of the parachute landing filling bin. The unmanned aerial vehicle is provided with the parachute filling bin and the parachute function bin, the parachute filling bin is inserted into the parachute function bin to complete combination of the parachute filling bin and the parachute function bin, meanwhile, the parachute main body is arranged in the parachute cabin groove, and the barometric altimeter, the attitude sensor and the acceleration sensor are arranged in the parachute cabin groove, so that when the unmanned aerial vehicle is abnormal in attitude and angular velocity or suddenly changed in height, the unmanned aerial vehicle can be automatically parked. According to the unmanned aerial vehicle parachute, the jetting device can be automatically detonated without manual intervention, the parachute body can be automatically unfolded, then the parachute landing effect is achieved, the unmanned aerial vehicle is protected, and losses are reduced.

Description

Technical Field

[0001] This utility model belongs to the field of drone parachute technology, and in particular relates to a drone parachute protection device. Background Technology

[0002] During drone operations, accidents and crashes can occur due to factors such as mechanical or electronic equipment failure, electromagnetic interference, operational errors, battery depletion, and severe weather. After a drone crashes, the crash location cannot be accurately pinpointed, especially when it crashes in forests or grassy areas, making it difficult to locate. Even if it is found, the aircraft is often disintegrated and beyond repair. If an aircraft crashes over densely populated cities, it can cause significant loss of life and property on the ground, with unimaginable consequences. Therefore, there is an urgent need for a parachute protection device that can automatically deploy when a drone malfunctions. Utility Model Content

[0003] In view of the above-mentioned shortcomings of the existing technology, the present invention provides a parachute protection device for unmanned aerial vehicles, which can effectively solve the problems of the existing technology.

[0004] To solve the above-mentioned technical problems, this utility model is achieved through the following technical solution:

[0005] This utility model relates to a parachute protection device for unmanned aerial vehicles (UAVs), including a UAV fuselage, an unmanned aerial vehicle (UAV) support connected to the side of the UAV fuselage, and UAV propellers connected to the top of the UAV support. It also includes:

[0006] The parachute compartment is attached to the top of the drone fuselage. A parachute filling compartment is located on one side of the parachute compartment. A detonation compartment is fixed at the front end of the parachute filling compartment. The surface of the parachute compartment has a slot that allows the detonation compartment to be inserted. An explosive ejector is located on the top of the parachute filling compartment. The main body of the parachute is installed in the groove of the parachute compartment. A locking mechanism is provided between the parachute compartment and the parachute filling compartment.

[0007] Furthermore, an explosive catapult is provided at the center of the parachute compartment groove, and the explosive catapult is attached to the inner wall of the parachute compartment groove by adhesive backing.

[0008] Furthermore, the top of the parachute filling chamber is equipped with a hatch, and a cover plate is attached to the hatch.

[0009] Furthermore, the main body of the parachute is made of 20D grade high-toughness lightweight fabric, with a special smooth and dense coating on the surface.

[0010] Furthermore, the bottom of the parachute compartment is fixed with a support plate for supporting the parachute filling compartment and the bottom of the detonation compartment.

[0011] Furthermore, the locking mechanism includes a positioning support rod, a rotating shaft, a supporting positioning rod, and a through hole. The rotating shaft is rotatably connected to the side of the parachute filling compartment, the supporting positioning rod is fixed to the side wall of the parachute functional compartment, the positioning support rod is fixed to the end face of the rotating shaft, and the through hole is opened on the side of the positioning support rod. The supporting positioning rod and the through hole are inserted and adapted to each other.

[0012] Furthermore, the end of the support positioning rod is provided with a threaded part, and the bent part of the support positioning rod is in contact with the top of the positioning support rod.

[0013] This utility model has the following beneficial effects:

[0014] This utility model is equipped with a parachute filling compartment and a parachute function compartment. The parachute filling compartment is inserted into the parachute function compartment to complete the combination of the two. At the same time, the parachute compartment groove houses the main body of the parachute, as well as a barometric altimeter, attitude sensor and acceleration sensor. When the drone experiences abnormal attitude, angular velocity or sudden altitude change, the spray device can be automatically activated without human intervention, so that the main body of the parachute can be automatically deployed, thereby achieving the effect of parachute descent, protecting the drone and reducing losses. Attached Figure Description

[0015] To more clearly illustrate the technical solutions of the embodiments of this utility model, the accompanying drawings used in the description of the embodiments will be briefly introduced below. Obviously, the drawings described below are only some embodiments of this utility model. For those skilled in the art, other drawings can be obtained based on these drawings without creative effort.

[0016] Figure 1 This is a schematic diagram of the present invention;

[0017] Figure 2 This is a split view of the parachute functional compartment and the parachute filling compartment of this utility model;

[0018] Figure 3 This is a schematic diagram of the structure of the parachute filling compartment of this utility model;

[0019] Figure 4 This is a schematic diagram of the connection between the positioning rod and the supporting positioning rod of this utility model.

[0020] The attached diagram lists the components represented by each number as follows:

[0021] 1. UAV fuselage; 2. UAV support frame; 3. UAV propellers; 4. Parachute compartment; 5. Parachute filling compartment; 6. Compartment cover; 7. Parachute compartment recess; 8. Explosive ejector; 9. Parachute body; 10. Detonation compartment; 11. Support plate; 12. Positioning rod; 13. Rotating shaft; 14. Support positioning rod; 15. Perforated part; 16. Strap loop; 17. Restraint strap. Detailed Implementation

[0022] The technical solutions of the present invention will be clearly and completely described below with reference to the accompanying drawings of the embodiments of the present invention.

[0023] Please see Figure 1-4 As shown, this utility model is a parachute protection device for unmanned aerial vehicles (UAVs), including a UAV fuselage 1, an unmanned aerial vehicle (UAV) support frame 2 connected to the side of the UAV fuselage 1, and UAV propellers 3 connected to the top of the UAV support frame 2. A parachute compartment 4 is attached to the top of the UAV fuselage 1. A parachute filling compartment 5 is provided on one side of the parachute compartment 4 and connected to it. A support plate 11 for supporting the parachute filling compartment 5 and the bottom of the detonation chamber 10 is fixed to the bottom of the parachute compartment 4. The parachute filling compartment 5 is equipped with a parachute body 9. The parachute compartment 4 contains a barometric altimeter, attitude sensor, and accelerometer to monitor the UAV's flight status in real time. It also includes a positioning module for real-time... The system displays the entire parachute protection period and the drone's location. It includes a built-in power supply and control module. A recessed parachute compartment 7 is located at the top of the parachute filling compartment 5. The parachute body 9 is placed inside the compartment 7, and is adhered to the wall of the compartment 7 via adhesive at the center of the bottom. The parachute body 9 is then pressed onto the explosive ejector 8. The opening at the top of the compartment 7 is secured by a cover plate 6. Notably, the cover plate 6 is forced open after the parachute body 9 deploys, allowing it to unfold and form the parachute. The parachute body 9 is made of 20D-grade high-toughness, lightweight fabric with a special smooth and dense coating to aid in the drone's slow descent. A wire groove is located at the bottom of the compartment 7, into which red and black wires are inserted. These wires connect to a triggering device inside the detonation chamber 10 to detonate the explosive ejector 8. This device is connected to the control module. This detonation method is existing technology.

[0024] The surface of the parachute filling chamber 5 is fixedly connected to the detonation chamber 10, and the detonation chamber 10 and the parachute filling chamber 5 are stepped. A slot is opened on the surface of the parachute functional chamber 4 to allow the detonation chamber 10 to be inserted. The detonation chamber 10 is inserted laterally into the slot, so that the surfaces of the parachute functional chamber 4 and the parachute filling chamber 5 are in contact to complete the installation. In order to maintain a high connection, a locking mechanism is provided between the parachute functional chamber 4 and the parachute filling chamber 5. The locking mechanism includes a positioning support rod 12, a rotating shaft 13, a support positioning rod 14, and a through hole 15. The rotating shaft 13 is rotatably connected to the side of the parachute filling chamber 5, the support positioning rod 14 is fixed to the side wall of the parachute functional chamber 4, the positioning support rod 12 is fixed to the end face of the rotating shaft 13, and the through hole 15 is opened on the side of the positioning support rod 12. The perforated part 15 is inserted and adapted. The end of the support positioning rod 14 is provided with the perforated part 15, and the bent part of the support positioning rod 14 is attached to the top of the positioning support rod 12. When the parachute filling chamber 5 approaches the parachute functional chamber 4, the rotating shaft part 13 and the positioning support rod 12 move synchronously toward the support positioning rod 14. After the detonation chamber 10 is completely submerged in the slot of the parachute functional chamber 4, the rotating shaft part 13 is rotated toward the support positioning rod 14, so that the end of the positioning support rod 12 is attached to the bent part of the support positioning rod 14. Then the support positioning rod 14 is inserted into the perforated part 15, and the threaded part of the support positioning rod 14 protrudes upward from the perforated part 15. At this time, the positioning support rod 12 is limited and locked by screwing the nut into the threaded part. At this time, the connection strength between the parachute functional chamber 4 and the parachute filling chamber 5 can be strengthened. Meanwhile, before the positioning rod 12 falls into the support positioning rod 14, a strap collar 16 can be fitted onto the positioning rod 12. After the nut is screwed into the threaded part of the support positioning rod 14, the strap collar 16 can be assembled simultaneously. The assembled strap collar 16 is wrapped around the body of the drone body 1. It is worth noting that when the restraint strap 17 is tied to the body of the drone body 1, it should not cover the sensors of the drone body 1 itself.

[0025] The above are merely preferred embodiments of the present utility model and do not limit the present utility model. Any modifications, equivalent substitutions, or improvements made to the technical solutions described in the foregoing embodiments, or to some of the technical features, shall fall within the protection scope of the present utility model.

Claims

1. A parachute protection device for unmanned aerial vehicles (UAVs), comprising a UAV fuselage (1), an unmanned aerial vehicle (UAV) support frame (2) connected to the side of the UAV fuselage (1), and UAV propellers (3) connected to the top of the unmanned aerial vehicle (UAV) support frame (2), characterized in that, Also includes: The parachute compartment (4) is attached to the top of the UAV fuselage (1). A parachute filling compartment (5) is provided on one side of the parachute compartment (4). A detonation compartment (10) is fixed at the front end of the parachute filling compartment (5). A slot is provided on the surface of the parachute compartment (4) to allow the detonation compartment (10) to be inserted. An explosive ejector (8) is provided on the top of the parachute filling compartment (5). The parachute body (9) is installed in the groove of the parachute compartment groove (7). A locking mechanism is provided between the parachute compartment (4) and the parachute filling compartment (5).

2. The UAV parachute protection device according to claim 1, characterized in that, An explosive catapult (8) is provided at the center of the parachute compartment groove (7). The explosive catapult (8) is attached to the inner wall of the parachute compartment groove (7) by adhesive backing.

3. The UAV parachute protection device according to claim 2, characterized in that, The top of the parachute filling chamber (5) is provided with a chamber opening, and a chamber cover plate (6) is attached to the chamber opening.

4. The UAV parachute protection device according to claim 1, characterized in that, The main body of the parachute (9) is made of 20D grade high toughness lightweight fabric, and the surface is coated with a special smooth and dense coating.

5. The UAV parachute protection device according to claim 1, characterized in that, The bottom of the parachute function compartment (4) is fixed with a support plate (11) at the bottom of the parachute filling compartment (5) and the detonation compartment (10).

6. The UAV parachute protection device according to claim 1, characterized in that, The locking mechanism includes a positioning support rod (12), a rotating shaft (13), a supporting positioning rod (14), and a through hole (15). The rotating shaft (13) is rotatably connected to the side of the parachute filling chamber (5). The supporting positioning rod (14) is fixed to the side wall of the parachute functional chamber (4). The positioning support rod (12) is fixed to the end face of the rotating shaft (13). The through hole (15) is opened on the side of the positioning support rod (12), and the supporting positioning rod (14) and the through hole (15) are inserted and adapted to each other.

7. A UAV parachute protection device according to claim 6, characterized in that, The end of the support positioning rod (14) is provided with a threaded part, and the bent part of the support positioning rod (14) is in contact with the top of the positioning support rod (12).

Images