CN113176090B - Wing strength detection device for unmanned aerial vehicle manufacturing - Google Patents
Wing strength detection device for unmanned aerial vehicle manufacturing Download PDFInfo
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- CN113176090B CN113176090B CN202110657052.6A CN202110657052A CN113176090B CN 113176090 B CN113176090 B CN 113176090B CN 202110657052 A CN202110657052 A CN 202110657052A CN 113176090 B CN113176090 B CN 113176090B
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
- G01M13/00—Testing of machine parts
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
- B64F5/60—Testing or inspecting aircraft components or systems
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Abstract
The invention discloses a wing strength detection device for manufacturing an unmanned aerial vehicle, which comprises a basic module, a feeding module, a clamping module, a detection module and a lifting module, and comprises a U-shaped plate, a table body fixedly connected with the U-shaped plate, a test table arranged between the U-shaped plate and the table body and a transverse plate arranged inside the U-shaped plate, wherein the U-shaped plate is provided with an opening, and the feeding module comprises a material frame fixedly connected with the test table. According to the invention, the movable end of the first electric push rod drives the first triangular plate to move towards the front end of the L-shaped pipe through the plate body, the first triangular plate jacks up the frame body, the frame body enables the space between the camera and the wing to be detected to be increased, the motor drives the turntable to rotate, the turntable drives the camera to be installed to move circularly through the rod body, the surface of the wing is shot and detected, when the surface of the wing is detected to be cracked, the wing is directly taken down, the strength of the wing can be visually detected, the wing detection is comprehensive, and the detection efficiency is improved.
Description
Technical Field
The invention relates to the technical field of wing detection for manufacturing of unmanned aerial vehicles, in particular to a wing strength detection device for manufacturing of unmanned aerial vehicles.
Background
The unmanned plane is called unmanned plane for short, and is an unmanned plane operated by radio remote control equipment and a self-contained program control device. The machine has no cockpit, but is provided with an automatic pilot, a program control device and other equipment. The personnel on the ground, the naval vessel or the mother aircraft remote control station can track, position, remotely control, telemeter and digitally transmit the personnel through equipment such as a radar. The aircraft can take off like a common airplane under the radio remote control or launch and lift off by a boosting rocket, and can also be thrown into the air by a mother aircraft for flying. During recovery, the aircraft can land automatically in the same way as the common aircraft landing process, and can also be recovered by a parachute or a barrier net for remote control. Can be repeatedly used for many times. The method is widely used for aerial reconnaissance, monitoring, communication, anti-submergence, electronic interference and the like.
The wing is when aerial, for the aircraft provides lift, buckle from top to bottom in view of the wing needs, the perk upwards in the air, ground is bent downwards, therefore, the overall structure design of wing must satisfy the standard and can not have wearing and tearing, it is ageing, tired etc. reason, cause it not to satisfy unmanned aerial vehicle flight safety requirement, because the shape of wing speciality, make the wing difficult tightly to be pressed from both sides in the detection, and then current intensity detects and mostly stops on manual detection, the condition of false retrieval appears easily in this method, the missed measure is examined, not only detection effect is poor, detection efficiency is still low.
Disclosure of Invention
The present invention is directed to solving one of the technical problems of the prior art or the related art.
Therefore, the technical scheme adopted by the invention is as follows:
wing intensity detection device is used in unmanned aerial vehicle manufacturing, including basic module, material loading module, clamping module, detection module and lifting module, including the U-shaped plate, with the table body of U-shaped plate rigid coupling, install in testboard between U-shaped plate and the table body with install in the inside diaphragm of U-shaped plate, the opening has been seted up on the U-shaped plate, the material loading module include with the material frame of testboard rigid coupling, connect in between material frame and the testboard and about the riser of material frame symmetry, with the conveyer that the riser is connected with set up in feed inlet on the testboard, clamping module including install in the L venturi tube at table body top, with L venturi tube swing joint's piston rod, with the plate body of piston rod rigid coupling, connect in first venturi tube electric putter between plate body and the L venturi tube, place in the L venturi tube just extend to the vaulting pole at L venturi tube top, A top plate fixedly connected with the stay bar, a rubber rod movably connected with the top plate and symmetrical about the vertical central line of the stay bar, a rope body fixedly connected with the rubber rod and a limit component connected with the clamping module, the detection module comprises a first triangular plate fixedly connected with the plate body, a frame body movably sleeved on the outer side of the first triangular plate and connected with the table body in a sliding manner, a motor fixedly connected with the frame body, a turntable fixedly connected with the output shaft of the motor, a rod body fixedly connected with the turntable, a semicircular ball body sleeved on the outer side of the rod body, a ring body movably sleeved on the outer side of the semicircular ball body and fixedly connected with the frame body and a camera fixedly connected with the rod body, the lifting module comprises a second electric push rod fixedly connected with the U-shaped plate, a second triangular plate fixedly connected with the second electric push rod and a pulley arranged between the second triangular plate and the test board.
Through adopting above-mentioned technical scheme, adopt material loading module structural design, the wing can accomplish the material loading by oneself, reduces and detects the cost, then adopts and presss from both sides tight module structural design, can press from both sides the wing of tight arbitrary size, increases the application range of product, adopts detection module and lifting module structural design at last, can high-efficient and comprehensive detection wing, detection effect is good, and detection effect is high.
The present invention in a preferred example may be further configured to: the limiting assembly comprises a pressing plate fixedly connected with the rope body, a T-shaped rod movably penetrating through the pressing plate, a spring sleeved on the outer side of the T-shaped rod and a disc body sleeved on the outer side of the T-shaped rod.
Through adopting above-mentioned technical scheme, set up spacing subassembly and can press from both sides the wing tightly, make the wing satisfy the condition that intensity detected.
The present invention in a preferred example may be further configured to: the table is characterized in that the piston rod and the support rod are located inside the L-shaped pipe, the piston rod is located on the front side of the support rod, the piston rod movably penetrates through the front end of the L-shaped pipe, the bottom of the plate body is in contact with the top of the table body, and the first electric push rod is located on the top of the L-shaped pipe.
Through adopting above-mentioned technical scheme, the plate body can link together piston rod and first triangle-shaped board, makes first electric putter can drive piston rod and the motion of first triangle-shaped board simultaneously.
The present invention in a preferred example may be further configured to: the table body is provided with a sliding groove suitable for the rope body to slide, and the bottom end of the rope body extends into the opening.
Through adopting above-mentioned technical scheme, set up the spout and can provide the space of moving for the rope body.
The present invention in a preferred example may be further configured to: the clamp plate sets up to two and about diaphragm vertical center line symmetry, T shape pole sets up to four, four the T shape pole is located both sides around the diaphragm respectively, is close to the left disk body of U-shaped plate is located the diaphragm bottom, keeps away from the left disk body of U-shaped plate is located the diaphragm top, the diaphragm top sets up to the inclined plane.
By adopting the technical scheme, the structural design is adopted, the left side of the wing is clamped with the transverse plate by the disc body and the pressing plate which are positioned on the left side of the transverse plate, and then the disc body and the pressing plate which are positioned on the right side of the transverse plate are matched with each other to only clamp the other side of the wing, so that the wing meets the condition of strength detection.
The present invention in a preferred example may be further configured to: the first triangular plate is located at the top of the first electric push rod, the bottom end of the frame body extends to the bottom of the table body, and the ring body is located between the rotary table and the camera.
Through adopting above-mentioned technical scheme, first triangle-shaped board can control the distance between camera and the wing through pushing up the framework.
The present invention in a preferred example may be further configured to: unmanned aerial vehicle makes and still includes the support frame with wing intensity detection device, the support frame is installed between second triangle-shaped board and testboard, the support frame activity is cup jointed in a plurality of T shape pole outsides, it is suitable for to have seted up on the support frame the gliding slide of T shape pole.
Through adopting above-mentioned technical scheme, set up the support frame and can provide the support to the diaphragm, increase the stability of diaphragm and wash.
The present invention in a preferred example may be further configured to: being close to the mounting groove has all been seted up to two T shape pole bottoms on U-shaped plate right side, the pulley sets up to two and installs respectively inside two mounting grooves, the pulley is through pivot and mounting groove swing joint.
Through adopting above-mentioned technical scheme, set up the space that the mounting groove can provide the installation for the pulley, meanwhile, it can carry on spacingly to the pulley, makes the pulley motion more steady.
The present invention in a preferred example may be further configured to: the table is characterized in that an arc plate is fixedly connected to the rear side of the plate body and movably mounted between the L-shaped pipe and the first electric push rod, and a rectangular block is mounted between the L-shaped pipe and the table body and located on the rear side of the first electric push rod.
Through adopting above-mentioned technical scheme, the arc leads the plate body to a certain extent, makes the tight operation of clamp and detect the operation more stable, then the rectangular block has increased the area of contact of L venturi tube with the table body, makes the installation of L venturi tube more firm.
By adopting the technical scheme, the invention has the beneficial effects that:
1. according to the invention, the movable end of the first electric push rod drives the first triangular plate to move towards the front end of the L-shaped pipe through the plate body, the first triangular plate jacks up the frame body, the frame body enables the space between the camera and the wing to be detected to be increased, the motor drives the turntable to rotate, the turntable drives the camera to be installed to move circularly through the rod body, the surface of the wing is shot and detected, when the surface of the wing is detected to be cracked, the wing is directly taken down, the strength of the wing can be visually detected, the wing detection is comprehensive, and the detection efficiency is improved.
2. According to the invention, the movable end of the first electric push rod drives the piston rod to move towards the front end of the L-shaped pipe through the plate body, the top plate moves downwards, the rope body is loosened, the pressing plate is extruded downwards by the spring after being not influenced by the tensile force of the rope body, the left side of the wing is clamped with the transverse plate by the plate body and the pressing plate on the left side of the transverse plate, and then the plate body and the pressing plate on the right side of the transverse plate are matched with each other to only clamp the other side of the wing, so that the wing meets the strength detection condition, the application range of the product is enlarged, and the market competitiveness is increased.
3. According to the invention, the second electric push rod drives the second triangular plate to move towards the right side of the U-shaped plate, the pulley is jacked upwards by the top of the U-shaped plate, the pulley transmits force to the T-shaped rod, and then the T-shaped rod lifts one side of the wing upwards through the disk body, so that the flexibility strength of the wing is detected.
Drawings
FIG. 1 is a perspective view of the overall structure of the present invention;
FIG. 2 is a front sectional view of the overall structure of the present invention;
FIG. 3 is a schematic cross-sectional view of the overall structure of the present invention;
FIG. 4 is a left side sectional view of the overall structure of the present invention;
FIG. 5 is a perspective view of a detection module of the present invention;
FIG. 6 is a perspective view of the stand of the present invention;
FIG. 7 is an enlarged view of the portion A of FIG. 5 according to the present invention;
FIG. 8 is an enlarged view of the portion B of FIG. 4 according to the present invention.
Reference numerals:
100. a base module; 110. a U-shaped plate; 120. a table body; 130. a test bench; 140. a transverse plate;
200. a feeding module; 210. material frame; 220. a vertical plate; 230. a conveyor; 240. a feed inlet;
300. a clamping module; 310. an L-shaped tube; 320. a piston rod; 330. a plate body; 340. a first electric push rod; 350. a stay bar; 360. a top plate; 370. a rubber rod; 380. a rope body; 390. a limiting component; 391. pressing a plate; 392. a T-shaped rod; 393. a spring; 394. a tray body;
400. a detection module; 410. a first triangular plate; 420. a frame body; 430. a motor; 440. a turntable; 450. a rod body; 460. a semicircular sphere; 470. a ring body; 480. a camera;
500. a lifting module; 510. a second electric push rod; 520. a second triangular plate; 530. a pulley;
600. a support frame.
Detailed Description
In order to make the objects, technical solutions and advantages of the present invention more apparent, the present invention will be described in further detail with reference to the accompanying drawings in conjunction with the following detailed description. It should be noted that the embodiments of the present invention and features of the embodiments may be combined with each other without conflict.
It is to be understood that this description is made only by way of example and not as a limitation on the scope of the invention.
The wing strength detection device for manufacturing the unmanned aerial vehicle provided by some embodiments of the invention is described below with reference to the accompanying drawings.
The first embodiment is as follows:
with reference to fig. 1 to 8, the wing strength detection device for manufacturing an unmanned aerial vehicle provided by the invention comprises a base module 100, a feeding module 200, a clamping module 300, a detection module 400 and a lifting module 500, and comprises a U-shaped plate 110, a table body 120 fixedly connected with the U-shaped plate 110, a test table 130 installed between the U-shaped plate 110 and the table body 120, and a transverse plate 140 installed inside the U-shaped plate 110, wherein an opening is formed in the U-shaped plate 110, the U-shaped plate 110 is used for supporting the feeding module 200 and the clamping module 300 to ensure that mechanical detection operation can be normally performed, and then the table body 120 is used for supporting the detection module 400 and providing a space for placing detection wings;
the feeding module 200 comprises a material frame 210 fixedly connected with the test bench 130, a vertical plate 220 connected between the material frame 210 and the test bench 130 and symmetrical with respect to the material frame 210, a conveyor 230 connected with the vertical plate 220, and a feeding port 240 arranged on the test bench 130; by adopting the structural design of the feeding module 200, the automatic feeding function of the wings can be realized, and in the process, the wings are supplemented one by one, so that the situation that the wings are stacked mutually is avoided, and the detection effect is improved;
the clamping module 300 comprises an L-shaped pipe 310 installed at the top of the table body 120, a piston rod 320 movably connected with the L-shaped pipe 310, a plate body 330 fixedly connected with the piston rod 320, a first electric push rod 340 connected between the plate body 330 and the L-shaped pipe 310, a stay bar 350 arranged in the L-shaped pipe 310 and extending to the top of the L-shaped pipe 310, a top plate 360 fixedly connected with the stay bar 350, a rubber rod 370 movably connected with the top plate 360 and symmetrical about the vertical center line of the stay bar 350, a rope body 380 fixedly connected with the rubber rod 370, and a limiting component 390 connected with the clamping module 300; in the using process, the first electric push rod 340 drives the piston rod 320 connected with the first electric push rod to move towards the front end of the L-shaped pipe 310 through the plate body 330, the piston rod 320 extracts air in the L-shaped pipe 310, air pressure in the L-shaped pipe 310 is increased, then the piston rod 350 connected with the top plate 360 is driven to move downwards, the top plate 360 releases the rope body 380 through the rubber rod 370, then the pressing plate 391 becomes flexible, the spring 390 transmits elastic force to the pressing plate 391 to enable the pressing plate 391 to press the wing tightly, and the strength detection operation of the wing is convenient to carry out
The detection module 400 comprises a first triangular plate 410 fixedly connected with the plate body 330, a frame body 420 movably sleeved outside the first triangular plate 410 and slidably connected with the table body 120, a motor 430 fixedly connected with the frame body 420, a turntable 440 fixedly connected with an output shaft of the motor 430, a rod body 450 fixedly connected with the turntable 440, a semicircular sphere 460 sleeved outside the rod body 450, a ring body 470 movably sleeved outside the semicircular sphere 460 and fixedly connected with the frame body 420, and a camera 480 fixedly connected with the rod body 450; the first electric push rod 340 drives the first triangular plate 410 to move towards the front end of the L-shaped pipe 310 through the plate body 330, the top of the first triangular plate 410 jacks up the frame body 420, then the frame body 420 drives the motor 430 and the ring body 470, the camera 480 is far away from the top of the wing, the shooting range of the camera 480 is increased, then the motor 430 drives the turntable 440 to rotate, the turntable 440 drives the camera 480 to do circular motion through the rod body 450, and the surface of the wing can be shot and detected;
the lifting module 500 comprises a second electric push rod 510 fixedly connected with the U-shaped plate 110, a second triangular plate 520 fixedly connected with the second electric push rod 510, and a pulley 530 installed between the second triangular plate 520 and the test bench 130, in the use process, the second electric tail 510 drives the second triangular plate 520 to move towards the right side of the U-shaped plate 110, during the period, the pulley 530 is jacked upwards by the top of the U-shaped plate 110, the pulley 530 transmits force to the T-shaped rod 392, and then the T-shaped rod 392 lifts one side of the wing upwards through the tray 394, so as to detect the flexible strength of the wing.
Specifically, the position-limiting component 390 comprises a pressing plate 391 fixed to the rope 380, a T-shaped rod 392 movably penetrating the pressing plate 391, a spring 393 sleeved outside the T-shaped rod 392, and a tray 394 sleeved outside the T-shaped rod 392, the pressing plates 391 are arranged in two and are symmetrical about the vertical center line of the transverse plate 140, the number of the T-shaped rods 392 is four, four T-shaped rods 392 are respectively arranged at the front and rear sides of the transverse plate 140, the plate 394 close to the left side of the U-shaped plate 110 is arranged at the bottom of the transverse plate 140, the plate 394 far away from the left side of the U-shaped plate 110 is arranged at the top of the transverse plate 140, the top of the transverse plate 140 is provided with an inclined surface, and by adopting the structural design, the plate body 394 and the pressure plate 391 which are positioned at the left side of the transverse plate 140 clamp the left side of the wing and the transverse plate 140, then the plate 394 on the right side of the cross plate 140 and the pressure plate 391 cooperate with each other to clamp only the other side of the wing, so that the wing meets the condition of strength detection.
Further, the piston rod 320 and the stay bar 350 are both located inside the L-shaped tube 310, the piston rod 320 is located on the front side of the stay bar 350, the piston rod 320 movably penetrates through the front end of the L-shaped tube 310, the bottom of the plate body 330 is in contact with the top of the table body 120, the first electric push rod 340 is located on the top of the L-shaped tube 310, by adopting the structural design, the work of the piston rod 320 and the work of the stay bar 350 are mutually related but do not interfere with each other, and the piston rod 320 can control the lifting movement of the stay bar 350, so that the control of the wing clamping operation is realized.
Further, a sliding groove suitable for the rope body 380 to slide is formed in the table body 120, the bottom end of the rope body 380 extends into the opening, the sliding groove provides a moving space for the rope body 380, the abrasion degree of the rope body 380 is reduced, and the service life of the rope body 380 is prolonged to a certain extent.
Further, the first triangular plate 410 is located at the top of the first electric push rod 340, the bottom end of the frame body 420 extends to the bottom of the table body 120, the ring body 470 is located between the turntable 440 and the camera 480, the first triangular plate 410 reciprocates back and forth, so that the frame body 420 repeatedly moves up and down, and then the frame body 420 controls the distance between the camera 480 and the wing to be detected.
Further, be close to the mounting groove has all been seted up to two T shape pole 392 bottoms on U-shaped plate 110 right side, pulley 530 sets up to two and installs respectively inside two mounting grooves, pulley 530 sets up the space that the mounting groove can provide the installation for pulley 530 through pivot and mounting groove swing joint, and meanwhile, the mounting groove inner wall is spacing to pulley 530, makes the motion that pulley 530 can be steady.
Example two:
with reference to fig. 1-4 and fig. 6, on the basis of the first embodiment, the wing strength detection device for manufacturing the unmanned aerial vehicle further includes a support frame 600, the support frame 600 is installed between the second triangular plate 520 and the test bench 130, the support frame 600 is movably sleeved outside the plurality of T-shaped rods 392, a slideway suitable for the T-shaped rods 392 to slide is formed in the support frame 600, the support frame 600 is arranged to improve the stability of the transverse plate 140, so that the transverse plate can support the wing, and then the slideway guides the movement track of the T-shaped rods 392 to make the T-shaped rods 392 move more stably.
Example three:
as shown in fig. 1, 2, 4 and 8, in the above embodiment, an arc plate is fixedly connected to the rear side of the plate body 330, the arc plate is movably installed between the L-shaped tube 310 and the first electric push rod 340, a rectangular block is installed between the L-shaped tube 310 and the table body 120, the rectangular block is located at the rear side of the first electric push rod 340, the arc plate is arranged to guide the plate body 330, so that the plate body 330 can stably drive the piston rod 320 and the first triangular plate 410 to stably move, and then the rectangular block increases the contact area between the L-shaped tube 310 and the table body 120, so that the L-shaped tube 310 is firmer.
The working principle and the using process of the invention are as follows: in an initial state, the material frame 210 is filled with wings to be detected, then the piston rod 320 is positioned inside the L-shaped tube 310, under the action of air pressure, the stay rod 350 drives the top plate 360 connected with the rope body 380 to move upwards, the rope body 380 pulls up the pressing plate 391, when the device is put into practical use, the wings fall onto the conveyor 230 under the influence of gravity, then the wings slide onto the transverse plate 140 through the feed inlet, then the first electric push rod 340 is started, the movable end of the first electric push rod 340 drives the piston rod 320 and the first triangular plate 410 to move towards the front end of the L-shaped tube 310 through the plate body 330, then the top plate 360 moves downwards, the rope body 380 is loosened, the pressing plate 391 is pressed downwards by the spring 393 after being not influenced by the pulling force of the rope body 380, the left side of the wing transverse plate 140 is clamped with the transverse plate 140 by the disc body 394 and the pressing plate 391 positioned on the left side of the transverse plate 140, then the disc body 394 and the pressing plate 391 positioned on the right side of the transverse plate 140 are matched with each other side to clamp only the wings on the other side, the wing meets the strength detection condition, during the period, the first triangular plate 410 jacks up the frame body 420, the frame body 420 enlarges the distance between the camera 480 and the wing to be detected, the shooting area of the camera 480 is increased, then the motor 430 drives the rotary disc 440 to rotate, the rotary disc 440 drives the camera 480 to do circular motion through the rod body 450, the surface of the wing is shot and detected, when the surface of the wing is detected to be cracked, the wing is directly taken down, the detection efficiency is improved, then the second electric push rod 510 is started, the second triangular plate 520 is driven by the second electric push rod 510 to move towards the right side of the U-shaped plate 110, during the period, the pulley 530 is jacked up from the top of the U-shaped plate 110, the pulley 530 transmits force to the T-shaped rod 392, then the T-shaped rod 392 jacks up one side of the wing upwards through the plate 394, and the flexibility strength of the wing is detected.
In the present invention, the term "plurality" means two or more unless explicitly defined otherwise. As used herein, the term "and/or" includes any and all combinations of one or more of the associated listed items. The terms "mounted," "connected," "fixed," and the like are to be construed broadly, and for example, "connected" may be a fixed connection, a removable connection, or an integral connection; "coupled" may be direct or indirect through an intermediary. The specific meanings of the above terms in the present invention can be understood by those skilled in the art according to specific situations.
It will be understood that when an element is referred to as being "mounted to," "secured to" or "disposed on" another element, it can be directly on the other element or intervening elements may also be present. When an element is referred to as being "connected" to another element, it can be directly connected to the other element or intervening elements may also be present. The terms "vertical," "horizontal," "upper," "lower," "left," "right," and the like as used herein are for illustrative purposes only and do not denote a unique embodiment.
In the description herein, the description of the terms "one embodiment," "some embodiments," "specific embodiments," etc., means that a particular feature, structure, material, or characteristic described in connection with the embodiment or example is included in at least one embodiment or example of the invention. In this specification, the schematic representations of the terms used above do not necessarily refer to the same embodiment or example. Furthermore, the particular features, structures, materials, or characteristics described may be combined in any suitable manner in any one or more embodiments or examples.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the claims and their equivalents.
Claims (5)
1. Unmanned aerial vehicle makes and uses wing intensity detection device, its characterized in that includes:
the base module (100) comprises a U-shaped plate (110), a table body (120) fixedly connected with the U-shaped plate (110), a test bench (130) arranged between the U-shaped plate (110) and the table body (120) and a transverse plate (140) arranged inside the U-shaped plate (110), wherein an opening is formed in the U-shaped plate (110);
the feeding module (200) comprises a material frame (210) fixedly connected with the test bench (130), a vertical plate (220) connected between the material frame (210) and the test bench (130) and symmetrical about the material frame (210), a conveyor (230) connected with the vertical plate (220) and a feeding hole (240) formed in the test bench (130);
the clamping module (300) comprises an L-shaped pipe (310) arranged at the top of the table body (120), a piston rod (320) movably connected with the L-shaped pipe (310), a plate body (330) fixedly connected with the piston rod (320), a first electric push rod (340) connected between the plate body (330) and the L-shaped pipe (310), a support rod (350) arranged in the L-shaped pipe (310) and extending to the top of the L-shaped pipe (310), a top plate (360) fixedly connected with the support rod (350), a rubber rod (370) movably connected with the top plate (360) and symmetrical about a vertical center line of the support rod (350), a rope body (380) fixedly connected with the rubber rod (370) and a limiting assembly (390) connected with the clamping module (300);
the limiting assembly (390) comprises a pressing plate (391) fixedly connected with the rope body (380), T-shaped rods (392) movably penetrating through the pressing plate (391), springs (393) sleeved outside the T-shaped rods (392) and a disc body (394) sleeved outside the T-shaped rods (392), the two pressing plates (391) are arranged and are symmetrical about the vertical center line of the transverse plate (140), the four T-shaped rods (392) are arranged in four, the four T-shaped rods (392) are respectively positioned at the front side and the rear side of the transverse plate (140), the disc body (394) close to the left side of the U-shaped plate (110) is positioned at the bottom of the transverse plate (140), the disc body (394) far away from the left side of the U-shaped plate (110) is positioned at the top of the transverse plate (140), and the top of the transverse plate (140) is arranged as an inclined plane;
the piston rod (320) and the support rod (350) are both positioned inside the L-shaped pipe (310), the piston rod (320) is positioned on the front side of the support rod (350), the piston rod (320) movably penetrates through the front end of the L-shaped pipe (310), the bottom of the plate body (330) is in contact with the top of the table body (120), and the first electric push rod (340) is positioned on the top of the L-shaped pipe (310);
the detection module (400) comprises a first triangular plate (410) fixedly connected with the plate body (330), a frame body (420) movably sleeved on the outer side of the first triangular plate (410) and slidably connected with the table body (120), a motor (430) fixedly connected with the frame body (420), a turntable (440) fixedly connected with an output shaft of the motor (430), a rod body (450) fixedly connected with the turntable (440), a semicircular sphere (460) sleeved on the outer side of the rod body (450), a ring body (470) movably sleeved on the outer side of the semicircular sphere (460) and fixedly connected with the frame body (420), and a camera (480) fixedly connected with the rod body (450);
the first triangular plate (410) is positioned at the top of the first electric push rod (340), the bottom end of the frame body (420) extends to the bottom of the table body (120), and the ring body (470) is positioned between the rotary disc (440) and the camera (480);
the lifting module (500) comprises a second electric push rod (510) fixedly connected with the U-shaped plate (110), a second triangular plate (520) fixedly connected with the second electric push rod (510), and a pulley (530) arranged between the second triangular plate (520) and the test bench (130).
2. The wing strength detection device for unmanned aerial vehicle manufacturing of claim 1, wherein the table body (120) is provided with a sliding groove suitable for the rope body (380) to slide, and a bottom end of the rope body (380) extends into the opening.
3. The wing strength detection device for unmanned aerial vehicle manufacturing of any one of claims 1-2, characterized in that the wing strength detection device for unmanned aerial vehicle manufacturing further comprises a support frame (600), the support frame (600) is installed between the second triangular plate (520) and the test bench (130), the support frame (600) is movably sleeved on the outer sides of the plurality of T-shaped rods (392), and a slideway suitable for the T-shaped rods (392) to slide is formed in the support frame (600).
4. The wing strength detection device for unmanned aerial vehicle manufacturing of claim 1, wherein two T-shaped rods (392) near the right side of the U-shaped plate (110) are provided with mounting grooves at the bottom ends, the two pulleys (530) are respectively mounted inside the two mounting grooves, and the pulleys (530) are movably connected with the mounting grooves through rotating shafts.
5. The wing strength detection device for unmanned aerial vehicle manufacturing of claim 1, wherein an arc-shaped plate is fixedly connected to the rear side of the plate body (330), the arc-shaped plate is movably mounted between the L-shaped pipe (310) and the first electric push rod (340), a rectangular block is mounted between the L-shaped pipe (310) and the table body (120), and the rectangular block is located on the rear side of the first electric push rod (340).
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