Fixing device for hydrogen storage cylinder of hydrogen energy unmanned aerial vehicle
By designing a hydrogen energy UAV hydrogen storage cylinder fixing device including a flip mechanism and a rolling mechanism, the problem of inconvenience in the extraction process of the hydrogen storage cylinder is solved, the convenient level of hydrogen storage cylinder is realized, and the removal efficiency and stability are improved. sex.
Patent Information
- Application Number
- CN202421367052.8
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-06-17
- Publication Date
- 2025-02-14
- Estimated Expiration
- 2034-06-17
AI Technical Summary
The existing hydrogen energy UAV hydrogen storage cylinder fixing device is inconvenient when removing the hydrogen storage cylinder. Staff need to discharge the gas in the airbag, lower the fixing plate and lift the hydrogen cylinder in a vertical direction.
A fixing device including a base plate, a lifting mechanism, a connecting plate, a fixing plate, a flip mechanism, a support mechanism and a pushing mechanism are designed. The fixed plate is flipped 90 degrees to the horizontal position through the flip mechanism, and then the hydrogen storage cylinder at the horizontal position is pushed out to the outside of the shell through the push mechanism, so as to facilitate the removal of the hydrogen storage cylinder.
The process of taking out the hydrogen storage cylinder is simplified. Staff can directly remove the hydrogen storage cylinder horizontally from the port, which improves the removal efficiency, solves the problem of inconvenient removal of the hydrogen storage cylinder, and ensures the fixing through the support mechanism and clamping assembly. Stability of plate and hydrogen storage cylinder.
Smart Images

Figure CN222474454U_ABST
Abstract
Description
Technical Field
[0001] The utility model relates to the technical field of unmanned aerial vehicles, and in particular to a hydrogen energy unmanned aerial vehicle hydrogen storage cylinder fixing device. Background Art
[0002] Hydrogen energy has been widely used as a clean energy. Hydrogen energy needs to be packaged in hydrogen storage cylinders. The interior of a hydrogen energy drone needs to be fixed with hydrogen storage cylinders at designated locations.
[0003] After searching, the existing patent (Announcement No.: CN217674104U) discloses a hydrogen energy hydrogen cylinder transportation fixing device, which relates to the technical field of hydrogen cylinder transportation devices. The hydrogen energy hydrogen cylinder transportation fixing device includes a base plate, a vertical plate, a threaded rod, an upper bevel gear, a transmission rod, a lower bevel gear, a knob, a sliding hole, a lifting rod, a fixing plate, a fixing hole, an airbag, a cushion block, a hydrogen cylinder, a buffer column, a support leg, a buffer spring, a limit groove, and a limit block. The upper surface of the base plate is fixedly installed with a vertical plate. In the hydrogen energy hydrogen cylinder transportation fixing device, the shaking generated by transportation will be absorbed by the airbag, thereby avoiding collisions on the outer surface of the hydrogen cylinder. At the same time, the vibration generated by transportation will also be transmitted to the buffer spring through the support leg and cause the buffer spring to deform. The buffer spring's own elasticity can absorb the vibration generated by transportation, thereby maintaining the stability of the base plate and the hydrogen cylinder and avoiding violent shaking of the hydrogen cylinder.
[0004] However, in the implementation of the relevant technology, it was found that the above-mentioned problems exist: in the above-mentioned method, after the hydrogen cylinder is placed in the fixing hole on the fixing plate, gas is pumped into the airbag through an inflation tool to expand the airbag and tightly wrap the outer surface of the hydrogen cylinder, thereby completing the fixation of the hydrogen cylinder. When the hydrogen cylinder needs to be removed, the staff first discharges the gas in the airbag and lowers the fixing plate to the upper surface of the bottom plate. The staff needs to lift the hydrogen cylinder upwards to move it out of the fixing hole. After that, the staff needs to lift the hydrogen cylinder in a vertical direction to remove it, which makes the removal process of the hydrogen cylinder very inconvenient. Utility Model Content
[0005] The utility model provides a device for fixing a hydrogen storage cylinder of a hydrogen energy UAV, which solves the problem in the related art that the hydrogen storage cylinder is inconvenient to take out.
[0006] The technical solution of the utility model is as follows: A hydrogen energy drone hydrogen storage cylinder fixing device comprises a base plate, a lifting mechanism is arranged on one side of the upper surface of the base plate, a connecting plate is arranged on one side of the lifting mechanism, the lifting mechanism is used to lift and lower the connecting plate, a fixing plate for fixing the hydrogen storage cylinder is arranged at one end of the connecting plate, a flipping mechanism for flipping the fixing plate is arranged on the connecting plate, an outer shell is fixedly connected to the periphery of the upper surface of the base plate, a supporting mechanism for supporting the flipping process of the fixing plate is arranged between one end of the fixing plate away from the connecting plate and the inner side wall of the outer shell, a through opening is opened through one side of the outer shell, and a pushing mechanism for pushing the hydrogen storage cylinder through the through opening is arranged on the other side of the outer shell.
[0007] Preferably, the flipping mechanism includes a first gear and a motor, the first gear is rotatably connected to one end of the connecting plate, and the first gear is fixedly connected to one end of the fixed plate, the motor is fixedly connected to the upper surface of the connecting plate, and the output end of the motor is fixedly connected to the second gear.
[0008] Preferably, the second gear is meshed with the first gear, and an outer ring diameter of the second gear is smaller than an outer ring diameter of the first gear.
[0009] Preferably, the supporting mechanism comprises a connecting shaft and a bearing, the connecting shaft is fixedly connected to one end of the fixing plate, the bearing is fixedly embedded in the inner wall of the outer shell, and the connecting shaft is rotatably connected to the inner wall of the outer shell through the bearing.
[0010] Preferably, the ejection mechanism includes a first electric cylinder, which is fixedly connected to the outer wall of the shell, and the output end of the first electric cylinder extends into the shell and is fixedly connected to a box body, and two clamping assemblies are symmetrically distributed on the inner wall of the box body.
[0011] Preferably, the clamping assembly comprises a second electric cylinder, the second electric cylinder is fixedly connected to the outer side wall of the box body, and the output end of the second electric cylinder extends into the box body and is fixedly connected to a clamping plate.
[0012] Preferably, the clamping plate is an arc-shaped structure, the box body is a circular structure, and the arc curvature of the clamping plate is consistent with the circular curvature of the box body.
[0013] Preferably, a rubber pad is bonded to the inner ring side wall of the clamping plate, and the rubber pad is an arc-shaped structure.
[0014] The working principle and beneficial effects of the utility model are:
[0015] 1. In the utility model, the hydrogen storage cylinder fixed on the fixed plate is flipped to a horizontal position by a flipping mechanism, and then the hydrogen storage cylinder in the horizontal position is pushed out to a part of the outer side of the shell through the opening by a pushing mechanism, so that the staff can directly take out the hydrogen storage cylinder horizontally from the opening, which facilitates the process of taking out the hydrogen storage cylinder and solves the problem of inconvenient removal of the hydrogen storage cylinder in the related art.
[0016] 2. In the utility model, through the support mechanism, during the rotation of the fixed plate, the fixed plate will drive the connecting shaft and rotate along with it through the bearing, thereby supporting the rotation and flipping process of the fixed plate, which not only ensures the stability of the fixed plate during the flipping process, but also prevents the fixed plate from being subjected to excessive pressure and easily causing breakage and damage.
[0017] 3. In the utility model, through the clamping assembly, when the hydrogen storage cylinder is pushed out, the two clamping plates always clamp the hydrogen storage cylinder, thereby improving the stability of the hydrogen storage cylinder during the pushing out process and preventing it from falling. BRIEF DESCRIPTION OF THE DRAWINGS
[0018] The utility model is further described in detail below in conjunction with the accompanying drawings and specific implementation methods.
[0019] Figure 1 This is a structural schematic diagram of a hydrogen storage cylinder fixing device for a hydrogen energy UAV proposed in the utility model;
[0020] Figure 2 This is a schematic diagram of the internal structure of a hydrogen storage cylinder fixing device for a hydrogen energy UAV proposed in the utility model;
[0021] Figure 3 This is a structural schematic diagram of a fixing plate, a flipping mechanism, a supporting mechanism and a pushing mechanism of a hydrogen storage cylinder fixing device for a hydrogen energy UAV proposed in the utility model;
[0022] Figure 4 This is a structural schematic diagram of a flipping mechanism and a supporting mechanism of a hydrogen storage cylinder fixing device for a hydrogen energy UAV proposed in the utility model;
[0023] Figure 5 This is a structural schematic diagram of a pushing mechanism of a hydrogen storage cylinder fixing device for a hydrogen energy UAV proposed by the utility model.
[0024] In the figure: 1. bottom plate; 2. lifting mechanism; 3. connecting plate; 4. fixing plate; 5. flipping mechanism; 51. first gear; 52. motor; 53. second gear; 6. supporting mechanism; 61. connecting shaft; 62. bearing; 7. fixing hole; 8. airbag; 9. ejection mechanism; 91. first electric cylinder; 92. box body; 93. second electric cylinder; 94. clamping plate; 10. outer shell; 11. through opening. DETAILED DESCRIPTION
[0025] In order to make the technical means, creative features, objectives and effects achieved by the present invention easy to understand, the present invention is further described below in conjunction with specific implementation methods.
[0026] See also Figure 1 , Figure 2 and Figure 3 The utility model provides a technical solution: a hydrogen energy drone hydrogen storage cylinder fixing device, comprising a bottom plate 1, a lifting mechanism 2 is arranged on one side of the upper surface of the bottom plate 1, a connecting plate 3 is arranged on one side of the lifting mechanism 2, the lifting mechanism 2 is used to lift and lower the connecting plate 3, a fixing plate 4 for fixing the hydrogen storage cylinder is arranged at one end of the connecting plate 3, a flipping mechanism 5 for flipping the fixing plate 4 is arranged on the connecting plate 3, a shell 10 is fixedly connected to the periphery of the upper surface of the bottom plate 1, a supporting mechanism 6 for supporting the flipping process of the fixing plate 4 is arranged between one end of the fixing plate 4 away from the connecting plate 3 and the inner side wall of the shell 10, a through opening 11 is opened through one side of the shell 10, and a pushing mechanism 9 for pushing the hydrogen storage cylinder through the through opening 11 is arranged on the other side of the shell 10.
[0027] When in use, the entire device can be fixed by fixing the bottom plate 1 to the designated installation position inside the drone. When the hydrogen storage cylinder needs to be fixed, the connecting plate 3 is first driven down to the upper surface of the bottom plate 1 by the lifting mechanism 2, and the connecting plate 3 drives the fixing plate 4 to descend to the upper surface of the bottom plate 1, and then the hydrogen storage cylinder is placed in the fixing hole 7 that penetrates and is opened on the fixing plate 4. After the hydrogen storage cylinder is placed stably, the connecting plate 3 is driven up by the lifting mechanism 2, so that the connecting plate 3 drives the fixing plate 4 to rise to the middle position of the hydrogen storage cylinder, and the staff pushes the fixing hole 7 on the inner wall of the fixing hole 7. When the airbag 8 is inflated, the airbag 8 will fix the hydrogen storage cylinder, and the fixing process of the hydrogen storage cylinder can be completed; when the hydrogen storage cylinder needs to be taken out, the fixing plate 4 in the horizontal position is turned 90 degrees to the vertical position through the flip mechanism 5, and the fixing plate 4 will drive the hydrogen storage cylinder in the vertical position to turn 90 degrees to the horizontal position, and then the staff will deflate the airbag 8, and push the hydrogen storage cylinder in the horizontal position to the through-port 11 through the pushing mechanism 9, and the pushing mechanism 9 will eventually push the hydrogen storage cylinder through the through-port 11 to the outer part of the shell 10, at this time, the staff can directly and conveniently take out the hydrogen storage cylinder horizontally. Therefore, the hydrogen storage cylinder fixed on the fixing plate 4 is turned 90 degrees to the horizontal position through the flip mechanism 5, and then the hydrogen storage cylinder in the horizontal position is pushed through the through-port 11 to the outer part of the shell 10 through the pushing mechanism 9, so that it is convenient for the staff to directly take out the hydrogen storage cylinder horizontally from the through-port 11, which facilitates the process of taking out the hydrogen storage cylinder and solves the problem of the inconvenience of taking out the hydrogen storage cylinder in the related art.
[0028] See also Figure 3 and Figure 4 The flipping mechanism 5 includes a first gear 51 and a motor 52. The first gear 51 is rotatably connected to one end of the connecting plate 3, and the first gear 51 is fixedly connected to one end of the fixed plate 4. The motor 52 is fixedly connected to the upper surface of the connecting plate 3. The output end of the motor 52 is fixedly connected to a second gear 53. The second gear 53 is meshed with the first gear 51, and the outer ring diameter of the second gear 53 is smaller than the outer ring diameter of the first gear 51. By starting the motor 52, the motor 52 drives the second gear 53 to rotate, the second gear 53 drives the first gear 51 to rotate, and the first gear 51 drives the fixed plate 4 in the horizontal position to rotate so that it flips 90 degrees to a vertical position.
[0029] See also Figure 2 , Figure 3 and Figure 4 The supporting mechanism 6 includes a connecting shaft 61 and a bearing 62. The connecting shaft 61 is fixedly connected to one end of the fixing plate 4, and the bearing 62 is fixedly embedded in the inner wall of the shell 10. The connecting shaft 61 is rotatably connected to the inner wall of the shell 10 through the bearing 62. During the rotation of the fixing plate 4, the fixing plate 4 will drive the connecting shaft 61 and rotate through the bearing 62, thereby supporting the rotation and flipping process of the fixing plate 4, which not only ensures the stability of the fixing plate 4 during the flipping process, but also prevents the fixing plate 4 from being subjected to excessive pressure and easily causing breakage and damage.
[0030] See also Figure 2 , Figure 3 and Figure 5The ejection mechanism 9 includes a first electric cylinder 91, which is fixedly connected to the outer wall of the housing 10, and the output end of the first electric cylinder 91 extends into the housing 10 and is fixedly connected to a box body 92. Two clamping assemblies are symmetrically distributed on the inner wall of the box body 92, and the clamping assembly includes a second electric cylinder 93, which is fixedly connected to the outer wall of the box body 92, and the output end of the second electric cylinder 93 extends into the box body 92 and is fixedly connected to a clamping plate 94. The clamping plate 94 is an arc-shaped structure, and the box body 92 is a circular structure, and the arc of the clamping plate 94 is consistent with the circular arc of the box body 92. A rubber pad is bonded to the inner ring side wall of the clamping plate 94, and the rubber pad is an arc-shaped structure. When the fixed plate 4 drives When the hydrogen storage cylinder in the vertical position is turned 90 degrees to the horizontal position, the first electric cylinder 91 is started to push the box body 92 forward, so that the bottom of the hydrogen storage cylinder moves into the box body 92, and then the two second electric cylinders 93 are started respectively, and the two second electric cylinders 93 push the two clamps 94 respectively until the two clamps 94 clamp the hydrogen storage cylinder, and then the staff deflates the airbag 8, and then the first electric cylinder 91 continues to push the box body 92 forward, and the box body 92 will push the clamped hydrogen storage cylinder through the opening 11 to a part of the outer side of the shell 10. At this time, the two second electric cylinders 93 are respectively adjusted to make the two clamps 94 release the hydrogen storage cylinder, and the staff can directly and conveniently take out the hydrogen storage cylinder horizontally. In the process of the hydrogen storage cylinder being pushed out, the two clamps 94 always clamp the hydrogen storage cylinder, so as to improve the stability of the hydrogen storage cylinder in the process of being pushed out and prevent it from falling.
[0031] The working principle and use process of the utility model are as follows: when in use, the entire device can be fixed by fixing the bottom plate 1 to the designated installation position inside the drone. When the hydrogen storage cylinder needs to be fixed, the connecting plate 3 is first driven down to the upper surface of the bottom plate 1 by the lifting mechanism 2, and the connecting plate 3 drives the fixing plate 4 to descend to the upper surface of the bottom plate 1, and then the hydrogen storage cylinder is placed in the fixing hole 7 that is penetrated and opened on the fixing plate 4. After the hydrogen storage cylinder is placed stably, the connecting plate 3 is driven up by the lifting mechanism 2, so that the connecting plate 3 drives the fixing plate 4 to rise to the middle position of the hydrogen storage cylinder, and the staff inflates the airbag 8 on the inner wall of the fixing hole 7, and the airbag 8 will fix the hydrogen storage cylinder, and the fixing process of the hydrogen storage cylinder can be completed; when the hydrogen storage cylinder needs to be taken out, the motor 52 is started, and the motor 52 drives the second gear 53 to rotate, and the second gear 53 drives the first gear 51 to rotate, and the first gear 51 drives the fixed plate 4 in the horizontal position to rotate and flip it 90 degrees to the vertical position. The fixed plate 4 will drive the hydrogen storage bottle in the vertical position to flip 90 degrees to the horizontal position, and then, by starting the first electric cylinder 91, the box body 92 is pushed forward so that the bottom of the hydrogen storage bottle moves into the box body 92, and then by starting the two second electric cylinders 93 respectively, the two second electric cylinders 93 push the two clamping plates 94 respectively until the two clamping plates 94 clamp the hydrogen storage bottle, and then, the staff deflates the airbag 8, and then continues to push the box body 92 forward through the first electric cylinder 91, and the box body 92 will push the clamped hydrogen storage bottle through the opening 11 to a part of the outer side of the shell 10. At this time, the two second electric cylinders 93 are respectively adjusted to make the two clamping plates 94 loosen the hydrogen storage bottle, and the staff can directly and conveniently take out the hydrogen storage bottle horizontally. During the process of the hydrogen storage cylinder being pushed out, the two clamping plates 94 always clamp the hydrogen storage cylinder tightly, thereby improving the stability of the hydrogen storage cylinder during the process of being pushed out and preventing it from falling.
[0032] The above are only preferred embodiments of the present invention and are not intended to limit the present invention. Any modifications, equivalent substitutions, improvements, etc. made within the spirit and principles of the present invention should be included in the protection scope of the present invention.
Claims
1. A hydrogen energy drone hydrogen storage cylinder fixing device, comprising a base plate (1), a lifting mechanism (2) is provided on one side of the upper surface of the base plate (1), characterized in that: A connecting plate (3) is provided on one side of the lifting mechanism (2), and the lifting mechanism (2) is used to lift and lower the connecting plate (3). A fixing plate (4) for fixing a hydrogen storage cylinder is provided at one end of the connecting plate (3), and a flipping mechanism (5) for flipping and adjusting the fixing plate (4) is provided on the connecting plate (3). An outer shell (10) is fixedly connected to the periphery of the upper surface of the bottom plate (1), and a supporting mechanism (6) for supporting the flipping process of the fixing plate (4) is provided between an end of the fixing plate (4) away from the connecting plate (3) and an inner side wall of the outer shell (10). A through opening (11) is provided on one side of the outer shell (10), and a pushing mechanism (9) for pushing the hydrogen storage cylinder out through the through opening (11) is provided on the other side of the outer shell (10).
2. The hydrogen energy drone hydrogen storage cylinder fixing device according to claim 1 is characterized by: The flipping mechanism (5) comprises a first gear (51) and a motor (52); the first gear (51) is rotatably connected to one end of the connecting plate (3), and the first gear (51) is fixedly connected to one end of the fixing plate (4); the motor (52) is fixedly connected to the upper surface of the connecting plate (3), and the output end of the motor (52) is fixedly connected to a second gear (53).
3. The hydrogen storage cylinder fixing device for a hydrogen energy UAV according to claim 2 is characterized in that: The second gear (53) is meshed with the first gear (51), and the outer diameter of the second gear (53) is smaller than the outer diameter of the first gear (51).
4. The hydrogen energy drone hydrogen storage cylinder fixing device according to claim 1 is characterized by: The supporting mechanism (6) comprises a connecting shaft (61) and a bearing (62); the connecting shaft (61) is fixedly connected to one end of the fixing plate (4); the bearing (62) is fixedly embedded in the inner wall of the outer shell (10); and the connecting shaft (61) is rotatably connected to the inner wall of the outer shell (10) via the bearing (62).
5. The hydrogen storage cylinder fixing device for a hydrogen energy UAV according to claim 1 is characterized in that: The ejection mechanism (9) comprises a first electric cylinder (91), the first electric cylinder (91) being fixedly connected to the outer wall of the housing (10), the output end of the first electric cylinder (91) extending into the housing (10) and being fixedly connected to a box body (92), and two clamping assemblies being symmetrically arranged on the inner wall of the box body (92).
6. The hydrogen storage cylinder fixing device for a hydrogen energy UAV according to claim 5 is characterized in that: The clamping assembly comprises a second electric cylinder (93), the second electric cylinder (93) is fixedly connected to the outer wall of the box body (92), and the output end of the second electric cylinder (93) extends into the box body (92) and is fixedly connected to a clamping plate (94).
7. The hydrogen storage cylinder fixing device for a hydrogen energy UAV according to claim 6 is characterized in that: The clamping plate (94) is an arc-shaped structure, the box body (92) is a circular structure, and the arc radius of the clamping plate (94) is consistent with the arc radius of the box body (92).
8. The hydrogen storage cylinder fixing device for a hydrogen energy UAV according to claim 7 is characterized in that: A rubber pad is bonded to the inner ring side wall of the clamping plate (94), and the rubber pad is an arc-shaped structure.
Citation Information
Patent Citations
Device for transporting and fixing hydrogen cylinders of hydrogen energy
CN217674104U
Cited By
Fixing device for hydrogen storage cylinder of hydrogen energy unmanned aerial vehicle
CN120423086A