Pod damping structure and unmanned aerial vehicle
By setting up multiple shock absorbing ball mounts and lever structures on the pod mounting table, combined with the secondary shock absorbing buckle, the problem of single shock absorbing effect in the existing technology is solved, and multi-directional shock absorption and stability are achieved Sex improvement.
Patent Information
- Application Number
- CN202411228194.0
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- Filing Date
- 2024-09-03
- Publication Date
- 2024-12-27
- Estimated Expiration
- 2044-09-03
AI Technical Summary
The existing pod shock absorption structure has a single shock absorption effect in the vertical direction, resulting in insufficient pod stability.
Adopt a pod mounting platform structure including first-stage and second-stage shock absorbing mechanisms. Multiple shock absorbing ball mounts are arranged inclined between the first-stage shock absorbing mount and the first-stage shock absorbing chassis, and use the second-stage shock absorbing The arm and the secondary shock absorber column form a lever structure, combined with the secondary shock absorber buckle to absorb impact energy and provide multi-directional shock absorption effect.
It significantly improves the shock absorption effect and stability of the pod, and can effectively buffer impact in vertical and horizontal four-way directions, extending the life of the shock absorption mechanism.
Smart Images

Figure CN119190383A_ABST
Abstract
Description
Technical Field
[0001] The present invention relates to the technical field of unmanned aerial vehicles, and in particular to a pod shock absorbing structure and an unmanned aerial vehicle. Background Art
[0002] The prior art pod shock-absorbing structures are mostly to set a plurality of vertical shock-absorbing balls between the pod bearing plate and the fuselage connecting plate. For example, a Chinese patent with a publication number of CN205480075U uses a plurality of vertical shock-absorbing balls to reduce the vibration of the pod in the vertical direction. However, since this structure can only reduce the impact in the vertical direction, it has a single shock-absorbing function and poor shock-absorbing effect, resulting in insufficient stability of the pod. Summary of the invention
[0003] The technical problem to be solved by the present invention is to overcome the deficiencies of the prior art, and the first purpose is to provide a pod shock absorbing structure with good shock absorbing effect and improved pod stability.
[0004] The second purpose of the present invention is to provide a UAV with good shock absorption effect and improved pod stability.
[0005] The technical solution adopted by the present invention is: the pod shock-absorbing structure comprises a pod mounting platform, a pod is mounted on the pod mounting platform, the pod mounting platform comprises a first-level shock-absorbing mechanism, the first-level shock-absorbing mechanism comprises a first-level shock-absorbing base frame and a first-level shock-absorbing mounting frame, the first-level shock-absorbing mounting frame is located above the first-level shock-absorbing base frame, a plurality of shock-absorbing ball mounting frames are obliquely arranged between the first-level shock-absorbing mounting frame and the first-level shock-absorbing base frame, and shock-absorbing balls are arranged on the plurality of shock-absorbing ball mounting frames.
[0006] Furthermore, the pod mounting platform also includes a secondary shock absorbing mechanism arranged on the primary shock absorbing mechanism, the secondary shock absorbing mechanism includes a secondary shock absorbing mounting frame, a fuselage connecting plate and two secondary shock absorbing arms, the secondary shock absorbing mounting frame is arranged opposite to the fuselage connecting plate, one end of the two secondary shock absorbing arms are connected to the secondary shock absorbing mounting frame, and the other ends are connected to the lower part of the fuselage connecting plate through a secondary shock absorbing column, and a secondary shock absorbing buckle is connected between the upper part of the fuselage connecting plate and the secondary shock absorbing mounting frame.
[0007] Furthermore, the two secondary shock absorbing arms are connected to the primary shock absorbing base frame, and the primary shock absorbing base frame, the secondary shock absorbing mounting frame and the two secondary shock absorbing arms form a lever structure, with the connection point between the two secondary shock absorbing arms and the primary shock absorbing base frame serving as a fulcrum.
[0008] Furthermore, the two secondary shock absorbing columns are located close to the fulcrum.
[0009] Furthermore, the secondary shock-absorbing buckle includes a first fastener, a second fastener and a shock-absorbing column, the first fastener is connected to the secondary shock-absorbing mounting frame, the opening of the first fastener faces the secondary shock-absorbing mounting frame, the second fastener is connected to the fuselage connecting plate, the opening of the second fastener faces the fuselage connecting plate, the opening of the first fastener is engaged with the opening of the second fastener, and the shock-absorbing column is connected between the first fastener and the second fastener.
[0010] Furthermore, the bottom of the pod mounting platform is connected to the pod via a pod connecting portion, and an unlocking mechanism is also provided on the pod mounting platform, and the unlocking mechanism is used to unlock the pod.
[0011] Furthermore, the unlocking mechanism includes a lever bracket, a lever is rotatably connected to the lever bracket, one end of the lever has a toggle portion, and the other end has a trigger end, an unlocking trigger switch is provided on the pod mounting platform, and the trigger end triggers the unlocking trigger switch to unlock when the toggle portion is toggled.
[0012] Furthermore, a limit feedback protrusion is provided on the lever bracket, and the lever is limited by the limit feedback protrusion when the unlocking trigger switch is triggered at the trigger end.
[0013] Furthermore, a plurality of the shock absorbing balls are arranged around the first-level shock absorbing mounting frame.
[0014] In addition, the present invention also provides a drone, which includes a main body and the pod shock absorbing structure, wherein the main body is connected to the body connecting plate.
[0015] The beneficial effects of the present invention are:
[0016] With respect to the deficiencies of the prior art, in the present invention, a plurality of shock-absorbing ball mounting frames are obliquely arranged between the primary shock-absorbing mounting frame and the primary shock-absorbing base frame, so that the plurality of shock-absorbing balls located on the plurality of shock-absorbing ball mounting frames can provide buffering when subjected to impacts in the vertical and horizontal directions, so that the pod shock-absorbing structure has the advantages of good shock-absorbing effect and improved pod stability. BRIEF DESCRIPTION OF THE DRAWINGS
[0017] In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings required for use in the embodiments or the description of the prior art will be briefly introduced below. Obviously, the drawings described below are only some embodiments of the present invention. For ordinary technicians in this field, other drawings can be obtained based on the structures shown in these drawings without paying creative work.
[0018] Figure 1 It is a three-dimensional structural schematic diagram of the present invention;
[0019] Figure 2 The three-dimensional structure of the pod installation platform of the present invention is shown in FIG. Figure 1 ;
[0020] Figure 3 The three-dimensional structure of the pod installation platform of the present invention is shown in FIG. Figure 2 ;
[0021] Figure 4 The three-dimensional structure of the pod installation platform of the present invention is shown in FIG. Figure 3 ;
[0022] Figure 5 The three-dimensional structure of the pod installation platform of the present invention is shown in FIG. Figure 4 ;
[0023] Figure 6 It is a three-dimensional structural schematic diagram of the secondary shock absorbing mechanism of the present invention;
[0024] Figure 7 It is a three-dimensional structural schematic diagram of the secondary shock-absorbing buckle ring of the present invention.
[0025] The reference numerals are as follows:
[0026] 1. Pod mounting platform; 2. Pod; 3. Primary shock-absorbing mechanism; 5. Primary shock-absorbing chassis; 6. Primary shock-absorbing mounting frame; 7. Shock-absorbing ball mounting frame; 8. Shock-absorbing ball; 9. Secondary shock-absorbing mechanism; 10. Secondary shock-absorbing mounting frame; 11. Fuselage connecting plate; 12. Secondary shock-absorbing arm; 13. Secondary shock-absorbing column; 14. Fulcrum; 15. Secondary shock-absorbing buckle; 16. First fastener; 17. Second fastener; 18. Shock-absorbing column; 19. Pod connecting part; 20. Unlocking mechanism; 21. Lever bracket; 22. Lever; 23. Toggle part; 25. Trigger end; 26. Unlocking trigger switch; 27. Limit feedback bump.
[0027] The realization of the purpose, functional features and advantages of the present invention will be further explained in conjunction with embodiments and with reference to the accompanying drawings. DETAILED DESCRIPTION
[0028] The following will be combined with the drawings in the embodiments of the present invention to clearly and completely describe the technical solutions in the embodiments of the present invention. Obviously, the described embodiments are only part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the present invention.
[0029] It should be noted that all directional indications in the embodiments of the present invention, such as up, down, left, right, front, back, clockwise, counterclockwise, etc., are only used to explain the relative position relationship, movement status, etc. between the components in a certain specific posture. If the specific posture changes, the directional indication will also change accordingly.
[0030] In addition, the descriptions of "first", "second", etc. in the present invention are only used for descriptive purposes and cannot be understood as indicating or implying their relative importance or implicitly indicating the number of the indicated technical features. Therefore, the features defined as "first" and "second" may explicitly or implicitly include at least one of the features. In addition, the technical solutions between the various embodiments can be combined with each other, but they must be based on the ability of ordinary technicians in the field to implement them. When the combination of technical solutions is contradictory or cannot be implemented, it should be considered that such a combination of technical solutions does not exist and is not within the scope of protection required by the present invention.
[0031] like Figures 1 to 5 As shown, in this embodiment, the pod shock-absorbing structure includes a pod mounting platform 1, a pod 2 is mounted on the pod mounting platform 1, the pod mounting platform 1 includes a primary shock-absorbing mechanism 3, the primary shock-absorbing mechanism 3 includes a primary shock-absorbing base frame 5 and a primary shock-absorbing mounting frame 6, the primary shock-absorbing mounting frame 6 is located above the primary shock-absorbing base frame 5, a plurality of shock-absorbing ball mounting frames 7 are obliquely arranged between the primary shock-absorbing mounting frame 6 and the primary shock-absorbing base frame 5, and shock-absorbing balls 8 are arranged on the plurality of shock-absorbing ball mounting frames 7.
[0032] With respect to the deficiencies of the prior art, in the present invention, a plurality of shock-absorbing ball mounting frames 7 are obliquely arranged between the primary shock-absorbing mounting frame 6 and the primary shock-absorbing base frame 5, so that the plurality of shock-absorbing balls 8 located on the plurality of shock-absorbing ball mounting frames 7 can provide buffering when subjected to impacts in the vertical and horizontal directions, so that the pod shock-absorbing structure has the advantages of good shock-absorbing effect and improved pod stability.
[0033] like Figures 2 to 3 As shown, in some embodiments, the pod mounting platform 1 further includes a secondary shock absorbing mechanism 9 arranged on the primary shock absorbing mechanism 3, the secondary shock absorbing mechanism 9 includes a secondary shock absorbing mounting frame 10, a fuselage connecting plate 11 and two secondary shock absorbing arms 12, the secondary shock absorbing mounting frame 10 is arranged opposite to the fuselage connecting plate 11, one end of the two secondary shock absorbing arms 12 are both connected to the secondary shock absorbing mounting frame 10, and the other end is connected to the lower part of the fuselage connecting plate 11 through a secondary shock absorbing column 13, and a secondary shock absorbing buckle 15 is connected between the upper part of the fuselage connecting plate 11 and the secondary shock absorbing mounting frame 10. Among them, the fuselage connecting plate 11 is used to be connected to the main body of the drone.
[0034] It should be noted that when the primary shock absorbing mechanism 3 is subjected to an excessive impact, the impact energy can be absorbed by the secondary shock absorbing mechanism 9 to achieve a stronger shock absorbing effect. Specifically, the secondary shock absorbing column 13 and the secondary shock absorbing buckle 15 are used to achieve the secondary shock absorbing effect.
[0035] like Figures 2 to 3 As shown, in some embodiments, the two secondary shock absorbing arms 12 are connected to the primary shock absorbing chassis 5, the primary shock absorbing chassis 5, the secondary shock absorbing mounting frame 10 and the two secondary shock absorbing arms 12 form a lever structure, and the connection point between the two secondary shock absorbing arms 12 and the primary shock absorbing chassis 5 is used as the fulcrum 14. Specifically, the lever structure formed by the primary shock absorbing chassis 5, the secondary shock absorbing mounting frame 10 and the two secondary shock absorbing arms 12 can convert the vertical vibration tendency of the pod 2 into the tendency of rotation along the fulcrum 14. Since the tendency of rotation is smoother during movement, the impact on the visual effect is smaller; moreover, through the setting of the above-mentioned lever structure, the energy absorption and shock absorbing effect of the secondary shock absorbing mounting frame 10 and the secondary shock absorbing buckle 15 on the primary shock absorbing mechanism 3 and the pod 2 will be multiplied by a force arm factor, thereby improving the shock absorbing effect, thereby improving the stability of the pod.
[0036] like Figures 2 to 3 As shown, in some embodiments, the two secondary shock absorbing columns 13 are located close to the fulcrum 14. Specifically, by placing the two secondary shock absorbing columns 13 close to the fulcrum 14, on the one hand, a shock absorbing effect can be achieved, and on the other hand, the direct impact of the fulcrum 14 on the fuselage connecting plate 11 can be avoided, thereby playing a buffering and protective role.
[0037] like Figure 6 to Figure 7 As shown, in some embodiments, the secondary shock-absorbing buckle 15 includes a first fastener 16, a second fastener 17 and a shock-absorbing column 18, wherein the first fastener 16 is connected to the secondary shock-absorbing mounting frame 10, and the opening of the first fastener 16 faces the secondary shock-absorbing mounting frame 10, the second fastener 17 is connected to the fuselage connecting plate 11, and the opening of the second fastener 17 faces the fuselage connecting plate 11, the opening of the first fastener 16 is engaged with the opening of the second fastener 17, and the shock-absorbing column 18 is connected between the first fastener 16 and the second fastener 17. The shock-absorbing column 18 is located in the opening of the first fastener 16 and the opening of the second fastener 17 at the same time. Specifically, when the pod 2 is connected to the primary shock absorbing mechanism 3, the secondary shock absorbing mounting frame 10 and the secondary shock absorbing buckle 15 connected thereto have a tendency to rotate toward the pod 2, thereby squeezing the shock absorbing column 18 located between the first fastener 16 and the second fastener 17, and then being fixed under the action of the secondary shock absorbing buckle 15 connected to the fuselage connecting plate 11.
[0038] It is worth mentioning that since the shock absorbing material / mechanism usually achieves shock absorption by squeezing energy absorption, although it can also be achieved by spring stretching, its energy absorption and shock absorption effect is weak, and the spring stretching is prone to fatigue and has a limited life. Therefore, by setting the secondary shock absorbing buckle 15, the separation trend of the secondary shock absorbing mounting frame 10 and the fuselage connecting plate 11 is converted into the approach trend of the first fastener 16 and the second fastener 17, and then the stretching of the secondary shock absorbing mounting frame 10 and the fuselage connecting plate 11 is converted into the squeezing of the shock absorbing column 18 between the first fastener 16 and the second fastener 17, thereby improving the stability of the connection, the shock absorbing effect and the life of the shock absorbing mechanism.
[0039] like Figures 4 to 5 As shown, in some embodiments, the bottom of the pod mounting platform 1 is connected to the pod 2 via a pod connecting portion 19, and an unlocking mechanism 20 is also provided on the pod mounting platform 1, and the unlocking mechanism 20 is used to unlock the pod 2. Specifically, the unlocking of the pod 2 is triggered by the unlocking mechanism 20, so that the pod 2 can be separated from the pod connecting portion 19.
[0040] like Figures 4 to 5 As shown, in some embodiments, the unlocking mechanism 20 includes a lever bracket 21, a lever 22 is rotatably connected to the lever bracket 21, one end of the lever 22 has a toggle portion 23, and the other end has a trigger end 25, and an unlocking trigger switch 26 is provided on the pod mounting platform 1, and the trigger end 25 triggers the unlocking trigger switch 26 to unlock when the toggle portion 23 is toggled. Specifically, since the unlocking mechanism 20 of the prior art is often provided near the pod 2 or the pod connection portion 19, it is inconvenient to operate; at the same time, in the present invention, by toggling the toggle portion 23 of the lever 22, the trigger end 25 of the lever 22 is rotated to trigger the unlocking trigger switch 26 to achieve unlocking. Therefore, the present invention can expand the operation range and increase the convenience of operation by toggling the lever 22 to achieve unlocking.
[0041] like Figures 4 to 5 As shown, in some embodiments, a limit feedback protrusion 27 is provided on the lever bracket 21, and the lever 22 is limited by the limit feedback protrusion 27 when the trigger end 25 triggers the unlock trigger switch 26. Specifically, the limit feedback protrusion 27 is used to limit the position of the lever 22 and give the operator feedback that the lever 22 is in place; when the operator moves the lever 22 to the limit feedback protrusion 27, the trigger end 25 of the lever 22 presses the unlock trigger switch 26, thereby releasing the lock of the pod 2, and the operator can remove the pod 2.
[0042] like Figures 1 to 4As shown, in some embodiments, a plurality of the shock absorbing balls 8 are arranged around the primary shock absorbing mounting frame 6. Specifically, the number of the shock absorbing balls 8 can be four, and the four shock absorbing balls 8 are arranged around the primary shock absorbing mounting frame 6.
[0043] In addition, the present invention also provides a drone, which includes a main body and the pod shock absorbing structure, wherein the main body is connected to the body connecting plate 11.
[0044] The specific structure of the drone is referred to the above embodiments. Since the drone adopts all the technical solutions of all the above embodiments, it at least has all the beneficial effects brought by the technical solutions of the above embodiments, which will not be described one by one here.
[0045] The above description is only a preferred embodiment of the present invention, and does not limit the patent scope of the present invention. All equivalent structural changes made by using the contents of the present invention specification and drawings under the inventive concept of the present invention, or directly / indirectly applied in other related technical fields are included in the patent protection scope of the present invention.
Claims
1. A pod shock absorbing structure, characterized in that: The invention comprises a pod mounting platform (1), a pod (2) being mounted on the pod mounting platform (1), the pod mounting platform (1) comprising a primary shock absorbing mechanism (3), the primary shock absorbing mechanism (3) comprising a primary shock absorbing base frame (5) and a primary shock absorbing mounting frame (6), the primary shock absorbing mounting frame (6) being located above the primary shock absorbing base frame (5), a plurality of shock absorbing ball mounting frames (7) being obliquely arranged between the primary shock absorbing mounting frame (6) and the primary shock absorbing base frame (5), and shock absorbing balls (8) being arranged on the plurality of shock absorbing ball mounting frames (7).
2. A pod shock absorbing structure according to claim 1, characterized in that: The pod mounting platform (1) further comprises a secondary shock absorbing mechanism (9) arranged on the primary shock absorbing mechanism (3), the secondary shock absorbing mechanism (9) comprising a secondary shock absorbing mounting frame (10), a fuselage connecting plate (11) and two secondary shock absorbing arms (12), the secondary shock absorbing mounting frame (10) being arranged opposite to the fuselage connecting plate (11), one end of the two secondary shock absorbing arms (12) being connected to the secondary shock absorbing mounting frame (10), and the other end of the two secondary shock absorbing arms (12) being connected to the lower part of the fuselage connecting plate (11) through a secondary shock absorbing column (13), and a secondary shock absorbing buckle (15) being connected between the upper part of the fuselage connecting plate (11) and the secondary shock absorbing mounting frame (10).
3. A pod shock absorbing structure according to claim 2, characterized in that: The two secondary shock absorbing arms (12) are both connected to the primary shock absorbing base frame (5); the primary shock absorbing base frame (5), the secondary shock absorbing mounting frame (10) and the two secondary shock absorbing arms (12) form a lever structure, and the connection point between the two secondary shock absorbing arms (12) and the primary shock absorbing base frame (5) serves as a fulcrum (14).
4. A pod shock absorbing structure according to claim 3, characterized in that: The two secondary shock absorbing columns (13) are located close to the supporting point (14).
5. The pod shock absorbing structure according to claim 2, characterized in that: The secondary shock-absorbing buckle ring (15) comprises a first fastener (16), a second fastener (17) and a shock-absorbing column (18); the first fastener (16) is connected to the secondary shock-absorbing mounting frame (10); the opening of the first fastener (16) faces the secondary shock-absorbing mounting frame (10); the second fastener (17) is connected to the fuselage connecting plate (11); the opening of the second fastener (17) faces the fuselage connecting plate (11); the opening of the first fastener (16) is engaged with the opening of the second fastener (17); and the shock-absorbing column (18) is connected between the first fastener (16) and the second fastener (17).
6. A pod shock absorbing structure according to any one of claims 1 to 5, characterized in that: The bottom of the pod mounting platform (1) is connected to the pod (2) via a pod connecting portion (19); an unlocking mechanism (20) is also provided on the pod mounting platform (1); the unlocking mechanism (20) is used to unlock the pod (2).
7. A pod shock absorbing structure according to claim 6, characterized in that: The unlocking mechanism (20) comprises a lever bracket (21), a lever (22) is rotatably connected to the lever bracket (21), one end of the lever (22) has a toggle portion (23), and the other end has a trigger end (25), an unlocking trigger switch (26) is arranged on the pod mounting platform (1), and the trigger end (25) triggers the unlocking trigger switch (26) to unlock when the toggle portion (23) is toggle.
8. The pod shock absorbing structure according to claim 7, characterized in that: A limit feedback protrusion (27) is provided on the lever bracket (21), and the lever (22) is limited by the limit feedback protrusion (27) when the trigger end (25) triggers the unlocking trigger switch (26).
9. The pod shock absorbing structure according to claim 1, characterized in that: A plurality of the shock absorbing balls (8) are arranged around the first-level shock absorbing mounting frame (6).
10. A drone, characterized in that: It comprises a main body and a pod shock absorbing structure as claimed in any one of claims 1 to 9, wherein the main body is connected to the body connecting plate (11).
Citation Information
Patent Citations
Suspension cabin damping mechanism
CN110466791A
Damping device and pod assembly
CN115163730A
Photoelectricity nacelle physics damping device
CN205113732U
Pod with vibration reduction effect and unmanned aerial vehicle
CN214776628U
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