Support frame device for installing fault indicator on unmanned aerial vehicle

Abstract

The invention discloses a support frame device for installing a fault indicator on an unmanned aerial vehicle, and the device comprises a support unit which comprises an installation part, a placement part disposed at the top of the installation part, limiting parts disposed at the two sides of the placement part, an adjustment part in threaded connection with the limiting parts, and a locking part disposed at one end of the adjustment part. The device can be connected with the unmanned aerial vehicle through the arrangement of the mounting part, meanwhile, the fault indicator can be fixed through the arrangement of the adjusting part, the locking part and the stopping part, the fault indicator can be fixed in the placement part in the initial mounting process, and the fault indicator can be conveniently and rapidly placed in the placement part. And furthermore, an operator can open the fault indicator conveniently to complete later installation, so that the installation efficiency is greatly improved, the waste of human resources is reduced, and the installation efficiency is improved.

Description

Technical Field

[0001] The invention relates to the technical field of fault indicator installation, in particular to a support frame device and a method for installing a fault indicator on an unmanned aerial vehicle. Background Art

[0002] High-voltage overhead line fault indicator is a device specially installed on high-voltage overhead lines. It is mainly used to detect and indicate grounding or short-circuit fault points in the line. The high-voltage line fault indicator is suitable for 6-35kV distribution overhead lines and can adapt to various grounding methods. It is suitable for overhead insulated and bare conductors 35mm 2 ~240mm 2 They have line load monitoring, short circuit fault, and ground fault indication functions, which can help line finders quickly find the fault point, shorten power outage time, improve power supply reliability, and can be disassembled under power.

[0003] During the installation process of the existing fault indicator, the fault indicator needs to be placed inside the installation bracket. During the process of fixing the fault indicator, the user not only has to resist the elastic force of the return spring inside the installation bracket, but also has to resist the elastic force of the torsion spring on the fault indicator. This is extremely inconvenient during installation and requires the assistance of others, which greatly increases the difficulty and time of fixing. Summary of the invention

[0004] The purpose of this section is to summarize some aspects of embodiments of the present invention and briefly introduce some preferred embodiments. Some simplifications or omissions may be made in this section and the specification abstract and the invention title of this application to avoid blurring the purpose of this section, the specification abstract and the invention title, and such simplifications or omissions cannot be used to limit the scope of the present invention.

[0005] In view of the above problems or problems existing in the prior art, the present invention is proposed.

[0006] Therefore, the purpose of the present invention is to provide a support frame device for installing a fault indicator on a drone, which support frame device can not only be installed on the drone but also can play a fixing effect on the fault indicator when the fault indicator is connected to the support frame. In this way, the fault indicator can be connected to the support frame with one person operating, which greatly improves work efficiency and reduces operation difficulty.

[0007] In order to solve the above technical problems, the present invention provides the following technical solutions: a support frame device for installing a fault indicator on an unmanned aerial vehicle, which includes a support unit, the support unit includes a mounting member, a placing member arranged on the top of the mounting member, a limiting member arranged on both sides of the placing member, an adjusting member threadedly connected to the limiting member, a locking member arranged at one end of the adjusting member, and a stop member arranged inside the locking member.

[0008] As a preferred solution of the support frame device for installing a fault indicator on a drone of the present invention, the mounting member includes a mounting seat, two groups of first threaded holes are opened on the top of the mounting seat, and a support rod fixedly connected to the top of the mounting seat.

[0009] As a preferred solution of the support frame device for installing a fault indicator on a UAV of the present invention, the placement member includes a connecting pipe threadedly connected to the support rod, and a placement tube fixedly connected to the connecting pipe.

[0010] As a preferred solution of the support frame device for installing a fault indicator on a drone of the present invention, the limiting member includes a group of concave brackets fixedly connected to the outside of the placement tube, and a rotatable connection buckle on the outer wall of the concave bracket.

[0011] As a preferred solution of the support frame device for installing a fault indicator on the drone of the present invention, the adjusting part includes a threaded rod threadedly connected to the concave bracket, a turntable is fixedly installed at one end of the threaded rod, a T-shaped limit groove is opened at the other end of the threaded rod, a connecting rod rotatably connected to the threaded rod, a limit plate is fixedly installed at one end of the connecting rod, and a limit block is fixedly installed at the other end of the connecting rod.

[0012] As a preferred solution of the support frame device for installing a fault indicator on the drone of the present invention, the locking member includes a card plate connected to the limit block, a first arc-shaped buckle is fixedly installed on the outer side of the card plate, a limit hole is opened on one side of the card plate, positioning rods are fixedly installed on both sides of the limit hole, and limiting strips are fixedly installed on the outer side of the positioning rod.

[0013] As a preferred solution of the support frame device for installing a fault indicator on the drone of the present invention, the stopper includes a second arc-shaped buckle arranged on the top of the limit block, the second arc-shaped buckle is connected to the reset spring, the other end of the reset spring is connected to the first arc-shaped buckle, mounting holes are opened on both sides of the limit block, and arc-shaped grooves are opened on both sides of the limit block with the center of the mounting hole as the center.

[0014] As a preferred solution of the support frame device for installing a fault indicator on a UAV of the present invention, the positioning rod is embedded in the installation hole, and the limiting bar is slidably installed in the arc-shaped groove.

[0015] As a preferred solution of the support frame device for installing a fault indicator on a UAV of the present invention, the connecting rod and the limiting plate are rotatably installed inside the T-shaped limiting groove.

[0016] As a preferred solution of the support frame device for installing a fault indicator on a drone of the present invention, the width of the limiting hole is adapted to the width of the limiting block, the height of the limiting hole is greater than the height of the limiting block, and one end of the limiting block is arranged in an arc shape.

[0017] The beneficial effects of the present invention are as follows: the present invention enables the device to be connected to the drone through the setting of the mounting parts, and at the same time, the setting of the adjusting parts, the locking parts and the stop parts can have a fixing effect on the fault indicator. During the initial installation process, the fault indicator can be fixed inside the placement part, which further facilitates the operator to open the fault indicator to complete the subsequent installation, greatly improving the installation efficiency, reducing the waste of human resources, and improving the installation efficiency. BRIEF DESCRIPTION OF THE DRAWINGS

[0018] In order to more clearly illustrate the technical solutions of the embodiments of the present invention, the following briefly introduces the drawings required for describing the embodiments. Obviously, the drawings described below are only some embodiments of the present invention. For ordinary technicians in this field, other drawings can be obtained based on these drawings without creative labor. Among them:

[0019] Figure 1 Schematic diagram of the overall structure of the support frame device for installing a fault indicator for a UAV.

[0020] Figure 2 Schematic diagram of the limiter structure of the support frame device for installing a fault indicator on a UAV.

[0021] Figure 3 Schematic diagram of the stopper structure of the support frame device for installing a fault indicator for a UAV.

[0022] Figure 4 A cross-sectional view of the adjustment components of a support frame assembly for installing a fault indicator on an unmanned aerial vehicle. DETAILED DESCRIPTION

[0023] In order to make the above-mentioned objects, features and advantages of the present invention more obvious and easy to understand, the specific implementation methods of the present invention are described in detail below in conjunction with the accompanying drawings.

[0024] In the following description, many specific details are set forth to facilitate a full understanding of the present invention, but the present invention may also be implemented in other ways different from those described herein, and those skilled in the art may make similar generalizations without violating the connotation of the present invention. Therefore, the present invention is not limited to the specific embodiments disclosed below.

[0025] Secondly, the term "one embodiment" or "embodiment" as used herein refers to a specific feature, structure, or characteristic that may be included in at least one implementation of the present invention. The term "in one embodiment" that appears in different places in this specification does not necessarily refer to the same embodiment, nor does it refer to a separate or selective embodiment that is mutually exclusive with other embodiments.

[0026] Example 1

[0027] Reference Figures 1-2 , which is the first embodiment of the present invention, and this embodiment provides a support frame device for installing a fault indicator on a drone, which includes a support unit 100, and the support unit 100 includes a mounting member 101, a placement member 102 arranged on the top of the mounting member 101, a limiting member 103 arranged on both sides of the placement member 102, an adjusting member 104 threadedly connected to the limiting member 103, a locking member 105 arranged at one end of the adjusting member 104, and a stopper 106 arranged inside the locking member 105.

[0028] Furthermore, the mounting member 101 includes a mounting seat 101a, a top of the mounting seat 101a is provided with two groups of first threaded holes 101b, and a support rod 101c fixedly connected to the top of the mounting seat 101a.

[0029] Furthermore, the placement member 102 includes a connection tube 102a threadedly connected to the support rod 101c, and a placement tube 102b fixedly connected to the connection tube 102a.

[0030] Furthermore, the limiting member 103 includes a group of concave brackets 103a fixedly connected to the outer side of the placement tube 102b, and a rotatable connection buckle 103b on the outer wall of the concave bracket 103a.

[0031] Preferably, the mounting base 101a cooperates with the first threaded hole 101b set on the top and cooperates with the bolt to install the mounting base 101a on the top of the drone. Furthermore, the height of the support rod 101c is greater than 30 cm, which can reduce the impact on the wings of the drone. At the same time, the threaded connection between the connecting tube 102a and the support rod 101c can quickly disassemble and install the placement tube 102b, and the setting of the buckle 103b can limit the spring buckle on the indicator.

[0032] Furthermore, the adjusting member 104 includes a threaded rod 104a threadedly connected to the concave bracket 103a, a turntable 104b is fixedly installed at one end of the threaded rod 104a, a T-shaped limit groove 104c is opened at the other end of the threaded rod 104a, a connecting rod 104d rotatably connected to the threaded rod 104a, a limit plate 104e is fixedly installed at one end of the connecting rod 104d, and a limit block 104f is fixedly installed at the other end of the connecting rod 104d.

[0033] Furthermore, the locking member 105 includes a card plate 105a connected to the limit block 104f, a first arc-shaped buckle 105b is fixedly installed on the outer side of the card plate 105a, a limiting hole 105c is opened on one side of the card plate 105a, positioning rods 105d are fixedly installed on both sides of the limiting hole 105c, and a limiting strip 105e is fixedly installed on the outer side of the positioning rod 105d.

[0034] It should be noted that the clamping plate 105a is tilted at a certain angle under the elastic action of the return spring 106b.

[0035] Furthermore, the stopper 106 includes a second arc-shaped buckle 106a arranged on the top of the limit block 104f, the second arc-shaped buckle 106a is connected to the return spring 106b, the other end of the return spring 106b is connected to the first arc-shaped buckle 105b, mounting holes 106c are provided on both sides of the limit block 104f, and arc-shaped grooves 106d are provided on both sides of the limit block 104f with the center of the mounting hole 106c as the center.

[0036] Preferably, the threaded rod 104a can be moved laterally in conjunction with the threaded connection with the concave bracket 103a, driving the limit block 104f set at one end to move laterally. At the same time, the limit block 104f drives the card plate 105a to move in the direction close to the fault indicator. The bottom of the card plate 105a fits against the top of the fault indicator, which has a limiting effect on the fault indicator. In this way, during the installation process, the user only needs to lift the spring buckle on the fault indicator, and there is no need to struggle to resist the force of the reset spring inside the bracket, which greatly improves work efficiency and increases stability during installation.

[0037] Furthermore, the positioning rod 105d is embedded in the installation hole 106c, and the limiting bar 105e is slidably installed in the arc-shaped groove 106d.

[0038] Furthermore, the connecting rod 104d and the limiting plate 104e are rotatably installed inside the T-shaped limiting groove 104c.

[0039] Furthermore, the width of the limiting hole 105c matches the width of the limiting block 104f, the height of the limiting hole 105c is greater than the height of the limiting block 104f, and one end of the limiting block 104f is configured to be arc-shaped.

[0040] When in use, when installing the fault indicator, the buckle 103b is pushed to the other side of the concave bracket 103a, and the turntable 104b is further rotated. The turntable 104b drives the threaded rod 104a to rotate, and the threaded rod 104a cooperates with the threaded connection with the concave bracket 103a to move toward the center position of the placement tube 102b. The limit block 104f is connected to the threaded rod 104a in a movable connection manner. When the threaded rod 104a rotates, it will not drive the limit block 104f to connect. After adjusting to a suitable position, stop rotating the turntable 104b, and further install the fault indicator into the placement tube 102b. During the downward movement of the fault indicator, the card plate 105a is squeezed, and the card plate 105a cooperates with the positioning rod 105d and the mounting hole 106c to form a lever effect. The limit bar 105e is The arc groove 106d rotates inside to limit the rotation angle of the card plate 105a, and the end of the card plate 105a that contacts the fault indicator moves toward the side away from the fault indicator. When the fault indicator is completely installed in the placement tube 102b, the card plate 105a is reset under the action of the reset spring 106b, and the bottom of the card plate 105a is stuck on the top of the fault indicator. The spring set on the top of the fault indicator is further picked up and connected with the buckle 103b to fix the fault indicator. The turntable 104b is further rotated in the opposite direction to reset the threaded rod 104a to its original position, and the placement tube 102b is further connected to the support rod 101c through the connecting tube 102a. The mounting seat 101a is further installed on the drone, and the fault indicator is sent to the sky by the drone, and the fault indicator is installed on the cable.

[0041] When removing the fault indicator installed on the cable, push the buckle 103b to the other side of the concave bracket 103a, and further rotate the turntable 104b. The turntable 104b drives the threaded rod 104a to rotate. The threaded rod 104a cooperates with the threaded connection with the concave bracket 103a to move toward the center position of the placement tube 102b. The limit block 104f is connected to the threaded rod 104a in a movable connection. When the threaded rod 104a rotates, it will not drive the limit block 104f to connect. After adjusting to a suitable position, stop rotating the turntable 104b, further connect the placement tube 102b with the support rod 101c through the connecting tube 102a, and further install the mounting seat 101a on the drone. The placement tube 102b is sent to a high altitude, and the placement tube 102b is connected with the fault indicator. The fault indicator is further inserted into the placement tube 102b through the lift of the drone. The fault indicator squeezes the card plate 105a during the downward movement. The card plate 105a cooperates with the positioning rod 105d and the installation hole 106c to form a lever effect. The end of the card plate 105a that contacts the fault indicator moves toward the side away from the fault indicator. When the fault indicator is completely installed in the placement tube 102b, the card plate 105a is reset under the action of the reset spring 106b, and the bottom of the card plate 105a is stuck on the top of the fault indicator. The drone is further rapidly descended to pull the fault indicator off the cable to complete the disassembly of the fault indicator.

[0042] In summary, the present invention enables the device to be connected to the drone through the setting of the mounting parts, and at the same time, the setting of the adjusting parts, locking parts and stop parts can have a fixing effect on the fault indicator. During the initial installation process, the fault indicator can be fixed inside the placement part, which further facilitates the operator to open the fault indicator to complete the subsequent installation, greatly improving the installation efficiency, reducing the waste of human resources, and improving the installation efficiency.

[0043] Importantly, it should be noted that the construction and arrangement of the present application shown in a plurality of different exemplary embodiments are only exemplary. Although only a few embodiments are described in detail in this disclosure, it should be readily understood by those who refer to this disclosure that many modifications are possible (e.g., the size, scale, structure, shape and proportion of various elements, as well as parameter values ​​(e.g., temperature, pressure, etc.), mounting arrangements, use of materials, color, directional changes, etc.) without substantially departing from the novel teachings and advantages of the subject matter described in the application. For example, the element shown as integrally formed can be composed of multiple parts or elements, the position of the element can be inverted or otherwise changed, and the nature or number or position of the discrete element can be changed or changed. Therefore, all such modifications are intended to be included in the scope of the present invention. The order or sequence of any process or method steps can be changed or reordered according to alternative embodiments. In the claims, any "device plus function" clause is intended to cover the structure of performing the function described herein, and is not only structurally equivalent but also equivalent structure. Without departing from the scope of the present invention, other replacements, modifications, changes and omissions can be made in the design, operating conditions and arrangement of the exemplary embodiments. Therefore, the invention is not limited to a specific embodiment, but extends to numerous modifications still falling within the scope of the appended claims.

[0044] Additionally, in order to provide a concise description of exemplary embodiments, all features of an actual embodiment (ie, those features that are not relevant to the best mode presently contemplated for carrying out the invention or those that are not relevant to implementing the invention) may not be described.

[0045] It will be appreciated that in the development of any actual implementation, as in any engineering or design project, numerous implementation-specific decisions may be made. Such a development effort may be complex and time-consuming, but will be a routine task of design, fabrication, and production for those of ordinary skill having the benefit of this disclosure without undue experimentation.

[0046] It should be noted that the above embodiments are only used to illustrate the technical solutions of the present invention rather than to limit it. Although the present invention has been described in detail with reference to the preferred embodiments, those skilled in the art should understand that the technical solutions of the present invention may be modified or replaced by equivalents without departing from the spirit and scope of the technical solutions of the present invention, which should all be included in the scope of the claims of the present invention.

Claims

1. A support frame device for installing a fault indicator on an unmanned aerial vehicle, characterized in that: include, A support unit (100), the support unit (100) comprising a mounting member (101), a placement member (102) arranged on the top of the mounting member (101), a limiting member (103) arranged on both sides of the placement member (102), an adjusting member (104) threadedly connected to the limiting member (103), a locking member (105) arranged at one end of the adjusting member (104), and a stopping member (106) arranged inside the locking member (105).

2. The support frame device for installing a fault indicator on an unmanned aerial vehicle according to claim 1, characterized in that: The mounting member (101) comprises a mounting seat (101a), the top of the mounting seat (101a) is provided with two groups of first threaded holes (101b), and a support rod (101c) fixedly connected to the top of the mounting seat (101a).

3. The support frame device for installing a fault indicator on an unmanned aerial vehicle according to claim 2, characterized in that: The placement member (102) comprises a connection tube (102a) threadedly connected to the support rod (101c), and a placement tube (102b) fixedly connected to the connection tube (102a).

4. The support frame device for installing a fault indicator on an unmanned aerial vehicle according to claim 3, characterized in that: The limiting member (103) comprises a group of concave brackets (103a) fixedly connected to the outside of the placement tube (102b), and a rotatable connection buckle (103b) on the outer wall of the concave bracket (103a).

5. The support frame device for installing a fault indicator on an unmanned aerial vehicle according to claim 4, characterized in that: The adjusting member (104) comprises a threaded rod (104a) threadedly connected to the concave bracket (103a), a rotating disk (104b) fixedly mounted on one end of the threaded rod (104a), a T-shaped limiting groove (104c) provided on the other end of the threaded rod (104a), a connecting rod (104d) rotatably connected to the threaded rod (104a), a limiting disk (104e) fixedly mounted on one end of the connecting rod (104d), and a limiting block (104f) fixedly mounted on the other end of the connecting rod (104d).

6. The support frame device for installing a fault indicator on an unmanned aerial vehicle according to claim 5, characterized in that: The locking member (105) comprises a card plate (105a) rotatably connected to the limit block (104f), a first arc-shaped buckle (105b) is fixedly installed on the outer side of the card plate (105a), a limit hole (105c) is provided on one side of the card plate (105a), positioning rods (105d) are fixedly installed on both sides of the limit hole (105c), and a limit strip (105e) is fixedly installed on the outer side of the positioning rod (105d).

7. The support frame device for installing a fault indicator on an unmanned aerial vehicle according to claim 6, characterized in that: The stopper (106) comprises a second arc-shaped buckle (106a) arranged on the top of the limit block (104f), the second arc-shaped buckle (106a) is connected to the reset spring (106b), the other end of the reset spring (106b) is connected to the first arc-shaped buckle (105b), both sides of the limit block (104f) are provided with mounting holes (106c), and both sides of the limit block (104f) are provided with arc-shaped grooves (106d) centered on the center of the mounting hole (106c).

8. The support frame device for installing a fault indicator on a drone according to any one of claims 6 to 7, characterized in that: The positioning rod (105d) is embedded in the installation hole (106c), and the limiting strip (105e) is slidably installed in the arc-shaped groove (106d).

9. The support frame device for installing a fault indicator on an unmanned aerial vehicle according to claim 6, characterized in that: The connecting rod (104d) and the limiting plate (104e) are rotatably mounted inside the T-shaped limiting groove (104c).

10. The support frame device for installing a fault indicator on an unmanned aerial vehicle according to claim 9, characterized in that: The width of the limiting hole (105c) is adapted to the width of the limiting block (104f), the height of the limiting hole (105c) is greater than the height of the limiting block (104f), and one end of the limiting block (104f) is arranged in an arc shape.

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