CN113484147A - Airship strength detection device and using method thereof - Google Patents

Airship strength detection device and using method thereof Download PDF

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Publication number
CN113484147A
CN113484147A CN202110843225.3A CN202110843225A CN113484147A CN 113484147 A CN113484147 A CN 113484147A CN 202110843225 A CN202110843225 A CN 202110843225A CN 113484147 A CN113484147 A CN 113484147A
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wall
main body
airship
fixed
bracket
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CN202110843225.3A
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CN113484147B (en
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胡豆
胡明程
刘天福
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Chongqing Lvhangjia Aviation Technology Co ltd
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Hubei Hangte Aircraft Co ltd
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    • GPHYSICS
    • G01MEASURING; TESTING
    • G01NINVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N3/00Investigating strength properties of solid materials by application of mechanical stress
    • G01N3/08Investigating strength properties of solid materials by application of mechanical stress by applying steady tensile or compressive forces
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64FGROUND 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
    • B64F5/00Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
    • B64F5/60Testing or inspecting aircraft components or systems
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01NINVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N3/00Investigating strength properties of solid materials by application of mechanical stress
    • G01N3/02Details
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01NINVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N2203/00Investigating strength properties of solid materials by application of mechanical stress
    • G01N2203/0001Type of application of the stress
    • G01N2203/0003Steady
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01NINVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N2203/00Investigating strength properties of solid materials by application of mechanical stress
    • G01N2203/0014Type of force applied
    • G01N2203/0016Tensile or compressive
    • G01N2203/0019Compressive
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01NINVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N2203/00Investigating strength properties of solid materials by application of mechanical stress
    • G01N2203/003Generation of the force
    • G01N2203/0032Generation of the force using mechanical means
    • G01N2203/0041Human or animal power
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01NINVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N2203/00Investigating strength properties of solid materials by application of mechanical stress
    • G01N2203/0058Kind of property studied
    • G01N2203/006Crack, flaws, fracture or rupture
    • G01N2203/0067Fracture or rupture
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01NINVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N2203/00Investigating strength properties of solid materials by application of mechanical stress
    • G01N2203/02Details not specific for a particular testing method
    • G01N2203/025Geometry of the test
    • G01N2203/0258Non axial, i.e. the forces not being applied along an axis of symmetry of the specimen
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01NINVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N2203/00Investigating strength properties of solid materials by application of mechanical stress
    • G01N2203/02Details not specific for a particular testing method
    • G01N2203/06Indicating or recording means; Sensing means
    • G01N2203/067Parameter measured for estimating the property
    • G01N2203/0676Force, weight, load, energy, speed or acceleration

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  • Health & Medical Sciences (AREA)
  • Life Sciences & Earth Sciences (AREA)
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  • General Health & Medical Sciences (AREA)
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Abstract

The invention discloses an airship strength detection device and a using method thereof, relating to the technical field of airship strength detection; to facilitate flexible detection; the device comprises a main body, wherein the main body is of a U-shaped structure, densely distributed rolling balls are connected in the main body in a rolling manner, a first arc-shaped tray is connected to the inner wall of one end of the main body in a sliding manner, and a pressing rod is arranged on the outer wall of one side of the first arc-shaped tray; the use method of the device comprises the following steps: taking the detection head out of the containing box and installing the detection head in the threaded cylinder; holding the handle to attach the sucker to the surface to be tested. According to the invention, the main body, the rolling ball and other structures are arranged, so that the appearance of the device similar to a pistol structure can be formed, the rolling ball is pushed by pressing the pressing plate, the detection head is pushed out, the piercing strength of the airship is detected by the detection head, the rolling ball can smoothly convert the pressing force into pushing force in the period, the detection can be completed by only one-hand operation, and the use convenience is improved.

Description

Airship strength detection device and using method thereof
Technical Field
The invention relates to the technical field of airship strength detection, in particular to an airship strength detection device and a using method thereof.
Background
An airship is a lighter-than-air craft that differs from a hot-air balloon in having means to propel and control the flight conditions. The airship consists of a huge streamline hull, a nacelle positioned below the hull, a tail surface with a stable control function and a propelling device; the air bag of the airship body is filled with buoyancy gas with density smaller than that of air so as to generate buoyancy force to lift the airship; the nacelle is used for passengers to take and load goods; the tail surface is used for controlling and keeping the stability of course and pitching; the large civil airship can also be used for transportation, entertainment, disaster relief, film and television shooting, scientific experiments and the like; the serious consequences can be caused when the air bag of the airship and the like are damaged, so that the airship needs to be reliably detected in production in order to ensure the safety of the airship, and the conventional detection device is usually heavy and has poor use flexibility, so that the improvement is needed.
Through retrieval, chinese patent application No. CN201721381080.5 discloses a cardboard puncture strength detection device, which structurally comprises: the support frame, the spirit level, the bottom plate, the control cabinet, the balancing weight, balanced callus on the sole, the organism, the protection casing, the weighting block, the action arm, the fixed axle, the sensor, the support frame is installed perpendicularly in the bottom plate left side and is adopted bolted connection, the organism is installed in the bottom plate right side and is adopted the welding, the organism openly installs the control cabinet and adopts screw connection, the balanced callus on the sole is installed and is adopted threaded connection to the bottom plate below, the action arm is the arc and passes through the fixed axle to be installed in the organism left side and adopt clearance fit, the weighting block is fixed in the action arm top through the centre bore and adopts clearance fit. The detection device in the above patent has the following disadvantages: the device is heavy and has poor use flexibility, so the improvement is needed.
Disclosure of Invention
The invention aims to solve the defects in the prior art and provides an airship strength detection device and a using method thereof.
In order to achieve the purpose, the invention adopts the following technical scheme:
the airship strength detection device comprises a main body, wherein the main body is of a U-shaped structure, densely distributed rolling balls are connected in the main body in a rolling manner, a first arc-shaped tray is connected to the inner wall of one end of the main body in a sliding manner, a pressing rod is arranged on the outer wall of one side of the first arc-shaped tray, a pressing plate is fixed to one end of the pressing rod, the same pressing spring is fixed between the outer wall of one side of the pressing plate and the outer wall of one end of the main body, a second arc-shaped tray is connected to the inner wall of the other end of the main body in a sliding manner, a pushing rod is arranged on the outer wall of one side of the second arc-shaped tray, a pushing mechanism is arranged at one end of the pushing rod, and a detection head is arranged on one side, away from the pushing rod, of the pushing mechanism; a grab handle is fixed at the bottom of the main body.
Preferably: a display is fixed on the outer wall of the top of the main body, the pushing mechanism comprises a first support and a second support, a guide rod is arranged on one side, close to the first support, of the second support, the guide rod is connected to the inner wall of the first support in a sliding mode, a limiting block is fixed at one end of the guide rod, the same pushing spring is fixed between the limiting block and the first support, a conductive sheet matched with the first support is arranged between the first support and the second support, a pressure detection assembly is installed on the outer wall of one side of the second support, a threaded cylinder is installed on one side, away from the second support, of the pressure detection assembly, and a detection head is detachably installed on the inner wall of the threaded cylinder through threads; the main body is provided with a control unit, and the control unit is electrically connected with the pressure detection assembly, the display and the two conducting strips.
Further: the outer wall of one side of the pushing rod is provided with a pushing frame, the outer wall of one side of the main body is provided with a sliding groove, and the pushing frame is connected to the inner wall of the sliding groove in a sliding mode.
Further preferred is: the outer wall of one end of the main body is provided with an annular connecting seat, the outer wall of the annular connecting seat is provided with a thread cover through thread detachable, a hollow seat is fixed on the outer wall of one side of the thread cover, the outer wall of the hollow seat, which is far away from the thread cover, is provided with suckers distributed uniformly and circumferentially, the suckers are located on the outer side of the detection head, the outer walls of two sides of the main body are fixed with the same air pressure generating device through a fixing seat, and the output end of the air pressure generating device is connected inside the hollow seat through an air pipe.
As a preferable aspect of the present invention: the outer wall of one side of the grab handle is provided with finger grooves which are uniformly distributed and are of arc structures.
Further preferred as the invention: the outer wall of one side of the grab handle is provided with a finger ring, and the position of the finger ring is matched with the finger groove.
As a still further scheme of the invention: a hanging rope is fixed on the outer wall of one side of the main body, and a hanging ring is fixed at one end of the hanging rope.
On the basis of the scheme: the outer wall of the bottom of the main body is fixedly provided with an accommodating box, and the size of the accommodating box is matched with that of the detection head.
On the basis of the foregoing scheme, it is preferable that: the spin has worn to connect and has connect the rope with one root in, and the both ends of connecting the rope are fixed in one side outer wall of first arc tray and second arc tray respectively.
A use method of the airship strength detection device comprises the following steps:
s1: taking the detection head out of the containing box and installing the detection head in the threaded cylinder;
s2: holding the grab handle, and attaching the sucker to the surface to be detected;
s3: controlling the air pressure generating device to work, and sucking and fixing the surface to be detected by using a sucking disc;
s4: pressing the pressing plate to push out the detection head and stabbing the surface to be detected;
s5: and acquiring a display result of the display after the puncture.
The invention has the beneficial effects that:
1. according to the invention, the main body, the rolling ball and other structures are arranged, so that the appearance of the device similar to a pistol structure can be formed, the rolling ball is pushed by pressing the pressing plate, the detection head is pushed out, the piercing strength of the airship is detected by the detection head, the rolling ball can smoothly convert the pressing force into pushing force in the period, the detection can be completed by only one-hand operation, and the use convenience is improved.
2. Through the arrangement of the conducting strips, the pushing spring and other structures, in the detection process, the detection head is pushed to contact with an airship material, along with the increase of the pushing force, the pushing spring deforms to enable the second support to approach the first support, the two conducting strips are further contacted, the control unit receives an electric signal and reads the value fed back by the pressure detection assembly in real time, along with the increase of the pushing force, at the moment that the airship material is punctured by the detection head, the first support is separated from the second support by utilizing the resilience force of the pushing spring, so that the two conducting strips are separated, the control unit finishes the recording of the pressure detection assembly and feeds back the value through the display; the method is beneficial to data acquisition and ensures the reliability.
3. By arranging the pushing frame, the structures such as the rolling balls can be controlled to reset by pushing the pushing frame, so that the practicability is improved; through setting up sucking disc, air pressure generating device isotructure, can utilize the sucking disc attached in waiting to detect the surface before the propelling movement detects the head, control air pressure generating device work makes the sucking disc adsorb the surface to avoid waiting that the surface deformation volume is too big and influence detects, promoted the practicality.
4. The finger grooves are arranged, so that a user can hold the finger grooves conveniently, and the anti-skidding function is achieved; the finger ring is arranged, so that the grab handle can be effectively prevented from being separated from the hand, and the reliability is improved; by arranging the hanging rope and the hanging ring, the device is convenient to hang and place, is favorable for storage, and improves the practicability; hold the box through setting up, can will detect the head when not using and take off and place in holding the box, place and detect the head and hinder the people, promoted practicality and security.
5. Through setting up connection rope isotructure, can utilize to connect rope pulling second arc tray synchronous reset at the in-process that resets based on pressing the spring resilience force according to the clamp plate to make spin between the two reset, promoted the practicality.
Drawings
Fig. 1 is a schematic structural diagram of an entire airship strength detection device provided by the invention;
fig. 2 is a schematic structural diagram of the other side of the airship strength detection device provided by the invention;
fig. 3 is a schematic structural diagram of a cross section of a hollow seat of an airship strength detection device provided by the invention;
fig. 4 is a schematic structural diagram of the interior of a main body of an airship strength detection device provided by the invention;
fig. 5 is a schematic structural diagram of a first bracket and a second bracket of an airship strength detection device according to the present invention;
fig. 6 is a schematic structural diagram of a section of a rolling ball of an airship strength detection device according to embodiment 2 of the present invention.
In the figure: 1 main part, 2 trachea, 3 screw thread covers, 4 hollow seats, 5 sucking discs, 6 pressing springs, 7 pressing plates, 8 rings, 9 finger grooves, 10 grab handles, 11 hold the box, 12 hang and put the ring, 13 hang and put the rope, 14 air pressure generating device, 15 fixing bases, 16 displays, 17 detection head, 18 annular connecting seats, 19 push away the frame, 20 threaded cylinder, 21 second support, 22 spin, 23 pressure detection subassembly, 24 propelling movement pole, 25 conducting strip, 26 first support, 27 stopper, 28 second arc tray, 29 propelling movement springs, 30 guide bars, 31 pressing bars, 32 first arc tray, 33 connection rope.
Detailed Description
The technical solution of the present patent will be described in further detail with reference to the following embodiments.
Reference will now be made in detail to embodiments of the present patent, examples of which are illustrated in the accompanying drawings, wherein like or similar reference numerals refer to the same or similar elements or elements having the same or similar function throughout. The embodiments described below with reference to the drawings are exemplary only for the purpose of explaining the present patent and are not to be construed as limiting the present patent.
In the description of this patent, it is to be understood that the terms "center," "upper," "lower," "front," "rear," "left," "right," "vertical," "horizontal," "top," "bottom," "inner," "outer," and the like are used in the orientations and positional relationships indicated in the drawings for the convenience of describing the patent and for the simplicity of description, and are not intended to indicate or imply that the referenced devices or elements must have a particular orientation, be constructed and operated in a particular orientation, and are not to be considered limiting of the patent.
In the description of this patent, it is noted that unless otherwise specifically stated or limited, the terms "mounted," "connected," and "disposed" are to be construed broadly and can include, for example, fixedly connected, disposed, detachably connected, disposed, or integrally connected and disposed. The specific meaning of the above terms in this patent may be understood by those of ordinary skill in the art as appropriate.
Example 1:
an airship strength detection device is shown in figures 1-6 and comprises a main body 1, wherein the main body 1 is of a U-shaped structure, rolling balls 22 which are densely distributed are connected in the main body 1 in a rolling manner, the inner wall of one end of the main body 1 is connected with a first arc-shaped tray 32 in a sliding manner, the outer wall of one side of the first arc-shaped tray 32 is integrally provided with a pressing rod 31, one end of the pressing rod 31 is fixedly provided with a pressing plate 7 through screws, the same pressing spring 6 is welded between the outer wall of one side of the pressing plate 7 and the outer wall of one end of the main body 1, the inner wall of the other end of the main body 1 is connected with a second arc-shaped tray 28 in a sliding manner, the outer wall of one side of the second arc-shaped tray 28 is integrally provided with a pushing rod 24, one end of the pushing rod 24 is provided with a pushing mechanism, and one side of the pushing mechanism, which is far away from the pushing rod 24, is provided with a detection head 17; a grab handle 10 is fixed at the bottom of the main body 1 through a screw; through setting up main part 1, spin 22 isotructure, can form the device appearance of a similar pistol structure, utilize the mode of pressing down press plate 7, promote spin 22, will detect head 17 and release then, utilize and detect head 17 and detect the stabbing intensity of airship, spin 22 can be smooth during convert the pushing pressure into the propelling force with pressing force, and only need the one-hand operation can accomplish, has promoted the convenience of use.
To facilitate acquisition of the detection data; as shown in fig. 2 and 5, the display 16 is fixed on the outer wall of the top of the main body 1 through a screw, the pushing mechanism includes a first support 26 and a second support 21, a guide rod 30 is integrally arranged on one side of the second support 21 close to the first support 26, the guide rod 30 is slidably connected to the inner wall of the first support 26, one end of the guide rod 30 is fixed with a limiting block 27 through a screw, a same pushing spring 29 is fixed between the limiting block 27 and the first support 26, a conductive sheet 25 which is matched with the first support 26 and the second support 21 is arranged between the first support 26 and the second support 21, a pressure detection assembly 23 is mounted on the outer wall of one side of the second support 21, a threaded cylinder 20 is mounted on one side of the pressure detection assembly 23 away from the second support 21, and a detection head 17 is detachably mounted on the inner wall of the threaded cylinder 20 through a thread; the main body 1 is provided with a control unit which is electrically connected with the pressure detection assembly 23, the display 16 and the two conducting strips 25; by arranging the conducting strips 25, the pushing spring 29 and other structures, in the detection process, the detection head 17 is pushed to contact with the airship material, along with the increase of the pushing force, the pushing spring 29 deforms, the second support 21 is made to approach the first support 26, the two conducting strips 25 are further contacted, the control unit receives an electric signal and reads the value fed back by the pressure detection assembly 23 in real time, along with the increase of the pushing force, at the moment that the airship material is punctured by the detection head 17, the first support 26 is separated from the second support 21 by the resilience force of the pushing spring 29, so that the two conducting strips 25 are separated, the control unit finishes the recording of the pressure detection assembly 23 and feeds back the value through the display 16; the method is beneficial to data acquisition and ensures the reliability.
To facilitate repositioning; as shown in fig. 2 and 4, the outer wall of one side of the pushing rod 24 is integrally provided with a pushing frame 19, the outer wall of one side of the main body 1 is provided with a sliding groove, and the pushing frame 19 is slidably connected to the inner wall of the sliding groove; through setting up and pushing away frame 19, can control spin 22 isotructures through promoting to push away frame 19 and reset, promote the practicality.
To facilitate detection; as shown in fig. 1-3, an annular connecting seat 18 is integrally arranged on the outer wall of one end of the main body 1, a thread cover 3 is detachably mounted on the outer wall of the annular connecting seat 18 through threads, a hollow seat 4 is fixed on the outer wall of one side of the thread cover 3 through screws, sucking discs 5 which are uniformly distributed circumferentially are mounted on the outer wall, away from the thread cover 3, of the hollow seat 4, the sucking discs 5 are located outside a detection head 17, the same air pressure generating device 14 is fixed on the outer walls of two sides of the main body 1 through a fixing seat 15, and the output end of the air pressure generating device 14 is connected to the inside of the hollow seat 4 through an air pipe 2; through setting up sucking disc 5, air pressure generating device 14 isotructures, can utilize sucking disc 5 attached in waiting to detect the surface before the propelling movement detects head 17, control air pressure generating device 14 work, make sucking disc 5 adsorb the surface to avoid the surperficial deformation volume of awaiting measuring too big and influence the detection, promoted the practicality.
To facilitate holding; as shown in fig. 1, finger grooves 9 are uniformly distributed on the outer wall of one side of the grab handle 10, and the finger grooves 9 are of an arc structure; through setting up finger groove 9, can be convenient for the user and hold, played skid-proof function.
To further facilitate handling; as shown in fig. 1, a finger ring 8 is arranged on the outer wall of one side of the grab handle 10, and the position of the finger ring 8 is matched with the finger groove 9; through setting up ring 8, can prevent effectively that grab handle 10 from taking off the hand, promote the reliability.
In order to improve the practicability; as shown in fig. 1, a hanging rope 13 is fixed on the outer wall of one side of the main body 1 through screws, and a hanging ring 12 is fixed on one end of the hanging rope 13 through screws; through setting up and hanging rope 13 and hanging ring 12, be convenient for hang the device and put and place, do benefit to and accomodate, promoted the practicality.
In order to improve the practicability; as shown in fig. 1 and 4, the outer wall of the bottom of the main body 1 is fixed with an accommodating box 11 through screws, and the size of the accommodating box 11 is matched with that of the detection head 17; hold box 11 through the setting, can will detect when not using head 17 and take off and place in holding box 11, place and detect head 17 and hinder the people, promote practicality and security.
Example 2:
an airship strength detection device is shown in fig. 6, and is convenient for resetting a rolling ball 22; the present embodiment is modified from embodiment 1 as follows: the same connecting rope 33 is connected in the rolling ball 22 in a penetrating way, and two ends of the connecting rope 33 are respectively fixed on the outer walls of one sides of the first arc-shaped tray 32 and the second arc-shaped tray 28; through setting up connection rope 33 isotructures, can utilize connection rope 33 pulling second arc tray 28 to reset in step at the in-process that resets based on pressing the 6 resilience force of spring according to pressure board 7 to make spin 22 between the two reset, promoted the practicality.
Example 3:
a use method of the airship strength detection device comprises the following steps:
s1: the detection head 17 is taken out of the containing box 11 and is installed in the threaded cylinder 20;
s2: holding the handle 10, attaching the suction cup 5 to the surface to be measured;
s3: controlling the air pressure generating device 14 to work, and sucking and fixing the surface to be detected by using the sucking disc 5;
s4: pressing the pressing plate 7 to push out the detection head 17 and poking the surface to be detected;
s5: and obtaining the display result of the display 16 after the puncture.
The above description is only for the purpose of illustrating the preferred embodiments of the present invention and is not intended to limit the scope of the present invention, which is defined by the claims and their equivalents, and all changes which come within the meaning and range of equivalency of the art are therefore intended to be embraced therein.

Claims (10)

1. An airship strength detection device comprises a main body (1) and is characterized in that the main body (1) is of a U-shaped structure, densely distributed rolling balls (22) are connected in the main body (1) in a rolling manner, a first arc-shaped tray (32) is connected with the inner wall of one end of the main body (1) in a sliding way, a pressing rod (31) is arranged on the outer wall of one side of the first arc-shaped tray (32), a pressing plate (7) is fixed at one end of the pressing rod (31), a same pressing spring (6) is fixed between the outer wall of one side of the pressing plate (7) and the outer wall of one end of the main body (1), a second arc tray (28) is connected with the inner wall of the other end of the main body (1) in a sliding way, a pushing rod (24) is arranged on the outer wall of one side of the second arc-shaped tray (28), a pushing mechanism is arranged at one end of the pushing rod (24), and a detection head (17) is arranged on one side, far away from the pushing rod (24), of the pushing mechanism; a grab handle (10) is fixed at the bottom of the main body (1).
2. The airship strength detection device according to claim 1, wherein a display (16) is fixed on the outer wall of the top of the main body (1), the pushing mechanism comprises a first bracket (26) and a second bracket (21), a guide rod (30) is arranged on one side of the second bracket (21) close to the first bracket (26), the guide rod (30) is connected to the inner wall of the first bracket (26) in a sliding manner, a limiting block (27) is fixed on one end of the guide rod (30), the same pushing spring (29) is fixed between the limiting block (27) and the first bracket (26), a conductive sheet (25) which is matched with the first bracket (26) is arranged between the first bracket (26) and the second bracket (21), a pressure detection component (23) is installed on the outer wall of one side of the second bracket (21), and a threaded barrel (20) is installed on one side of the pressure detection component (23) far away from the second bracket (21), the detection head (17) is detachably arranged on the inner wall of the threaded cylinder (20) through threads; the main body (1) is provided with a control unit, and the control unit is electrically connected with the pressure detection assembly (23), the display (16) and the two conducting strips (25).
3. The airship strength detection device according to claim 2, wherein the pushing rod (24) is provided with a pushing frame (19) on one side of the outer wall, the main body (1) is provided with a sliding groove on one side of the outer wall, and the pushing frame (19) is slidably connected to the inner wall of the sliding groove.
4. The airship strength detection device according to claim 3, wherein an annular connecting seat (18) is arranged on an outer wall of one end of the main body (1), a screw thread cover (3) is detachably mounted on an outer wall of the annular connecting seat (18) through screw threads, a hollow seat (4) is fixed on an outer wall of one side of the screw thread cover (3), suckers (5) which are uniformly distributed circumferentially are mounted on an outer wall of the hollow seat (4) far away from the screw thread cover (3), the suckers (5) are located on the outer side of the detection head (17), the same air pressure generation device (14) is fixed on outer walls of two sides of the main body (1) through a fixing seat (15), and an output end of the air pressure generation device (14) is connected inside the hollow seat (4) through an air pipe (2).
5. The airship strength detection device according to claim 4, wherein the outer wall of one side of the grab handle (10) is provided with evenly distributed finger grooves (9), and the finger grooves (9) are arc-shaped.
6. The airship strength detection device according to claim 5, wherein the outer wall of one side of the grab handle (10) is provided with a finger ring (8), and the position of the finger ring (8) is matched with the finger groove (9).
7. The airship strength detection device according to claim 6, wherein a hanging rope (13) is fixed on an outer wall of one side of the main body (1), and a hanging ring (12) is fixed at one end of the hanging rope (13).
8. The airship strength testing device according to claim 7, characterized in that a containing box (11) is fixed on the outer wall of the bottom of the main body (1), and the size of the containing box (11) is matched with that of the testing head (17).
9. The airship strength detection device according to claim 8, wherein the same connecting rope (33) is threaded in the rolling ball (22), and two ends of the connecting rope (33) are respectively fixed on one side outer wall of the first arc-shaped tray (32) and one side outer wall of the second arc-shaped tray (28).
10. The use method of the airship strength detection device is characterized by comprising the following steps:
s1: the detection head (17) is taken out of the containing box (11) and is arranged in the threaded cylinder (20);
s2: a holding handle (10) for attaching the sucker (5) to the surface to be detected;
s3: controlling an air pressure generating device (14) to work, and sucking and fixing the surface to be detected by using a sucking disc (5);
s4: pressing the pressing plate (7) to push out the detection head (17) and poke the surface to be detected;
s5: and obtaining the display result of the display (16) after the puncture.
CN202110843225.3A 2021-07-26 2021-07-26 Airship strength detection device and using method thereof Active CN113484147B (en)

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CN207318216U (en) * 2017-10-25 2018-05-04 苏州国奥印刷科技有限公司 A kind of cardboard pokes intensity detecting device
CN108254138A (en) * 2018-04-21 2018-07-06 张方亮 The coarse leakage detection method of non-breathable packaging bag and device
JP2018179868A (en) * 2017-04-19 2018-11-15 国立研究開発法人建築研究所 Method and system for inspecting degree of deterioration of existing soft material and measuring device
CN209043734U (en) * 2018-09-14 2019-06-28 山东国鸿防水材料股份有限公司 A kind of anti-thorn test device of waterproof roll
CN112504807A (en) * 2019-09-15 2021-03-16 南京理工大学 Testing arrangement suitable for flexible membrane material puncture performance

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN204679332U (en) * 2015-04-22 2015-09-30 东莞市魔方新能源科技有限公司 Barrier film puncture strength test fixture
JP2018179868A (en) * 2017-04-19 2018-11-15 国立研究開発法人建築研究所 Method and system for inspecting degree of deterioration of existing soft material and measuring device
CN207318216U (en) * 2017-10-25 2018-05-04 苏州国奥印刷科技有限公司 A kind of cardboard pokes intensity detecting device
CN108254138A (en) * 2018-04-21 2018-07-06 张方亮 The coarse leakage detection method of non-breathable packaging bag and device
CN209043734U (en) * 2018-09-14 2019-06-28 山东国鸿防水材料股份有限公司 A kind of anti-thorn test device of waterproof roll
CN112504807A (en) * 2019-09-15 2021-03-16 南京理工大学 Testing arrangement suitable for flexible membrane material puncture performance

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