CN218762328U - Reinforced structure of laser wind finding radar - Google Patents

Reinforced structure of laser wind finding radar Download PDF

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Publication number
CN218762328U
CN218762328U CN202223138589.0U CN202223138589U CN218762328U CN 218762328 U CN218762328 U CN 218762328U CN 202223138589 U CN202223138589 U CN 202223138589U CN 218762328 U CN218762328 U CN 218762328U
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China
Prior art keywords
groove
seat
support frame
connecting seat
block
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CN202223138589.0U
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Chinese (zh)
Inventor
高彬
陈昊
闫铁雷
章天亮
马燕
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China Power Investment Xinjiang Energy Chemical Group Hami Co ltd
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State Power Investment Group Xinjiang Energy Chemical Co ltd
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Priority to CN202223138589.0U priority Critical patent/CN218762328U/en
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Abstract

The utility model discloses a laser wind finding radar reinforcing structure, including the laser wind finding radar, the bottom of laser wind finding radar is equidistant to be provided with the reinforcement support frame, the bottom of laser wind finding radar is fixed with the fixing base, the end fixing of reinforcement support frame has the connecting seat, the bottom of reinforcement support frame is provided with the supporting seat, be provided with the supplementary counterpoint mechanism between fixing base and the connecting seat, the bottom of supporting seat is provided with anti-skidding mechanism; the utility model discloses a spread groove, connecting block, spacing groove, gag lever post, expanding spring and the operation piece of design can realize letting the quick interim spacing butt joint that carries on of reinforcement support frame and laser wind-finding radar, let locating hole and constant head tank can be accurate counterpoint simultaneously to it is fixed to use positioning screw to run through to twist, compares current technique, has made things convenient for greatly to carry out the dismouting work of consolidating to the laser wind-finding radar.

Description

Reinforced structure of laser wind finding radar
Technical Field
The utility model belongs to the technical field of laser anemometry radar consolidates, concretely relates to reinforced structure of laser anemometry radar.
Background
The laser wind measuring radar can measure wind direction and wind speed information 80 meters in front of the fan, can be integrated with a fan main control system, and can transmit the measured wind direction and wind speed information in front of the fan to a fan host control system in real time before wind reaches a wind wheel. The accurate yawing of the fan can be guaranteed by acquiring the accurate wind direction information, so that the generated energy of the fan is improved, the load on a key part is reduced, and when the laser wind measuring radar is required to be connected with the fan, the support frame is required to be used for connection and reinforcement.
Current laser wind finding radar consolidates the support frame when being connected with laser wind finding radar main part, generally close fixed connection through the bolt twist, at the in-process of consolidating the connection, owing to need to screw and the accurate counterpoint of mounting hole, but there is not any guide structure who assists the counterpoint, so only can finely tune the position of consolidating the support frame through manual many times, just can let screw and mounting hole align, consequently at the in-process of consolidating the connection, it is very troublesome, be difficult to quick dismouting reinforcement, for this we propose a laser wind finding radar's reinforced structure
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a reinforced structure of laser wind finding radar to solve this laser wind finding radar reinforced structure who provides in the above-mentioned background art and comparatively trouble problem when being connected with the radar main part.
In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides a reinforced structure of laser wind finding radar, includes the laser wind finding radar, the bottom equidistance of laser wind finding radar is provided with the reinforcement support frame, the bottom mounting of laser wind finding radar has the fixing base, the end fixing of reinforcement support frame has the connecting seat, the bottom of reinforcement support frame is provided with the supporting seat, be provided with supplementary counterpoint mechanism between fixing base and the connecting seat, the bottom of supporting seat is provided with anti-skidding mechanism, supplementary counterpoint mechanism includes:
the connecting component is arranged at the connecting position between the fixed seat and the connecting seat;
the limiting assembly is arranged at the top end of the connecting part opposite to the connecting part at the connecting part between the fixed seat and the connecting seat;
the guide assembly is arranged on the inner side of the limiting assembly;
the reset assembly is arranged inside the limiting assembly;
the operating assembly is arranged at the end part of the connecting seat;
the positioning assembly is arranged on the surface of the connecting seat and opposite to the two sides of the reinforcing support frame.
Preferably, coupling assembling includes that the equidistance is seted up at the spread groove of fixing base bottom and is fixed at the inboard connecting block of connecting seat, the connecting block is connected with the spread groove block.
Preferably, the limiting assembly comprises limiting grooves formed in the surface of the fixing seat at equal intervals and built-in grooves formed in the inner side of the connecting seat relative to the top end of the connecting block, limiting rods are arranged in the built-in grooves, and the limiting rods are connected with the built-in grooves in a clamping mode.
Preferably, the guide assembly comprises guide grooves symmetrically formed in two sides of the limiting rod and guide blocks symmetrically fixed on the inner wall of the built-in groove, and the guide blocks are connected with the guide grooves in a sliding mode.
Preferably, the reset assembly comprises a through groove which is formed in the surface of the limiting rod in a penetrating mode and a fixing block which is fixed inside the built-in groove and penetrates through the inside of the through groove, and an expansion spring is connected between the fixing block and the through groove.
Preferably, the operating assembly comprises an operating groove formed in the end of the connecting seat and connected with the built-in groove and an operating block arranged in the operating groove and fixedly connected with the limiting rod.
Preferably, the positioning assembly comprises positioning holes symmetrically formed in the surface of the fixing seat at equal intervals and positioning grooves symmetrically formed in the surface of the connecting seat and opposite to two sides of the reinforcing support frame in a penetrating mode, and positioning screws penetrating through the positioning grooves and connected with the positioning holes in a screwing mode are arranged on the surface of the connecting seat.
Preferably, the anti-skidding mechanism sets up the butt joint groove in the supporting seat bottom including setting up the rubber pad and the symmetry in the supporting seat bottom, the top symmetry of rubber pad is fixed with the butt joint piece, the butt joint piece is connected with butt joint groove block, the draw-in groove has been seted up to the bilateral symmetry of butt joint piece, the inner wall symmetry in butt joint groove is fixed with the buckle, the buckle is connected with the draw-in groove block.
Compared with the prior art, the beneficial effects of the utility model are that:
the utility model discloses a spread groove, connecting block, spacing groove, gag lever post, expanding spring and the operation piece of design can realize letting that reinforcement support frame and laser wind finding radar are quick carry on temporarily spacing butt joint, let locating hole and constant head tank can accurate errorless counterpoint simultaneously to it is fixed to use positioning screw to run through to twist, and the current technique of comparing has made things convenient for greatly to carry out reinforced (rfd) dismouting work to laser wind finding radar.
Drawings
Fig. 1 is a schematic view of the appearance structure of the present invention;
fig. 2 is an enlarged schematic view of the utility model at a in fig. 1;
FIG. 3 is a schematic view of the positioning hole structure of the present invention;
fig. 4 is an enlarged schematic view of the utility model at the point B in fig. 2;
fig. 5 is an enlarged schematic view of the present invention at C of fig. 1;
in the figure: 1. a laser wind radar; 2. reinforcing the support frame; 3. a fixed seat; 4. a connecting seat; 5. a supporting seat; 100. connecting grooves; 101. connecting blocks; 200. a limiting groove; 201. a built-in groove; 202. a limiting rod; 300. a guide groove; 301. a guide block; 400. a through groove; 401. a fixed block; 402. a tension spring; 500. an operation slot; 501. an operation block; 600. positioning holes; 601. positioning a groove; 602. positioning a screw rod; 700. a rubber pad; 701. a butt joint groove; 702. a butt joint block; 800. a card slot; 801. and (5) buckling.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
Example 1
Referring to fig. 1, the present invention provides a technical solution: the utility model provides a reinforced structure of laser wind finding radar, includes laser wind finding radar 1, the bottom equidistance of laser wind finding radar 1 is provided with reinforcement support frame 2, and laser wind finding radar 1's bottom welded fastening has fixing base 3, and reinforcement support frame 2's tip welded fastening has connecting seat 4, and reinforcement support frame 2's bottom is provided with twists the supporting seat 5 of connecting, is provided with supplementary counterpoint mechanism between fixing base 3 and the connecting seat 4, and the bottom of supporting seat 5 is provided with anti-skidding mechanism, and supplementary counterpoint mechanism includes:
the connecting component can connect the fixed seat 3 with the connecting seat 4, and is arranged at the connecting position between the fixed seat 3 and the connecting seat 4;
the limiting assembly can temporarily limit and fix the fixed seat 3 and the connecting seat 4, and is arranged at the top end of the connecting part, opposite to the connecting assembly, of the connecting position between the fixed seat 3 and the connecting seat 4;
the guide assembly can guide the limiting assembly and is arranged on the inner side of the limiting assembly;
the reset assembly can drive the limit assembly to reset and pop up, and is arranged inside the limit assembly;
the operating assembly can pull the limiting assembly to move and is arranged at the end part of the connecting seat 4;
the locating component can locate the fixing seat 3 and the connecting seat 4, and the locating component is arranged on the surface of the connecting seat 4 and opposite to the two sides of the reinforced support frame 2.
Example 2
Referring to fig. 1 to 4, the present invention provides a technical solution: the utility model provides a reinforced structure of laser wind finding radar, includes laser wind finding radar 1, the bottom equidistance of laser wind finding radar 1 is provided with reinforcement support frame 2, and laser wind finding radar 1's bottom welded fastening has fixing base 3, and reinforcement support frame 2's tip welded fastening has connecting seat 4, and reinforcement support frame 2's bottom is provided with twists the supporting seat 5 of connecting, is provided with supplementary counterpoint mechanism between fixing base 3 and the connecting seat 4, and the bottom of supporting seat 5 is provided with anti-skidding mechanism, and supplementary counterpoint mechanism includes:
the connecting component can connect the fixed seat 3 with the connecting seat 4, and is arranged at the connecting position between the fixed seat 3 and the connecting seat 4;
the limiting assembly can temporarily limit and fix the fixed seat 3 and the connecting seat 4, and is arranged at the top end of the connecting part, opposite to the connecting assembly, of the connecting position between the fixed seat 3 and the connecting seat 4;
the guide assembly can guide the limiting assembly and is arranged on the inner side of the limiting assembly;
the reset assembly can drive the limit assembly to reset and pop up, and is arranged inside the limit assembly;
the operating assembly can pull the limiting assembly to move and is arranged at the end part of the connecting seat 4;
the positioning assembly can position the fixing seat 3 and the connecting seat 4, and is arranged on the surface of the connecting seat 4 and opposite to the two sides of the reinforcing support frame 2.
In this embodiment, preferably, the connection assembly includes that the equidistance is seted up at the connecting groove 100 of fixing base 3 bottom and welded fastening is at the inboard connecting block 101 of connecting seat 4, is connected through connecting block 101 and connecting groove 100 block, can let fixing base 3 and connecting seat 4 dock.
In this embodiment, preferably, the limiting member includes limiting grooves 200 formed on the surface of the fixing base 3 at equal intervals and a built-in groove 201 formed inside the connecting base 4 opposite to the top end of the connecting block 101, and a limiting rod 202 is disposed inside the built-in groove 201, and the connecting base 4 can be temporarily fixed by engaging and connecting the limiting rod 202 with the built-in groove 201.
In this embodiment, preferably, the guide assembly includes guide grooves 300 symmetrically formed on both sides of the limiting rod 202 and guide blocks 301 symmetrically welded and fixed to the inner wall of the built-in groove 201, and the guide blocks 301 are slidably connected to the guide grooves 300, so as to guide the limiting rod 202.
In this embodiment, preferably, the subassembly that resets runs through the fixed block 401 that runs through the inside fixed block that runs through groove 400 that runs through on gag lever post 202 surface and welded fastening and run through the groove 400 inside in built-in groove 201, admittedly through fixed block 401 and run through groove 400 sliding connection, can drive gag lever post 202 and remove, is connected with expanding spring 402 between fixed block 401 and the groove 400 that runs through, can drive gag lever post 202 and reset and pop out.
In this embodiment, preferably, the operation assembly includes an operation groove 500 provided at the end of the connecting seat 4 and connected to the built-in groove 201 and an operation block 501 provided inside the operation groove 500 and fixedly connected to the limiting rod 202 by welding, and the operation block 501 is pulled to drive the limiting rod 202 to move.
In this embodiment, preferably, the positioning assembly includes positioning holes 600 symmetrically formed in the surface of the fixing base 3 at equal intervals and positioning grooves 601 symmetrically formed in the surface of the connecting base 4 opposite to the two sides of the reinforcing support frame 2, a positioning screw 602 penetrating through the inside of the positioning groove 601 and screwed into the positioning hole 600 is disposed on the surface of the connecting base 4, and the connecting base 4 can be fixed by screwing the positioning screw 602.
Example 3
Referring to fig. 1 to 5, the present invention provides a technical solution: anti-skidding mechanism is including setting up rubber pad 700 and the symmetry of 5 bottoms of supporting seats in the setting and seting up the butt joint groove 701 in 5 bottoms of supporting seats, and the top symmetry welded fastening of rubber pad 700 has butt joint piece 702, is connected through butt joint piece 702 and butt joint groove 701 block, can fix rubber pad 700, and draw-in groove 800 has been seted up to butt joint piece 702's bilateral symmetry, and butt joint groove 701's inner wall symmetry welded fastening has buckle 801, is connected through buckle 801 and draw-in groove 800 block, can fix butt joint piece 702.
The utility model discloses a theory of operation and use flow: when the utility model needs to reinforce and support the laser wind-measuring radar 1, the top end of the reinforcing support frame 2 is firstly jointed with the bottom end of the laser wind-measuring radar 1, so that the connecting seat 4 is connected with the bottom end of the fixed seat 3 in a sliding way, and the limiting rod 202 is extruded, the limiting rod 202 plays a guiding role in the surface sliding of the guide block 301 through the guide groove 300, and drives the penetrating groove 400 to extrude the expansion spring 402 to deform in the surface sliding of the fixed block 401, so that the limiting rod 202 can be retracted into the internal groove 201, and simultaneously drives the operating block 501 to withdraw from the internal part of the operating groove 500, so that the connecting block 101 is embedded into the connecting groove 100 in a sliding way, the connecting seat 4 is tightly jointed with the fixed seat 3, when the connecting block 101 is completely clamped with the connecting groove 100, the internal groove 201 is aligned with the limiting groove 200, at this moment, the limiting rod 202 is popped out from the inside of the built-in groove 201 to be clamped into the inside of the limiting groove 200 under the action of the expansion spring 402, so that the connecting seat 4 can be temporarily limited, the positioning hole 600 is accurately aligned with the positioning groove 601, then the positioning screw 602 inside the positioning groove 601 is screwed, the positioning screw 602 is screwed with the positioning hole 600 to be fixedly connected, the reinforcing support frame 2 can be connected with the laser wind-measuring radar 1, so that the reinforcing support effect is achieved, when the supporting seat 5 needs to have the anti-slip effect, the rubber pad 700 is firstly attached to the bottom end of the supporting seat 5, the butt joint block 702 is embedded into the butt joint groove 701, the clamping groove 800 is connected with the clamping buckle 801 in an extruding and clamping manner, the rubber pad 700 can be fixed and limited, and the supporting seat 5 can be more stably supported.
Although embodiments of the present invention have been shown and described (with particularity and detail in the foregoing description), it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.

Claims (8)

1. The utility model provides a reinforced structure of laser wind finding radar, includes laser wind finding radar (1), the bottom equidistance of laser wind finding radar (1) is provided with consolidates support frame (2), the bottom mounting of laser wind finding radar (1) has fixing base (3), the end fixing of consolidating support frame (2) has connecting seat (4), the bottom of consolidating support frame (2) is provided with supporting seat (5), its characterized in that: be provided with supplementary counterpoint mechanism between fixing base (3) and connecting seat (4), the bottom of supporting seat (5) is provided with anti-skidding mechanism, supplementary counterpoint mechanism includes:
the connecting component is arranged at the connecting position between the fixed seat (3) and the connecting seat (4);
the limiting assembly is arranged at the top end of the connecting part corresponding to the connecting part at the connecting part between the fixed seat (3) and the connecting seat (4);
the guide assembly is arranged on the inner side of the limiting assembly;
the reset assembly is arranged inside the limiting assembly;
an operating assembly arranged at the end of the connecting seat (4);
the positioning components are arranged on two sides of the surface of the connecting seat (4) relative to the reinforcing support frame (2).
2. The reinforcement structure of a lidar according to claim 1, wherein: coupling assembling includes that equidistance sets up in connecting groove (100) of fixing base (3) bottom and fixes connecting block (101) at connecting seat (4) inboard, connecting block (101) are connected with connecting groove (100) block.
3. The reinforcement structure of a lidar according to claim 1, wherein: the limiting assembly comprises limiting grooves (200) which are formed in the surface of the fixing seat (3) at equal intervals and built-in grooves (201) which are formed in the inner side of the connecting seat (4) and opposite to the top end of the connecting block (101), limiting rods (202) are arranged in the built-in grooves (201), and the limiting rods (202) are connected with the built-in grooves (201) in a clamping mode.
4. The reinforcement structure of a lidar according to claim 1, wherein: the guide assembly comprises guide grooves (300) symmetrically formed in two sides of the limiting rod (202) and guide blocks (301) symmetrically fixed on the inner wall of the built-in groove (201), and the guide blocks (301) are connected with the guide grooves (300) in a sliding mode.
5. The reinforcement structure of a lidar according to claim 1, wherein: the reset assembly comprises a through groove (400) which penetrates through the surface of the limiting rod (202) and a fixed block (401) which is fixed inside the built-in groove (201) and penetrates through the inside of the through groove (400), and a telescopic spring (402) is connected between the fixed block (401) and the through groove (400).
6. The reinforcement structure of a lidar according to claim 1, wherein: the operation assembly comprises an operation groove (500) which is arranged at the end part of the connecting seat (4) and connected with the built-in groove (201) and an operation block (501) which is arranged in the operation groove (500) and fixedly connected with the limiting rod (202).
7. The reinforcement structure of a lidar according to claim 1, wherein: the positioning assembly comprises positioning holes (600) symmetrically formed in the surface of the fixing seat (3) at equal intervals and positioning grooves (601) symmetrically formed in the surface of the connecting seat (4) and opposite to the two sides of the reinforcing support frame (2), and positioning screws (602) penetrating through the inner portions of the positioning grooves (601) and connected with the positioning holes (600) in a screwed mode are arranged on the surface of the connecting seat (4).
8. The reinforcement structure of a lidar according to claim 1, wherein: anti-skidding mechanism sets up butt joint groove (701) in supporting seat (5) bottom including setting up rubber pad (700) and the symmetry in supporting seat (5) bottom, the top symmetry of rubber pad (700) is fixed with butt joint piece (702), butt joint piece (702) are connected with butt joint groove (701) block, draw-in groove (800) have been seted up to the bilateral symmetry of butt joint piece (702), the inner wall symmetry of butt joint groove (701) is fixed with buckle (801), buckle (801) are connected with draw-in groove (800) block.
CN202223138589.0U 2022-11-25 2022-11-25 Reinforced structure of laser wind finding radar Active CN218762328U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202223138589.0U CN218762328U (en) 2022-11-25 2022-11-25 Reinforced structure of laser wind finding radar

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202223138589.0U CN218762328U (en) 2022-11-25 2022-11-25 Reinforced structure of laser wind finding radar

Publications (1)

Publication Number Publication Date
CN218762328U true CN218762328U (en) 2023-03-28

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ID=85675648

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202223138589.0U Active CN218762328U (en) 2022-11-25 2022-11-25 Reinforced structure of laser wind finding radar

Country Status (1)

Country Link
CN (1) CN218762328U (en)

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Effective date of registration: 20240103

Address after: Floor 6 and 7, building 1, Hanlin Huayuan, No.17, Hanlin Road, Yizhou District, Hami City, Xinjiang Uygur Autonomous Region 839000

Patentee after: China Power Investment Xinjiang energy chemical group Hami Co.,Ltd.

Address before: 830000 Oriental Wisdom Park, No. 559, Kashi East Road, High-tech Zone (New Urban Area), Urumqi, Xinjiang Uygur Autonomous Region

Patentee before: State Power Investment Group Xinjiang Energy Chemical Co.,Ltd.

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