CN216560986U - Airborne laser is controlling means for anemometry radar - Google Patents
Airborne laser is controlling means for anemometry radar Download PDFInfo
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- CN216560986U CN216560986U CN202123128442.9U CN202123128442U CN216560986U CN 216560986 U CN216560986 U CN 216560986U CN 202123128442 U CN202123128442 U CN 202123128442U CN 216560986 U CN216560986 U CN 216560986U
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02A—TECHNOLOGIES FOR ADAPTATION TO CLIMATE CHANGE
- Y02A90/00—Technologies having an indirect contribution to adaptation to climate change
- Y02A90/10—Information and communication technologies [ICT] supporting adaptation to climate change, e.g. for weather forecasting or climate simulation
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Abstract
The utility model discloses a control device for an airborne laser wind finding radar, which comprises a control device main body, wherein the front surface of the control device main body is provided with a mounting groove, a cover plate is arranged inside the mounting groove, the rear surface of the control device main body is provided with a rear mounting plate, two ends of the rear mounting plate are both provided with clamping grooves, and two sides of the rear surface of the control device main body are both provided with first grooves; through the first spring of internal design and the fixture block at first recess, and the internal design draw-in groove at rear mounting panel, can be through bolt with rear mounting panel fixed mounting in the cabin of radar test, the closed surface at rear mounting panel of controlling means main part makes the inside of fixture block embedding draw-in groove, loosen the shifting block, the effect that takes place elastic deformation in the inside of first recess through first spring sticiss the fixture block in the inside of draw-in groove, be convenient for with controlling means main part fastening installation, easily install and use, otherwise convenient to detach.
Description
Technical Field
The utility model belongs to the technical field of control devices, and particularly relates to a control device for an airborne laser wind finding radar.
Background
The existing control device is used for realizing the control of a certain object or certain objects, thereby ensuring the safe and reliable operation of controlled equipment, and has the main functions of: the device has the advantages of automatic control, protection, monitoring and measurement, convenient application to different devices for control and use, and easy operation and use; the existing control device is directly fixed and installed through a bolt when being installed, is complex in operation when being installed, and is inconvenient to assemble and disassemble, and the front surface cover plate of the control device is directly fixed and installed through a screw, so that the cover plate is inconvenient to assemble and disassemble quickly when the inside of the control device is damaged, and the problem of inconvenience in maintenance is solved.
SUMMERY OF THE UTILITY MODEL
The utility model aims to provide a control device for an airborne laser wind finding radar, and aims to solve the problems that the existing control device provided in the background art is directly fixedly installed through a bolt during installation, the operation is complex during installation, the disassembly and assembly operation is inconvenient, a cover plate on the front surface of the control device is directly fixedly installed through a bolt, the cover plate is inconvenient to disassemble and assemble quickly when the interior of the control device is damaged, and the maintenance is inconvenient.
In order to achieve the purpose, the utility model provides the following technical scheme: a control device for an airborne laser wind finding radar comprises a control device main body, wherein the front surface of the control device main body is provided with a mounting groove, a cover plate is arranged in the mounting groove, a rear mounting plate is arranged on the rear surface of the control device main body, the two ends of the rear mounting plate are both provided with clamping grooves, the two sides of the rear surface of the control device main body are both provided with first grooves, a first spring is fixedly arranged in the first groove through a screw, the end part of the first spring is elastically connected with a clamping block, the end part of the clamping block extends to the rear surface of the control device main body, the two sides of the upper surface of the control device main body are provided with shifting blocks, and the end part of the shifting block is screwed with the end part of the clamping block through a thread structure, and the first spring and the rear mounting plate are clamped and connected with the clamping groove through the clamping block.
Preferably, the card hole has all been seted up to the both sides of apron, the both sides of mounting groove are located the second recess has been seted up to the inside of controlling means main part, the kelly is installed to the inside block of second recess, the surface sliding connection of kelly has the slide, just the tip extension of slide extremely the inside of mounting groove, one side of slide is located the surface registrate of kelly installs the second spring, there is the card post one side of slide through screw fixed mounting, the pull ring is passed through to the opposite side of slide, just the slide with the apron passes through the card post with card hole block is connected.
Preferably, the outer surface of the sliding plate is in relative sliding connection with the outer surface of the clamping rod, and the sliding plate is elastically connected with the clamping rod through the second spring.
Preferably, the clamping hole and the cover plate are of an integrated structure, and the clamping column penetrates through the clamping hole.
Preferably, the clamping block is of an L-shaped structure, and the clamping block is elastically connected with the control device main body through the first spring.
Preferably, the end part of the clamping block is embedded into the clamping groove, and the end part of the clamping block is matched with the internal structure of the clamping groove.
Preferably, the cover plate is of a rectangular structure, and the cover plate is embedded in the mounting groove.
Compared with the prior art, the utility model has the beneficial effects that:
(1) through the first spring of internal design and fixture block at first recess, and the internal design draw-in groove at rearmounted mounting panel, can be through bolt with rearmounted mounting panel fixed mounting in the cabin of radar test, the closed surface at rearmounted mounting panel of controlling means main part makes the inside of fixture block embedding draw-in groove, loosen the shifting block, the effect that takes place elastic deformation through first spring in the inside of first recess sticiss the fixture block in the inside of draw-in groove, be convenient for with controlling means main part fastening installation, easily install and use, otherwise convenient to detach, it directly passes through bolt fixed mounting when having solved controlling means, complex operation when the installation, the inconvenient problem of dismouting operation.
(2) Through the tip design card post at the slide, and the tip design card hole at the apron, can be when long-time operation damages, the pulling pull ring, slide and card post for the card post breaks away from in the inside in card hole, be convenient for break away from the apron in the inside of mounting groove, the maintenance is conveniently dismantled, otherwise be convenient for install and use, the front surface apron of having solved controlling means directly passes through screw fixed mounting, quick assembly disassembly apron is not convenient for when controlling means's inside damages, the inconvenient problem of maintenance.
Drawings
FIG. 1 is a schematic structural view of the present invention;
FIG. 2 is a schematic structural diagram of a control device body, a cover plate and a rear mounting plate according to the present invention;
FIG. 3 is an enlarged view of portion A of FIG. 2 according to the present invention;
FIG. 4 is a schematic view of a partial structure of the dial block, the clamping block and the control device body according to the present invention;
FIG. 5 is an enlarged view of portion B of FIG. 2 according to the present invention;
in the figure: 1. shifting blocks; 2. a control device main body; 3. a cover plate; 4. mounting grooves; 5. a slide plate; 6. a pull ring; 7. a rear mounting plate; 8. a card slot; 9. a clamping block; 10. a first spring; 11. a first groove; 12. a clamping hole; 13. clamping the column; 14. a second groove; 15. a second spring; 16. and (5) clamping the rod.
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 to 5, the present invention provides a technical solution: a control device for an airborne laser wind finding radar comprises a control device main body 2, wherein a mounting groove 4 is formed in the front surface of the control device main body 2, a cover plate 3 is arranged inside the mounting groove 4, a rear mounting plate 7 is arranged on the rear surface of the control device main body 2, the control device main body is convenient to mount and use, clamping grooves 8 are formed in two ends of the rear mounting plate 7, clamping blocks 9 are easy to mount in a clamping mode, first grooves 11 are formed in two sides of the rear surface of the control device main body 2, first springs 10 are fixedly mounted inside the first grooves 11 through screws, the clamping blocks 9 are convenient to elastically connect and easy to tightly press and connect, clamping blocks 9 are elastically connected to the ends of the first springs 10, the clamping blocks are convenient to mount and dismount, the ends of the clamping blocks 9 extend to the rear surface of the control device main body 2, shifting blocks 1 are arranged on two sides of the upper surface of the control device main body 2, and the positions of the clamping blocks 9 are convenient to adjust, and the end part of the shifting block 1 is screwed with the end part of the clamping block 9 through a thread structure, and the first spring 10 and the rear mounting plate 7 are clamped with the clamping groove 8 through the clamping block 9, so that the control device main body 2 is convenient to disassemble and assemble in the engine room, and the operation is simpler.
In this embodiment, preferably, both sides of the cover plate 3 are provided with the fastening holes 12, both sides of the mounting groove 4 are located inside the control device main body 2 and are provided with the second grooves 14, the fastening rods 16 are installed inside the second grooves 14 in a fastened manner to facilitate sliding connection of the sliding plate 5, the sliding plate 5 is connected to the outer surface of the fastening rods 16 in a sliding manner to facilitate driving of the fastening posts 13 to connect, the end portion of the sliding plate 5 extends into the mounting groove 4, one side of the sliding plate 5 is located on the outer surface of the fastening rods 16 and is provided with the second springs 15 in a sleeved manner to facilitate elastic connection of the sliding plate 5 and facilitate pressing installation, the fastening posts 13 are fixedly installed on one side of the sliding plate 5 through screws to facilitate fastening installation, the pull rings 6 are installed on the other side of the sliding plate 5 through screws to facilitate pulling of the sliding plate 5, and the sliding plate 5 and the cover plate 3 are connected to the fastening holes 12 through the fastening posts 13 to facilitate dismounting and mounting the cover plate 3, the control device main body 2 is easy to maintain and convenient to repair when damaged.
In order to facilitate the installation with 5 elastic connection of slide, easily sticis, the surface relative sliding connection of slide 5 and kelly 16, and slide 5 passes through second spring 15 elastic connection with kelly 16, in order to facilitate the installation of the closed back fastening of apron 3, card hole 12 and 3 formula structures as an organic whole of apron, and card post 13 runs through in the inside of card hole 12, in order to with fixture block 9 elastic connection, be convenient for sticis fixed, fixture block 9 is L type structure, and fixture block 9 passes through first spring 10 elastic connection with controlling means main part 2, in order to facilitate the block installation, easy dismounting, the inside of the tip embedding draw-in groove 8 of fixture block 9, and the inside structure phase-match of the tip of fixture block 9 and draw-in groove 8, in order to facilitate the dismouting, easy maintenance, apron 3 is the rectangle structure, and the inside of apron 3 embedding mounting groove 4.
The working principle and the using process of the utility model are as follows: before the control device for the airborne laser wind finding radar is used, firstly, a pull ring 6 is held by hand to pull a sliding plate 5 to drive a clamping column 13 to be positioned on the surface of a control device main body 2, a cover plate 3 is clamped in an installation groove 4, the pull ring 6 is loosened after clamping, the sliding plate 5 slides on the outer surface of a clamping rod 16 under the action of elastic deformation of a second spring 15, the end part of the clamping column 13 is driven to be clamped in a clamping hole 12 through the sliding plate 5, the cover plate 3 is conveniently and fixedly installed after the cover plate 3 is closed in the installation groove 4, then when the control device is installed, a rear installation plate 7 is fixedly installed in a cabin of a radar test through a bolt, a clamping block 9 is driven by a hand-held poking block 1 to slide in a first groove 11, the end part of the clamping block 9 is poked towards two sides, at the moment, the control device main body 2 is closed on the surface of the rear installation plate 7 to enable the clamping block 9 to be embedded in a clamping groove 8, loosen shifting block 1 this moment, take place elastic deformation's effect through first spring 10 in the inside of first recess 11 and sticis fixture block 9 in the inside of draw-in groove 8, be convenient for with the fastening installation of controlling means main part 2, easily install and use, otherwise convenient to detach, directly be connected controlling means main part 2 with radar test cabin internal power source and equipment through the wire when using, the convenience is used with laser anemometry radar control, at last when long-time operation damages, can operate pulling pull ring 6 equally, slide 5 and card post 13, make card post 13 break away from in the inside of card hole 12, be convenient for break away from apron 3 in the inside of mounting groove 4, the maintenance is dismantled to the convenience.
Although embodiments of the present invention have been shown and described, 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 utility model, the scope of which is defined in the appended claims and their equivalents.
Claims (7)
1. The utility model provides an airborne laser anemometry controlling means for radar, includes controlling means main part (2), mounting groove (4) have been seted up to the front surface of controlling means main part (2), the inside of mounting groove (4) is provided with apron (3), its characterized in that: the rear surface of the control device main body (2) is provided with a rear mounting plate (7), the two ends of the rear mounting plate (7) are both provided with clamping grooves (8), the two sides of the rear surface of the control device main body (2) are both provided with first grooves (11), a first spring (10) is fixedly arranged in the first groove (11) through a screw, the end part of the first spring (10) is elastically connected with a clamping block (9), and the end of the latch (9) extends to the rear surface of the control device body (2), the two sides of the upper surface of the control device main body (2) are provided with shifting blocks (1), the end part of the shifting block (1) is screwed and connected with the end part of the clamping block (9) through a thread structure, and the first spring (10) and the rear mounting plate (7) are connected with the clamping groove (8) in a clamping manner through the clamping block (9).
2. The control device for an airborne laser wind-finding radar according to claim 1, characterized in that: card hole (12) have all been seted up to the both sides of apron (3), the both sides of mounting groove (4) are located second recess (14) have been seted up to the inside of controlling means main part (2), kelly (16) are installed to the inside block of second recess (14), the surface sliding connection of kelly (16) has slide (5), just the tip extension of slide (5) extremely the inside of mounting groove (4), one side of slide (5) is located the surface registrate of kelly (16) installs second spring (15), there is card post (13) one side of slide (5) through screw fixed mounting, the opposite side of slide (5) passes through the screw and installs pull ring (6), just slide (5) with apron (3) pass through card post (13) with card hole (12) block is connected.
3. The control device for an airborne laser wind-finding radar according to claim 2, characterized in that: the outer surface of the sliding plate (5) is in relative sliding connection with the outer surface of the clamping rod (16), and the sliding plate (5) is elastically connected with the clamping rod (16) through the second spring (15).
4. The control device for an airborne laser wind-finding radar according to claim 2, characterized in that: the clamping hole (12) and the cover plate (3) are of an integrated structure, and the clamping column (13) penetrates through the clamping hole (12).
5. The control device for an airborne laser wind-finding radar according to claim 1, characterized in that: the clamping block (9) is of an L-shaped structure, and the clamping block (9) is elastically connected with the control device main body (2) through the first spring (10).
6. The control device for an airborne laser wind-finding radar according to claim 1, characterized in that: the end part of the clamping block (9) is embedded into the clamping groove (8), and the end part of the clamping block (9) is matched with the internal structure of the clamping groove (8).
7. The control device for an airborne laser wind-finding radar according to claim 1, characterized in that: the cover plate (3) is of a rectangular structure, and the cover plate (3) is embedded into the mounting groove (4).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202123128442.9U CN216560986U (en) | 2021-12-13 | 2021-12-13 | Airborne laser is controlling means for anemometry radar |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202123128442.9U CN216560986U (en) | 2021-12-13 | 2021-12-13 | Airborne laser is controlling means for anemometry radar |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN216560986U true CN216560986U (en) | 2022-05-17 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202123128442.9U Active CN216560986U (en) | 2021-12-13 | 2021-12-13 | Airborne laser is controlling means for anemometry radar |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN216560986U (en) |
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2021
- 2021-12-13 CN CN202123128442.9U patent/CN216560986U/en active Active
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