CN-122016476-A - Unmanned aerial vehicle resistance to compression test machine

Abstract

The invention relates to the technical field of material strength detection, in particular to an unmanned aerial vehicle compression-resistant testing machine which comprises an organic table, a mounting plate, mounting frames and the like, wherein the mounting plate is connected to the machine table, one mounting frame positioned in front of the mounting plate is connected to the machine table, a plurality of linear guide rails are connected to the mounting plate, each linear guide rail is provided with an electric sliding block, all the electric sliding blocks are commonly connected with another mounting frame positioned in front of the mounting plate, the two mounting frames are arranged in a vertically opposite mode, the mounting frames positioned on the electric sliding blocks are connected with a plurality of first electric push rods, the mounting frames positioned on the machine table are connected with bearing plates, and telescopic ends of all the first electric push rods are commonly connected with a compression plate. When the pressure-resistant detection is carried out on the sample, the sample is positioned in the closed space formed by the bearing plate, the pressing plate, the transparent blocking frame and the collecting frame, so that the splashed fragments are prevented from polluting the ground and injuring operators during subsequent detection.

Inventors

• XIE HONGXIANG
• ZHOU CHENGLAN
• XIE WENXU

Assignees

• 江西金凯自动化设备有限公司

Dates

Publication Date

20260512

Application Date

20260309

Claims (10)

1. 1. The unmanned aerial vehicle compression-resistant testing machine comprises an organic table (1) and a mounting plate (2), wherein the mounting plate (2) is connected to the machine table (1), the unmanned aerial vehicle compression-resistant testing machine is characterized by further comprising a mounting frame (101), the machine table (1) is connected with the mounting frame (101) positioned in front of the mounting plate (2), the mounting plate (2) is connected with a plurality of linear guide rails (102), each linear guide rail (102) is provided with an electric slide block (103), all the electric slide blocks (103) are commonly connected with the other mounting frame (101) positioned in front of the mounting plate (2), the two mounting frames (101) are arranged in an up-down opposite mode, the mounting frame (101) positioned on the electric slide blocks (103) is connected with a plurality of first electric push rods (104), the first electric push rods (104) are provided with pressure sensors, the mounting frame (101) positioned on the machine table (1) is connected with a bearing plate (105), the telescopic ends of all the first electric push rods (104) are commonly connected with a pressing plate (106), the bearing plate (105) and the pressing plate (106) are positioned between the two mounting frames (101), the length and the width of the supporting plate (105) are smaller than those of the pressing plate (106), the mounting frame (101) arranged on the machine table (1) is connected with a plurality of second electric push rods (107), the telescopic ends of all the second electric push rods (107) are commonly connected with a transparent blocking frame (108), the length and the width of the inner space of the transparent blocking frame (108) are the same as those of the pressing plate (106), the supporting plate (105) is connected with a collecting frame (109), the collecting frame (109) is provided with a collecting cavity (10901), the length and the width of the collecting frame (109) are the same as those of the pressing plate (106), the transparent blocking frame (108) is connected with a plurality of hollow connecting frames (1010), the hollow connecting frames (1010) are connected with the telescopic ends of the second electric push rods (107), and an air outlet (10801) communicated with the hollow connecting frames (1010) is formed in the area of the transparent blocking frame (108) located in the hollow connecting frames (1010).
2. 2. A stress-resistant testing machine for unmanned aerial vehicle according to claim 1, wherein a filter screen (201) for blocking debris is connected to each vent (10801) of the transparent barrier frame (108).
3. 3. A stress-resistant testing machine for unmanned aerial vehicle according to claim 2, wherein the lower portion of the exhaust port (10801) is provided in an inclined shape toward the collecting frame (109).
4. 4. A stress-resistant testing machine for unmanned aerial vehicle according to claim 3, wherein the lower part of the transparent barrier frame (108) is provided with a restriction part (10802) for restricting the upward movement distance of the transparent barrier frame (108).
5. 5. The unmanned aerial vehicle compression testing machine is characterized by further comprising a third electric push rod (301), wherein a mounting frame (101) arranged on a machine table (1) is connected with a plurality of third electric push rods (301), telescopic ends of all the third electric push rods (301) are connected with a supporting plate (105), the mounting frame (101) arranged on the machine table (1) is connected with a plurality of fourth electric push rods (302), a tension sensor is arranged on the fourth electric push rods (302), the mounting frame (101) arranged on an electric sliding block (103) is connected with a plurality of servo motors (303), torsion sensors are arranged on the servo motors (303), telescopic ends of all the fourth electric push rods (302) and output ends of all the servo motors (303) are connected with a two-finger electric clamping jaw (304), a semicircular block (305) is connected to a driving part (30401) of each two-finger electric clamping jaw (304), the two semicircular blocks (305) on the same two-finger electric clamping jaw (304) form a complete block, and a plurality of pressing clamping jaw (305) are arranged on the semicircular block (105) and the supporting plate (106) is provided with a plurality of pressing through holes.
6. 6. A stress-resistant testing machine for unmanned aerial vehicle according to claim 1, wherein a plurality of separating parts (10803) are arranged at each exhaust port (10801) of the transparent barrier frame (108).
7. 7. The unmanned aerial vehicle compression resistance testing machine is characterized by further comprising a guide plate (401), wherein a plurality of discharge holes (10902) communicated with a collecting cavity (10901) are formed in a collecting frame (109), the lowest point of the discharge holes (10902) and the lowest point of the upper surface of the guide plate (401) are positioned on the same horizontal line, the guide plate (401) with the inverted V-shaped upper surface is connected to the collecting frame (109), a plurality of first avoidance grooves (40101) which are identical to the main body of an electric clamping jaw (304) in appearance are formed in the guide plate (401), the main body of the two-finger electric clamping jaw (304) is located in the first avoidance grooves (40101), a plurality of second avoidance grooves (40102) which are identical to the diameter of the telescopic ends of a third electric push rod (301) are formed in the guide plate (401), and the telescopic ends of the third electric push rod (301) are located in the second avoidance grooves (40102).
8. 8. The unmanned aerial vehicle compression testing machine is characterized by further comprising a shielding block (501), wherein shielding blocks (501) for shielding scraps are arranged between two semicircular blocks (305) on each two-finger electric clamping jaw (304), and the upper surface of the shielding block (501) positioned below is in an inverted V shape.
9. 9. The unmanned aerial vehicle compression testing machine is characterized by further comprising connecting plates (601), wherein one connecting plate (601) is connected in each hollow connecting frame (1010), a plurality of through holes (60101) are formed in each connecting plate (601), one connecting block (602) is connected in each through hole (60101), one connecting belt (603) is connected to one side, facing the transparent blocking frame (108), of each connecting block (602), and one rubber column (604) is connected to one end, far away from the connecting block (602), of each connecting belt (603).
10. 10. A stress-resistant testing machine for unmanned aerial vehicle according to claim 9, wherein the thickness of the side of each connecting block (602) facing away from the transparent barrier frame (108) is smaller than the thickness of the side of each connecting block (602) facing towards the transparent barrier frame (108).

Description

Unmanned aerial vehicle resistance to compression test machine Technical Field The invention relates to the technical field of material strength detection, in particular to an unmanned aerial vehicle compression resistance testing machine. Background Along with technical development, unmanned aerial vehicle uses very extensively in fields such as commodity circulation, inspection and hoist and mount, among the prior art, for promoting unmanned aerial vehicle bulk strength, performance and life, unmanned aerial vehicle generally uses carbon fiber, carbon fiber composite, glass fiber composite and Kevlar fiber material to prepare, and when unmanned aerial vehicle prepares, need carry out intensity detection to the material that uses in the preparation process, guarantee to accord with expecting for unmanned aerial vehicle strength, and among the prior art, when carrying out intensity detection to the material, the piece that splashes exists and causes the injury to operating personnel, the piece that splashes simultaneously is owing to drop the position uncertainty, has increased the clearance degree of difficulty of follow-up operating personnel to the piece. Disclosure of Invention In order to overcome the defects in the prior art, the invention provides an unmanned aerial vehicle compression resistance testing machine. The technical scheme is that the unmanned aerial vehicle compression testing machine comprises an organic table and a mounting plate, wherein the mounting plate is connected to the machine table, the unmanned aerial vehicle compression testing machine further comprises mounting frames, linear guide rails, electric sliding blocks, first electric push rods, supporting plates, pressing plates, second electric push rods, transparent blocking frames, collecting frames and hollow connecting frames, the machine table is connected with the mounting frame located in front of the mounting plate, the mounting plate is connected with a plurality of linear guide rails, each linear guide rail is provided with one electric sliding block, all the electric sliding blocks are commonly connected with the other mounting frame located in front of the mounting plate, the two mounting frames are arranged in an up-down opposite mode, the mounting frames located on the electric sliding blocks are connected with a plurality of first electric push rods, the first electric push rods are provided with pressure sensors, the mounting frames located on the machine table are connected with the supporting plates, the telescopic ends of all the first electric push rods are commonly connected with one pressing plate, the supporting plates and the pressing plates are located between the two mounting frames, the lengths and the widths of the supporting plates are smaller than those of the pressing plates, the mounting frames located on the machine table are connected with the second electric push rods, the mounting frames located on the machine table are commonly connected with the second electric push rods, the two transparent blocking frames are connected with the transparent blocking frames and the hollow connecting the collecting frames and the transparent blocking frames and the hollow connecting the collecting frames with the hollow connecting frames. Further, a filter screen for blocking debris is connected to each vent of the transparent blocking frame. Further, the lower portion of the exhaust port is provided in an inclined shape toward the collection frame. Further, a limiting part for limiting the upward moving distance of the transparent blocking frame is arranged at the lower part of the transparent blocking frame. The device comprises a machine table, a support plate, a plurality of electric pushing rods, a plurality of servo motors, a torque sensor, two-finger electric clamping jaws, a semicircular block, a clamping jaw driving part, a supporting plate and a pressing plate, wherein the machine table is provided with a plurality of electric pushing rods, the servo motors, the two-finger electric clamping jaws and the semicircular block are arranged on the mounting frame, the mounting frame is connected with the support plate, the four electric pushing rods are arranged on the mounting frame, the four electric pushing rods are arranged on the electric pushing rods, the servo motors are connected with the servo motors, the torque sensor is arranged on the servo motors, the two-finger electric clamping jaws are connected with the telescopic end of each fourth electric pushing rod and the output end of each servo motor, the semicircular block is connected to the clamping jaw driving part of each two-finger electric clamping jaw, the two semicircular blocks on the same two-finger electric clamping jaw form a complete circular block, and the support plate and the pressing plate are provided with a plurality of circular through holes with the same diameter as the semicircular block. Further, each exhaust port of the tran