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CN-224225308-U - Unmanned vehicles production is with lifting test equipment

CN224225308UCN 224225308 UCN224225308 UCN 224225308UCN-224225308-U

Abstract

The utility model discloses lifting force testing equipment for unmanned aerial vehicle production, which comprises a base, wherein a lifting force meter is fixedly arranged at the top of the base, a fixed barrel is fixedly arranged at the top of the base, a fixed rod is fixedly connected with the top of the fixed barrel in a penetrating and sliding manner, a supporting plate positioned right above the base is fixedly arranged at the top of the fixed rod, an annular groove is integrally formed in the top of the supporting plate, a lower sliding block is fixedly connected with the bottom of the interior of the annular groove in a sliding manner, a threaded rod is integrally connected with the top of the lower sliding block, an upper sliding plate positioned right above the lower sliding block is fixedly connected with the interior of the annular groove in a sliding manner, and a fixed knob is rotationally connected to the middle of the upper sliding plate. The movable block drives the clamping ring to move to a position suitable for clamping, and the clamping ring is fixed with the unmanned aerial vehicle arm, so that the rapid and stable fixing treatment of the unmanned aerial vehicle is realized, and the lifting force test is convenient to carry out.

Inventors

  • ZHOU JINGTAO

Assignees

  • 南京铠甲无人机技术有限公司

Dates

Publication Date
20260512
Application Date
20250616

Claims (7)

  1. 1. The lift force test equipment for unmanned aerial vehicle production comprises a base (1), and is characterized in that a lift force meter (2) is fixedly arranged at the top of the base (1), a fixed cylinder (3) is fixedly arranged at the top of the base (1), a fixed rod (4) is connected with the top of the fixed cylinder (3) in a penetrating and sliding manner, a supporting plate (5) arranged right above the base (1) is fixedly arranged at the top of the fixed rod (4), an annular groove (7) is integrally arranged at the top of the supporting plate (5), a lower sliding block (8) is connected with the bottom of the inside of the annular groove (7) in a sliding manner, a threaded rod (9) is integrally connected with the top of the lower sliding block (8), an upper sliding plate (11) arranged right above the lower sliding block (8) in a sliding manner is connected with the inside of the annular groove (7), a fixed knob (10) is rotationally connected with the middle of the upper sliding plate (11) in a penetrating and threaded manner with the threaded rod (9), an adjusting chute (12) is arranged at the top of the upper sliding plate (11), an adjusting chute (12) is connected with one end of an adjusting screw (13) in a rotating manner, and one end of the adjusting screw (13) is fixedly arranged outside the adjusting screw (13), the inside sliding connection of adjusting lead screw (13) has movable block (15), the top rotation of movable block (15) is connected with grip ring (16), the middle part of movable block (15) runs through threaded connection with adjusting lead screw (13).
  2. 2. The lift force testing device for unmanned aerial vehicle production according to claim 1, wherein four fixing cylinders (3) are fixedly installed at four corners of the top of the base (1), the inner diameter of each fixing cylinder (3) is the same as the diameter of the fixing rod (4), and the size of the supporting plate (5) is the same as the size of the base (1).
  3. 3. The lifting force testing device for unmanned aerial vehicle production according to claim 1, wherein a connecting plate is arranged at the measuring end of the top of the lifting force meter (2), connecting pull ropes (6) are fixedly arranged in the middle of the bottom of the supporting plate (5), and the bottoms of the four connecting pull ropes (6) are fixedly arranged at four corners of the top of each connecting plate.
  4. 4. The lifting force testing device for unmanned aerial vehicle production according to claim 1, wherein a convex ring is integrally arranged in the middle of the inside of the annular groove (7), the lower sliding block (8) is positioned below the convex ring, the bottom of the upper sliding plate (11) is positioned above the convex ring, and the threaded rod (9) penetrates through the middle of the convex ring.
  5. 5. The lifting force testing device for unmanned aerial vehicle production according to claim 1, wherein the middle part of the upper sliding plate (11) is provided with a through groove, the fixing knob (10) is positioned in the through groove, and the diameter of the fixing knob (10) is larger than the thickness of the upper sliding plate (11).
  6. 6. The lifting force testing device for unmanned aerial vehicle production according to claim 1, wherein the top of the moving block (15) is provided with a convex edge with a width larger than the width of the adjusting chute (12), and the convex edge at the top of the moving block (15) is in sliding contact with the top of the adjusting chute (12).
  7. 7. The lift force testing device for unmanned aerial vehicle production according to claim 1, wherein an anti-slip pad is arranged on the inner side of the clamping ring (16), the clamping ring (16) is composed of two semi-rings which are connected in a rotating manner, and a threaded locking assembly is arranged on the other ends of the two semi-rings which form the clamping ring (16).

Description

Unmanned vehicles production is with lifting test equipment Technical Field The utility model relates to the technical field of unmanned aerial vehicle tools, in particular to lift test equipment for unmanned aerial vehicle production. Background Nowadays, with the rapid development of remote control technology, the remote control technology is applied to a plurality of fields, such as common unmanned aerial vehicles, wherein the unmanned aerial vehicles are unmanned aerial vehicles operated by using radio remote control equipment and self-provided program control devices, and in the production process of the unmanned aerial vehicles, multiple tests are required to be carried out on the produced unmanned aerial vehicles, and the common unmanned aerial vehicles are provided with lifting force test devices. At present, when the existing unmanned aerial vehicle is used for carrying out lift test, a rope is mostly adopted to fix a foot rest of the unmanned aerial vehicle, the unmanned aerial vehicle is controlled to carry out lift test, but in the use process of the lift test device, the rope fixing method is complex and inconvenient to fix, the foot rest of the unmanned aerial vehicle cannot be rapidly and stably fixed, and the use is inconvenient. For this purpose, we propose a lift test device for unmanned aerial vehicle production. Disclosure of utility model The utility model aims to provide lifting force testing equipment for unmanned aerial vehicle production, so as to solve the problems in the background technology. In order to achieve the purpose, the lift test equipment for unmanned aerial vehicle production comprises a base, wherein a lift meter is fixedly arranged at the top of the base, a fixed cylinder is fixedly arranged at the top of the base, a fixed rod is connected with the top of the fixed cylinder in a penetrating and sliding manner, a supporting plate positioned right above the base is fixedly arranged at the top of the fixed rod, an annular groove is integrally formed in the top of the supporting plate, a lower sliding block is connected with the bottom inside the annular groove in a sliding manner, a threaded rod is integrally connected with the top of the lower sliding block, an upper sliding plate positioned right above the lower sliding block is connected with the inside of the annular groove in a sliding manner, a fixed knob is rotationally connected with the middle of the fixed knob in a penetrating and threaded manner, an adjusting sliding groove is formed in the top of the upper sliding plate, an adjusting screw is rotationally connected with an adjusting screw rod, one end of the adjusting screw rod is fixedly arranged at the outer part of the adjusting screw rod, a moving block is connected with the inside of the adjusting screw rod in a sliding manner, a clamping ring is rotationally connected with the top of the moving block, and the middle part of the moving block is in a penetrating and threaded manner with the adjusting screw rod. Optionally, four fixed cylinders are respectively fixedly installed at four corners of the top of the base, the inner diameter of each fixed cylinder is the same as the diameter of each fixed rod, and the size of the tray is the same as the size of the base. Optionally, the measuring end at lift meter top is provided with the connecting plate, the middle part fixed mounting of layer board bottom has the connection stay cord, four the bottom of connection stay cord and the four corners fixed mounting at connecting plate top respectively. Optionally, the inside middle part of ring channel is integrative to be provided with the bulge loop, lower sliding block is located the below of bulge loop, the bottom of going up the sliding plate is located the top of bulge loop, the threaded rod runs through the middle part of bulge loop. Optionally, the middle part of going up the sliding plate has seted up logical groove, fixed knob is located the inside of logical groove, the diameter of fixed knob is greater than the thickness of going up the sliding plate. Optionally, the top of movable block sets up the chimb that the width is greater than the width of regulation spout, the chimb at movable block top and the top sliding contact of regulation spout. Optionally, the inboard of grip ring is provided with the slipmat, the grip ring comprises two semi-rings of rotating the connection, constitutes the other end of two semi-rings of grip ring is provided with screw thread locking subassembly. Compared with the prior art, the utility model has the beneficial effects that: 1. This unmanned vehicles production is with lifting test equipment, through setting up the ring channel, slip sliding plate and lower sliding block to suitable position in the ring channel, rethread fixed knob for go up sliding plate and lower sliding block and press from both sides tightly in the middle of the ring channel and fix, rethread adjust knob drives and adjusts the lead screw rotatio