CN113376587A - Mounting bracket of airborne wind-measuring radar - Google Patents
Mounting bracket of airborne wind-measuring radar Download PDFInfo
- Publication number
- CN113376587A CN113376587A CN202110714921.4A CN202110714921A CN113376587A CN 113376587 A CN113376587 A CN 113376587A CN 202110714921 A CN202110714921 A CN 202110714921A CN 113376587 A CN113376587 A CN 113376587A
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- Prior art keywords
- platform
- fixed
- mounting bracket
- airborne wind
- flat plate
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- 230000007246 mechanism Effects 0.000 claims abstract description 21
- 239000003507 refrigerant Substances 0.000 claims description 4
- 239000002274 desiccant Substances 0.000 claims description 2
- 239000003755 preservative agent Substances 0.000 claims description 2
- 230000002335 preservative effect Effects 0.000 claims 1
- 238000009434 installation Methods 0.000 abstract description 15
- 230000000694 effects Effects 0.000 description 8
- 241000272165 Charadriidae Species 0.000 description 7
- 210000001503 joint Anatomy 0.000 description 6
- 238000005260 corrosion Methods 0.000 description 4
- 230000007797 corrosion Effects 0.000 description 3
- 230000017525 heat dissipation Effects 0.000 description 3
- 239000000843 powder Substances 0.000 description 3
- 230000033228 biological regulation Effects 0.000 description 2
- 239000000110 cooling liquid Substances 0.000 description 2
- 230000001681 protective effect Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000000151 deposition Methods 0.000 description 1
- 239000002245 particle Substances 0.000 description 1
- 239000011435 rock Substances 0.000 description 1
Images
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S7/00—Details of systems according to groups G01S13/00, G01S15/00, G01S17/00
- G01S7/02—Details of systems according to groups G01S13/00, G01S15/00, G01S17/00 of systems according to group G01S13/00
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S13/00—Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
- G01S13/88—Radar or analogous systems specially adapted for specific applications
- G01S13/95—Radar or analogous systems specially adapted for specific applications for meteorological use
-
- 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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- Engineering & Computer Science (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- Computer Networks & Wireless Communication (AREA)
- General Physics & Mathematics (AREA)
- Electromagnetism (AREA)
- Devices Affording Protection Of Roads Or Walls For Sound Insulation (AREA)
Abstract
The invention belongs to the technical field of wind-measuring radars, and discloses an installation support of an airborne wind-measuring radar, which comprises a flat plate, a middle platform and an inner platform, wherein the middle platform is installed at the upper end of the flat plate, a platform cavity is formed in the inner side of the middle platform, and the middle platform is installed in the platform cavity; the flat plate is provided with a plurality of fixing holes, lower fixing mechanisms are arranged in the fixing holes, and the flat plate and the engine room are connected and fixed through the lower fixing mechanisms; a sliding seat is fixed at the bottom of the inner platform and is in sliding connection with the middle platform, so that the height of the inner platform is convenient to adjust, and the installation height of the airborne wind measuring radar can be quickly adjusted; open the top of interior platform has a plurality of platform hole, and a plurality of slide has been seted up to the lateral wall of interior platform, installs the backplate on the slide, and the tip at the interior platform is installed to airborne formula wind-measuring radar accessible platform hole, can pass through movable backplate simultaneously, and it can protect the wind-measuring radar side of installation to go up the backplate, prevents that it from appearing rocking the unstable condition such as waiting at strong wind weather.
Description
Technical Field
The invention belongs to the technical field of wind-measuring radars, and particularly relates to an installation support of an airborne wind-measuring radar.
Background
The wind radar is a "weather radar" for measuring the velocity of particles in the atmosphere moving radially relative to an observer by using the doppler effect, and is capable of measuring horizontal wind, vertical movement, turbulence, wind shear, and the like at various heights, and is often mounted by using a mounting bracket.
The existing mounting bracket of the airborne wind-measuring radar has the defects that:
1. the existing mounting bracket of the airborne wind measuring radar is inconvenient for protecting the radar part assembled at the upper end of the body, the mounting structure is easy to shake and cannot resist larger outdoor wind force, so that the radar has poor stability when in use;
2. the existing mounting bracket of the airborne wind-measuring radar is inconvenient to be firmly fixed according to the mounting environment, and if the body structure cannot be firmly mounted on an engine room, the stability of the mounting bracket in use is poor;
3. the protection and heat dissipation performance of the radar is not ideal.
Disclosure of Invention
The invention aims to provide an installation support of an airborne wind finding radar, and solves the problems that an existing installation support is easy to shake and cannot resist large outdoor wind power.
The invention is realized by the following technical scheme:
a mounting bracket of an airborne wind-measuring radar comprises a flat plate, a middle platform and an inner platform, wherein the middle platform is mounted at the upper end of the flat plate, a platform cavity is formed in the inner side of the middle platform, and the middle platform is mounted in the platform cavity;
the flat plate is provided with a plurality of fixing holes, and lower fixing mechanisms are arranged in the fixing holes;
the top end of the inner platform is provided with a plurality of platform holes, the outer side wall of the inner platform is provided with a plurality of slideways, the slideways are provided with guard plates, and the guard plates and the inner platform form a sliding structure through the slideways;
a sliding seat is fixed at the bottom of the inner platform and is in sliding connection with the middle platform;
the outer side end of the middle platform is provided with a side fixing mechanism.
Further, lower stationary mechanism includes the stationary mast and the lower stationary seat of an organic whole connection, and lower stationary seat joint is in dull and stereotyped top, and the outer wall of stationary mast is prefabricated on has the external screw thread and runs through in dull and stereotyped below, and the stationary mast is connected with the cabin.
Furthermore, a plurality of column grooves are formed in the fixed column along the longitudinal direction of the fixed column, a plurality of lower scales which are discontinuously distributed are arranged on the inner side of the fixed column from top to bottom, and drying agents or/and preservatives are stored in the lower scales.
Further, the fixed column is provided with a clamping hole on the inner side, the outer side of the lower scale is provided with a buckle, and the fixed column and the lower scale are mutually clamped through the clamping hole and the buckle.
Furthermore, the column grooves are distributed in an annular shape relative to the central line of the fixed column, and the lower scales are distributed at equal intervals.
Further, the side fixing mechanism comprises a fixed frame, a side piece and an outer piece, wherein the side piece is arranged on one side of the fixed frame;
the inner part of the side piece is in a hollow groove shape, the outer piece is inserted into the side piece, and the outer piece is movably connected with the side piece;
the extending end of the outer plate is fixed with a radiating fin; open on the outer leaf and have the open holding tank in upper portion, be used for depositing refrigerant medium in the holding tank.
Furthermore, the fixed frame is arranged on the outer side wall of the middle platform and is used for installing the fixed frame, and the outer side wall of the middle platform is provided with a sliding groove which is connected with the fixed frame in a sliding manner.
Furthermore, a plurality of through holes are formed in the side wall of the middle table.
Furthermore, when the inner platform moves to the required height, the sliding seat and the middle platform are fixed through screwing screws, and the screwing screws penetrate through the side wall of the middle platform.
Further, follow the gliding slider of slide on the inner wall of backplate, the slider setting is in the downside of backplate.
Compared with the prior art, the invention has the following beneficial technical effects:
the invention discloses a mounting bracket of an airborne wind-measuring radar, which comprises a flat plate, a middle platform and an inner platform, wherein the middle platform is mounted at the upper end of the flat plate, a platform cavity is formed in the inner side of the middle platform, and the middle platform is mounted in the platform cavity; the flat plate is provided with a plurality of fixing holes, lower fixing mechanisms are arranged in the fixing holes, and the flat plate and the engine room are connected and fixed through the lower fixing mechanisms; the side end of the middle platform is provided with a side fixing mechanism for installing a radar component, and meanwhile, the side end of the inner platform can be simply radiated; a sliding seat is fixed at the bottom of the inner platform and is in sliding connection with the middle platform, so that the height of the inner platform is convenient to adjust, and the installation height of the airborne wind measuring radar can be quickly adjusted; open the top of interior platform has a plurality of platform hole, and a plurality of slide has been seted up to the lateral wall of interior platform, installs the backplate on the slide, and the tip at the interior platform is installed to airborne formula wind-measuring radar accessible platform hole, can pass through movable backplate simultaneously, and it can protect the wind-measuring radar side of installation to go up the backplate, prevents that it from appearing rocking the unstable condition such as waiting at strong wind weather.
Further, lower stationary mechanism includes the stilt of body coupling and decides the seat down, but through stilt screw thread butt joint cabin tip screw in, conveniently with body and cabin montage, carry out firm fixed, the stilt can be rotatory with dull and stereotyped screw thread simultaneously, during the use, can remove the top to dull and stereotyped earlier with the stilt, then install the body at the cabin terminal surface of required installation, later rotatory lower stilt, the stilt and the stilt of linkage move down, dock with the cabin, fixed with the firm connection in cabin.
Furthermore, a plurality of column grooves are formed in the fixed column in the longitudinal direction of the fixed column, a plurality of lower scales which are discontinuously distributed are arranged on the inner side of the fixed column from top to bottom, the lower scales are placed into the fixed column through openings of the column grooves, and dry and anticorrosive powder can be stored on the lower scales, so that potential safety hazards such as corrosion after the lower scales are fixed with the engine room are prevented, and the stability of the fixed column after the lower scales are installed is improved.
Further, the side is decided the mechanism and is including deciding frame, lateral plate and outer piece, through the activity between lateral plate, the outer piece, can move the outer piece outward, and the upper end of outer piece is equipped with the cavity groove, and the refrigerant medium can be added, then with in the outer piece stopper side piece, through the cooperation use of the refrigerant medium matter in the outer piece and fin, carries out simple and easy heat dissipation to the side of interior platform, plays the effect to the protection of installation support body.
Drawings
FIG. 1 is a schematic structural view of a mounting bracket of the present invention;
FIG. 2 is a perspective view of the middle stage of the present invention;
FIG. 3 is a schematic view of the structure of the flat plate and the middle stage of the present invention;
fig. 4 is a schematic perspective view of the inner stage of the present invention.
Wherein 1 is a flat plate; 2 is a middle platform; 3 is a lower fixing mechanism; 4 is a fixed column; 5 is a column groove; 6 is lower scale; 7 is a lower fixed seat; 8 is a table cavity; 9 is an inner platform; 10 is a table hole; 11 is a sliding seat; 12 is a screwing screw; 13 is a side fixing mechanism; 14 is a fixed frame; 15 is a side sheet; 16 is an outer sheet; 17 is a heat sink; 18 is a guard plate; and 19 is a slide way.
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.
In the description of the present invention, it should be noted that the terms "upper", "lower", "inner", "outer", "front", "rear", "both ends", "one end", "the other end", and the like indicate orientations or positional relationships based on those shown in the drawings, and are only for convenience of description and simplicity of description, but do not indicate or imply that the referred device or element must have a specific orientation, be constructed in a specific orientation, and be operated, and thus, should not be construed as limiting the present invention. Furthermore, the terms "first" and "second" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.
In the description of the present invention, it is to be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "disposed," "connected," and the like are to be construed broadly, such as "connected," which may be fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meanings of the above terms in the present invention can be understood in specific cases to those skilled in the art.
Referring to fig. 1-4, the invention discloses a mounting bracket of an airborne wind-measuring radar, which comprises a flat plate 1, a middle platform 2 and an inner platform 9, wherein the middle platform 2 is mounted at the upper end of the flat plate 1, a platform cavity 8 is formed in the inner side of the middle platform 2, and the middle platform 2 is mounted in the platform cavity 8; the flat plate 1 is provided with a plurality of fixing holes, and lower fixing mechanisms 3 are arranged in the fixing holes; the top end of the inner platform 9 is provided with a plurality of platform holes 10, the outer side wall of the inner platform 9 is provided with a plurality of slide ways 19, the slide ways 19 are provided with guard plates 18, and the guard plates 18 and the inner platform 9 form a sliding structure through the slide ways 19; a sliding seat 11 is fixed at the bottom of the inner platform 9, and the sliding seat 11 is connected with the middle platform 2 in a sliding way; the side end of the middle table 2 is provided with a side fixing mechanism 13.
Specifically, be swing joint between the inner wall of slide 11 and well platform 2, through well platform 2, cooperation activity between the slide 11, the height of portable regulation slide 11, and then the upper and lower slip of platform 9 in can driving in step, rotatory screw 12 of screwing this moment can let slide 11 fix at well platform 2 side, fix in step slide 11 top fixed connection's interior platform 9, convenient interior platform 9 cooperation is carried out the regulation of mounted position and is controlled, small-size components and parts and bind the cable can be deposited in step to the side end notch department of slide 11, conveniently assemble the use.
And the slide block slides along the slide rail 19 on the inner wall of the protection plate 18 and is arranged on the lower side of the protection plate 18. This ensures that the guard 18 can slide to the maximum extent of travel above.
The lower fixing mechanism 3 comprises a fixed column 4 and a lower fixed seat 7, a plurality of column grooves 5 are formed in the fixed column 4 along the longitudinal direction of the fixed column 4, lower scales 6 are installed at the inner side ends of the column grooves 5, the lower fixed seat 7 is fixed at the top end of the fixed column 4, the fixed columns 4 are four, the fixed columns 4 are symmetrically distributed about the center of the flat plate 1, the flat plate 1 and the fixed columns 4 are movably connected with each other, the body and the cabin can be conveniently assembled and fixedly connected through a threaded structure of the outer wall of the fixed column 4 in a threaded butt joint mode in a threaded hole at the end part of the cabin, the body and the cabin can be firmly and stably installed, the four fixed columns 4 can be firmly and stably installed on the body, the fixed columns 4 can rotate with the flat plate 1 in a threaded mode, when the fixed columns 4 can be firstly moved to the top end of the flat plate 1, then the body is installed on the end face of the cabin needing to be installed, the lower fixed seat 7 is rotated, the lower fixed seat 7 and the fixed columns 4 are linked to move downwards to be in a butt joint with the cabin, and the engine room is firmly connected and fixed.
More preferably, the column groove 5 is distributed annularly about the center of the fixed column 4, the fixed column 4 and the lower scale 6 are matched with each other to form a clamping structure, the lower scale 6 is distributed equidistantly about the end wall of the fixed column 4, the lower scale 6 is placed into the fixed column 4 through the column groove 5, and dry and anti-corrosion powder can be stored in the lower scale 6, so that potential safety hazards such as corrosion after the fixed column 4 and the engine room are fixed are prevented, and the stability of the fixed column after installation is improved.
The 5 inboard card holes that are equipped with of post groove, 6 inboards of lower scale are equipped with the buckle, and the post groove is in the same place through the mutual joint of card hole, buckle between 5 and the lower scale 6, forms the block structure.
Preferably, the side fixing mechanism 13 includes a fixed frame 14, a side piece 15, an outer piece 16 and a heat sink 17, wherein the side piece 15 is mounted at the end of the fixed frame 14, the outer piece 16 is mounted at the side end of the side piece 15, and the heat sink 17 is fixed at the end wall of the outer piece 16. The fixed frame 14 is fixedly connected with the side piece 15, the middle part of the fixed frame 14 is in a hollow groove shape, the side piece 15 is in a hollow groove shape, the outer piece 16 is inserted into the side piece 15, the side piece 15 and the outer piece 16 are movably connected with each other, the upper end wall of the outer piece 16 is in a hollow groove shape, the outer piece 16 and the radiating fin 17 are fixedly connected with each other, the outer piece 16 can be moved outwards through the movement between the side piece 15 and the outer piece 16, the hollow groove is formed in the upper end of the outer piece 16, cooling media such as cooling liquid can be added, then the outer piece 16 is plugged into the side piece 15, the side end of the body is simply radiated through the matching use of the outer piece 16 and the radiating fin 17, the effect of protecting the installation frame body is achieved, meanwhile, the airborne wind measuring radar can be installed at the end part of the inner platform 9 through the platform hole 10, meanwhile, the movable protecting plate 18 can be used for protecting the side end, the unstable condition such as rock appears in the strong wind weather to prevent it.
As shown in figure 1, the fixed frame 14 is arranged on the outer side wall of the middle platform 2, a sliding groove is formed in the side wall of the middle platform 2 for fixing the frame 14, the fixed frame 14 is matched with the middle platform 2 through the sliding groove and movably connected together, the fixed frame 14 can slide up and down along the sliding groove to adjust the upper position and the lower position, a radar component can be arranged at the upper end of the fixed frame 14, the assembling and assembling function is mainly provided, and the butt joint mode of a main body is enriched.
The working principle is as follows: but through the screw thread butt joint cabin tip screw hole of the stationary post 4, facilitate the body and cabin montage, go on firm fixed, and four stationary posts 4 can go on firm and stable installation to the body, the stationary post 4 can rotate with the flat board 1 screw thread at the same time, while using, can move the stationary post 4 to the top of the flat board 1 first, then install the body in the cabin terminal surface of needing to install, then rotate the lower stationary seat 7, lower stationary seat 7 and stationary post 4 of the linkage move down, in the locating through hole of the cabin butt joint portion, with cabin firm connection fixed, can install the lower scale 6 through the column trough 5, and the lower scale 6 passes the opening of the end wall of side, can store dry and anticorrosive powder, prevent it from appearing the potential safety hazards such as corrosion after fixing with the cabin, improve its stability after installing, through the activity between lateral plate 15, the outer plate 16, can move the outer plate 16 outward, and the upper end of the outer plate 16 is equipped with the hollow trough, can add cooling liquid, then fill in lateral plate 15 with outer piece 16 in, use through the cooperation of outer piece 16 and fin 17, carry out simple and easy heat dissipation to the side of body, play the effect to the protection of installation support body, the tip at interior platform 9 is installed to airborne formula wind measuring radar accessible platform hole 10 simultaneously, can pass through movable protective plate 18 simultaneously, it can protect the wind measuring radar side of installation to go up movable protective plate 18, prevent that it from appearing rocking etc. unstable condition in strong wind weather.
It will be evident to those skilled in the art that the invention is not limited to the details of the foregoing illustrative embodiments, and that the present invention may be embodied in other specific forms without departing from the spirit or essential attributes thereof. The present embodiments are therefore to be considered in all respects as illustrative and not restrictive, the scope of the invention being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein. Any reference sign in a claim should not be construed as limiting the claim concerned.
Claims (10)
1. The mounting bracket of the airborne wind-measuring radar is characterized by comprising a flat plate (1), a middle platform (2) and an inner platform (9), wherein the middle platform (2) is mounted at the upper end of the flat plate (1), a platform cavity (8) is formed in the inner side of the middle platform (2), and the middle platform (2) is mounted in the platform cavity (8);
a plurality of fixing holes are formed in the flat plate (1), and a lower fixing mechanism (3) is arranged in each fixing hole;
the top end of the inner platform (9) is provided with a plurality of platform holes (10), the outer side wall of the inner platform (9) is provided with a plurality of slideways (19), the slideways (19) are provided with guard plates (18), and the guard plates (18) and the inner platform (9) form a sliding structure through the slideways (19);
a sliding seat (11) is fixed at the bottom of the inner platform (9), and the sliding seat (11) is connected with the middle platform (2) in a sliding way;
the outer side end of the middle platform (2) is provided with a side fixing mechanism (13).
2. The mounting bracket for the airborne wind-measuring radar according to claim 1, wherein the lower fixing mechanism (3) comprises a fixed column (4) and a lower fixing seat (7) which are integrally connected, the lower fixing seat (7) is clamped above the flat plate (1), external threads are prefabricated on the outer wall of the fixed column (4) and penetrate below the flat plate (1), and the fixed column (4) is connected with the engine room.
3. The mounting bracket for the airborne wind-measuring radar according to claim 2, wherein a plurality of column grooves (5) are formed in the fixed column (4) along the longitudinal direction of the fixed column (4), a plurality of lower scales (6) which are discontinuously arranged are arranged on the inner side of the fixed column (4) from top to bottom, and a drying agent or/and a preservative are/is stored in the lower scales (6).
4. The mounting bracket for an airborne wind-measuring radar according to claim 2, wherein the inner side of the fixed column (4) is provided with a clamping hole, the outer side of the lower scale (6) is provided with a buckle, and the fixed column (4) and the lower scale (6) are mutually clamped and connected through the clamping hole and the buckle.
5. The mounting bracket for an airborne wind-finding radar according to claim 2, characterized in that the pillar slots (5) are distributed annularly about the center line of the fixed pillar (4) and the lower scales (6) are distributed equidistantly.
6. The mounting bracket of an airborne wind-finding radar according to claim 1, characterized in that the side fixing mechanism (13) comprises a fixed frame (14), a side piece (15) and an outer piece (16), the side piece (15) being mounted on one side of the fixed frame (14);
the inner part of the side piece (15) is in a hollow groove shape, the outer piece (16) is inserted into the side piece (15), and the outer piece (16) is movably connected with the side piece (15);
a radiating fin (17) is fixed at the extending end of the outer sheet (16); an accommodating groove with an open upper part is formed in the outer sheet (16), and a refrigerant medium is stored in the accommodating groove.
7. The mounting bracket for the airborne wind-measuring radar according to claim 6, wherein the fixed frame (14) is mounted on the outer side wall of the middle platform (2), a sliding groove is formed on the outer side wall of the middle platform (2) for mounting the fixed frame (14), and the fixed frame (14) is slidably connected with the middle platform (2) through the sliding groove.
8. The mounting bracket for an airborne wind-finding radar as claimed in claim 1, wherein the side wall of the central platform (2) is provided with a plurality of through holes.
9. The mounting bracket for an airborne wind-finding radar according to claim 1, characterized in that when the inner platform (9) is moved to a desired height, the sliding base (11) and the middle platform (2) are fixed by the tightening screw (12), and the tightening screw (12) penetrates through the side wall of the middle platform (2).
10. A mounting bracket for an airborne wind lidar according to claim 1, wherein the slide block on the inner wall of the backplate (18) slides along a slide (19), the slide block being provided on the underside of the backplate (18).
Priority Applications (1)
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CN202110714921.4A CN113376587A (en) | 2021-06-25 | 2021-06-25 | Mounting bracket of airborne wind-measuring radar |
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CN202110714921.4A CN113376587A (en) | 2021-06-25 | 2021-06-25 | Mounting bracket of airborne wind-measuring radar |
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CN213118330U (en) * | 2020-08-26 | 2021-05-04 | 罗瑶 | Aerospace radar fixing device convenient to adjust |
CN215067262U (en) * | 2021-06-25 | 2021-12-07 | 华能陇东能源有限责任公司 | Mounting bracket of airborne wind-measuring radar |
-
2021
- 2021-06-25 CN CN202110714921.4A patent/CN113376587A/en active Pending
Patent Citations (10)
Publication number | Priority date | Publication date | Assignee | Title |
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JP2006308510A (en) * | 2005-05-02 | 2006-11-09 | Mitsubishi Denki Tokki System Kk | Weather radar apparatus |
US20170023674A1 (en) * | 2015-07-20 | 2017-01-26 | Ford Global Technologies, Llc | Vehicular radar adjustment mechanism |
US20170234482A1 (en) * | 2016-02-17 | 2017-08-17 | Tesla, Inc. | Attachment bracket with adjustment mechanisms and pivot |
CN207093544U (en) * | 2017-08-22 | 2018-03-13 | 浙江群力标准件有限公司 | It is a kind of that there is the bolt for removing and installing function |
CN108196228A (en) * | 2018-01-25 | 2018-06-22 | 合肥驼峰电子科技发展有限公司 | A kind of millimetre-wave radar |
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CN215067262U (en) * | 2021-06-25 | 2021-12-07 | 华能陇东能源有限责任公司 | Mounting bracket of airborne wind-measuring radar |
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