CN117647346B - Output pressure testing device of elastic brake actuator of small unmanned aerial vehicle - Google Patents

Output pressure testing device of elastic brake actuator of small unmanned aerial vehicle Download PDF

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Publication number
CN117647346B
CN117647346B CN202410118959.9A CN202410118959A CN117647346B CN 117647346 B CN117647346 B CN 117647346B CN 202410118959 A CN202410118959 A CN 202410118959A CN 117647346 B CN117647346 B CN 117647346B
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sliding
wall
brake actuator
test
transmission case
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CN117647346A (en
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朱军科
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Shaanxi Hangyu Engineering Technology Co ltd
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Shaanxi Hangyu Engineering Technology Co ltd
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Abstract

The invention relates to an output pressure testing device of an elastic brake actuator of a small unmanned aerial vehicle, which comprises the following components: the transmission case and test box, the transmission case is located the top of test box, transmission case bottom and cavity one end intercommunication, the cavity other end and test box top intercommunication, the test box top is provided with the notch body, be provided with a plurality of range upon range of test boards in the notch body, the test board top is provided with the clamp plate, the clamp plate top is connected with depression bar one end, be provided with pressure sensor in the depression bar, the depression bar other end and the pressure output end threaded connection of elasticity brake actuator body, the transmission case below is provided with the mounting panel, be provided with the mounting groove on the mounting panel, elasticity brake actuator body is located the mounting groove, test box top right side is provided with the cleaning brush. The invention can measure the corresponding output pressure values of the spring of the elastic brake actuator under different expansion lengths, and the cleaning brush can clean the working surface of the pressing plate before each measurement, so that foreign matters are prevented from remaining on the working surface of the pressing plate to influence the measurement accuracy.

Description

Output pressure testing device of elastic brake actuator of small unmanned aerial vehicle
Technical Field
The invention belongs to the technical field of unmanned aerial vehicle brake testing, and particularly relates to an output pressure testing device of an elastic brake actuator of a small unmanned aerial vehicle.
Background
The drone is an unmanned aircraft that is maneuvered using a radio remote control device and a self-contained programming device, or is operated autonomously, either entirely or intermittently, by an on-board computer. With the rapid development of unmanned aerial vehicle technology, unmanned aerial vehicles have been widely used in civil and military fields. In the flight process of a small unmanned aerial vehicle, an elastic brake actuator is a device for realizing rapid stopping or reducing the flight speed. In unmanned aerial vehicle field, elasticity brake actuator is used for controlling unmanned aerial vehicle's speed reduction or stop action. The elastic brake actuator generates corresponding braking force by outputting certain pressure, thereby realizing deceleration or stopping. It is typically comprised of a spring and a controllable valve. When braking is needed, the control system sends a signal to the elastic braking actuator, and the valve is opened to release pressure, so that the spring expands and applies braking force. The magnitude and duration of the braking force can be controlled by adjusting the opening degree of the valve and the magnitude of the release pressure, so that the unmanned aerial vehicle can be accurately controlled. The existing elastic brake actuator controls the magnitude of braking force through the expansion length of a spring, and the corresponding output pressure values of different spring expansion lengths cannot be accurately calibrated, so that the output pressure testing device of the elastic brake actuator of the small unmanned aerial vehicle needs to be designed.
Disclosure of Invention
Therefore, the invention aims to solve the problem that the output pressure values corresponding to different spring expansion lengths cannot be accurately calibrated in the prior art.
Therefore, the technical scheme is that the output pressure testing device of the elastic brake actuator of the small unmanned aerial vehicle comprises the following components: the device comprises a transmission box and a test box, wherein the transmission box is positioned above the test box, the bottom end of the transmission box is communicated with one end of a cavity, the other end of the cavity is communicated with the top end of the test box, a groove body is arranged at the top end of the test box, a plurality of laminated test boards are arranged in the groove body, a pressing plate is arranged above the test boards, the top end of the pressing plate is connected with one end of the pressing rod, a pressure sensor is arranged in the pressing rod, the other end of the pressing rod is in threaded connection with the pressure output end of an elastic brake actuator body, a mounting plate is arranged below the transmission box, a mounting groove is formed in the mounting plate, fastening screws are respectively arranged on two sides of the mounting groove, the elastic brake actuator body is positioned in the mounting groove, a cleaning brush is arranged on the right side of the top end of the test box, and a driving device is arranged in the transmission box and can drive the pressing plate to circularly move along an L-shaped movement track and intermittently contact with the test boards and the cleaning brush.
Preferably, a processor is arranged in the transmission case, a display screen is arranged on the outer wall of the cavity, the pressure sensor is in wireless communication with the processor, and the processor is electrically connected with the display screen.
Preferably, the driving device includes: the driving motor is arranged in the transmission case, the driving motor is connected with the inner wall of the transmission case, the output end of the driving motor is coaxially connected with one end of the rotation shaft, the other end of the rotation shaft is connected with one end of the crank, the other end of the crank is rotationally connected with one end of the connecting rod, the other end of the connecting rod is hinged with the left end of the sliding plate, the right side of the driving motor is provided with a guiding groove body in the horizontal direction, the guiding groove body is connected with the inner wall of the transmission case, the sliding plate can slide in a left-right reciprocating manner along the guiding groove body, an inclined sliding groove is arranged on the sliding plate, an L-shaped sliding groove is arranged on the bottom wall of the guiding groove body, a sliding block is connected in a sliding manner in the L-shaped sliding groove, one end of the sliding column is connected with the sliding block, the other end of the sliding column penetrates through the inclined sliding groove and is connected with the upper end of the driving shaft in the vertical direction, the lower end of the driving shaft penetrates through the opening groove in the horizontal direction and is connected with the upper end of the mounting plate.
Preferably, a plurality of nozzles are arranged on the cleaning brush, a liquid storage tank is arranged at the top end of the test tank, one end of the liquid delivery pipe is communicated with the liquid storage tank, the other end of the liquid delivery pipe is respectively communicated with the plurality of nozzles, an infusion pump is arranged in the liquid storage tank, and the infusion pump is used for providing power for liquid flow of the liquid delivery pipe.
Preferably, a liquid inlet pipe is arranged on the side wall of the liquid storage tank, one end of the liquid inlet pipe is communicated with the liquid storage tank, and the other end of the liquid inlet pipe is connected with a cover in a threaded manner.
Preferably, be provided with vertical opening on the recess body left wall, be provided with horizontal opening on the recess body diapire, vertical opening lower extreme and horizontal opening left end intercommunication, the recess body below is provided with the slide rail of horizontal direction, sliding connection has the movable block on the slide rail, the slide rail both ends are provided with the fixed block respectively, fixed block one side and sliding connection, the fixed block opposite side is connected with the test box inner wall, the movable block top is provided with the push rod, the push rod can pass vertical opening and horizontal opening, be provided with the export on the recess body right side wall, the test board can pass the export.
Preferably, a sliding rod is arranged on the moving block, a sliding groove extending along the length direction is arranged at one end of the swinging rod, the sliding rod penetrates through the sliding groove and can slide in the sliding groove, the other end of the swinging rod is hinged with the inner wall of the test box, the swinging rod can swing left and right, a roller is rotationally connected to the swinging rod, a first fixing column is arranged on the swinging rod, the first fixing column is positioned between the sliding groove and the roller, a second fixing column is arranged on the right side of the swinging rod, the second fixing column is connected with the inner wall of the test box, the first fixing column is connected with the second fixing column through a first spring, two ends of a wheel shaft are respectively rotationally connected with the inner wall of the test box, a first belt pulley and a second belt pulley are coaxially arranged on the wheel shaft, an incomplete turntable is arranged between the first belt pulley and the second belt pulley, the wheel shaft penetrates through the circle center of the incomplete turntable and is connected with the incomplete turntable, the circumferential outer wall of the incomplete turntable is composed of a first arc surface, a second arc surface and two inclined surfaces, two ends of the first arc surface are respectively connected with the circumferential outer wall of the roller through two inclined surfaces, a third belt pulley is coaxially arranged on the rotating shaft, and the first belt pulley penetrates through the first belt and the first belt cavity.
Preferably, the right side of the groove body is provided with two U-shaped groove bodies, the opening of the U-shaped groove bodies is upward and is connected with the top of the inner wall of the test box, a sliding block is slidably connected in the U-shaped groove bodies, the top end of the sliding block is connected with one end of a second spring, the other end of the second spring is connected with the top wall of the test box, two ends of a first roller shaft are respectively rotationally connected with the two sliding blocks, a first roller is coaxially arranged on the first roller shaft, two ends of a second roller shaft are respectively rotationally connected with the inner wall of the test box, a second roller and a fourth belt pulley are coaxially arranged on the second roller shaft, the second roller shaft is positioned below the first roller shaft, and the second belt pulley and the fourth belt pulley are connected through a second belt.
Preferably, a material guide opening is formed in the side wall of the test box, close to the first roller, and a material guide plate is arranged below the material guide opening, and one end of the material guide plate is connected with the side wall of the test box.
Preferably, the side wall of the test box is provided with a box door.
The technical scheme of the invention has the following advantages:
1. according to the device for testing the output pressure of the elastic brake actuator of the small unmanned aerial vehicle, the pressing plate vertically moves downwards to press the testing plate, namely the working stroke of the elastic actuator, the pressing plate horizontally moves back and forth to contact with the cleaning brush, so that the working surface of the pressing plate is cleaned, and the working surface of the pressing plate is kept clean. The clamp plate is compressed with the contact of test board top, and the maximum pressure value that pressure sensor tested is the maximum pressure output value of elasticity brake actuator, later, at every turn measure, take out a test board from recess body top, just can measure the output pressure value that the spring of elasticity brake actuator corresponds under different expansion length, all can clean the clamp plate working face before measuring at every turn the cleaning brush, prevents that the foreign matter from remaining on the clamp plate working face and influencing the precision of measurement.
2. According to the device for testing the output pressure of the elastic brake actuator of the small unmanned aerial vehicle, the pressing plate presses downwards, so that the device continuously circulates, the pressing plate presses downwards each time, the thickness of the test plate group is automatically reduced relative to the last thickness, the corresponding output pressure value of the spring of the elastic brake actuator under different expansion lengths is correspondingly measured, the measurement is more intelligent, the measurement accuracy is high, and the measurement efficiency is also improved.
Additional features and advantages of the invention will be set forth in the description which follows, and in part will be obvious from the description, or may be learned by practice of the invention. The objectives and other advantages of the invention may be realized and attained by the structure particularly pointed out in the written description and drawings.
The technical scheme of the invention is further described in detail through the drawings and the embodiments.
Drawings
The accompanying drawings are included to provide a further understanding of the invention and are incorporated in and constitute a part of this specification, illustrate the invention and together with the embodiments of the invention, serve to explain the invention. In the drawings:
FIG. 1 is a schematic diagram of the structure of the present invention;
FIG. 2 is a schematic view of the internal structure of the present invention;
FIG. 3 is a schematic view of the structure of the guide slot body, L-shaped chute, slider and strut in the present invention;
FIG. 4 is a schematic illustration of the connection of the nozzle and the reservoir according to the present invention;
FIG. 5 is a schematic view showing the internal structure of the test chamber according to the present invention;
FIG. 6 is a bottom view of the groove body of the present invention;
FIG. 7 is a left side view of the groove body of the present invention;
FIG. 8 is a right side view of the groove body of the present invention;
FIG. 9 is a schematic view of the structure of the incomplete turntable of the present invention;
FIG. 10 is a schematic view of the construction of the first roller and the second roller of the present invention;
reference numerals illustrate:
1. a transmission case; 2. a test box; 3. a cavity; 4. a groove body; 5. a test board; 6. a pressing plate; 7. a compression bar; 8. a pressure sensor; 9. an elastic brake actuator body; 10. a pressure output; 11. a mounting plate; 12. a mounting groove; 13. a fastening screw; 14. a cleaning brush; 15. a processor; 16. a display screen; 17. a drive motor; 18. a rotating shaft; 19. a crank; 20. a connecting rod; 21. a slide plate; 22. a guide groove body; 23. an inclined chute; 24. an L-shaped chute; 25. a slide block; 26. a spool; 27. a drive shaft; 28. an open slot; 29. a nozzle; 30. a liquid storage tank; 31. an infusion tube; 32. a liquid inlet pipe; 33. a cover; 34. a vertical opening; 35. a horizontal opening; 36. a slide rail; 37. a moving block; 38. a fixed block; 39. a push rod; 40. an outlet; 41. a slide bar; 42. swing rod; 43. a slip groove; 44. a roller; 45. a first fixing column; 46. a second fixing column; 47. a first spring; 48. a wheel axle; 49. a first pulley; 50. a second pulley; 51. an incomplete turntable; 52. a third pulley; 53. a first belt; 54. a U-shaped groove body; 55. a sliding block; 56. a second spring; 57. a first roller shaft; 58. a first roller; 59. a second roller shaft; 60. a second roller; 61. a fourth pulley; 62. a second belt; 63. a material guiding port; 64. a material guide plate; 511. A first arc surface; 512. a second arc surface; 513. and (5) an inclined plane.
Detailed Description
In order to make the technical problems, technical schemes and beneficial effects to be solved more clear, the invention is further described in detail below with reference to the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are for purposes of illustration only and are not intended to limit the scope of the invention.
It will be understood that when an element is referred to as being "mounted" or "disposed" on another element, it can be directly on the other element or be indirectly on the other element. When an element is referred to as being "connected to" another element, it can be directly or indirectly connected to the other element.
It is to be understood that the terms "length," "width," "upper," "lower," "front," "rear," "left," "right," "vertical," "horizontal," "top," "bottom," "inner," "outer," and the like are merely for convenience in describing and simplifying the description based on the orientation or positional relationship shown in the drawings, and do not indicate or imply that the devices or elements referred to must have a particular orientation, be constructed and operated in a particular orientation, and thus are not to be construed as limiting the invention.
Furthermore, the terms "first," "second," and the like, are used for descriptive purposes only and are not to be construed as indicating or implying a relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defining "a first" or "a second" may explicitly or implicitly include one or more such feature. In the description of the present invention, the meaning of "a plurality" is two or more, unless explicitly defined otherwise.
Example 1
The invention provides an output pressure testing device of an elastic brake actuator of a small unmanned aerial vehicle, which is shown in figures 1-4 and comprises: the transmission case 1 and the test case 2, transmission case 1 is located the top of test case 2, transmission case 1 bottom and cavity 3 one end intercommunication, the cavity 3 other end and test case 2 top intercommunication, test case 2 top is provided with recess body 4, be provided with a plurality of stacked test boards 5 in the recess body 4, test board 5 top is provided with clamp plate 6, clamp plate 6 top is connected with depression bar 7 one end, be provided with pressure sensor 8 in the depression bar 7, the pressure bar 7 other end and the pressure output end 10 threaded connection of elasticity brake actuator body 9, transmission case 1 below is provided with mounting panel 11, be provided with mounting groove 12 on the mounting panel 11, be provided with fastening screw 13 respectively on the mounting groove 12 both sides, elasticity brake actuator body 9 is located mounting groove 12, test case 2 top right side is provided with cleaning brush 14, be provided with drive arrangement in the transmission case 1, drive arrangement can drive clamp plate 6 along L shape motion trail cyclic motion, and with test board 5 and cleaning brush 14 intermittent type contact respectively.
The transmission case 1 is internally provided with a processor 15, the outer wall of the cavity 3 is provided with a display screen 16, the pressure sensor 8 is in wireless communication with the processor 15, the processor 15 is electrically connected with the display screen 16, and the display screen 16 is used for displaying the measured value of the pressure sensor. A battery is provided in the transmission case 1 for supplying electric power to each electronic device.
The driving device includes: the driving motor 17, the rotating shaft 18, the crank 19, the connecting rod 20 and the sliding plate 21 are arranged in the transmission case 1, the driving motor 17 is connected with the inner wall of the transmission case 1, the output end of the driving motor 17 is coaxially connected with one end of the rotating shaft 18, the other end of the rotating shaft 18 is connected with one end of the crank 19, the other end of the crank 19 is rotationally connected with one end of the connecting rod 20, the other end of the connecting rod 20 is hinged with the left end of the sliding plate 21, the right side of the driving motor 17 is provided with a guiding groove 22 in the horizontal direction, the guiding groove 22 is connected with the inner wall of the transmission case 1, the sliding plate 21 can slide back and forth along the guiding groove 22, an inclined sliding groove 23 is arranged on the sliding plate 21, an L-shaped sliding groove 24 is arranged on the bottom wall of the guiding groove 22, a sliding block 25 is connected in a sliding manner in the L-shaped sliding groove 24, one end of the sliding column 26 is connected with the sliding block 25, the other end of the sliding column 26 passes through the inclined sliding groove 23 and is connected with the upper end of the driving shaft 27 in the vertical direction, the sliding column 26 can slide reciprocally slide in the inclined sliding groove 23, the bottom wall of the transmission case 1 is provided with an opening groove 28 in the horizontal direction, the lower end of the driving shaft 27 passes through the opening groove 28 and is connected with the upper end of the mounting plate 11.
Be provided with a plurality of nozzles 29 on the cleaning brush 14, test tank 2 top is provided with liquid reserve tank 30, is provided with the washing liquid in the liquid reserve tank 30, transfer line 31 one end and liquid reserve tank 30 intercommunication, the transfer line 31 other end respectively with a plurality of nozzles 29 intercommunication, be provided with the transfer pump in the liquid reserve tank 30, the transfer pump is used for providing power for the liquid flow of transfer line 31, when needs are cleaned clamp plate 6 surface, start the transfer pump, spray the washing liquid on cleaning brush 14 through nozzle 29, cleaning brush 14 and clamp plate 6 relative friction, clean the clamp plate.
Be provided with feed liquor pipe 32 on the liquid reserve tank 30 lateral wall, feed liquor pipe 32 one end and liquid reserve tank 30 intercommunication, threaded connection has lid 33 on the other end of feed liquor pipe 32, is convenient for open lid 33 and supplements the washing liquid through feed liquor pipe 32.
The technical scheme has the working principle and beneficial technical effects that: the elastic brake actuator body 9 to be tested is fixed in the mounting groove 12 through the fastening screw 13, the pressure output end 10 of the elastic brake actuator body 9 is in threaded connection with the upper end of the pressing rod 7, the opening of the regulating valve of the elastic brake actuator body 9 is started to be maximum, the driving motor 17 is started to drive the rotating shaft 18 and the crank 19 to rotate, the crank 19 drives the connecting rod 20 to move, the connecting rod 20 drives the sliding plate 21 to reciprocate left and right along the guide groove body 22, when the sliding plate 21 slides left along the horizontal sliding groove of the L-shaped sliding groove 24, the sliding block 25 and the sliding column 26 slide left along the horizontal track, when the sliding plate 21 moves to the vertical sliding groove of the L-shaped sliding groove 24, the sliding block 25 and the sliding column 26 slide downwards along the vertical direction, when the sliding plate 21 moves right, the sliding block 25 and the sliding column 26 move vertically upwards first, then move horizontally right, and correspondingly, the pressing plate 6 fixedly connected with the sliding column 26 is driven to move circularly along the L-shaped track. The vertical downward movement of the pressing plate 6 presses the test plate 5, namely the working stroke of the elastic actuator, and the horizontal direction of the pressing plate 6 reciprocates to be in contact with the cleaning brush 14 for cleaning the working surface of the pressing plate 6, so that the working surface of the pressing plate is kept clean. The pressing plate 6 is in contact with the top end of the test plate 5 for compression, the maximum pressure value tested by the pressure sensor is the maximum pressure output value of the elastic brake actuator, then, after each measurement, the test plate 5 is taken out from the upper part of the groove body 4, the corresponding output pressure value of the spring of the elastic brake actuator under different expansion lengths can be measured, and the working surface of the pressing plate 6 can be cleaned by the cleaning brush 14 before each measurement, so that foreign matters are prevented from remaining on the working surface of the pressing plate to influence the measurement precision.
Example two
On the basis of the first embodiment, as shown in fig. 1-10, a vertical opening 34 is arranged on the left side wall of the groove body 4, a horizontal opening 35 is arranged on the bottom wall of the groove body 4, the lower end of the vertical opening 34 is communicated with the left end of the horizontal opening 35, a sliding rail 36 in the horizontal direction is arranged below the groove body 4, a moving block 37 is connected to the sliding rail 36 in a sliding manner, two ends of the sliding rail 36 are respectively provided with a fixed block 38, one side of the fixed block 38 is connected with the sliding rail 36, the other side of the fixed block 38 is connected with the inner wall of the test box 2, a push rod 39 is arranged at the top end of the moving block 37, the push rod 39 can pass through the vertical opening 34 and the horizontal opening 35, an outlet 40 is arranged on the right side wall of the groove body 4, and the test board 5 can pass through the outlet 40.
A slide bar 41 is arranged on the moving block 37, one end of a swing rod 42 is provided with a sliding groove 43 extending along the length direction, the slide bar 41 passes through the sliding groove 43 and can slide in the sliding groove 43, the other end of the swing rod 42 is hinged with the inner wall of the test box 2, the swing rod 42 can swing left and right, a roller 44 is rotationally connected on the swing rod 42, a first fixed column 45 is arranged on the swing rod 42, the first fixed column 45 is positioned between the sliding groove 43 and the roller 44, the right side of the swing rod 42 is provided with a second fixed column 46, the second fixed column 46 is connected with the inner wall of the test box 2, the first fixed column 45 is connected with the second fixed column 46 through a first spring 47, two ends of a wheel axle 48 are respectively rotationally connected with the inner wall of the test box 2, the wheel axle 48 is coaxially provided with a first belt pulley 49 and a second belt pulley 50, an incomplete rotary table 51 is arranged between the first belt pulley 49 and the second belt pulley 50, the wheel axle 48 penetrates through the center of the incomplete rotary table 51 and is connected with the incomplete rotary table 51, the circumferential outer wall of the incomplete rotary table 51 is composed of a first arc surface 511, a second arc surface 512 and two inclined planes 513, two ends of the first arc surface 511 and two ends of the second arc surface 512 are respectively connected through the two inclined planes 513, the circumferential outer wall of the incomplete rotary table 51 is in contact with the circumferential outer wall of the roller 44, a third belt pulley 52 is coaxially arranged on the rotating shaft 18, the first belt pulley 49 is connected with the third belt pulley 52 through a first belt 53, and the first belt 53 penetrates through the cavity 3.
The right side of the groove body 4 is provided with two U-shaped groove bodies 54, the openings of the U-shaped groove bodies 54 face upwards and are connected with the top of the inner wall of the test box 2, sliding blocks 55 are connected in a sliding mode in the U-shaped groove bodies 54, the top ends of the sliding blocks 55 are connected with one ends of second springs 56, the other ends of the second springs 56 are connected with the top wall of the test box 2, two ends of a first roller shaft 57 are respectively connected with the two sliding blocks 55 in a rotating mode, a first roller 58 is coaxially arranged on the first roller shaft 57, two ends of a second roller shaft 59 are respectively connected with the inner wall of the test box 2 in a rotating mode, a second roller 60 and a fourth belt pulley 61 are coaxially arranged on the second roller shaft 59, the second roller shaft 59 is located below the first roller shaft 57, and the second belt pulley 50 and the fourth belt pulley 61 are connected through a second belt 62.
The side wall of the test box 2 is provided with a material guide opening 63 close to the first roller 58, a material guide plate 64 is arranged below the material guide opening 63, one end of the material guide plate 64 is connected with the side wall of the test box 2, and the material guide plate plays a guiding role on the sliding-out of the test plate 5. The side wall of the test box 2 is provided with a box door, and the box door is opened to repair the components in the test box 2.
The technical scheme has the working principle and beneficial technical effects that: the rotating shaft 18 rotates to drive the third belt pulley 52 to rotate, the first belt 53 drives the first belt pulley 49 to rotate, the first belt pulley 49 drives the wheel shaft 48 and the incomplete rotary table 51 to rotate, and the incomplete rotary table 51 rolls with the circumferential outer wall of the roller 44, so that the swing rod 42 swings intermittently in a left-right reciprocating manner. When the roller 44 contacts the first arc surface 511, the swing rod 42 is in a stop state; when the roller 44 contacts the upper inclined surface 513, the swing rod 42 swings rightward; when the roller 44 contacts the second arc surface 512, the swing rod 42 is in a stop state; when the roller 44 contacts with the inclined plane 513 below, the swing rod 42 swings leftwards, so that the swing rod 42 is driven to swing leftwards and rightwards in a reciprocating manner, and the swing rod stops at the limit positions on two sides; by the cooperation of the sliding groove 43 at the upper end of the swing rod 42 and the sliding rod 41, the moving block 37 and the push rod 39 are driven to reciprocate left and right, and stop at the limit positions at the left end and the right end. When the push rod 39 moves rightwards, the test plate 5 at the bottom of the groove body 4 is pushed between the first roller 58 and the second roller 60, the first roller 58 and the second roller 60 rotate in opposite directions, and the test plate 5 is conveyed out of the test box 2 through the material guide opening 63 at the time of stopping the push rod 39; when the push rod 39 moves leftwards and stops at the limit position, the plurality of test boards 5 above the push rod drop, the whole thickness of the whole test board group drops, then the pressing plate 6 presses downwards, so that the circulation is continued, the pressing plate 6 presses downwards each time, the thickness of the test board group is reduced relative to the last thickness, the output pressure value corresponding to the spring of the elastic brake actuator under different expansion lengths is correspondingly measured, the measurement is more intelligent, the measurement precision is high, and the measurement efficiency is also improved. In addition, the axle 48 rotates to drive the second pulley 50 to rotate, the second belt 62 drives to drive the fourth pulley 61 to rotate, the fourth pulley 61 rotates to drive the second roller 60 to rotate, the first roller 58 and the peripheral outer wall of the second roller 60 are clung to each other due to the elastic force of the second spring 56, so that the second roller 60 drives the first roller 58 to move in opposite directions, the first roller 58 can move along with the sliding block 55 in the vertical direction, the driving of test boards with different thicknesses can be met, and the test boards are clamped between the first roller 58 and the second roller 60 so as to be transported out, so that the thickness of the test boards can be changed, and the output pressure measurement is carried out by the elastic actuators meeting different specifications.
It will be apparent to those skilled in the art that various modifications and variations can be made to the present invention without departing from the spirit or scope of the invention. Thus, it is intended that the present invention also include such modifications and alterations insofar as they come within the scope of the appended claims or the equivalents thereof.

Claims (7)

1. Output pressure testing arrangement of unmanned aerial vehicle elasticity brake actuator, its characterized in that includes: the transmission case (1) and the test case (2), transmission case (1) is located the top of test case (2), transmission case (1) bottom and cavity (3) one end intercommunication, cavity (3) other end and test case (2) top intercommunication, test case (2) top is provided with recess body (4), be provided with a plurality of range upon range of test boards (5) in recess body (4), test board (5) top is provided with clamp plate (6), clamp plate (6) top and depression bar (7) one end are connected, be provided with pressure sensor (8) in depression bar (7), the pressure bar (7) other end and the pressure output end (10) threaded connection of elasticity brake actuator body (9), transmission case (1) below is provided with mounting panel (11), be provided with mounting groove (12) on mounting panel (11), be located mounting groove (12) both sides respectively and be provided with fastening screw (13), elasticity brake actuator body (9) are located mounting groove (12), test case (2) top right side is provided with cleaning brush (14), be provided with in transmission case (1) other end and elasticity brake actuator body (9) pressure output end (10) threaded connection, be provided with mounting panel (11) below, be provided with mounting panel (12) mounting plate, be provided with respectively, and intermittently contact the test board (5) and the cleaning brush (14), respectively;
a processor (15) is arranged in the transmission case (1), a display screen (16) is arranged on the outer wall of the cavity (3), the pressure sensor (8) is in wireless communication with the processor (15), and the processor (15) is electrically connected with the display screen (16);
the driving device includes: the driving motor (17), the rotating shaft (18), the crank (19), the connecting rod (20) and the sliding plate (21), be provided with driving motor (17) in the transmission case (1), driving motor (17) are connected with the inner wall of the transmission case (1), driving motor (17) output and rotating shaft (18) one end coaxial coupling, rotating shaft (18) other end and crank (19) one end are connected, crank (19) other end and connecting rod (20) one end rotate and are connected, connecting rod (20) other end and sliding plate (21) left end are articulated, driving motor (17) right side is provided with horizontal direction's guide slot body (22), guide slot body (22) and transmission case (1) inner wall connection, sliding plate (21) can be along guide slot body (22) left and right reciprocating sliding, be provided with oblique spout (23) on the sliding plate (21), be provided with L shape spout (24) on the guide slot body (22) diapire, L shape spout (24) are connected with slider (25), slide post (26) one end and slider (25) are connected, slide post (26) other end passes oblique spout (23) and vertical direction's upper drive shaft (27) and slide post (26) are connected in the direction, can be provided with horizontal direction in the transmission case (28), the lower end of the driving shaft (27) passes through the open slot (28) to be connected with the upper end of the mounting plate (11), and the side wall of the test box (2) is provided with a box door.
2. The device for testing the output pressure of the elastic brake actuator of the unmanned aerial vehicle according to claim 1, wherein a plurality of nozzles (29) are arranged on the cleaning brush (14), a liquid storage tank (30) is arranged at the top end of the testing tank (2), one end of a liquid conveying pipe (31) is communicated with the liquid storage tank (30), the other end of the liquid conveying pipe (31) is respectively communicated with the plurality of nozzles (29), and an infusion pump is arranged in the liquid storage tank (30) and is used for providing power for the liquid flow of the liquid conveying pipe (31).
3. The device for testing the output pressure of the elastic brake actuator of the unmanned aerial vehicle according to claim 2, wherein a liquid inlet pipe (32) is arranged on the side wall of the liquid storage tank (30), one end of the liquid inlet pipe (32) is communicated with the liquid storage tank (30), and a cover (33) is connected to the other end of the liquid inlet pipe (32) in a threaded mode.
4. The device for testing the output pressure of the elastic brake actuator of the unmanned aerial vehicle according to claim 1, wherein a vertical opening (34) is formed in the left side wall of the groove body (4), a horizontal opening (35) is formed in the bottom wall of the groove body (4), the lower end of the vertical opening (34) is communicated with the left end of the horizontal opening (35), a sliding rail (36) in the horizontal direction is arranged below the groove body (4), a moving block (37) is connected onto the sliding rail (36) in a sliding manner, fixing blocks (38) are respectively arranged at two ends of the sliding rail (36), one side of each fixing block (38) is connected with the sliding rail (36), the other side of each fixing block (38) is connected with the inner wall of the test box (2), a push rod (39) is arranged at the top end of each moving block (37), the push rod (39) can penetrate through the vertical opening (34) and the horizontal opening (35), an outlet (40) is formed in the right side wall of the groove body (4), and the test plate (5) can penetrate through the outlet (40).
5. The device for testing the output pressure of the elastic brake actuator of the small unmanned aerial vehicle according to claim 4, wherein a sliding rod (41) is arranged on the moving block (37), one end of the swinging rod (42) is provided with a sliding groove (43) extending along the length direction, the sliding rod (41) penetrates through the sliding groove (43) and can slide in the sliding groove (43), the other end of the swinging rod (42) is hinged with the inner wall of the test box (2), the swinging rod (42) can swing left and right, a roller (44) is rotationally connected on the swinging rod (42), a first fixed column (45) is arranged on the swinging rod (42), the first fixed column (45) is positioned between the sliding groove (43) and the roller (44), a second fixed column (46) is arranged on the right side of the swinging rod (42), the second fixed column (46) is connected with the inner wall of the test box (2), the first fixed column (45) is connected with the second fixed column (46) through a first spring (47), the two ends of a wheel axle (48) are rotationally connected with the inner wall of the test box (2), a first belt pulley (49) and a second belt pulley (50) are coaxially arranged on the wheel axle (48), the first belt pulley (50) and the second belt pulley (50) are not completely connected with the wheel axle (51) through the wheel (51) completely, and the first belt pulley (50) and the second belt pulley (50) does not completely pass through the wheel (51) completely and completely passes through the wheel axle (51), the circumference outer wall of incomplete carousel (51) comprises first arc surface (511), second arc surface (512) and two inclined planes (513), and first arc surface (511) both ends and second arc surface (512) both ends are connected through two inclined planes (513) respectively, and the circumference outer wall of incomplete carousel (51) contacts with the circumference outer wall of gyro wheel (44), is provided with third belt pulley (52) on pivot (18) coaxial, and first belt pulley (49) are connected through first belt (53) with third belt pulley (52), and first belt (53) pass cavity (3).
6. The device for testing the output pressure of the elastic brake actuator of the unmanned aerial vehicle according to claim 5, wherein two U-shaped groove bodies (54) are arranged on the right side of the groove body (4), the openings of the U-shaped groove bodies (54) face upwards and are connected with the top of the inner wall of the test box (2), sliding blocks (55) are connected in the sliding mode in the U-shaped groove bodies (54), the top ends of the sliding blocks (55) are connected with one end of a second spring (56), the other end of the second spring (56) is connected with the top wall of the test box (2), two ends of a first roller shaft (57) are respectively connected with the two sliding blocks (55) in a rotating mode, a first roller (58) is coaxially arranged on the first roller shaft (57), two ends of a second roller shaft (59) are respectively connected with the inner wall of the test box (2) in a rotating mode, a second roller (60) and a fourth belt pulley (61) are coaxially arranged on the second roller shaft (59), and the second roller shaft (59) is located below the first roller shaft (57) and the fourth belt pulley (61) are connected through the second belt (62).
7. The device for testing the output pressure of the elastic brake actuator of the unmanned aerial vehicle according to claim 6, wherein a material guide opening (63) is formed in the side wall of the test box (2) close to the first roller (58), a material guide plate (64) is arranged below the material guide opening (63), and one end of the material guide plate (64) is connected with the side wall of the test box (2).
CN202410118959.9A 2024-01-29 2024-01-29 Output pressure testing device of elastic brake actuator of small unmanned aerial vehicle Active CN117647346B (en)

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Publication number Priority date Publication date Assignee Title
CN117906818B (en) * 2024-03-12 2024-05-28 陕西航宇工程科技有限责任公司 Load testing device for brake actuator

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CH626448A5 (en) * 1977-09-07 1981-11-13 Reto Gabriel Braking test stand for vehicles
SU1379677A1 (en) * 1986-07-04 1988-03-07 Проектно-Конструкторское Бюро Территориального Объединения "Куйбышевавтотранс" Stand for proximate diagnostics of motor vehicle brakes
DE4039957A1 (en) * 1990-12-14 1992-06-17 Iveco Magirus Testing vehicle pneumatic braking system in static mode - measuring and evaluating pressure versus time, response, threshold time, filling time and pressure drop
CN110758041A (en) * 2019-10-14 2020-02-07 陕西汽车集团有限责任公司 Integrated self-powered active suspension actuator control system and control method thereof
CN110803300A (en) * 2019-11-22 2020-02-18 航天时代飞鸿技术有限公司 Tool and method for testing braking moment of airplane wheel of unmanned aerial vehicle
CN111855064A (en) * 2020-08-21 2020-10-30 成都飞机工业集团电子科技有限公司 Wheel braking torque testing arrangement
CN113716025A (en) * 2021-08-30 2021-11-30 西安微电子技术研究所 Unmanned aerial vehicle electro-hydrostatic brake control device and dynamic pressure maintaining method
CN218330385U (en) * 2022-06-29 2023-01-17 成都成飞新航航空科技有限公司 Brake pressure detection device

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH626448A5 (en) * 1977-09-07 1981-11-13 Reto Gabriel Braking test stand for vehicles
SU1379677A1 (en) * 1986-07-04 1988-03-07 Проектно-Конструкторское Бюро Территориального Объединения "Куйбышевавтотранс" Stand for proximate diagnostics of motor vehicle brakes
DE4039957A1 (en) * 1990-12-14 1992-06-17 Iveco Magirus Testing vehicle pneumatic braking system in static mode - measuring and evaluating pressure versus time, response, threshold time, filling time and pressure drop
CN110758041A (en) * 2019-10-14 2020-02-07 陕西汽车集团有限责任公司 Integrated self-powered active suspension actuator control system and control method thereof
CN110803300A (en) * 2019-11-22 2020-02-18 航天时代飞鸿技术有限公司 Tool and method for testing braking moment of airplane wheel of unmanned aerial vehicle
CN111855064A (en) * 2020-08-21 2020-10-30 成都飞机工业集团电子科技有限公司 Wheel braking torque testing arrangement
CN113716025A (en) * 2021-08-30 2021-11-30 西安微电子技术研究所 Unmanned aerial vehicle electro-hydrostatic brake control device and dynamic pressure maintaining method
CN218330385U (en) * 2022-06-29 2023-01-17 成都成飞新航航空科技有限公司 Brake pressure detection device

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