CN115604962A - Rapid disassembly and assembly structure of unmanned aerial vehicle interference unit and implementation method thereof - Google Patents
Rapid disassembly and assembly structure of unmanned aerial vehicle interference unit and implementation method thereof Download PDFInfo
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- 238000000034 method Methods 0.000 title claims abstract description 35
- 238000003825 pressing Methods 0.000 claims description 112
- 229910000831 Steel Inorganic materials 0.000 claims description 43
- 239000010959 steel Substances 0.000 claims description 43
- 238000009434 installation Methods 0.000 claims description 29
- 238000003780 insertion Methods 0.000 claims description 21
- 230000037431 insertion Effects 0.000 claims description 21
- 230000000694 effects Effects 0.000 claims description 9
- 230000002441 reversible effect Effects 0.000 claims description 8
- 230000000670 limiting effect Effects 0.000 claims description 6
- 230000000149 penetrating effect Effects 0.000 claims description 6
- 238000000926 separation method Methods 0.000 claims description 4
- 230000002337 anti-port Effects 0.000 claims description 2
- 230000002452 interceptive effect Effects 0.000 claims description 2
- 239000002699 waste material Substances 0.000 abstract description 5
- 230000007613 environmental effect Effects 0.000 abstract description 4
- 238000001125 extrusion Methods 0.000 description 5
- 230000006835 compression Effects 0.000 description 4
- 238000007906 compression Methods 0.000 description 4
- 230000002829 reductive effect Effects 0.000 description 3
- 102000014150 Interferons Human genes 0.000 description 1
- 108010050904 Interferons Proteins 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 238000002788 crimping Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
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- 238000012423 maintenance Methods 0.000 description 1
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- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05K—PRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
- H05K5/00—Casings, cabinets or drawers for electric apparatus
- H05K5/02—Details
- H05K5/0217—Mechanical details of casings
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02S—GENERATION OF ELECTRIC POWER BY CONVERSION OF INFRARED RADIATION, VISIBLE LIGHT OR ULTRAVIOLET LIGHT, e.g. USING PHOTOVOLTAIC [PV] MODULES
- H02S20/00—Supporting structures for PV modules
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- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05K—PRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
- H05K5/00—Casings, cabinets or drawers for electric apparatus
- H05K5/02—Details
- H05K5/0247—Electrical details of casings, e.g. terminals, passages for cables or wiring
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- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05K—PRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
- H05K7/00—Constructional details common to different types of electric apparatus
- H05K7/14—Mounting supporting structure in casing or on frame or rack
- H05K7/1401—Mounting supporting structure in casing or on frame or rack comprising clamping or extracting means
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Abstract
The invention discloses a quick disassembly and assembly structure of an Unmanned Aerial Vehicle (UAV) interference unit and an implementation method thereof, belonging to the technical field of UAV interference units. The quick dismounting structure of the unmanned aerial vehicle interference unit and the implementation method thereof effectively improve the service life, prolong the power supply time, greatly save electric energy, utilize new energy to supply power, save the cost, reduce the waste and improve the environmental protection efficiency.
Description
Technical Field
The invention relates to the technical field of unmanned aerial vehicle interferometers, in particular to a quick disassembly and assembly structure of an unmanned aerial vehicle interferon and an implementation method thereof.
Background
Along with the popularization of unmanned aerial vehicles, the problem that unmanned aerial vehicles fly black disturb airports is endless, the unmanned aerial vehicle interference unit forces the unmanned aerial vehicle to hover, automatically land or drive away the unmanned aerial vehicle through suppressing communication between the unmanned aerial vehicle and a remote controller, so that the safety of low-altitude airspace is guaranteed, the driving away and the forced landing are different, the two modes can interfere with a positioning system of the unmanned aerial vehicle, the driving away cannot influence the control of an unmanned aerial vehicle operator, and the forced landing completely cuts off the contact between the unmanned aerial vehicle and the operator.
Current unmanned aerial vehicle interference unit mounting structure is complicated, mostly is integral type mounting structure, wastes a large amount of time when needing to be changed or dismantling the unmanned aerial vehicle interference unit, also causes the damage of unmanned aerial vehicle interference unit easily after the dismantlement, can't accomplish to make things convenient for to carry out the dismouting fast.
Disclosure of Invention
The invention aims to provide a quick disassembly and assembly structure of an unmanned aerial vehicle interference unit and an implementation method thereof, which effectively prolong the service life, prolong the power supply time, greatly save electric energy, utilize new energy to supply power, save cost, reduce waste and improve the environmental protection efficiency.
In order to achieve the purpose, the invention provides the following technical scheme:
the utility model provides a quick assembly disassembly structure of unmanned aerial vehicle interference unit, includes the interference unit shell, the front end of interference unit shell is provided with the interfering signal delivery outlet, and the top of interference unit shell is provided with connects the extension board, connects extension board one end below and is provided with the grafting mounting panel, and in the mounting panel inserted to close and is provided with the fixing base, the locating plate was installed at the rear of fixing base, was connected by dismouting subassembly block between mounting panel and the fixing base, connect by the joint structural connection between extension board and the interference unit shell.
Furthermore, an inclined solar collector plate is mounted above the connecting support plate through a support rod, and the solar collector plate is conducted with a storage power supply inside the shell of the interference unit through a wire connector.
Further, the dismouting subassembly is including inserting groove, left joint subassembly, right joint subassembly and dismantlement subassembly, inserts the groove of closing and sets up in the fixing base, is provided with left joint subassembly and right joint subassembly in the fixing base of inserting groove interlude both sides respectively, and left joint subassembly and right joint subassembly tail end are connected with the dismantlement subassembly respectively, and left joint subassembly and right joint subassembly structure are the same and the symmetry sets up, and the mounting panel is inserted and is closed the setting and at the inslot of inserting.
Further, left side joint subassembly includes built-in groove, the joint post, ejecting spring and extension groove, built-in inslot interpolation closes and is provided with the joint post, be connected with ejecting spring on the joint post rear end, ejecting spring fixes the built-in inslot at joint post rear end, the extension groove has been seted up in the rear end extension of built-in groove, extension groove rear end and dismantlement subassembly intercommunication, joint post rear end is connected with the dismantlement subassembly, the front end upper side of joint post is seted up and is equipped with oblique type pressfitting face, the both sides end of mounting panel is provided with arc joint groove, arc joint groove respectively with the joint post activity joint of left joint subassembly and right joint subassembly.
Furthermore, the dismounting component comprises a left pressing rod, a right pressing rod, a transverse compression rod, a left pressing groove, a right pressing groove, a left linkage steel rope, a right linkage steel rope and a reset spring, wherein the left pressing groove and the right pressing groove are respectively arranged in the fixing base, the left pressing groove and the right pressing groove are respectively provided with the left pressing rod and the right pressing rod in an inserting manner, the left pressing groove and the right pressing groove are respectively provided with the reset spring, the reset springs in the left pressing groove and the right pressing groove are respectively connected with the bottom ends of the left pressing rod and the right pressing rod, the upper ends of the left pressing rod and the right pressing rod are connected through the transverse compression rod, the side ends of the left pressing rod and the right pressing rod are respectively connected with the left linkage steel rope and the right linkage steel rope, and the left linkage steel rope and the right linkage steel rope are respectively connected with the left clamping component and the right clamping component.
Furthermore, the side ends of the left pressing groove and the right pressing groove are respectively provided with an inclined groove communicated with the left clamping assembly and the right clamping assembly, and the left linkage steel rope and the right linkage steel rope respectively penetrate through the inclined grooves to be connected with the left clamping assembly and the right clamping assembly.
Further, the joint structure is including rotating the nut, inserting the post, inserting the hole, the joint piece, bar draw-in groove and sliding clamping groove, rotates the nut setting on connecting the extension board, and the below of rotating the nut is connected with inserts the post, and the bottom outside of inserting the post is provided with the joint piece, inserts the hole and sets up in the top of interference ware shell, sets up the bar draw-in groove that inserts the joint piece activity on the inner wall in inserting the hole, and the bottom extension of bar draw-in groove is provided with the sliding clamping groove with joint piece sliding clamping.
Furthermore, a hole groove used for penetrating the inserting-combining column is formed in the connecting support plate, the hole groove and the inserting-combining column are sleeved by a bearing, a limiting slot used for penetrating the inserting-combining column is formed in the inner wall of the bearing, and the inserting-combining column is in limiting insertion connection with the inner wall of the bearing.
The invention provides another technology, which comprises an implementation method of a quick disassembly and assembly structure of an unmanned aerial vehicle interference unit, and the implementation method comprises the following steps:
the method comprises the following steps: the rear part of the fixed seat is fixed at the installation position through the positioning plate, the interference device shell is inserted into the fixed seat for installation through the installation plate below the connecting support plate, and the inclined solar collector plate can store power for a power supply inside the interference device shell in the use process;
step two: when the connecting support plate and the mounting plate are required to be dismounted, the transverse pressing rod is extruded to drive the left pressing rod and the right pressing rod to press downwards, and in the process of pressing down the left pressing rod and the right pressing rod, the left linkage steel rope and the right linkage steel rope are driven to pull and pull, the clamping columns in the left clamping assembly and the right clamping assembly are pulled backwards and cannot be clamped with the arc-shaped clamping groove in the mounting plate, so that the connecting support plate and the mounting plate are lifted upwards and directly taken out to be dismounted;
step three: when the interference ware shell with be connected the extension board and dismantle, twist reverse rotation nut and drive and insert the post rotation, the joint piece slides in the sliding groove when the pivoted, when slide to with insert the hole counterpoint after, carry and draw the rotation nut and drive and insert post and joint piece and the separation of inserting the hole, make the interference ware shell with be connected the extension board split, during the installation, the block installation is carried out in the antiport, carries out the dismouting through the pivoted mode.
Further, to step one, when the mounting panel with insert the groove and insert when closing, the tip face of mounting panel bottom extrudees with the cooperation of the oblique pressfitting face of upper end before the joint post, drives the joint post and moves backward under the effect of pressure, makes the mounting panel pierce through the joint post and moves down, after arc joint groove and joint post counterpoint, under ejection spring's effect, joint post and arc joint groove joint are fixed.
Compared with the prior art, the invention has the beneficial effects that:
1. the invention provides a rapid disassembly and assembly structure of an unmanned aerial vehicle interference unit and an implementation method thereof, wherein an inclined solar collector plate is arranged above a connecting support plate through a support rod, the solar collector plate is conducted with a storage power supply in the interference unit shell through a lead connector, the rear part of a fixed seat is fixed at the installation position through a positioning plate, the interference unit shell is inserted and combined in the fixing base through the mounting panel of connecting the extension board below and is installed, and oblique type solar energy collecting plate can carry out the electric power storage to the inside power supply of interference unit shell in the use, effectively improves live time, and extension power supply time saves the electric energy greatly, utilizes the new forms of energy power supply, saves the cost, and the waste that reduces improves the environmental protection efficiency.
2. The invention provides a quick disassembly and assembly structure of an unmanned aerial vehicle interference device and an implementation method thereof.A slant-shaped pressing surface is arranged on the upper side of the front end of a clamping column, arc-shaped clamping grooves are arranged on the two side ends of a mounting plate and are movably clamped with the clamping columns of a left clamping assembly and a right clamping assembly respectively, when the mounting plate is inserted into the inserting grooves, a tip end surface of the bottom end of the mounting plate is matched with the slant-shaped pressing surface on the front upper end of the clamping column for extrusion, the clamping column is driven to move backwards under the action of pressure, so that the mounting plate penetrates through the clamping column to move downwards, and after the arc-shaped clamping grooves are aligned with the clamping column, the clamping column is clamped with the arc-shaped clamping grooves under the action of an ejection spring for fixing.
3. The invention provides a quick disassembly and assembly structure of an unmanned aerial vehicle interference device and an implementation method thereof.A diagonal groove communicated with a left clamping assembly and a right clamping assembly is respectively arranged at the side ends of a left pressing groove and a right pressing groove, a left linkage steel rope and a right linkage steel rope respectively penetrate through the diagonal groove to be connected with the left clamping assembly and the right clamping assembly, when disassembly is needed, a transverse compression bar is extruded to drive a left pressing rod and a right pressing rod to press downwards, the left linkage steel rope and the right linkage steel rope are driven to pull and pull in the process of pressing and pressing the left pressing rod and the right pressing rod downwards, clamping columns in the left clamping assembly and the right clamping assembly are pulled backwards and cannot be clamped with an arc-shaped clamping groove on a mounting plate, so that a connecting support plate and the mounting plate are lifted and directly taken out for disassembly, clamping is relieved by pressing downwards, the disassembly speed is greatly improved, the disassembly trouble is reduced, the use convenience is increased, and a reset spring can drive the whole pressing piece to automatically reset.
4. The invention provides a quick disassembly and assembly structure of an unmanned aerial vehicle interference unit and an implementation method thereof, wherein a sliding clamping groove in sliding clamping connection with a clamping block is arranged at the bottom end of a strip-shaped clamping groove in an extending mode, a hole groove used for penetrating an insertion column is formed in a connection support plate, the hole groove and the insertion column are sleeved through a bearing, a limiting slot penetrating the insertion column is formed in the inner wall of the bearing, the insertion column is in limiting insertion with the inner wall of the bearing, when an interference unit shell is disassembled from the connection support plate, a torsional rotating nut drives the insertion column to rotate, the clamping block slides in the sliding clamping groove while rotating, when the interference unit shell is aligned with the insertion hole, the rotating nut is lifted to drive the insertion column and the clamping block to be separated from the insertion hole, so that the interference unit shell is disassembled from the connection support plate, during installation, reverse rotation is carried out clamping installation, disassembly and assembly are carried out in a rotating mode, the interference unit shell is convenient to be disassembled independently, the convenience of disassembly and assembly is improved, the convenience of the interference unit is effectively and assembly for independent replacement or maintenance of the interference unit, and the practicability is increased.
Drawings
FIG. 1 is a schematic view of the overall structure of the present invention;
FIG. 2 is an exploded view of the overall structure of the present invention;
FIG. 3 is a sectional view of the structure of the removable assembly of the present invention;
FIG. 4 is an enlarged view taken at A of FIG. 3 according to the present invention;
FIG. 5 is a half sectional view of the mounting plate insertion structure of the present invention;
FIG. 6 is a cross-sectional view of the structure of the detachment assembly of the present invention;
FIG. 7 is an exploded view of the clamping structure of the present invention;
FIG. 8 is a partial cross-sectional view of the clamping structure of the present invention.
In the figure: 1. an interferer housing; 11. an interference signal output port; 12. connecting the support plate; 121. a solar collector panel; 13. mounting a plate; 131. an arc-shaped clamping groove; 2. a fixed seat; 21. positioning a plate; 3. disassembling and assembling the components; 31. a plugging groove; 32. a left clamping component; 321. a built-in groove; 322. a clamping column; 323. ejecting a spring; 324. an extension groove; 33. a right clamping component; 34. disassembling the assembly; 341. a left press fit rod; 342. a right press fit rod; 343. a transverse compression bar; 344. a left press fit groove; 345. a right crimping slot; 346. a left linkage steel rope; 347. a right linkage steel rope; 348. a return spring; 4. a clamping structure; 41. rotating the nut; 42. a plug-in post; 43. inserting and combining holes; 44. a clamping block; 45. a strip-shaped clamping groove; 46. a sliding slot.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Referring to fig. 1-2, a fast dismounting structure of an unmanned aerial vehicle jammer and an implementation method thereof include a jammer housing 1, a disturbing signal output port 11 is disposed at a front end of the jammer housing 1, a connecting support plate 12 is disposed above the jammer housing 1, a socket mounting plate 13 is disposed below one end of the connecting support plate 12, the mounting plate 13 is inserted into a fixing seat 2, a positioning plate 21 is mounted behind the fixing seat 2, the mounting plate 13 is connected with the fixing seat 2 in a clamping manner through a dismounting component 3, the connecting support plate 12 is connected with the jammer housing 1 through a clamping structure 4, an inclined solar collecting plate 121 is mounted above the connecting support plate 12 through a support rod, the solar collecting plate 121 is conducted with a storage power supply inside the jammer housing 1 through a wire connector, a position at which the rear side of the fixing seat 2 is fixed first through the positioning plate 21, the jammer housing 1 is mounted in the fixing seat 2 through the mounting plate 13 below the connecting support plate 12, and the inclined solar collecting plate can store power for the power supply inside the jammer housing 121 in a use process, thereby effectively increasing service time, greatly saving power, and reducing power supply cost.
Referring to fig. 3-5, the dismounting assembly 3 includes an insertion groove 31, a left clamping assembly 32, a right clamping assembly 33 and a dismounting assembly 34, the insertion groove 31 is disposed in the fixing base 2, the fixing base 2 at two sides of the middle section of the insertion groove 31 is respectively provided with the left clamping assembly 32 and the right clamping assembly 33, the tail ends of the left clamping assembly 32 and the right clamping assembly 33 are respectively connected with the dismounting assembly 34, the left clamping assembly 32 and the right clamping assembly 33 are identical in structure and symmetrically disposed, the mounting plate 13 is inserted and disposed in the insertion groove 31, the left clamping assembly 32 includes an inner groove 321, a clamping post 322, a push-out spring 323 and an extension groove 324, the clamping post 322 is inserted and disposed in the inner groove 321, the push-out spring 323 is connected to the rear end of the clamping post 322, the push-out spring 323 is fixed in the inner groove 321 at the rear end of the inner groove 321, the extension groove 324 is provided with the extension groove 324, the rear end of the clamping post 322 is communicated with the dismounting assembly 34, the front end of the clamping post 322 is provided with an oblique pressing surface, the arc-shaped clamping surface 131 of the mounting plate 13 is provided with the clamping post 131 and the movable clamping assembly 32 at two sides of the clamping post 322, when the mounting plate 13 is inserted into the insertion groove 31, the tip end surface of the bottom end of the mounting plate 13 is matched with the inclined pressing surface at the front upper end of the clamping column 322 for extrusion, the clamping post 322 is driven to move backwards under the action of pressure, so that the mounting plate 13 penetrates through the clamping post 322 to move downwards, when the arc-shaped clamping groove 131 is aligned with the clamping post 322, under ejecting spring 323's effect, joint post 322 and arc joint groove 131 joint are fixed, and the whole installation method is simple, can accomplish quick installation, and the fixity after the mode of both sides block improves the installation, and the mode dislocation increases stability in use.
Referring to fig. 6, the detaching assembly 34 includes a left pressing rod 341, a right pressing rod 342, a transverse pressing rod 343, a left pressing groove 344, a right pressing groove 345, a left linking steel cable 346, a right linking steel cable 347 and a return spring 348, the left pressing groove 344 and the right pressing groove 345 are respectively disposed in the fixing base 2, the left pressing groove 344 and the right pressing groove 345 are respectively inserted with the left pressing rod 341 and the right pressing rod 342, the return spring 348 is disposed in the left pressing groove 344 and the right pressing groove 345, the return spring 348 in the left pressing groove 344 and the right pressing groove 345 is respectively connected with the bottom ends of the left pressing rod 341 and the right pressing rod 342, the upper ends of the left pressing rod 341 and the right pressing rod 342 are connected by the transverse pressing rod 343, the side ends of the left pressing rod 341 and the right pressing rod 342 are respectively connected with the left linking steel cable 346 and the right linking steel cable 347, the left linking steel cable 346 and the right linking steel cable 347 are respectively connected with the left clamping assembly 32 and the right clamping assembly 33, the side ends of the left pressing groove 344 and the right pressing groove 345 are respectively provided with an inclined groove communicated with the left clamping component 32 and the right clamping component 33, the left linkage steel rope 346 and the right linkage steel rope 347 respectively penetrate through the inclined grooves to be connected with the left clamping component 32 and the right clamping component 33, when disassembly is needed, the transverse pressing rod 343 is extruded to drive the left pressing rod 341 and the right pressing rod 342 to press downwards, in the process of pressing the left pressing rod 341 and the right pressing rod 342 downwards, the left linkage steel rope 346 and the right linkage steel rope 347 are driven to pull and pull, the clamping columns 322 in the left clamping component 32 and the right clamping component 33 are pulled backwards and cannot be clamped with the arc-shaped clamping groove 131 on the mounting plate 13, so that the connecting support plate 12 and the mounting plate 13 are lifted upwards and directly taken out for disassembly, the clamping is removed in a downwards pressing mode, the disassembly speed is greatly improved, the disassembly trouble is reduced, and the use convenience is increased, the return spring 348 can drive the whole pressing piece to automatically return.
Referring to fig. 7-8, the locking structure 4 includes a rotating nut 41, an inserting post 42, an inserting hole 43, a locking block 44, a bar-shaped locking slot 45 and a sliding locking slot 46, the rotating nut 41 is disposed on the connecting support plate 12, the inserting post 42 is connected below the rotating nut 41, the locking block 44 is disposed on the outer side of the bottom end of the inserting post 42, the inserting hole 43 is disposed above the housing 1 of the jammer, the inner wall of the inserting hole 43 is disposed with the bar-shaped locking slot 45 movably inserted with the locking block 44, the sliding locking slot 46 slidably locked with the locking block 44 is extended from the bottom end of the bar-shaped locking slot 45, the connecting support plate 12 is disposed with a hole slot for the inserting post 42 to penetrate through, the hole slot is sleeved with the inserting post 42 by a bearing, the penetrable spacing slot of post 42 is offered in the bearing inner wall, insert and close post 42 and the spacing grafting of bearing inner wall, when interference ware shell 1 with connect the extension board 12 and dismantle, twist reverse rotation nut 41 and drive the rotation of inserting post 42, joint piece 44 slides in sliding groove 46 when the pivoted, after sliding to counterpoint with inserting hole 43, carry and pull rotation nut 41 and drive and insert post 42 and joint piece 44 and insert the separation of hole 43, make interference ware shell 1 and the split of connecting extension board 12, during the installation, reverse rotation carries out the block installation, carry out the dismouting through the pivoted mode, be convenient for interference ware shell 1 dismantles alone, improve the convenience of dismouting, effectively make things convenient for the interference ware to change alone or maintain, increase the practicality.
In order to better show the process of the rapid dismounting structure of the unmanned aerial vehicle jammer, the embodiment provides an implementation method of the rapid dismounting structure of the unmanned aerial vehicle jammer, which includes the following steps:
the method comprises the following steps: the rear part of the fixed seat 2 is fixed at the installation position through the positioning plate 21, the interference device shell 1 is inserted into the fixed seat 2 through the installation plate 13 below the connecting support plate 12 for installation, and the inclined solar collector plate 121 can store power for a power supply in the interference device shell 1 in the use process;
step two: when the connecting support plate 12 and the mounting plate 13 need to be lifted up and directly taken out for disassembly, the extrusion transverse pressure rod 343 drives the left pressing rod 341 and the right pressing rod 342 to press downwards, and in the process of pressing the left pressing rod 341 and the right pressing rod 342 downwards, the left linkage steel rope 346 and the right linkage steel rope 347 are driven to pull and pull, the clamping columns 322 in the left clamping assembly 32 and the right clamping assembly 33 are pulled backwards and cannot be clamped with the arc-shaped clamping groove 131 in the mounting plate 13;
step three: when the interference device shell 1 is detached from the connecting support plate 12, the rotating screw cap 41 is twisted to drive the inserting column 42 to rotate, the clamping block 44 slides in the sliding clamping groove 46 during rotation, and after the rotating screw cap 41 slides to be aligned with the inserting hole 43, the rotating screw cap 41 is pulled to drive the inserting column 42 and the clamping block 44 to be separated from the inserting hole 43, so that the interference device shell 1 is detached from the connecting support plate 12, during installation, the reverse rotation is performed for clamping installation, and the disassembly and the assembly are performed in a rotating mode.
In summary, the fast dismounting structure of the unmanned aerial vehicle jammer and the implementation method thereof provided by the invention are characterized in that an inclined solar collecting plate 121 is installed above a connecting support plate 12 through a support rod, the solar collecting plate 121 is conducted with a storage power supply inside a jammer housing 1 through a wire connector, the rear part of a fixed seat 2 is fixed at an installation position through a positioning plate 21, the jammer housing 1 is inserted into the fixed seat 2 through an installation plate 13 below the connecting support plate 12 for installation, and the inclined solar collecting plate 121 can store power of a power supply inside the jammer housing 1 in the using process, thereby effectively improving the service time, prolonging the power supply time, greatly saving electric energy, supplying power by using new energy, saving cost, reducing waste and improving the environmental protection efficiency, an inclined press-fit surface is arranged on the upper side of the front end of a clamp column 322, and arc-shaped clamp grooves 131 are arranged at the two side ends of the installation plate 13, the arc-shaped clamping groove 131 is movably clamped with the clamping posts 322 of the left clamping assembly 32 and the right clamping assembly 33 respectively, when the mounting plate 13 is inserted into the insertion groove 31, the tip end surface of the bottom end of the mounting plate 13 is matched with the inclined pressing surface at the front upper end of the clamping post 322 for extrusion, the clamping post 322 is driven to move backwards under the action of pressure, the mounting plate 13 penetrates through the clamping post 322 to move downwards, after the arc-shaped clamping groove 131 is aligned with the clamping post 322, the clamping post 322 is clamped with the arc-shaped clamping groove 131 under the action of the ejection spring 323 for fixation, the whole mounting method is simple, rapid mounting can be achieved, the fixity after mounting is improved in a two-side clamping mode, the mode is dislocated, the use stability is improved, inclined grooves communicated with the left clamping assembly 32 and the right clamping assembly 33 are formed at the side ends of the left pressing groove 344 and the right pressing groove 345 respectively, the left linkage steel rope 346 and the right linkage steel rope 347 penetrate through the inclined grooves respectively to be connected with the left clamping assembly 32 and the right clamping assembly 33, when the assembly needs to be disassembled, the extrusion transverse pressure lever 343 drives the left press-fit rod 341 and the right press-fit rod 342 to press downwards, and in the process of pressing down the left press-fit rod 341 and the right press-fit rod 342, the left linkage steel rope 346 and the right linkage steel rope 347 are driven to pull and pull, the clamping posts 322 in the left clamping assembly 32 and the right clamping assembly 33 are pulled backwards and can not be clamped with the arc-shaped clamping grooves 131 on the mounting plate 13, so that the connecting support plate 12 and the mounting plate 13 are lifted up and directly taken out for disassembly, the clamping position is removed by pressing down, the disassembly speed is greatly improved, the disassembly trouble degree is reduced, the use convenience is increased, the reset spring 348 can drive the whole press-fit piece to automatically reset, the bottom end of the strip-shaped clamping groove 45 is provided with the sliding clamping groove 46 which is in sliding clamping connection with the clamping block 44, and the connecting support plate 12 is provided with a hole groove for the insertion post 42 to penetrate through, hole groove and insert and to be cup jointed by the bearing between the post 42, the penetrable spacing slot of post 42 is offered to the bearing inner wall, insert and to close post 42 and the spacing grafting of bearing inner wall, when interference ware shell 1 with connect the extension board 12 and dismantle, it rotates to twist reverse rotation nut 41 and drive the rotation of insertion post 42, joint piece 44 slides in sliding groove 46 simultaneously in the pivoted, after sliding and inserting the hole 43 counterpoint with inserting, it drives insertion post 42 and joint piece 44 and the separation of inserting hole 43 to carry to pull rotation nut 41, make interference ware shell 1 and connect the extension board 12 split, during the installation, reverse rotation carries out the block installation, carry out the dismouting through the pivoted mode, be convenient for interference ware shell 1 dismantles alone, improve the convenience of dismouting, effectively make things convenient for the interference ware to change alone or maintain, increase the practicality.
The above description is only for the preferred embodiment of the present invention, but the scope of the present invention is not limited thereto, and any person skilled in the art should be able to cover the technical solutions and the inventive concepts of the present invention within the technical scope of the present invention.
Claims (10)
1. The utility model provides a quick assembly disassembly structure of unmanned aerial vehicle interference unit which characterized in that: including interference ware shell (1), the front end of interference ware shell (1) is provided with interfering signal delivery outlet (11), and the top of interference ware shell (1) is provided with connects extension board (12), connects extension board (12) one end below and is provided with grafting mounting panel (13), and in mounting panel (13) were inserted and are closed and are provided with fixing base (2), locating plate (21) were installed to the rear of fixing base (2), was connected by dismouting subassembly (3) block between mounting panel (13) and fixing base (2), be connected by joint structure (4) between connection extension board (12) and the interference ware shell (1).
2. The structure of claim 1, wherein the structure comprises: an inclined solar collector plate (121) is mounted above the connecting support plate (12) through a support rod, and the solar collector plate (121) is communicated with a storage power supply inside the interference device shell (1) through a wire connector.
3. The structure of claim 1, wherein the structure comprises: dismouting subassembly (3) are including inserting groove (31), left joint subassembly (32), right joint subassembly (33) and detaching assembly (34), insert groove (31) and set up in fixing base (2), insert and be provided with left joint subassembly (32) and right joint subassembly (33) in fixing base (2) of groove (31) interlude both sides respectively, left side joint subassembly (32) and right joint subassembly (33) tail end are connected with detaching assembly (34) respectively, left side joint subassembly (32) and right joint subassembly (33) the same and symmetry setting of structure, mounting panel (13) are inserted and are closed the setting and are being inserted and be closed in groove (31).
4. The structure of claim 3, wherein the structure comprises: left side joint subassembly (32) are including built-in groove (321), joint post (322), ejecting spring (323) and extension groove (324), it is provided with joint post (322) to close in built-in groove (321), be connected with ejecting spring (323) on joint post (322) rear end, ejecting spring (323) are fixed in built-in groove (321) of joint post (322) rear end, extension groove (324) have been seted up in the rear end extension of built-in groove (321), extension groove (324) rear end and dismantlement subassembly (34) intercommunication, joint post (322) rear end is connected with dismantlement subassembly (34), the side is opened on the front end of joint post (322) and is equipped with oblique type pressfitting face, the both sides end of mounting panel (13) is provided with arc joint groove (131), arc joint groove (131) respectively with the joint post (322) activity joint of left side joint subassembly (32) and right joint subassembly (33).
5. The structure of claim 3, wherein the structure comprises: the dismounting assembly (34) comprises a left pressing rod (341), a right pressing rod (342), a transverse pressing rod (343), a left pressing groove (344), a right pressing groove (345), a left linkage steel rope (346), a right linkage steel rope (347) and a return spring (348), the left pressing groove (344) and the right pressing groove (345) are respectively arranged in the fixing seat (2), the left pressing rod (341) and the right pressing groove (345) are respectively provided with the left pressing rod (342) and the right pressing rod (342) in an inserting and combining mode, the return spring (348) is respectively arranged in the left pressing groove (344) and the right pressing groove (345), the return spring (348) in the left pressing groove (344) and the right pressing groove (345) is respectively connected with the bottom ends of the left pressing rod (341) and the right pressing rod (342), the upper ends of the left pressing rod (341) and the right pressing rod (342) are connected through the transverse pressing rod (343), the side ends of the left pressing rod (341) and the right pressing rod (346) are respectively connected with the left linkage steel rope (347), and the right linkage steel rope (347) are respectively connected with the left linkage steel rope (347) and the right linkage steel rope (342), and the left linkage steel rope (33) are respectively connected with the left pressing rod (346).
6. The structure of claim 5, wherein the structure comprises: the side of left side pressfitting groove (344) and right pressfitting groove (345) is seted up respectively with left joint subassembly (32) and the oblique type groove of right joint subassembly (33) intercommunication, and left linkage steel cable (346) and right linkage steel cable (347) penetrate oblique type groove respectively and are connected with left joint subassembly (32) and right joint subassembly (33).
7. The structure of claim 1, wherein the structure comprises: joint structure (4) including rotating nut (41), insert and close post (42), insert and close hole (43), joint piece (44), bar draw-in groove (45) and sliding clamping groove (46), rotate nut (41) and set up on connecting extension board (12), the below of rotating nut (41) is connected with inserts and closes post (42), the bottom outside of inserting and closing post (42) is provided with joint piece (44), insert and close hole (43) and set up the top at interference ware shell (1), set up on the inner wall of inserting and close hole (43) and insert bar draw-in groove (45) that closes with joint piece (44) activity, the bottom extension of bar draw-in groove (45) is provided with sliding clamping groove (46) with joint piece (44) slip joint.
8. The structure of claim 7, wherein the structure comprises: the connecting support plate (12) is provided with a hole groove used for penetrating the inserting column (42), the hole groove and the inserting column (42) are sleeved by a bearing, the inner wall of the bearing is provided with a limiting slot used for penetrating the inserting column (42), and the inserting column (42) is in limiting insertion connection with the inner wall of the bearing.
9. The method of any one of claims 1-8, wherein the structure further comprises: the method comprises the following steps:
the method comprises the following steps: the rear part of the fixed seat (2) is fixed at an installation position through a positioning plate (21), the interference device shell (1) is inserted into the fixed seat (2) through an installation plate (13) below the connecting support plate (12) for installation, and the inclined solar collector plate (121) can store power for a power supply in the interference device shell (1) in the using process;
step two: when the connecting support plate needs to be disassembled, the transverse pressing rod (343) is extruded to drive the left pressing rod (341) and the right pressing rod (342) to press downwards, the left linkage steel rope (346) and the right linkage steel rope (347) are driven to pull and pull in the process that the left pressing rod (341) and the right pressing rod (342) press downwards, the clamping columns (322) in the left clamping assembly (32) and the right clamping assembly (33) are pulled backwards and cannot be clamped with the arc-shaped clamping groove (131) in the mounting plate (13), and therefore the connecting support plate (12) and the mounting plate (13) are lifted upwards and directly taken out for disassembly;
step three: when interference ware shell (1) is dismantled with connection extension board (12), twist reverse rotation nut (41) and drive and insert post (42) and rotate, joint piece (44) slide in sliding groove (46) during the pivoted, after sliding and inserting hole (43) counterpoint, carry and draw rotation nut (41) to drive and insert post (42) and joint piece (44) and insert hole (43) separation, make interference ware shell (1) and connection extension board (12) split, during the installation, the block installation is carried out in the antiport, carry out the dismouting through the pivoted mode.
10. The implementation method of the fast dismounting structure of the unmanned aerial vehicle disturber according to claim 9, characterized in that: step one, when mounting panel (13) and insert and close the groove (31) and insert the fashionable, the tip face of mounting panel (13) bottom extrudees with the cooperation of the oblique pressfitting face of upper end before joint post (322), drives joint post (322) retrogradation under the effect of pressure, makes mounting panel (13) pierce through joint post (322) and moves down, after arc joint groove (131) counterpoint with joint post (322), under the effect of ejecting spring (323), joint post (322) and arc joint groove (131) joint, fix.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202211410477.8A CN115604962A (en) | 2022-11-11 | 2022-11-11 | Rapid disassembly and assembly structure of unmanned aerial vehicle interference unit and implementation method thereof |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202211410477.8A CN115604962A (en) | 2022-11-11 | 2022-11-11 | Rapid disassembly and assembly structure of unmanned aerial vehicle interference unit and implementation method thereof |
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| CN202211410477.8A Pending CN115604962A (en) | 2022-11-11 | 2022-11-11 | Rapid disassembly and assembly structure of unmanned aerial vehicle interference unit and implementation method thereof |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN117240398A (en) * | 2023-11-10 | 2023-12-15 | 北京融合汇控科技有限公司 | Detachable unmanned aerial vehicle countering equipment |
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- 2022-11-11 CN CN202211410477.8A patent/CN115604962A/en active Pending
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN117240398A (en) * | 2023-11-10 | 2023-12-15 | 北京融合汇控科技有限公司 | Detachable unmanned aerial vehicle countering equipment |
| CN117240398B (en) * | 2023-11-10 | 2024-01-19 | 北京融合汇控科技有限公司 | Detachable unmanned aerial vehicle countering equipment |
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