CN217554208U - Quick detection device of many rotor unmanned aerial vehicle precision parts - Google Patents

Quick detection device of many rotor unmanned aerial vehicle precision parts Download PDF

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Publication number
CN217554208U
CN217554208U CN202221504091.9U CN202221504091U CN217554208U CN 217554208 U CN217554208 U CN 217554208U CN 202221504091 U CN202221504091 U CN 202221504091U CN 217554208 U CN217554208 U CN 217554208U
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China
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fixedly connected
clamping mechanism
fixed plate
splint
threaded rod
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CN202221504091.9U
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Chinese (zh)
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杨联明
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Shenzhen Jinchangxing Precision Machinery Co ltd
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Shenzhen Jinchangxing Precision Machinery Co ltd
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Abstract

The utility model discloses a quick detection device of accurate spare part of many rotor unmanned aerial vehicle, comprises an operation bench, the equal fixedly connected with supporting leg in operation panel lower extreme four corners, operation panel upper end left part fixedly connected with left fixed plate, operation panel upper end right part fixedly connected with right fixed plate, the common swing joint of right side fixed plate and left fixed plate has the threaded rod, the common swing joint of left side fixed plate and right fixed plate has spacing slide bar, spacing slide bar is located the threaded rod lower part, threaded rod surface left part threaded connection has left clamping mechanism, threaded rod surface right part threaded connection has right clamping mechanism, left side clamping mechanism and right clamping mechanism structural similarity, left side clamping mechanism and right clamping mechanism are common with spacing slide bar sliding connection. A many rotor unmanned aerial vehicle precision parts short-term test device, fixed efficient, accomodate effectually, stability is high, is fit for the use that the precision parts of unmanned aerial vehicle detected.

Description

Quick detection device of accurate spare part of many rotor unmanned aerial vehicle
Technical Field
The utility model relates to an unmanned air vehicle technique field, in particular to accurate spare part short-term test device of many rotor unmanned aerial vehicle.
Background
Unmanned aerial vehicle can divide into fixed wing formula according to flight characteristics, types such as rotor wing formula and flapping wing formula unmanned aerial vehicle, wherein miniature rotor wing unmanned aerial vehicle has the volume less, moreover, the steam generator is simple in structure, characteristics such as control is more nimble, can take off and land perpendicularly, hover freely, can also adapt to various natural environment, possess advantages such as autonomic flight and landing ability, can operate in some complex and dangerous environment that are unsuitable human to get into, in recent years, scientific research institution, government agency, broadcast media, personal application and military field all have more and more important application, at least following drawback in the inside spare part of unmanned aerial vehicle detects the maintenance process: 1. the existing quick detection device for the parts is inconvenient for placing tool screws and the like for detection and maintenance, and is often scattered and placed on a table top, so that the maintenance efficiency is reduced; 2. current spare part short-term test device is not convenient for press from both sides tightly not unidimensional spare part, so, we release a many rotor unmanned aerial vehicle precision parts short-term test device.
SUMMERY OF THE UTILITY MODEL
The utility model discloses a main aim at provides a many rotor unmanned aerial vehicle precision parts short-term test device, can effectively solve the problem in the background art.
In order to achieve the above purpose, the utility model adopts the following technical scheme:
the utility model provides a quick detection device of accurate spare part of many rotor unmanned aerial vehicle, includes the operation panel, the equal fixedly connected with supporting leg in operation panel lower extreme four corners, operation panel upper end left part fixedly connected with left fixed plate, operation panel upper end right part fixedly connected with right fixed plate, the common swing joint of right side fixed plate and left fixed plate has the threaded rod, the common swing joint of left side fixed plate and right fixed plate has spacing slide bar, spacing slide bar is located the threaded rod lower part, threaded rod surface left part threaded connection has left clamping mechanism, threaded rod surface right part threaded connection has right clamping mechanism, left side clamping mechanism and right clamping mechanism structure are the same, left side clamping mechanism and right clamping mechanism jointly with spacing slide bar sliding connection, operation panel upper end rear portion fixedly connected with strorage device.
Preferably, the left clamping mechanism comprises a movable plate, a threaded hole is formed in the middle of the right end of the movable plate, a perforation is formed in the lower portion of the right end of the movable plate, a fixing frame is inserted and movably connected to the upper portion of the right end of the movable plate, a limiting screw is connected to the front end of the movable plate in a threaded mode, a connecting column is fixedly connected to the upper end of the fixing frame, and a supporting frame is fixedly connected to the upper portion of the outer surface of the connecting column.
Preferably, the support frame front end fixedly connected with No. three splint, no. two splint of support frame right-hand member fixedly connected with, no. one splint of support frame rear end fixedly connected with, no. four splint of support frame left end fixedly connected with, stop screw and mount contact.
Preferably, no. three splint cross sectional area are greater than No. four splint cross sectional areas, no. four splint cross sectional areas are greater than No. two splint cross sectional areas, no. two splint cross sectional areas are greater than No. one splint cross sectional area.
Preferably, the storage device comprises a mounting frame, an upper supporting plate is fixedly connected to the upper portion of the front end of the mounting frame, a storage box is fixedly connected to the middle of the front end of the mounting frame, a partition plate is fixedly connected to the rear inner wall of the storage box, and a lower supporting plate is fixedly connected to the lower portion of the front end of the mounting frame.
Preferably, the mounting frame is fixedly connected with the operating platform.
Compared with the prior art, the utility model discloses following beneficial effect has:
1. in the utility model, the left clamping mechanism and the right clamping mechanism are connected with the threaded rod together by the threaded rod, and the left clamping mechanism and the right clamping mechanism can be close to each other to clamp parts by rotating the threaded rod;
2. the utility model discloses in, through setting up the mounting plate on strorage device, can put the great instrument of volume, through setting up the receiver, and be fixed with the baffle in the receiver, can classify to parts for maintenance such as different screws and deposit, through setting up the bottom plate, can put debris to can avoid the maintenance apparatus to stack on the mesa, convenient to use.
Drawings
Fig. 1 is a schematic view of the overall structure of the device for rapidly detecting the precision parts of the multi-rotor unmanned aerial vehicle of the present invention;
fig. 2 is a schematic view of the overall structure of the left clamping mechanism of the rapid detection device for the precise components of the multi-rotor unmanned aerial vehicle of the present invention;
fig. 3 is a schematic view of the overall structure of the support frame of the device for rapidly detecting the precision parts of the multi-rotor unmanned aerial vehicle of the present invention;
fig. 4 is the utility model relates to a many rotor unmanned aerial vehicle precision parts short-term test device's strorage device overall structure schematic diagram.
In the figure: 1. an operation table; 2. supporting legs; 3. a storage device; 4. a right clamping mechanism; 5. a left clamping mechanism; 6. a left fixing plate; 7. a limiting slide bar; 8. a threaded rod; 9. a right fixing plate; 31. a mounting frame; 32. a partition plate; 33. a storage box; 34. a lower supporting plate; 35. an upper supporting plate; 51. moving the plate; 52. a limit screw; 53. a support frame; 54. connecting columns; 55. a fixed mount; 56. a threaded hole; 57. perforating; 531. a first clamp plate; 532. a second splint; 533. a third splint; 534. and a fourth splint.
Detailed Description
In order to make the technical means, creation features, achievement purposes and functions of the present invention easy to understand, the present invention is further described below with reference to the following embodiments.
In the description of the present invention, it should be noted that the terms "upper", "lower", "inner", "outer", "front end", "rear end", "both ends", "one end", "the other end" and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and simplification of description, but do not indicate or imply that the device or element to which the reference is made must have a specific orientation, be constructed in a specific orientation, and be operated, and thus, should not be construed as limiting the present invention. Furthermore, the terms "first" and "second" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.
In the description of the present invention, it is to be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "disposed," "connected," and the like are to be construed broadly, and for example, "connected" may be either fixedly connected or detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meaning of the above terms in the present invention can be understood as a specific case by those skilled in the art.
Examples
Referring to fig. 1-4, the present invention provides a technical solution:
the utility model provides a quick detection device of accurate spare part of many rotor unmanned aerial vehicle, including operation panel 1, the equal fixedly connected with supporting leg 2 in 1 lower extreme four corners of operation panel, 1 upper end left part fixedly connected with left fixed plate 6 of operation panel, 1 upper end right part fixedly connected with right fixed plate 9 of operation panel, the common swing joint of right fixed plate 9 and left fixed plate 6 has threaded rod 8, the common swing joint of left fixed plate 6 and right fixed plate 9 has spacing slide bar 7, spacing slide bar 7 is located 8 lower parts of threaded rod, 8 surface left parts of threaded rod threaded connection have left clamping mechanism 5, 8 surface right parts of threaded rod threaded connection have right clamping mechanism 4, left side clamping mechanism 5 is the same with right clamping mechanism 4 structure, left side clamping mechanism 5 and right clamping mechanism 4 are common with spacing slide bar 7 sliding connection, 1 upper end rear portion fixedly connected with strorage device 3 of operation panel.
In this embodiment, the left clamping mechanism 5 includes a moving plate 51, a threaded hole 56 is formed in the middle of the right end of the moving plate 51, a through hole 57 is formed in the lower part of the right end of the moving plate 51, a fixing frame 55 is movably inserted into the upper part of the right end of the moving plate 51, a limiting screw 52 is connected to the front end of the moving plate 51 in a threaded manner, a connecting column 54 is fixedly connected to the upper end of the fixing frame 55, and a support frame 53 is fixedly connected to the upper part of the outer surface of the connecting column 54; a third clamping plate 533 is fixedly connected to the front end of the supporting frame 53, a second clamping plate 532 is fixedly connected to the right end of the supporting frame 53, a first clamping plate 531 is fixedly connected to the rear end of the supporting frame 53, a fourth clamping plate 534 is fixedly connected to the left end of the supporting frame 53, and the limit screw 52 is in contact with the fixing frame 55; the cross section area of the third clamping plate 533 is larger than that of the fourth clamping plate 534, the cross section area of the fourth clamping plate 534 is larger than that of the second clamping plate 532, the cross section area of the second clamping plate 532 is larger than that of the first clamping plate 531, the rotary limiting screw 52 is in contact with the fixing frame 55, and the fixing frame 55 inserted at different positions can be fixed and limited.
In this embodiment, the storage device 3 includes a mounting frame 31, an upper support plate 35 is fixedly connected to the upper portion of the front end of the mounting frame 31, a storage box 33 is fixedly connected to the middle portion of the front end of the mounting frame 31, a partition plate 32 is fixedly connected to the rear inner wall of the storage box 33, and a lower support plate 34 is fixedly connected to the lower portion of the front end of the mounting frame 31; mounting bracket 31 and 1 fixed connection of operation panel, mounting plate 35 are preceding low back high structure, can be convenient for put the instrument, and the staff of being convenient for simultaneously looks over.
It should be noted that, the utility model relates to a quick detection device for precise components of multi-rotor unmanned aerial vehicle, in the using process, firstly, the threaded rod 8 is rotated, because the left part of the outer surface of the threaded rod 8 is a forward thread groove, and the right part of the outer surface of the threaded rod 8 is a reverse thread groove, so that when the threaded rod 8 is rotated, the left clamping mechanism 5 and the right clamping mechanism 4 are mutually close to each other and limited by the limiting slide bar 7, so that the left clamping mechanism 5 and the right clamping mechanism 4 can only mutually close to each other and mutually keep away from each other to slide, after mutual close, the components can be clamped through the second clamping plate 532, the first clamping plate 531, the third clamping plate 533 and the fourth clamping plate 534 on the left clamping mechanism 5 and the right clamping mechanism 4, because the sizes of the second clamping plate 532, the first clamping plate 531, the third clamping plate 533 and the fourth clamping plate 534 are different, can adapt to not unidimensional spare part and press from both sides tightly, when needs are to No. two splint 532, no. one splint 531, no. three splint 533 and No. four splint 534 adjust the use, insert the movable plate 51 with the different positions of mount 55 in, it is spacing fixed to rotate stop screw 52 again to mount 55, thereby can be to No. two splint 532, no. one splint 531, no. three splint 533 and No. four splint 534's position is adjusted, when detecting the completion needs deposit the instrument, because be provided with the layer board 35 on the strorage device 3, can put the great instrument of volume, through setting up receiver 33, can deposit parts such as screw, whole detection device fixed efficiency is high, accomodate effectually, stability is high, be fit for the use that the accurate spare part of unmanned aerial vehicle detected.
The basic principles and the main features of the invention and the advantages of the invention have been shown and described above. It will be understood by those skilled in the art that the present invention is not limited to the above embodiments, and that the foregoing embodiments and descriptions are provided only to illustrate the principles of the present invention without departing from the spirit and scope of the present invention. The scope of the invention is defined by the appended claims and equivalents thereof.

Claims (6)

1. The utility model provides a quick detection device of accurate spare part of many rotor unmanned aerial vehicle, includes operation panel (1), its characterized in that: the utility model discloses an operation panel, including operation panel, left fixed plate, right fixed plate, threaded rod (8) and left fixed plate (6), equal fixedly connected with supporting leg (2) in operation panel (1) lower extreme four corners, operation panel (1) upper end left part fixedly connected with left fixed plate (6), right fixed plate (9) and the common swing joint of left fixed plate (6) have threaded rod (8), the common swing joint of left fixed plate (6) and right fixed plate (9) has spacing slide bar (7), spacing slide bar (7) are located threaded rod (8) lower part, threaded rod (8) surface left part threaded connection has left clamping mechanism (5), threaded rod (8) surface right part threaded connection has right clamping mechanism (4), left side clamping mechanism (5) are the same with right clamping mechanism (4) structure, left side clamping mechanism (5) and right clamping mechanism (4) are common with spacing slide bar (7) sliding connection, operation panel (1) upper end rear portion fixedly connected with strorage device (3).
2. The device of claim 1, wherein the device comprises: left side clamping mechanism (5) are including movable plate (51), open at movable plate (51) right-hand member middle part has screw hole (56), open movable plate (51) right-hand member lower part has perforation (57), movable plate (51) right-hand member upper portion alternates swing joint and has mount (55), movable plate (51) front end threaded connection has stop screw (52), mount (55) upper end fixedly connected with spliced pole (54), spliced pole (54) surface upper portion fixedly connected with support frame (53).
3. The device of claim 2, wherein the device comprises: support frame (53) front end fixedly connected with No. three splint (533), support frame (53) right-hand member fixedly connected with No. two splint (532), support frame (53) rear end fixedly connected with splint (531), support frame (53) left end fixedly connected with No. four splint (534), stop screw (52) and mount (55) contact.
4. The device of claim 3, wherein the device comprises: the cross section area of the third splint (533) is larger than that of the fourth splint (534), the cross section area of the fourth splint (534) is larger than that of the second splint (532), and the cross section area of the second splint (532) is larger than that of the first splint (531).
5. The device of claim 1, wherein the device comprises: storage device (3) include mounting bracket (31), mounting bracket (31) front end upper portion fixedly connected with upper bracket board (35), mounting bracket (31) front end middle part fixedly connected with receiver (33), inner wall fixedly connected with baffle (32) behind receiver (33), mounting bracket (31) front end lower part fixedly connected with bottom plate (34).
6. The device of claim 5, wherein the device comprises: the mounting rack (31) is fixedly connected with the operating platform (1).
CN202221504091.9U 2022-06-15 2022-06-15 Quick detection device of many rotor unmanned aerial vehicle precision parts Active CN217554208U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202221504091.9U CN217554208U (en) 2022-06-15 2022-06-15 Quick detection device of many rotor unmanned aerial vehicle precision parts

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202221504091.9U CN217554208U (en) 2022-06-15 2022-06-15 Quick detection device of many rotor unmanned aerial vehicle precision parts

Publications (1)

Publication Number Publication Date
CN217554208U true CN217554208U (en) 2022-10-11

Family

ID=83501389

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202221504091.9U Active CN217554208U (en) 2022-06-15 2022-06-15 Quick detection device of many rotor unmanned aerial vehicle precision parts

Country Status (1)

Country Link
CN (1) CN217554208U (en)

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