A six-axis, six-rotor unmanned aerial vehicle (UAV) flight training device
By designing adjustable rings and limiting components, the six-axis six-rotor UAV flight training equipment solves the problem of monotonous training difficulty, realizes diversified training scenarios, and improves trainees' operating skills.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- BEIJING JIXING INTELLIGENT TECHNOLOGY CO LTD
- Filing Date
- 2025-05-22
- Publication Date
- 2026-05-26
AI Technical Summary
Existing drone flight training equipment is relatively basic, making it difficult to adjust the training difficulty and provide diverse flight scenarios and environments, which makes it difficult for trainees to master the skills to cope with complex environments.
A six-axis, six-rotor UAV flight training device was designed. Through adjustable rings and limiting components, the training difficulty can be adjusted as needed. This includes rotatable connecting rods and limiting blocks, which enable diversified adjustments to the training difficulty.
By adjusting the training difficulty in various ways, trainees can better cope with complex environments in actual operation and improve their drone operation skills.
Smart Images
Figure CN224287670U_ABST
Abstract
Description
Technical Field
[0001] This utility model belongs to the technical field of unmanned aerial vehicle (UAV) flight training equipment, and in particular relates to a six-axis, six-rotor UAV flight training equipment. Background Technology
[0002] Through training, trainees will master the basic operational skills of drones, such as takeoff, landing, hovering, flight attitude control, and flight path planning. They will be able to accurately and stably control drones to complete various flight missions and cope with emergencies such as wind interference and signal loss, ensuring flight safety.
[0003] Existing training equipment is often limited in scope and doesn't allow for easy adjustment of training difficulty. Limited equipment provides only a narrow range of flight scenarios and conditions, preventing trainees from experiencing diverse environments and flight situations. This hinders their ability to master skills for handling complex environments and may leave them bewildered when encountering similar problems in actual operation. Therefore, we propose a six-axis, six-rotor UAV flight training device. Utility Model Content
[0004] The purpose of this invention is to provide a six-axis, six-rotor unmanned aerial vehicle (UAV) flight training device to solve the problems mentioned in the background art.
[0005] In view of this, the present invention provides a six-axis, six-rotor unmanned aerial vehicle (UAV) flight training device, comprising:
[0006] A base plate, on the top of which a U-shaped frame is fixedly installed, and two rotating rods are rotatably installed inside the U-shaped frame, with a connecting rod fixedly installed between the two rotating rods;
[0007] A limiting component, located within the U-shaped frame, is used to limit one of the rotating rods;
[0008] A first ring is fixedly installed on the top of the connecting rod. A second ring is provided inside the first ring, and a third ring is provided inside the second ring. Grooves are provided inside both the first and second rings. Insert rods are fixedly installed at the bottom of both the second and third rings, and one end of each of the two insert rods extends into the two grooves respectively.
[0009] Two sets of fixing components are located inside the two insertion rods respectively, and are used to fix the two insertion rods respectively.
[0010] In this technical solution, during drone training, users can install the second and third rings according to the required difficulty. When the difficulty is minimal, the second and third rings do not need to be installed, and the drone can be operated to pass through the first ring for training. When the difficulty needs to be increased, the operator can insert the rod on the second ring into the groove on the first ring, which will initially fix the second ring. Then, through the set fixing component, the fixing component fixes the rod on the second ring into the groove on the first ring, ensuring the stability of the second ring. At this time, the drone can be operated to fly through the middle of the second ring. If the difficulty needs to be further increased, the rod on the third ring can be installed into the groove on the second ring, thereby further reducing the drone's passage range and increasing the difficulty of operation.
[0011] Meanwhile, the operator can rotate the connecting rod, which will drive the two rotating rods to rotate within the U-shaped frame. At this time, the first ring will rotate. When it rotates to a certain angle, the limiting component will fix the position of one of the limiting blocks. Consequently, the angle of the connecting rod will be fixed, and the first ring will become tilted. When the second and third rings are pressed, they will also become tilted, thus increasing the difficulty and ensuring that trainees can perfectly control the drone after training.
[0012] In the above technical solution, the limiting component further includes:
[0013] A threaded hole is provided on a U-shaped frame. Several circular holes are provided on one of the rotating rods. A hand-tightening bolt is threaded into the threaded hole. A cylinder is fixedly installed at the bottom end of the hand-tightening bolt. One end of the cylinder extends into one of the circular holes.
[0014] In this technical solution, the operator can rotate the connecting rod, which will drive the two rotating rods to rotate inside the U-shaped frame. At this time, the first ring will rotate. When it rotates to a certain angle, one of the round holes will connect with the threaded hole. The operator can then thread the hand-tightening bolt into the threaded hole. At this time, the cylinder will enter one of the round holes, thereby fixing the position of one of the limiting blocks.
[0015] In the above technical solution, the cylinder and the circular holes are slidably connected, and the circular holes are distributed in a ring at equal intervals.
[0016] In this technical solution, the cylinder can be slidably installed into the circular hole, and the several circular holes are distributed in a ring at equal intervals to ensure that multiple angles of the connecting rod can be adjusted.
[0017] In the above technical solution, the fixing component further includes:
[0018] A T-shaped rod is inserted into a rod and located in a groove. One end of the T-shaped rod passes through one side of the groove and extends to the outside. The other end of the T-shaped rod passes through the other side of the groove and extends to the outside. A sliding groove is provided inside the T-shaped rod and on one side of the groove. A limit block is slidably installed in the sliding groove. A spring is fixedly installed at the bottom of the limit block and tightly welded to the inner wall of the sliding groove.
[0019] In this technical solution, the limiting block on the T-shaped rod can be pressed, causing the limiting block to move downward within the sliding groove. At this time, the spring will be compressed and contracted until the limiting block is fully inserted into the sliding groove. Then, one end of the T-shaped rod can be inserted into the groove on the first ring, and then the T-shaped rod can be moved so that one end of the T-shaped rod is inserted into the insert on the second ring and moved to the outside. At this time, under the action of the spring's rebound force, the spring will drive the limiting block to move upward, causing the top of the limiting block to move to the outside, and one side of the limiting block will contact the first ring. At this time, the position of the T-shaped rod will be fixed, thereby fixing the insert on the second ring into the groove on the first ring, ensuring the stability of the second ring.
[0020] In the above technical solution, the T-shaped rod is further configured to be inserted into the groove.
[0021] In this technical solution, it is ensured that the T-shaped rod can be inserted into the corresponding groove.
[0022] In the above technical solution, one end of the insertion rod is further engaged with the corresponding groove.
[0023] In this technical solution, it is ensured that one end of the insertion rod can be inserted into the corresponding groove.
[0024] In the above technical solution, the rotating rod and the connecting rod are integrally formed.
[0025] In this technical solution, the structural stability between the rotating rod and the connecting rod is ensured.
[0026] The beneficial effects of this utility model are:
[0027] This six-axis, six-rotor UAV flight training equipment, through the coordination of a base plate, U-shaped frame, connecting rod, cylinder, first ring, second ring, third ring, insert rod, groove, fixing component, and drive component, ensures that the difficulty of training can be adjusted in a variety of ways. This allows trainees to cope with more difficult flight scenarios in actual operation after training, making their operation more skillful. Attached Figure Description
[0028] Figure 1This is a schematic diagram of the overall structure of this utility model;
[0029] Figure 2 This is an exploded view of the first and second rings in this utility model.
[0030] Figure 3 This utility model Figure 2 Enlarged structural diagram at point A;
[0031] Figure 4 This is a schematic diagram of the internal structure of the U-shaped frame in this utility model;
[0032] Figure 5 This utility model Figure 4 Enlarged structural diagram at point B;
[0033] Figure 6 This is a schematic diagram of the internal structure of the T-shaped rod in this utility model.
[0034] The markings in the diagram are as follows:
[0035] 1. Base plate; 2. U-shaped frame; 3. Connecting rod; 4. Rotating rod; 5. First ring; 6. Second ring; 7. Third ring; 8. Insert rod; 9. T-shaped rod; 10. Groove; 11. Limiting block; 12. Round hole; 13. Threaded hole; 14. Hand-tightening bolt; 15. Cylinder; 16. Sliding groove; 17. Spring. Detailed Implementation
[0036] The technical solutions of the embodiments of this application will be clearly described below with reference to the accompanying drawings. Obviously, the described embodiments are only some, not all, of the embodiments of this application. All other embodiments obtained by those skilled in the art based on the embodiments of this application are within the scope of protection of this application.
[0037] In the description of this application, it should be noted that the terminology used herein is for the purpose of describing particular embodiments only and is not intended to limit the exemplary embodiments according to this application. For ease of description, the dimensions of the various parts shown in the drawings are not drawn to actual scale. Techniques, methods, and devices known to those skilled in the art may not be discussed in detail, but where appropriate, such techniques, methods, and devices should be considered part of the specification. In all examples shown and discussed herein, any specific values should be interpreted as merely exemplary and not as limitations. Therefore, other examples of exemplary embodiments may have different values. It should be noted that similar reference numerals and letters in the following drawings denote similar items; therefore, once an item is defined in one drawing, it need not be further discussed in subsequent drawings.
[0038] It should be noted that the terms "first," "second," etc., used in the specification and claims of this application are used to distinguish similar objects and not to describe a specific order or sequence. It should be understood that such use of data can be interchanged where appropriate so that embodiments of this application can be implemented in orders other than those illustrated or described herein, and the objects distinguished by "first," "second," etc., are generally of the same class and are not limited in number; for example, a first object can be one or more. Furthermore, in the specification and claims, "and / or" indicates at least one of the connected objects, and the character " / " generally indicates that the preceding and following objects are in an "or" relationship.
[0039] It should be noted that in the description of this application, the directional terms such as "front, back, up, down, left, right", "horizontal, vertical, horizontal" and "top, bottom" indicate the orientation or positional relationship based on the orientation or positional relationship shown in the accompanying drawings. They are only for the convenience of describing this application and simplifying the description. Unless otherwise stated, these directional terms do not indicate or imply that the device or element referred to must have a specific orientation or be constructed and operated in a specific orientation, and therefore should not be construed as a limitation on the scope of protection of this application. The directional terms "inner" and "outer" refer to the inner and outer contours relative to the outline of each component itself.
[0040] It should be noted that, in this application, the terms "comprising," "including," or any other variations thereof are intended to cover non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements includes not only those elements but also other elements not expressly listed, or elements inherent to such a process, method, article, or apparatus. Without further limitations, an element defined by the phrase "comprising one..." does not exclude the presence of other identical elements in the process, method, article, or apparatus that includes that element. Furthermore, it should be noted that the scope of the methods and apparatuses in the embodiments of this application is not limited to performing functions in the order shown or discussed, but may also include performing functions substantially simultaneously or in the reverse order, depending on the functions involved. For example, the described methods may be performed in a different order than described, and various steps may be added, omitted, or combined. Additionally, features described with reference to certain examples may be combined in other examples.
[0041] Example 1:
[0042] Please see Figure 1 - Figure 6 As shown, this embodiment provides a six-axis, six-rotor unmanned aerial vehicle (UAV) flight training device, including:
[0043] The base plate 1 has a U-shaped frame 2 fixedly installed on its top. Two rotating rods 4 are rotatably installed inside the U-shaped frame 2, and a connecting rod 3 is fixedly installed between the two rotating rods 4.
[0044] A limiting component is located inside the U-shaped frame 2 and is used to limit one of the rotating rods 4;
[0045] The first ring 5 is fixedly installed on the top of the connecting rod 3. The first ring 5 is provided with a second ring 6 and the second ring 6 is provided with a third ring 7. The first ring 5 and the second ring 6 are both provided with grooves 10. The bottom of the second ring 6 and the third ring 7 are both fixedly installed with insert rods 8. One end of the two insert rods 8 extends into the two grooves 10 respectively.
[0046] Two sets of fixing components are located inside the two insertion rods 8 respectively, and are used to fix the two insertion rods 8 respectively.
[0047] During drone training, users can install the second ring 6 and the third ring 7 according to the required difficulty. When the difficulty is minimal, there is no need to install the second ring 6 and the third ring 7. In this case, the drone can be operated to pass through the first ring 5 for training. When the difficulty needs to be increased, the staff can insert the stick 8 on the second ring 6 into the groove 10 on the first ring 5. At this time, the second ring 6 will be initially fixed. Then, through the set fixing component, the fixing component will fix the stick 8 on the second ring 6 into the groove 10 on the first ring 5 to ensure the stability of the second ring 6. At this time, the drone can be operated to fly through the middle of the second ring 6. If the difficulty needs to be further increased, the stick 8 on the third ring 7 can be installed into the groove 10 on the second ring 6, thereby further reducing the drone's passage range and increasing the difficulty of operation.
[0048] Meanwhile, the staff can rotate the connecting rod 3, which will drive the two rotating rods 4 to rotate within the U-shaped frame 2. At this time, the first ring 5 will rotate. When it rotates to a certain angle, the limiting component will fix the position of one of the limiting blocks 11. Subsequently, the angle of the connecting rod 3 will be fixed, and the first ring 5 will become tilted. When the second ring 6 and the third ring 7 are pressed, the second ring 6 and the third ring 7 will also become tilted, thereby increasing the difficulty and ensuring that trainees can perfectly control the drone after training.
[0049] Example 2:
[0050] This embodiment provides a six-axis, six-rotor unmanned aerial vehicle (UAV) flight training device. In addition to the technical solutions described in the above embodiments, it also has the following technical features, including a limiting component:
[0051] A threaded hole 13 is provided on the U-shaped frame 2. Several round holes 12 are provided on one of the rotating rods 4. A hand-tightening bolt 14 is installed in the threaded hole 13. A cylinder 15 is fixedly installed at the bottom end of the hand-tightening bolt 14. One end of the cylinder 15 extends into one of the round holes 12.
[0052] The operator can rotate the connecting rod 3, which will drive the two rotating rods 4 to rotate inside the U-shaped frame 2. At this time, the first ring 5 will rotate. When it rotates to a certain angle, one of the round holes 12 will be connected to the threaded hole 13. The operator can then thread the hand-tightening bolt 14 into the threaded hole 13. At this time, the cylinder 15 will enter one of the round holes 12, thereby fixing the position of one of the limiting blocks 11.
[0053] Example 3:
[0054] This embodiment provides a six-axis six-rotor UAV flight training device. In addition to the technical solution of the above embodiment, it also has the following technical features: the cylinder 15 is slidably connected to the circular hole 12, and the circular holes 12 are distributed in a ring at equal intervals.
[0055] Specifically, the cylinder 15 is slidably installed into the circular hole 12, and the circular holes 12 are distributed in a ring at equal intervals to ensure that multiple angles of the connecting rod 3 can be adjusted.
[0056] Example 4:
[0057] This embodiment provides a six-axis, six-rotor unmanned aerial vehicle (UAV) flight training device. In addition to the technical solutions described in the above embodiments, it also has the following technical features, including a fixed component:
[0058] T-shaped rod 9 is inserted into rod 8 and located in groove 10. One end of T-shaped rod 9 passes through one side of groove 10 and extends to the outside. The other end of T-shaped rod 9 passes through the other side of groove 10 and extends to the outside. A sliding groove 16 is provided in T-shaped rod 9 and located on one side of groove 10. Limiting block 11 is slidably installed in sliding groove 16. A spring 17 is fixedly installed at the bottom of limiting block 11 and tightly welded to the inner wall of sliding groove 16.
[0059] The limiting block 11 on the T-shaped rod 9 can be pressed, causing the limiting block 11 to move downward within the sliding groove 16. At this time, the spring 17 will be compressed and contracted until the limiting block 11 is fully inserted into the sliding groove 16. Then, one end of the T-shaped rod 9 can be inserted into the groove 10 on the first ring 5, and then the T-shaped rod 9 can be moved so that one end of the T-shaped rod 9 is inserted into the insertion rod 8 on the second ring 6 and moved to the outside. At this time, under the action of the rebound force of the spring 17, the spring 17 will drive the limiting block 11 to move upward, so that the top of the limiting block 11 moves to the outside, and one side of the limiting block 11 will contact the first ring 5. At this time, the position of the T-shaped rod 9 will be fixed, thereby fixing the insertion rod 8 on the second ring 6 into the groove 10 on the first ring 5, ensuring the stability of the second ring 6.
[0060] Example 5:
[0061] This embodiment provides a six-axis six-rotor UAV flight training device, which, in addition to the technical solution of the above embodiment, also has the following technical features: the T-shaped rod 9 and the groove 10 are inserted and matched.
[0062] Specifically, it is ensured that the T-shaped rod 9 can be inserted into the corresponding groove 10.
[0063] Example 6:
[0064] This embodiment provides a six-axis, six-rotor unmanned aerial vehicle (UAV) flight training device. In addition to the technical solutions of the above embodiments, it also has the following technical features: one end of the insertion rod 8 is inserted and engaged with the corresponding groove 10.
[0065] Specifically, ensure that one end of the insertion rod 8 can be inserted into the corresponding groove 10.
[0066] Example 7:
[0067] This embodiment provides a six-axis six-rotor UAV flight training device. In addition to the technical solutions of the above embodiments, it also has the following technical features: the rotating rod 4 and the connecting rod 3 are integrally formed structures.
[0068] Among these measures, it is essential to ensure the structural stability between the rotating rod 4 and the connecting rod 3.
[0069] Working Principle: During drone training, users can install the second ring 6 and the third ring 7 according to the required difficulty. When the difficulty is minimal, the second ring 6 and the third ring 7 do not need to be installed; the drone can then be operated to pass through the first ring 5 for training. When the difficulty needs to be increased, the operator can insert the insert rod 8 on the second ring 6 into the groove 10 on the first ring 5, initially fixing the second ring 6. Then, the limiting block 11 on the T-shaped rod 9 can be pressed, causing the limiting block 11 to move downward within the sliding groove 16. At this time, the spring 17 will be compressed and contracted until the limiting block 11 is fully inserted into the sliding groove 16. Then, one end of the T-shaped rod 9 can be inserted into the groove 10 on the first ring 5, and then the movement... The T-shaped rod 9 allows one end of it to be inserted into the insert rod 8 on the second ring 6 and displaced to the outside. At this time, under the action of the spring 17's rebound force, the spring 17 will drive the limiting block 11 to move upward, causing the top of the limiting block 11 to move to the outside, and one side of the limiting block 11 will contact the first ring 5. At this time, the position of the T-shaped rod 9 will be fixed, thereby fixing the insert rod 8 on the second ring 6 into the groove 10 on the first ring 5, ensuring the stability of the second ring 6. At this time, the drone can be operated to fly through the middle of the second ring 6. If it is necessary to increase the difficulty, the insert rod 8 on the third ring 7 can be installed in the groove 10 on the second ring 6 as described above, thereby further reducing the passage range of the six-axis six-rotor drone and increasing the difficulty of operation.
[0070] Meanwhile, the operator can rotate the connecting rod 3, which will drive the two rotating rods 4 to rotate within the U-shaped frame 2. At this time, the first ring 5 will rotate. When it rotates to a certain angle, one of the round holes 12 will connect with the threaded hole 13. The operator can then thread the hand-tightening bolt 14 into the threaded hole 13. At this time, the cylinder 15 will enter one of the round holes 12, thereby fixing the position of one of the limiting blocks 11. Subsequently, the angle of the connecting rod 3 will be fixed, and the first ring 5 will become tilted. When the second ring 6 and the third ring 7 are pressed, the second ring 6 and the third ring 7 will also become tilted, thereby increasing the difficulty and ensuring that trainees can perfectly control the six-axis six-rotor drone after training.
[0071] The embodiments of this application have been described above with reference to the accompanying drawings. Unless otherwise specified, the embodiments and features in the embodiments of this application can be combined with each other. This application is not limited to the specific embodiments described above. The specific embodiments described above are merely illustrative and not restrictive. Those skilled in the art can make many other forms under the guidance of this application without departing from the spirit and scope of the claims, and all of these forms are within the protection scope of this application.
Claims
1. A six-axis, six-rotor unmanned aerial vehicle (UAV) flight training device, characterized in that, include: A base plate (1) is fixedly installed on the top of the base plate (1). Two rotating rods (4) are rotatably installed inside the U-shaped frame (2). A connecting rod (3) is fixedly installed between the two rotating rods (4). A limiting component is located inside the U-shaped frame (2) and is used to limit one of the rotating rods (4); The first ring (5) is fixedly installed on the top of the connecting rod (3). The first ring (5) is provided with a second ring (6), and the second ring (6) is provided with a third ring (7). The first ring (5) and the second ring (6) are both provided with grooves (10). The bottom of the second ring (6) and the third ring (7) are both fixedly installed with insert rods (8). One end of each of the two insert rods (8) extends into the two grooves (10). Two sets of fixing components are located in the two inserts (8) respectively, and are used to fix the two inserts (8) respectively.
2. The six-axis, six-rotor unmanned aerial vehicle (UAV) flight training equipment according to claim 1, characterized in that, The limiting component includes: A threaded hole (13) is provided on a U-shaped frame (2). A plurality of round holes (12) are provided on one of the rotating rods (4). A hand-tightening bolt (14) is threaded inside the threaded hole (13). A cylinder (15) is fixedly installed at the bottom end of the hand-tightening bolt (14). One end of the cylinder (15) extends into one of the round holes (12).
3. The six-axis, six-rotor unmanned aerial vehicle (UAV) flight training equipment according to claim 2, characterized in that, The cylinder (15) is slidably connected to the circular holes (12), and the circular holes (12) are distributed in a ring at equal intervals.
4. The six-axis, six-rotor unmanned aerial vehicle (UAV) flight training equipment according to claim 1, characterized in that, The fixing component includes: A T-shaped rod (9) is inserted into a plug rod (8) and located in a groove (10). One end of the T-shaped rod (9) passes through one side of the groove (10) and extends to the outside. The other end of the T-shaped rod (9) passes through the other side of the groove (10) and extends to the outside. A sliding groove (16) is provided in the T-shaped rod (9) and located on one side of the groove (10). A limiting block (11) is slidably installed in the sliding groove (16). A spring (17) is fixedly installed at the bottom of the limiting block (11) and tightly welded to the inner wall of the sliding groove (16).
5. A six-axis, six-rotor unmanned aerial vehicle (UAV) flight training device according to claim 4, characterized in that, The T-shaped rod (9) is inserted into the groove (10).
6. The six-axis, six-rotor unmanned aerial vehicle (UAV) flight training device according to claim 1, characterized in that, One end of the insertion rod (8) is inserted into the corresponding groove (10).
7. A six-axis, six-rotor unmanned aerial vehicle (UAV) flight training device according to claim 1, characterized in that, The rotating rod (4) and the connecting rod (3) are integrally formed.