Three-dimensional space parameter adjusting device for spherical unmanned aerial vehicle
By using a spherical UAV three-dimensional spatial parameter adjustment device, which utilizes a gear rack, a detachable positioning plate, and a rotating parameter adjustment structure, the problem of simple UAV parameter adjustment support structure is solved, achieving multi-dimensional adjustment and error reduction.
Patent Information
- Application Number
- CN202423178297.9
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-12-23
- Publication Date
- 2025-11-21
- Estimated Expiration
- 2034-12-23
AI Technical Summary
Existing drone parameter tuning brackets have simple structures that cannot meet the requirements of drones for different types of parameter tuning settings. Furthermore, the attitude of drones is easily affected by vertical movement when tilting or rotating, leading to parameter tuning errors.
A spherical UAV three-dimensional spatial parameter adjustment device is adopted, which adjusts the height of the longitudinal support rod through gear and rack cooperation. Combined with a detachable positioning plate and a rotating parameter adjustment structure, including a first rotating parameter adjustment structure and a second rotating parameter adjustment structure, multi-dimensional adjustment is achieved.
It enables quick and efficient debugging of drone parameters, has a simple structure, is easy to disassemble and assemble and store parts, and reduces debugging errors.
Smart Images
Figure CN223574682U_ABST
Abstract
Description
TECHNICAL FIELD
[0001] The utility model belongs to unmanned plane technical field, concretely relates to a spherical unmanned plane three -dimensional space parameter setting device. BACKGROUND
[0002] The unmanned plane is the no -person carrier that utilizes radio remote control equipment and self -provided program control device to manipulate, it is widely used in aerial photography, surveying and mapping, disaster relief, agriculture and other fields, before the actual flight of unmanned plane, usually need to debug control parameter.
[0003] When the parameter of unmanned plane is debugged, first, the unmanned plane is fixed on the supporting plate, then the operator controls the unmanned plane to start running, and debugs the control parameter, the parameter setting support structure is simple in prior art, and inconvenient to store, when parameter setting is carried out, the form is single, for example, when the unmanned plane is parameter setting, the movement form of unmanned plane in vertical direction adopts fixed or sliding block sliding mode, this mode limits the freedom of unmanned plane in vertical direction, can not satisfy the requirement of different forms of parameter setting of unmanned plane.
[0004] When the unmanned plane is controlled to tilt or rotate, the position of unmanned plane in vertical direction is not fixed, the attitude of unmanned plane tilting or rotating is easily affected by the movement of unmanned plane in vertical direction, thereby bringing error to parameter debugging.
[0005] In view of the above factors, the utility model provides a spherical unmanned plane three -dimensional space parameter setting device, through setting adjustment device, the height of longitudinal support rod is adjusted through the cooperation of gear and rack when using, it is quick and efficient, simple structure, convenient to disassemble and assemble, and convenient to store parts. UTILITY MODEL CONTENTS
[0006] The utility model aims at providing a spherical unmanned plane three -dimensional space parameter setting device to solve the problems in the above background.
[0007] The utility model aims at providing a spherical unmanned plane three -dimensional space parameter setting device to solve the problems in the above background.
[0008] The detachable positioning plate is connected with the second rotary parameter setting structure in a detachable mode on the positioning plate.
[0009] Further, the detachable connection between the adjusting device and the positioning plate is screw connection.
[0010] The detachable connection between the positioning plate and the second rotation parameter adjusting structure is screw connection.
[0011] Further, the detachable connection between the transverse positioning rod and the first rotation parameter adjusting structure is sleeve joint connection.
[0012] The transverse positioning rod is provided with limiting holes between the first rotation parameter adjusting structures, the limiting holes are connected with pin shafts through plug-in connection, and the height of the pin shafts is higher than the circumferential plane of the first rotation parameter adjusting structures.
[0013] Further, the limiting holes are symmetrically arranged, the first rotation parameter adjusting structures are located between the limiting holes and do not contact the limiting holes.
[0014] Further, the first rotation parameter adjusting structure comprises a sleeve and a mounting plate fixedly connected with the sleeve.
[0015] The first rotation parameter adjusting structure can rotate along the transverse positioning rod.
[0016] Further, the second rotation parameter adjusting structure comprises a positioning column, a threaded connection section is fixedly arranged at the lower end of the positioning column, the threaded connection section is matched with a threaded hole on the positioning plate, and a steering head is detachably connected with the upper end of the positioning column.
[0017] The bottom of the steering head is connected with the positioning column through a threaded end, a connecting end is fixedly arranged on the steering head, and the connecting end is a threaded column structure.
[0018] Further, the detachable connection between the adjusting device and the longitudinal supporting rod is screw connection.
[0019] The adjusting device comprises a positioning box and a fixed box arranged in the positioning box, a rack is arranged in the fixed box, the rack is matched with a gear, the gear is arranged on the output shaft of a control motor, and the output end of the control motor is connected with the fixed box through a bearing seat.
[0020] The positioning box is provided with an outlet, and the size of the outlet is the same as that of the I-shaped rack.
[0021] Further, the second rotation parameter adjusting structure is vertically arranged and located below the first rotation parameter adjusting structure.
[0022] Compared with the prior art, the present application has the following beneficial effects:
[0023] The detachable mode between the adjusting device and the positioning plate is bolt connection, and the detachable mode between the positioning plate and the second rotary parameter adjusting structure is screw connection.
[0024] The utility model discloses two different forms for the spherical unmanned plane parameter adjusting operation, including the first rotary parameter adjusting structure and the second rotary parameter adjusting structure, the first rotary parameter adjusting structure is rotary, and the second rotary parameter adjusting structure is universal rotation, and can be adjusted according to the different needs of use.
[0025] The utility model discloses simple structure, convenient to dismount and assemble, and convenient for part storage.
[0026] The utility model discloses simple structure, convenient to dismount and assemble, and convenient for part storage. DRAWINGS
[0027] Figure 1 It is the three-dimensional schematic view of the utility model;
[0028] Figure 2 It is the plane schematic view of the utility model;
[0029] Figure 3 It is the plane schematic view of the utility model Figure 2 of the utility model;
[0030] Figure 4 It is the enlarged schematic view of the second rotary parameter adjusting structure of the utility model;
[0031] Figure 5 It is the enlarged schematic view of the utility model steering head;
[0032] Figure 6 It is the enlarged schematic view of the utility model rack section;
[0033] Figure 7 It is the cross section schematic view of the utility model adjusting device. DETAILED DESCRIPTION
[0034] The technical scheme in the embodiments of the utility model will be described clearly and completely below in conjunction with the drawings in the embodiments of the utility model, and obviously, the described embodiments are only part of the embodiments of the utility model, not all the embodiments, and all other embodiments obtained by the person skilled in the art without creative labor based on the embodiments in the utility model belong to the protection scope of the utility model.
[0035] In the description of the utility model, it needs to be explained that, unless there is definite stipulation and limitation, the terms "mount", "connect", "connection" should be understood in broad sense, for example, it can be fixed connection, also can be detachable connection, or integrally connected, it can be direct connection, also can be indirectly connected through intermediate medium. For ordinary skilled in the art, the specific meaning of the above terms in the utility model can be understood according to specific circumstances.
[0036] In the description of the utility model, it needs to be understood that, the orientation or positional relationship indicated by the terms "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer" and the like is based on the orientation or positional relationship shown in the drawings, and is only for the convenience of describing the utility model and simplifying the description, and therefore cannot be understood as a limitation on the utility model.
[0037] As Figures 1-7 The spherical unmanned aerial vehicle three-dimensional space parameter adjusting device, including adjusting device 1, adjusting device 1 is symmetrically arranged, and the longitudinal support rod 2 is detachably connected on adjusting device 1, the transverse positioning rod 3 is detachably connected on longitudinal support rod 2, and the first rotating parameter adjusting structure 4 is detachably connected on transverse positioning rod 3.
[0038] The detachable positioning plate is arranged between the adjusting device 1, and the detachable positioning plate is 2-5 centimeters away from the bottom surface of the adjusting device 1 or is horizontally consistent with the bottom surface of the adjusting device, and the second rotating parameter adjusting structure 5 is detachably connected on the positioning plate.
[0039] In the use state, the length of the positioning plate and the transverse positioning rod 3 is adjusted according to the distance between the symmetrical adjusting devices.
[0040] In order to facilitate disassembly and assembly in the use state, the detachable mode between the adjusting device 1 and the positioning plate is bolt connection.
[0041] The detachable mode between the positioning plate and the second rotating parameter adjusting structure 5 is screw connection.
[0042] In order to facilitate parameter adjustment in the rotating mode in the use state, the detachable mode between the transverse positioning rod 3 and the first rotating parameter adjusting structure 4 is sleeve connection.
[0043] The limiting hole 43 is arranged between the first rotating parameter adjusting structure 4 on the transverse positioning rod 3, the pin shaft rod is connected to the limiting hole 43 by plug-in connection, and the height of the pin shaft rod is higher than the circumferential plane of the first rotating parameter adjusting structure 4.
[0044] In order to ensure that the imbalance of the unmanned aerial vehicle in the state of movement is prevented from being moved in the state of use, the limiting holes 43 are symmetrically arranged, and the first rotating parameter adjusting structure 4 is located between the limiting holes 43 and does not contact the limiting holes 43.
[0045] The first rotating parameter adjusting structure 4 comprises a sleeve 41 and a mounting plate 42 fixedly connected with the sleeve 41.
[0046] In the state of use, the spherical unmanned aerial vehicle is fixed on the mounting plate 42 by bolts, the mounting plate is a positive direction structure, the size of the mounting plate is the same as the diameter of the spherical unmanned aerial vehicle, and a mounting hole is arranged on the mounting plate for fixing the spherical unmanned aerial vehicle by bolts.
[0047] The first rotating parameter adjusting structure 4 can rotate along the transverse positioning rod 3.
[0048] In order to be able to adjust the balance of the unmanned aerial vehicle in all directions in the state of use, the second rotating parameter adjusting structure 5 comprises a positioning column 51, a threaded connecting section 52 is fixedly arranged at the lower end of the positioning column 51, the threaded connecting section 52 cooperates with a threaded hole on the positioning plate, and a steering head 53 is detachably connected to the upper end of the positioning column 51.
[0049] The bottom of the steering head 53 is connected with the positioning column 51 through a threaded end, a connecting end is fixedly arranged on the steering head 53, the connecting end is a threaded column structure, and in the state of use, the spherical unmanned aerial vehicle is connected with the connecting end fixedly arranged on the steering head 53 to perform adjustment in each direction.
[0050] In the state of use, the end plate (which is a rectangular plate body structure and has a center hole arranged at the center position) for fixing the spherical unmanned aerial vehicle is installed on the step end in a sleeved manner and is locked by a nut in cooperation with the connecting end to fix the mounting plate, and the spherical unmanned aerial vehicle is fixed on the end plate by bolts.
[0051] During adjustment, the unmanned aerial vehicle can be tested and adjusted in different directions by the action of the steering head 53.
[0052] In order to facilitate replacement, adjustment and installation in the state of use, the detachable connection between the adjusting device 1 and the longitudinal supporting rod 2 is a threaded connection.
[0053] The adjusting device 1 comprises a positioning box 11 and a fixing box 12 arranged in the positioning box 11, a rack 13 is arranged in the fixing box 12, the rack 13 cooperates with a gear 14, the gear 14 is arranged on the output shaft of a control motor 15, and the output end of the control motor 15 is connected with the fixing box 12 through a bearing seat.
[0054] The positioning box 11 is provided with an outlet, which has the same size as the I-shaped rack 13.
[0055] The longitudinal support rod 2 is connected to the end face of the rack 13 in a detachable manner, which is a bolt connection manner, so that the longitudinal support rod 2 can be replaced in the use state.
[0056] The rack section adopts an I-shaped structure, wherein the rack is located in the fixed box and is limited by the I-shaped slot of the rack section and the limiting openings at the upper and lower ends of the fixed box.
[0057] In order to facilitate different unmanned aerial vehicle parameter adjustment forms in the use state, the second rotary parameter adjustment structure 5 is vertically arranged and located below the first rotary parameter adjustment structure 4.
[0058] The two first rotary parameter adjustment structures 4 and the second rotary parameter adjustment structure 5 can be adjusted and replaced at any time.
[0059] It is obvious for those skilled in the art that the present application is not limited to the details of the above exemplary embodiments, and can be implemented in other specific forms without departing from the spirit or essential characteristics of the present application. Therefore, the embodiments should be regarded as exemplary and non-limiting, and the scope of the present application is defined by the appended claims rather than the above description, and all changes falling within the meaning and scope of the equivalent elements of the claims should be included in the present application. Any reference signs in the claims should not be regarded as limiting the claims.
[0060] In addition, it should be understood that although the present application is described in the specification in terms of embodiments, each embodiment does not contain only one independent technical solution, and the description manner of the specification is only for the sake of clarity, and those skilled in the art should regard the specification as a whole, and the technical solutions in each embodiment can be combined to form other embodiments which can be understood by those skilled in the art.
Claims
1. A spherical unmanned aerial vehicle (UAV) three-dimensional spatial parameter adjustment device, characterized in that: It includes an adjustment device (1), the adjustment device (1) is symmetrically arranged, and a longitudinal support rod (2) is detachably connected to the adjustment device (1), a transverse positioning rod (3) is detachably connected to the longitudinal support rod (2), and a first rotary parameter adjustment structure (4) is detachably connected to the transverse positioning rod (3). A detachable positioning plate is provided between the adjustment devices (1), and a distance of 2-5 cm is left between the detachable positioning plate and the bottom surface of the adjustment device (1). The second rotary parameter adjustment structure (5) is detachably connected to the positioning plate.
2. The spherical UAV three-dimensional spatial parameter adjustment device according to claim 1, characterized in that: The adjustable device (1) and the positioning plate are detachably connected by bolts; The detachable connection between the positioning plate and the second rotary parameter adjustment structure (5) is a threaded connection.
3. The spherical UAV three-dimensional spatial parameter adjustment device according to claim 2, characterized in that: The detachable connection between the transverse positioning rod (3) and the first rotary parameter adjustment structure (4) is a sleeve connection; The transverse positioning rod (3) is provided with a limiting hole (43) between the first rotary parameter adjustment structure (4), and a pin is inserted into the limiting hole (43). The height of the pin is higher than the circumferential plane of the first rotary parameter adjustment structure (4).
4. The spherical UAV three-dimensional spatial parameter adjustment device according to claim 3, characterized in that: The limiting holes (43) are symmetrically arranged, and the first rotating parameter adjustment structure (4) is located between the limiting holes (43) and does not contact the limiting holes (43).
5. The spherical UAV three-dimensional spatial parameter adjustment device according to claim 4, characterized in that: The first rotary parameter adjustment structure (4) includes a sleeve (41) and a mounting plate (42) fixedly connected to the sleeve (41); The first rotating parameter adjustment structure (4) is capable of rotating along the transverse positioning rod (3).
6. The spherical UAV three-dimensional spatial parameter adjustment device according to claim 5, characterized in that: The second rotary parameter adjustment structure (5) includes a positioning post (51), the lower end of which is fixedly provided with a threaded connection section (52), the threaded connection section (52) is engaged with the threaded hole on the positioning plate, and the upper end of the positioning post (51) is detachably connected to the steering head (53). The bottom of the steering head (53) is connected to the positioning post (51) through a threaded end. A connecting end is fixedly provided on the steering head (53), and the connecting end is a threaded post structure.
7. The spherical UAV three-dimensional spatial parameter adjustment device according to claim 5, characterized in that: The detachable connection between the adjusting device (1) and the longitudinal support rod (2) is a threaded connection; The adjustment device (1) includes a positioning box (11) and a fixed box (12) disposed in the positioning box (11). A rack (13) is disposed in the fixed box (12). The rack (13) cooperates with a gear (14). The gear (14) is disposed on the output shaft of a control motor (15). The output end of the control motor (15) is connected to the fixed box (12) through a bearing seat. The positioning box (11) has an outlet, the size of which is the same as that of the I-shaped rack (13).
8. The spherical UAV three-dimensional spatial parameter adjustment device according to claim 7, characterized in that: The second rotating parameter tuning structure (5) is vertically arranged and located below the first rotating parameter tuning structure (4).