CN117401173B - Meteorological radar hangs and flies device - Google Patents

Meteorological radar hangs and flies device Download PDF

Info

Publication number
CN117401173B
CN117401173B CN202311725215.5A CN202311725215A CN117401173B CN 117401173 B CN117401173 B CN 117401173B CN 202311725215 A CN202311725215 A CN 202311725215A CN 117401173 B CN117401173 B CN 117401173B
Authority
CN
China
Prior art keywords
plate
flying
bin
hanging
radar
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
CN202311725215.5A
Other languages
Chinese (zh)
Other versions
CN117401173A (en
Inventor
马国利
刘科宏
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Shanxi Chenggong General Aviation Co ltd
Original Assignee
Shanxi Chenggong General Aviation Co ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Shanxi Chenggong General Aviation Co ltd filed Critical Shanxi Chenggong General Aviation Co ltd
Priority to CN202311725215.5A priority Critical patent/CN117401173B/en
Publication of CN117401173A publication Critical patent/CN117401173A/en
Application granted granted Critical
Publication of CN117401173B publication Critical patent/CN117401173B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D47/00Equipment not otherwise provided for
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02ATECHNOLOGIES FOR ADAPTATION TO CLIMATE CHANGE
    • Y02A90/00Technologies having an indirect contribution to adaptation to climate change
    • Y02A90/10Information and communication technologies [ICT] supporting adaptation to climate change, e.g. for weather forecasting or climate simulation

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Power-Operated Mechanisms For Wings (AREA)
  • Radar Systems Or Details Thereof (AREA)

Abstract

The utility model relates to a weather radar hangs and flies device belongs to the aircraft and hangs the technical field that flies, and it is in including hanging the storehouse and pegging graft hang fly the storehouse inside and with hang the support board that flies storehouse diapire sliding connection, it articulates to hang fly storehouse one side has the installing door, sliding connection has two curb plates that set up relatively in the storehouse of hanging, the curb plate upside be equipped with hang the roof that flies storehouse lateral wall sliding connection, hang and fly the storehouse and be close to be equipped with the drive on the inside wall of curb plate one side the curb plate with the driving piece of roof clamp radar. This application has the effect of being convenient for support tight with the radar, improves and hangs efficiency of flying.

Description

Meteorological radar hangs and flies device
Technical Field
The application relates to the technical field of aircraft hanging, in particular to a weather radar hanging device.
Background
Weather radar is used as aviation protection forest, artificial precipitation, the common equipment of manual work haze removal, uses with the aircraft cooperation generally, and in order to be convenient for install on the aircraft, adopts the mode of hanging the flight to be connected with the aircraft generally.
The Chinese patent with publication number CN113844657A discloses an airborne radar flying device, which comprises a bracket and a flying cabin, wherein the bracket is connected with a machine body, and the flying cabin is arranged on the bracket and used for placing a radar; the side propping mechanism is arranged in the hanging flying bin and is used for propping the radar placed in the hanging flying bin relatively from two sides, the top propping mechanism is used for propping the radar on the inner bottom wall of the hanging flying bin from the upper side of the radar, the side propping mechanism is in transmission connection with the top propping mechanism, and the side propping mechanism drives the top propping mechanism to synchronously prop against the radar in the radar propping process; one side opening of the hanging flying bin is provided, and an opening door is hinged at the opening of the hanging flying bin, so that the problem that the radar is difficult to disassemble and assemble when the hanging flying test is performed is solved.
In the related art, the radar is abutted tightly through the motor driving side abutting mechanism and the top abutting mechanism, so that when the radar enters the flying bin, the motor is required to be driven and the radar is abutted tightly, and the flying efficiency of the radar is affected.
Disclosure of Invention
In order to be convenient for support the radar tightly, improve and hang and fly efficiency, this application provides a meteorological radar and hangs and fly device.
The application provides a weather radar hangs device that flies adopts following technical scheme:
the utility model provides a weather radar flies device, is in including hanging flying the storehouse and pegging graft fly the storehouse inside and with hang flying storehouse diapire sliding connection's carrier plate, it articulates there is the installing door to hang flying storehouse one side, sliding connection has two curb plates of setting relatively in the storehouse that flies to hang, the curb plate upside be equipped with hang flying storehouse lateral wall sliding connection's roof, hang and fly the storehouse and be close to be equipped with the drive on the inside wall of curb plate one side the curb plate with the driving piece of roof clamp radar.
Through adopting above-mentioned technical scheme, the one end that the bearing board is close to the installing door removes to hang and fly the storehouse outside, places the radar on the bearing board this moment to the drive bearing board drives the radar and gets into completely and hang and fly in the storehouse, and bearing board passes through driving piece drive curb plate and roof simultaneously with the radar clamp, thereby is convenient for fix the radar, improves and hangs and fly efficiency.
Optionally, the curb plate is followed spandrel board width direction slides, the curb plate is close to hang the one end that flies the storehouse lateral wall all articulates there is the articulated lever, the articulated lever is kept away from the one end of curb plate is all articulated each other.
Through adopting above-mentioned technical scheme, when driving piece drive curb plate and roof press from both sides tight with the radar, the curb plate removes to the direction that is close to each other, and articulated end and the roof that articulated rod articulated each other kept away from the one end of installing the door all move down under the drive of driving piece this moment, reaches the effect of being convenient for support tightly the radar, improves and hangs flying efficiency.
Optionally, the driving piece is including pegging graft in the string flying storehouse lateral wall and with string flying storehouse lateral wall sliding connection's driving plate, articulated rod articulated one end each other with the driving plate is articulated, roof tip with driving plate fixed connection, string flying storehouse is close to one side grafting and sliding connection of driving plate have the drive piece, the drive piece with driving plate lateral wall butt drives the driving plate removes, hang flying storehouse lateral wall with be equipped with the same first spring of connecting both between the driving plate.
Through adopting above-mentioned technical scheme, the drive block removes to the direction that is close to the drive plate, and the drive plate moves down under the extrusion of drive block this moment to drive articulated end that articulated rod articulated each other and the one end that the roof is close to the drive plate simultaneously move down, until curb plate and roof all support tightly with the radar lateral wall, thereby reach the effect of being convenient for support tightly the radar, improve and hang and fly efficiency.
Optionally, the side wall of the driving plate, which is close to one end of the driving block and is located at the lower side of the driving block, is configured as a downward inclined surface, which is close to one side of the side plate.
Through adopting above-mentioned technical scheme, when the drive piece removes to the direction that is close to the drive plate, the inclined plane butt on drive piece and the drive plate and downwardly extrusion drive plate to make the drive plate drive articulated end that articulated pole is articulated each other and the one end that the roof is close to the drive plate simultaneously downwardly moving, be convenient for curb plate and roof press from both sides the radar clamp simultaneously, improve and hang and fly efficiency.
Optionally, the support board downside fixedly connected with is followed the rack that support board length direction set up, hang and fly the storehouse lower extreme rotation be connected with rack-meshed gear, the axle center department of gear one side installs the motor, support board tip can with the drive piece butt drives the drive piece gets into hang and fly in the storehouse.
Through adopting above-mentioned technical scheme, motor drive gear rotates to make with gear engagement's rack drive carrier board along hanging the length direction who flies the storehouse and slide, be convenient for place the radar on carrier board, and when carrier board moves to one side that is close to the curb plate and with hang the storehouse lateral wall butt down in the drive of rack, carrier board extrusion drive piece gets into and hangs in flying the storehouse lateral wall, and makes curb plate and roof support the radar tightly simultaneously, thereby improves and hangs and fly efficiency.
Optionally, one side in the installation door direction of height with hang and fly the storehouse lateral wall and hinge, the installation door be close to articulated side and the one end in the direction of height be equipped with hang fly the torsional spring that the storehouse is connected, torsional spring one end with installation door fixed connection, the other end with hang and fly storehouse lateral wall fixed connection, works as the bearing board is kept away from the one end of curb plate is moved to hang and fly the storehouse outside, bearing board tip with installation door lateral wall butt and drive the installation door rotates.
Through adopting above-mentioned technical scheme, the bearing board moves to the direction that is close to the installing door under the drive of rack and when with installing door lateral wall butt, continue to remove the bearing board and remove to the direction of keeping away from the curb plate, the installing door is opened under the removal of bearing board this moment, and the torsional spring is stretched, when the radar was placed on the bearing board, the bearing board moves to the direction that is close to the curb plate under the drive of rack, when the bearing board got into and flies in the storehouse, the torsional spring resumes deformation and pulling installing door shutoff and hangs the storehouse, accomplish the opening and the closing of installing door, further be convenient for improve and hang and fly efficiency.
Optionally, one end of the hinged side of the mounting door is fixedly connected with a ratchet wheel perpendicular to the mounting door, and the hanging flying bin is rotatably connected with a pawl meshed with the ratchet wheel.
Optionally, the inboard diapire of hanging the storehouse of flying is close to one side of installing the door and is equipped with vertical connecting block, the connecting block lower extreme is pegged graft in hanging the storehouse diapire and follow install the door direction of height and slide, hang the storehouse of flying with fixedly connected with same second spring between the connecting block, the connecting block with fixedly connected with same connecting rod between the pawl, works as when the connecting block slides in vertical orientation, the pawl moves along with the connecting block.
Through adopting above-mentioned technical scheme, when the bearing board moves to the direction that is close to the installing door, the bearing board extrudes the connecting block and drives the pawl downwardly moving, pawl and ratchet break away from this moment, the bearing board continues to move to the direction that is close to the installing door until opening the installing door, the torsional spring is stretched this moment, thereby be convenient for place the radar, after the radar is placed, the drive bearing board removes until fully get into and hang in flying the storehouse, extrusion on the connecting block disappears this moment, and torsional spring drive installing door shutoff hangs flying the storehouse, this moment the second spring resumes deformation and promotes the connecting block and drive pawl through the connecting rod and upwards move, until with the ratchet chucking, thereby be convenient for with the installing door locking, reduce the possibility that the radar breaks away from the installing door, improve radar stability.
Optionally, the holding tank that is used for placing the radar is offered to the spandrel board upside, spandrel board length direction's both sides all are equipped with vertical limiting plate.
Through adopting above-mentioned technical scheme, in the holding tank that the radar was placed on the spandrel board, increase the area of contact of radar and spandrel board, increase the stability of radar, and the limiting plate of spandrel board both sides carries out spacingly to the radar, reduces the possibility that the radar breaks away from spandrel board at spandrel board removal in-process, improves radar stability.
Optionally, the back sliding connection has the stripper plate on the carrier plate, the stripper plate is located in the holding tank, just fixedly connected with on the carrier plate with stripper plate downside fixed connection's third spring, the limiting plate with carrier plate upper side sliding connection, just the equal butt of limiting plate lower extreme have with carrier plate lateral wall rotates the supporting rod of being connected, the carrier plate keep away from the one end of limiting plate all with stripper plate downside butt.
Through adopting above-mentioned technical scheme, when the radar was placed on the bearing board, the bearing board downwardly moving and the one end that the downwardly extrusion bearing pole was close to the extrusion pole, the one end that the extrusion board was kept away from to the bearing pole was upwards rotated this moment to promote limiting plate upwardly moving until the upper end is located the bearing board upside outside, thereby carry out spacingly to the radar, improve radar stability.
In summary, the present application includes at least one of the following beneficial technical effects:
the radar is placed on the supporting plate and driven to drive the radar to completely enter the flying bin, and the supporting plate drives the side plate and the top plate to clamp the radar simultaneously through the driving piece, so that the radar is conveniently fixed, and the flying efficiency is improved;
the motor drives the gear to rotate, so that the rack meshed with the gear drives the bearing plate to slide along the length direction of the flying bin, the radar is conveniently placed on the bearing plate, and when the bearing plate is driven by the rack to move to one side close to the side plate and is abutted to the side wall of the flying bin, the bearing plate extrudes the driving block into the side wall of the flying bin, and the side plate and the top plate are abutted to the radar at the same time, so that the flying efficiency is improved;
when the bearing plate moves towards the direction close to the installation door, the bearing plate extrudes the connecting block to drive the pawl to move downwards, at the moment, the pawl is separated from the ratchet wheel, the bearing plate continues to move towards the direction close to the installation door until the installation door is opened, the torsion spring is stretched, thereby being convenient for placing the radar, after the radar is placed, the bearing plate is driven to move until the radar completely enters the hanging bin, at the moment, the extrusion on the connecting block disappears, the torsion spring drives the installation door to seal the hanging bin, at the moment, the second spring recovers deformation and pushes the connecting block to drive the pawl to move upwards through the connecting rod until the ratchet wheel is clamped, thereby being convenient for locking the installation door, reducing the possibility that the radar is separated from the installation door, and improving the radar stability.
Drawings
FIG. 1 is a schematic diagram of the overall structure of a weather radar flying device in an embodiment of the present application.
Fig. 2 is a schematic structural diagram showing a positional relationship between a side plate and a hanging bin in an embodiment of the present application.
Fig. 3 is a schematic structural view showing the positional relationship of the side plate and the driving plate in the embodiment of the present application.
Fig. 4 is a schematic structural view showing the positional relationship of the connection block and the mounting lever in the embodiment of the present application.
Fig. 5 is a schematic structural view showing the positional relationship of the pressing plate and the gear in the embodiment of the present application.
Reference numerals illustrate: 1. hanging a flying bin; 11. an opening; 12. installing a door; 121. a ratchet wheel; 122. a pawl; 123. a connecting block; 124. a second spring; 125. a mounting rod; 126. a connecting rod; 13. a torsion spring; 14. a sliding groove; 15. a driving groove; 16. a through hole; 17. a communication hole; 2. a bearing plate; 21. a receiving groove; 22. a rack; 23. a gear; 24. a motor; 25. extruding the hole; 26. a cavity; 3. a side plate; 31. a driving rod; 32. a hinge rod; 33. a driving member; 331. a driving plate; 3311. a moving groove; 332. a driving block; 333. a first spring; 4. a top plate; 5. an extrusion plate; 51. a limiting plate; 52. and a support rod.
Detailed Description
The present application is described in further detail below with reference to the accompanying drawings.
The embodiment of the application discloses a weather radar hanging device. Referring to fig. 1 and 2, a weather radar flying device includes a flying cabin 1, an opening 11 is formed on one side of the flying cabin 1, and a mounting door 12 for blocking the opening 11 is formed on one side of the box body close to the opening 11. Referring to fig. 2 and 3, one side of the installation door 12 in the height direction is hinged with the hanging flying bin 1, referring to fig. 1 and 4, torsion springs 13 are arranged at two ends of the hinged side of the installation door 12, one end of each torsion spring 13 is fixedly connected with the installation door 12, and the other end of each torsion spring 13 is fixedly connected with the side wall of the hanging flying bin 1. When the torsion spring 13 is in its original length, the mounting door 12 blocks the opening 11.
Referring to fig. 2 and 3, a horizontal supporting plate 2 is slidingly connected to the bottom wall inside the hanging flying bin 1, a containing groove 21 is formed in the middle of the supporting plate 2 and is arranged along the length direction of the supporting plate 2, a rack 22 parallel to the length direction of the supporting plate 2 is fixedly connected to the middle of the lower side of the supporting plate 2, a sliding groove 14 which is matched with the rack 22 is formed in the bottom wall inside the hanging flying bin 1, and the rack 22 is inserted into the sliding groove 14 and is slidingly connected with the bottom wall of the hanging flying bin 1. The lower end of the outer side of the hanging flight bin 1 is rotatably connected with a gear 23 which is vertical and meshed with a rack 22, and a motor 24 which is fixedly connected with the outer side wall of the hanging flight bin 1 is arranged at the axle center of one side of the gear 23.
Referring to fig. 2 and 3, the side opposite to the mounting door 12 inside the hanging flying bin 1 is provided with two arc-shaped side plates 3 symmetrically arranged on two sides of the bearing plate 2, the middle parts of the side plates 3 are recessed in the directions away from each other, and one side of the side plates 3 away from the bearing plate 2 is provided with an arc-shaped top plate 4 with the middle parts recessed in the directions away from the bearing plate 2. The equal fixedly connected with horizontally-driving rod 31 of one end that installing door 12 was kept away from to curb plate 3 and roof 4, the one end that curb plate 3 was kept away from to the driving rod 31 on the curb plate 3 all passes and hangs the storehouse 1 lateral wall that flies and slide along the direction that the horizontal direction is close to each other or keep away from, the one end that curb plate 3 was kept away from to the driving rod 31 on the curb plate 3 all articulates there is articulated rod 32, and articulated rod 32 keep away from the one end of curb plate 3 all to be located the curb plate 3 and be close to one side of bearing board 2 and articulated each other, hang the inside driving piece 33 that is equipped with drive curb plate 3 and roof 4 and support tight radar simultaneously of storehouse 1.
The one end that the carrier plate 2 is close to installing door 12 removes to and hangs the storehouse 1 outside, install door 12 is opened under the promotion of carrier plate 2 tip this moment, torsional spring 13 is stretched, place the radar in carrier plate 2's holding tank 21, and drive carrier plate 2 drives the radar and get into completely and hang and fly storehouse 1, torsional spring 13 pulling install door 12 shutoff opening 11 this moment, and carrier plate 2 all moves down under the drive of driver 33 through the articulated end that driver 33 drive articulated rod 32 each other and roof 4 kept away from installing door 12's one end, until curb plate 3 and roof 4 clamp the radar simultaneously, accomplish the radar and hang and fly.
Referring to fig. 2 and 3, the driving member 33 includes a vertical driving plate 331 disposed inside the hanging and flying bin 1 and near to one side of the side plate 3, a driving slot 15 adapted to the driving plate 331 is formed in a side wall of the hanging and flying bin 1 near to one side of the side plate 3, and the driving plate 331 is inserted into the driving slot 15 and slidably connected with the side wall of the hanging and flying bin 1. One end, away from the top plate 4, of the driving rod 31 corresponding to the top plate 4 penetrates through the side wall of the flying cabin 1 and is fixedly connected with the driving plate 331, a vertical penetrating hole 16 which is matched with the movement track of the top plate 4 is formed in the inner side wall of the flying cabin 1, and the penetrating hole 16 is communicated with the driving groove 15.
The hinged rod 32 is hinged with the drive plate 331 through the drive slot 15, the drive block 332 is arranged at the lower end of the side close to the side plate 3 inside the hanging cabin 1, the communication hole 17 which is matched with the drive block 332 and communicated with the drive slot 15 is arranged on the inner side wall of the hanging cabin 1, and one end of the drive block 332 away from the side plate 3 is inserted into the communication hole 17 and is abutted with the side wall of the drive plate 331.
The lower extreme that drive plate 331 is close to drive piece 332 one side has seted up the removal groove 3311 that suits with drive piece 332, and the lateral wall of removal groove 3311 downside sets up to the inclined plane that is close to one side of curb plate 3 and downward sloping, is equipped with the first spring 333 towards drive piece 332 in the drive groove 15, and first spring 333 one end and the one end fixed connection who hangs the storehouse 1 lateral wall, the other end and drive piece 332 insert the one end fixed connection in the drive groove 15. When the first spring 333 is in the original length, the end of the driving block 332 away from the driving plate 331 is located outside the inner side wall of the hanging cabin 1, and the end of the supporting plate 2 away from the mounting door 12 can be abutted with the end of the driving block 332 away from the driving plate 331.
The motor 24 drives the gear 23 to rotate, so that the rack 22 meshed with the gear 23 drives the supporting plate 2 to slide along the length direction of the flying bin 1 until the supporting plate 2 is abutted against the side wall of the mounting door 12, the mounting door 12 is opened under the movement of the supporting plate 2 at the moment and the torsion spring 13 is stretched, so that the radar is placed on the supporting plate 2, when the radar is placed on the supporting plate 2, the supporting plate 2 is driven by the rack 22 to move towards the direction close to the side plate 3, when the supporting plate 2 enters the flying bin 1, the torsion spring 13 is restored to deform and pulls the mounting door 12 to seal the flying bin 1, and when the supporting plate 2 is driven by the rack 22 to move to the side close to the side plate 3 and is abutted against the side wall of the flying bin 1, the supporting plate 2 extrudes the driving block 332 into the side wall of the flying bin 1, and enables the side plate 3 and the top plate 4 to abut against the radar at the same time, so that the flying of the radar is completed.
Referring to fig. 4, a horizontal ratchet 121 is fixedly connected to the lower end of the hinged side of the installation door 12, a pawl 122 engaged with the ratchet 121 is provided at the outer side of the hanging bin 1, and the ratchet 121 rotates with the installation door 12 when the installation door 12 is opened or closed. The sliding tray 14 is close to the one end grafting of installing door 12 has vertical connecting block 123, and connecting block 123 lower extreme fixedly connected with vertical second spring 124, second spring 124 lower extreme and hang the lateral wall fixed connection under the storehouse 1 that flies, and one side that connecting block 123 kept away from installing door 12 sets up to the inclined plane that is close to one side of curb plate 3 and downward sloping.
The lower end of the connecting block 123 is fixedly connected with a vertical mounting rod 125, and the lower end of the mounting rod 125 passes through and is in sliding connection with the lower side wall of the hanging flying bin 1. One end of the mounting rod 125, which is positioned outside the hanging flight bin 1, is fixedly connected with a connecting rod 126, and the pawl 122 is positioned on the upper side of one end of the connecting rod 126, which is far away from the mounting rod 125, and is rotatably connected with the connecting rod 126.
When the bearing plate 2 moves towards the direction close to the mounting door 12, the bearing plate 2 extrudes the connecting block 123 to drive the pawl 122 to move downwards, at the moment, the pawl 122 is separated from the ratchet wheel 121, the bearing plate 2 continues to move towards the direction close to the mounting door 12 until the mounting door 12 is opened, at the moment, the torsion spring 13 is stretched, so that the radar is conveniently placed, after the radar is placed, the bearing plate 2 is driven to move until the radar completely enters the hanging flying bin 1, at the moment, the extrusion on the connecting block 123 disappears, the torsion spring 13 drives the mounting door 12 to block the hanging flying bin 1, at the moment, the second spring 124 is restored to deform and pushes the connecting block 123 to drive the connecting rod 126 and the pawl 122 to move upwards until the ratchet wheel 121 is clamped, and the mounting door 12 is locked.
Referring to fig. 2 and 5, the middle part of the upper side of the supporting plate 2 is provided with a squeeze plate 5 which is horizontal and parallel to the length direction of the supporting plate 2, the supporting plate 2 is provided with a squeeze hole 25 which is adapted to the motion track of the squeeze plate 5, and the lower end of the squeeze plate 5 is inserted into the squeeze hole 25 and is in sliding connection with the supporting plate 2. The upper side of the bearing plate 2 is inserted into and connected with a vertical limiting plate 51 in a sliding manner along the two sides arranged in the length direction, a cavity 26 is formed in the bearing plate 2, two bearing rods 52 symmetrically arranged on the two sides of the lower end of the extrusion plate 5 are arranged in the cavity 26, and the bearing rods 52 are connected with the bearing plate 2 in a rotating manner. One end of the supporting rod 52, which is close to the extrusion plate 5, is abutted against the lower side wall of the extrusion plate 5, and one end of the supporting rod 52, which is far away from the extrusion plate 5, is inclined downwards and abutted against the lower end of the corresponding limiting plate 51.
When the radar is placed on the supporting plate 2, the extrusion plate 5 moves downwards and extrudes the supporting rod 52 downwards to be close to one end of the extrusion rod, and at the moment, one end of the supporting rod 52 away from the extrusion plate 5 rotates upwards, so that the limiting plate 51 is pushed to move upwards until the upper end is located outside the upper side surface of the supporting plate 2, and the radar is limited.
The implementation principle of the weather radar hanging device in the embodiment of the application is as follows: the supporting plate 2 slides until being abutted against the side wall of the mounting door 12, the mounting door 12 is opened under the movement of the supporting plate 2 at the moment, the torsion spring 13 is stretched, the radar is placed on the supporting plate 2, the supporting plate 2 is driven by the rack 22 to move towards the direction close to the side plate 3 until entering the flying bin 1, the torsion spring 13 recovers deformation and pulls the mounting door 12 to seal the flying bin 1, and when the supporting plate 2 is driven by the rack 22 to move to the side close to the side plate 3 and is abutted against the side wall of the flying bin 1, the supporting plate 2 extrudes the driving block 332 into the side wall of the flying bin 1, and the side plate 3 and the top plate 4 are enabled to simultaneously abut against the radar, so that the radar flying is completed.
The foregoing are all preferred embodiments of the present application, and are not intended to limit the scope of the present application in any way, therefore: all equivalent changes in structure, shape and principle of this application should be covered in the protection scope of this application.

Claims (8)

1. The utility model provides a weather radar flies device, is in including hanging flying storehouse (1) and grafting hang the inside and with hanging flying storehouse (1) diapire sliding connection's carrier plate (2), its characterized in that: one side of the flying bin (1) is hinged with an installation door (12), two side plates (3) which are oppositely arranged are connected in the flying bin (1) in a sliding manner, a top plate (4) which is connected with the side wall of the flying bin (1) in a sliding manner is arranged on the upper side of the side plates (3), and a driving piece (33) for driving the side plates (3) and the top plate (4) to clamp a radar is arranged on the inner side wall of the flying bin (1) close to one side of the side plates (3); the side plates (3) slide along the width direction of the bearing plate (2), one ends of the side plates (3) close to the side walls of the hanging flying bin (1) are hinged with hinge rods (32), and one ends of the hinge rods (32) far away from the side plates (3) are hinged with each other; the driving piece (33) comprises a driving plate (331) which is inserted into the side wall of the flying bin (1) and is in sliding connection with the side wall of the flying bin (1), one end of each hinged rod (32) is hinged with the driving plate (331), the end of the top plate (4) is fixedly connected with the driving plate (331), one side, close to the driving plate (331), of the flying bin (1) is inserted into a driving block (332) in sliding connection, the driving block (332) is in butt joint with the side wall of the driving plate (331) and drives the driving plate (331) to move, and a first spring (333) which is used for connecting the two is arranged between the side wall of the flying bin (1) and the driving plate (331).
2. A weather radar hanging device as claimed in claim 1, wherein: the side wall of the driving plate (331) close to one end of the driving block (332) and positioned at the lower side of the driving block (332) is provided with a slope which is inclined downwards towards one side close to the side plate (3).
3. A weather radar hanging device as claimed in claim 2, wherein: the utility model discloses a fly bin, including support board (2), drive piece (332) and drive piece (332), support board (2) downside fixedly connected with is followed rack (22) that support board (2) length direction set up, hang fly bin (1) lower extreme rotation be connected with rack (22) meshed gear (23), motor (24) are installed in axle center department of gear (23) one side, support board (2) tip can with drive piece (332) butt and drive piece (332) get into hang fly bin (1).
4. A weather radar boomerang apparatus according to claim 3, wherein: one side in the height direction of the mounting door (12) is hinged with the side wall of the hanging flying bin (1), one end, close to the hinged side, of the mounting door (12) in the height direction is provided with a torsion spring (13) connected with the hanging flying bin (1), one end of the torsion spring (13) is fixedly connected with the mounting door (12), the other end of the torsion spring is fixedly connected with the side wall of the hanging flying bin (1), and when one end, far away from the side plate (3), of the bearing plate (2) moves to the outer side of the hanging flying bin (1), the end of the bearing plate (2) is abutted with the side wall of the mounting door (12) and drives the mounting door (12) to rotate.
5. The weather radar hanging flight device as claimed in claim 4, wherein: one end of the hinged side of the mounting door (12) is fixedly connected with a ratchet wheel (121) perpendicular to the mounting door (12), and the hanging flying bin (1) is rotatably connected with a pawl (122) meshed with the ratchet wheel (121).
6. The weather radar hanging device as claimed in claim 5, wherein: a vertical connecting block (123) is arranged on one side of the bottom wall of the inner side of the flying cabin (1) close to the mounting door (12), the lower end of the connecting block (123) is inserted into the bottom wall of the flying cabin (1) and slides along the height direction of the mounting door (12), the utility model discloses a fly bin, hang fly bin (1) with be connected with same second spring (124) between connecting block (123), connecting block (123) with be connected with same connecting rod (126) between pawl (122) fixedly, work as connecting block (123) are in the vertical direction when sliding, pawl (122) are along with connecting block (123) remove.
7. A weather radar hanging device as claimed in claim 1, wherein: the radar support is characterized in that an accommodating groove (21) for accommodating a radar is formed in the upper side of the support plate (2), and vertical limiting plates (51) are arranged on two sides of the support plate (2) in the length direction.
8. The weather radar hanging flight device of claim 7, wherein: the bearing plate (2) upper side sliding connection has stripper plate (5), stripper plate (5) are located in holding tank (21), just fixedly connected with on bearing plate (2) with stripper plate (5) downside fixed connection's third spring, limiting plate (51) with bearing plate (2) upper side sliding connection, just limiting plate (51) lower extreme all butt have with bearing plate (2) lateral wall rotates supporting rod (52) of being connected, bearing plate (2) are kept away from one end of limiting plate (51) all with stripper plate (5) downside butt.
CN202311725215.5A 2023-12-15 2023-12-15 Meteorological radar hangs and flies device Active CN117401173B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202311725215.5A CN117401173B (en) 2023-12-15 2023-12-15 Meteorological radar hangs and flies device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202311725215.5A CN117401173B (en) 2023-12-15 2023-12-15 Meteorological radar hangs and flies device

Publications (2)

Publication Number Publication Date
CN117401173A CN117401173A (en) 2024-01-16
CN117401173B true CN117401173B (en) 2024-02-27

Family

ID=89498410

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202311725215.5A Active CN117401173B (en) 2023-12-15 2023-12-15 Meteorological radar hangs and flies device

Country Status (1)

Country Link
CN (1) CN117401173B (en)

Citations (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN203521593U (en) * 2013-09-24 2014-04-02 上海无线电设备研究所 Dual-antenna interference airborne captive flight structure
US9030149B1 (en) * 2014-07-29 2015-05-12 SZ DJI Technology Co., Ltd. Systems and methods for payload stabilization
CN108051787A (en) * 2017-12-05 2018-05-18 上海无线电设备研究所 A kind of missile-borne radar flying test method
WO2018183428A1 (en) * 2017-03-31 2018-10-04 Walmart Apollo, Llc Contact activated retail delivery package release systems and methods
CN109050933A (en) * 2018-08-20 2018-12-21 陈霞 A kind of unmanned plane carry frame
WO2020114427A1 (en) * 2018-12-06 2020-06-11 深圳市道通科技股份有限公司 Displacement apparatus and vehicle marking device
CN112693612A (en) * 2019-10-23 2021-04-23 北京东方瑞星科技发展有限公司南京分公司 Unmanned aerial vehicle carries shell carry device based on lever locking
CN113844657A (en) * 2021-10-12 2021-12-28 四川西华通用航空股份有限公司 Airborne radar hanging and flying device
CN215361884U (en) * 2021-03-04 2021-12-31 广西智能鹰机器人集团有限公司 Laser mapping unmanned aerial vehicle
CN216581038U (en) * 2021-12-30 2022-05-24 哈瓦国际航空技术(深圳)有限公司 Rocket launcher aerial launching cradle head and aircraft
CN217969932U (en) * 2022-09-01 2022-12-06 空天乘云(苏州)航空航天科技有限公司 Locking device of rail mounted unmanned aerial vehicle carries guided missile
CN218400985U (en) * 2022-10-24 2023-01-31 深圳市科卫泰实业发展有限公司 Unmanned aerial vehicle carries rifle device
WO2023023993A1 (en) * 2021-08-25 2023-03-02 成都航空职业技术学院 Aerospace radar fixture convenient to adjust
CN115946889A (en) * 2023-02-21 2023-04-11 朱吉龙 Unmanned aerial vehicle provided with linkage telescopic structure and used for laser radar surveying and mapping and use method thereof
CN219673814U (en) * 2023-05-15 2023-09-12 中国人民解放军空军工程大学 Lower visual angle adjustable mechanism for hanging radar guide head
CN219989496U (en) * 2023-04-21 2023-11-10 山西航友科技有限公司 Aircraft mounting throwing mechanism
CN117141718A (en) * 2023-10-28 2023-12-01 山西成功通用航空股份有限公司 Aviation rescue mounting device

Patent Citations (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN203521593U (en) * 2013-09-24 2014-04-02 上海无线电设备研究所 Dual-antenna interference airborne captive flight structure
US9030149B1 (en) * 2014-07-29 2015-05-12 SZ DJI Technology Co., Ltd. Systems and methods for payload stabilization
WO2018183428A1 (en) * 2017-03-31 2018-10-04 Walmart Apollo, Llc Contact activated retail delivery package release systems and methods
CN108051787A (en) * 2017-12-05 2018-05-18 上海无线电设备研究所 A kind of missile-borne radar flying test method
CN109050933A (en) * 2018-08-20 2018-12-21 陈霞 A kind of unmanned plane carry frame
WO2020114427A1 (en) * 2018-12-06 2020-06-11 深圳市道通科技股份有限公司 Displacement apparatus and vehicle marking device
CN112693612A (en) * 2019-10-23 2021-04-23 北京东方瑞星科技发展有限公司南京分公司 Unmanned aerial vehicle carries shell carry device based on lever locking
CN215361884U (en) * 2021-03-04 2021-12-31 广西智能鹰机器人集团有限公司 Laser mapping unmanned aerial vehicle
WO2023023993A1 (en) * 2021-08-25 2023-03-02 成都航空职业技术学院 Aerospace radar fixture convenient to adjust
CN113844657A (en) * 2021-10-12 2021-12-28 四川西华通用航空股份有限公司 Airborne radar hanging and flying device
CN216581038U (en) * 2021-12-30 2022-05-24 哈瓦国际航空技术(深圳)有限公司 Rocket launcher aerial launching cradle head and aircraft
CN217969932U (en) * 2022-09-01 2022-12-06 空天乘云(苏州)航空航天科技有限公司 Locking device of rail mounted unmanned aerial vehicle carries guided missile
CN218400985U (en) * 2022-10-24 2023-01-31 深圳市科卫泰实业发展有限公司 Unmanned aerial vehicle carries rifle device
CN115946889A (en) * 2023-02-21 2023-04-11 朱吉龙 Unmanned aerial vehicle provided with linkage telescopic structure and used for laser radar surveying and mapping and use method thereof
CN219989496U (en) * 2023-04-21 2023-11-10 山西航友科技有限公司 Aircraft mounting throwing mechanism
CN219673814U (en) * 2023-05-15 2023-09-12 中国人民解放军空军工程大学 Lower visual angle adjustable mechanism for hanging radar guide head
CN117141718A (en) * 2023-10-28 2023-12-01 山西成功通用航空股份有限公司 Aviation rescue mounting device

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
基于无人机的输电线路带电清障装置研制;箫振辉;《优秀硕士论文全文数据库工程科技Ⅱ辑》;第1-164页 *

Also Published As

Publication number Publication date
CN117401173A (en) 2024-01-16

Similar Documents

Publication Publication Date Title
CN203093692U (en) Sunroof guiding linkage device
CN117401173B (en) Meteorological radar hangs and flies device
CN111734929A (en) LED screen storage and fixing device
CN112141150B (en) Carriage and vehicle with same
CN216641899U (en) Intelligent building safety protection door
CN215068526U (en) Agricultural intelligent warning device
CN215889690U (en) C-groove flat-open heavy anti-falling hinge
CN202208322U (en) Spare tire carrier and van vehicle using same
CN111591327B (en) Multifunctional cart for practical training of hotel management major
CN112746763B (en) Hidden garage and parking area
CN211617529U (en) Special vehicle with hydraulic balance support system for mobile emergency command shelter
CN113556082A (en) Distributed photovoltaic power generation device and adjusting method thereof
CN113104224A (en) Unmanned aerial vehicle aerial fixed point device based on openmv
CN111619469A (en) Stable-matching connecting assembly for automobile roof liner and skylight
CN218806615U (en) Unmanned aerial vehicle buffering that rises and falls bears frame
CN215007168U (en) Automobile clay model support convenient for assembling and disassembling automobile door
CN211467661U (en) Bag supporting device for square bottom bag making machine
CN217205912U (en) Lock for wing-unfolding carriage
CN115817647A (en) Sliding type vehicle rear baffle cover assembly
CN211204278U (en) Vertical ecological type air purifier
CN220662896U (en) Vehicle-mounted unmanned aerial vehicle intelligent airport starting platform
CN219007740U (en) Screen wall screen installation and maintenance mechanism of light commercial vehicle
CN219228503U (en) Seedling incubator
CN219295668U (en) Mounting structure of aircraft side guide rail
CN215664995U (en) Freeze and deposit device suitable for deposit protease sample EP pipe

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant