CN217583725U

CN217583725U - Movable stable platform for radar for air control

Info

Publication number: CN217583725U
Application number: CN202122883795.3U
Authority: CN
Inventors: 申子阳
Original assignee: Shanxi Dashitong Electromechanical Technology Co ltd
Current assignee: Shanxi Dashitong Electromechanical Technology Co ltd
Priority date: 2021-11-23
Filing date: 2021-11-23
Publication date: 2022-10-14
Anticipated expiration: 2031-11-23

Abstract

The utility model discloses a portable stable platform of radar for air traffic control, including base and supporting platform, the inside outside of base is provided with the air pressure pole, the upper left side of base is provided with the rocking wheel, the commentaries on classics piece is installed to the inside intermediate position of base, the bearing is installed to the bottom of commentaries on classics piece, the top of base is provided with the support frame, the fixing base is installed to the top of support frame, the intermediate position of fixing base is provided with the locating part, servo motor is installed in the inside left side of fixing base, the upside of fixing base is connected with the rotating turret, supporting platform is installed to the upper right side of rotating turret. Be provided with the rotating turret, utilize pivoted gear can drive the rotating turret and rotate along the fixing base, can the multi-angle change supporting platform's direction, cooperation locating part for supporting platform is more stable, and supporting platform can change supporting platform's inclination through automatic telescopic link, and the user can change supporting platform's inclination in a flexible way.

Description

Movable stable platform for radar for air control

Technical Field

The utility model relates to a strutting arrangement technical field specifically is a portable stable platform of radar for air traffic control.

Background

The method is characterized in that the flight activities of the airplanes are monitored and controlled by utilizing communication and navigation technologies and monitoring means, the safe and orderly flight is ensured, different management airspaces including an airway, a flight information management area, an approach management area, a tower management area, a waiting airspace management area and the like are divided in the airspace of a flight route, different radar equipment is used according to different management areas, the management airspaces are divided at intervals, and the horizontal and vertical intervals among the airplanes form the basis of air traffic management.

The existing platform for air control is mostly a traditional fixed platform, the whole platform is inconvenient to move, the whole position, height and angle of the platform are fixed, and the position, height and angle of the platform are inconvenient to flexibly change according to the requirements of a user when the platform is used.

SUMMERY OF THE UTILITY MODEL

The utility model aims to provide a portable stabilized platform of radar for air control can effectively solve the current platform for air control in the background art, is traditional fixed platform mostly, and the platform is whole not be convenient for remove, and platform overall position, height and angle are fixed, inconvenient when using according to the nimble problem that changes position, height and the angle of platform of user's demand.

In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides a portable stabilized platform of radar for aerial control, includes base and supporting platform, the inside outside of base is provided with the air pressure pole, the upper left side of base is provided with the rocking wheel, the inside intermediate position of base is installed and is changeed the piece, change the bottom of piece and install the bearing, the top of base is provided with the support frame, the fixing base is installed to the top of support frame, the intermediate position of fixing base is provided with the locating part, servo motor is installed in the inside left side of fixing base, servo motor's output has cup jointed the gear, the upside of fixing base is connected with the rotating turret, supporting platform is installed to the upper right side of rotating turret, supporting platform's right-hand member is provided with the pivot.

Furthermore, the tail end of the air pressure rod is provided with a universal wheel, the upper surface of the universal wheel is tightly attached to the output end of the air pressure rod, the universal wheels are uniformly distributed along the bottom side of the base, and the universal wheel and the base form a telescopic structure through the air pressure rod.

Furthermore, a chain belt is connected to the right side of the rocking wheel, the chain belt is connected with a rotating block in a meshing mode, the rotating block forms a linkage structure with the rocking wheel through the chain belt, and the rotating block forms a rotating structure with the base through a bearing.

Further, a threaded rod is installed on the inner side of the support frame, the threaded rod is symmetrically distributed about the central axis of the support frame, the external thread of the threaded rod is matched with the internal thread of the support frame, the threaded rod is connected with the support frame in a threaded mode, and the support frame passes through a telescopic structure formed between the threaded rod and the base.

Further, the upside of gear is connected with the meshing teeth of a cogwheel, the connected mode between the meshing teeth of a cogwheel and the gear is connected for the meshing, the meshing teeth of a cogwheel is along rotating turret outer fringe evenly distributed, the rotating turret passes through to constitute revolution mechanic between bearing and the fixing base, the fixing base passes through to constitute the block structure between locating part and the rotating turret.

Furthermore, supporting platform's downside is connected with automatic telescopic link, supporting platform passes through to constitute rotating-structure between pivot and the rotating turret, constitute linkage between supporting platform and the automatic telescopic link, the locating part is the symmetric distribution about the axis position of rotating turret.

Compared with the prior art, the beneficial effects of the utility model are that:

1. the utility model discloses be provided with the support frame that can go up and down, the support frame utilizes the screw thread to be connected with the threaded rod, rotates through letting the threaded rod for the highly convenient change of support frame, the height of platform is changed in a flexible way to the convenience according to the user's demand.

2. The utility model discloses be provided with can the pivoted rotating turret, utilize the pivoted gear can drive the rotating turret and rotate along the fixing base, can the multi-angle change supporting platform's direction, cooperation locating part for supporting platform is more stable, and supporting platform can change supporting platform's inclination through automatic telescopic link, and the user can change supporting platform's inclination in a flexible way.

3. The utility model discloses be provided with the universal wheel, the universal wheel utilizes the air pressure bar can realize raising and lowering functions, conveniently removes and in the immigration base for the platform is whole can realize removing and the nimble transformation between fixed.

Drawings

Fig. 1 is a schematic view of a main view structure of a movable stable platform of a radar for air traffic control according to the present invention;

fig. 2 is a schematic view of a connection structure between a threaded rod and a base of the radar movable stabilized platform for air traffic control according to the present invention;

fig. 3 is the utility model relates to a but aerial control is with radar moving stabilization platform's rotating turret and fixing base connection structure sketch map.

In the figure: 1. a base; 2. a pneumatic rod; 3. a universal wheel; 4. shaking the wheel; 5. a chain belt; 6. rotating the block; 7. a bearing; 8. a support frame; 9. a threaded rod; 10. a fixed seat; 11. a stopper; 12. a servo motor; 13. a gear; 14. meshing gear teeth; 15. a rotating frame; 16. a support platform; 17. a rotating shaft; 18. automatic telescopic link.

Detailed Description

In order to make the technical means, creation features, achievement purposes and functions of the present invention easy to understand, the present invention is further described below with reference to the following embodiments.

Example 1

Referring to fig. 1-3, the present invention provides a technical solution: the utility model provides a portable stabilized platform of radar for aerial control, which comprises a base 1, air pressure bar 2, the universal wheel 3, rocking wheel 4, the chain belt 5, change the piece 6, bearing 7, support frame 8, threaded rod 9, fixing base 10, locating part 11, servo motor 12, gear 13, the meshing teeth of a cogwheel 14, rotating turret 15, supporting platform 16, the pivot 17, automatic telescopic link 18, the inside outside of base 1 is provided with air pressure bar 2, the upper left side of base 1 is provided with rocking wheel 4, the inside intermediate position of base 1 installs commentaries on classics piece 6, bearing 7 is installed to the bottom of commentaries on classics piece 6, the top of base 1 is provided with support frame 8, fixing base 10 is installed to support frame 8's top, the intermediate position of fixing base 10 is provided with locating part 11, servo motor 12 is installed on the inside left side of fixing base 10, gear 13 has been cup jointed to servo motor 12's output, the upside of fixing base 10 is connected with rotating turret 15, supporting platform 16 is installed to the upper right side of rotating turret 15, the right-hand member of supporting platform 16 is provided with pivot 17.

The universal wheel 3 is installed to the tail end of pneumatic cylinder 2, closely laminates between the upper surface of universal wheel 3 and the output of pneumatic cylinder 2, and the bottom side evenly distributed along base 1 is followed to the universal wheel 3, and the universal wheel 3 passes through to constitute extending structure between pneumatic cylinder 2 and the base 1. Utilize atmospheric pressure equipment to change the inside atmospheric pressure of pneumatic rod 2 for universal wheel 3 can stretch out and draw back along base 1, convenient removal and fixed equipment.

The right side of the rocking wheel 4 is connected with a chain belt 5, the chain belt 5 is connected with a rotating block 6 in a meshing manner, the rotating block 6 forms a linkage structure with the rocking wheel 4 through the chain belt 5, and the rotating block 6 forms a rotating structure with the base 1 through a bearing 7. The user is through rotating rocking wheel 4, cooperation chain belt 5 for the piece 6 that changes can drive threaded rod 9 and rotate, provides power for threaded rod 9 rotates.

Threaded rod 9 is installed to the inboard of support frame 8, and threaded rod 9 is the symmetric distribution about the axis position of support frame 8, and the external screw thread of threaded rod 9 is identical with the internal thread of support frame 8, and the connected mode between threaded rod 9 and the support frame 8 is threaded connection, and support frame 8 passes through to constitute extending structure between threaded rod 9 and the base 1. The supporting frame 8 is connected with the threaded rod 9 through threads, and the height direction of the supporting frame 8 is changed by rotating the threaded rod 9.

The upper side of the gear 13 is connected with meshing gear teeth 14, the meshing gear teeth 14 are connected with the gear 13 in a meshing manner, the meshing gear teeth 14 are uniformly distributed along the outer edge of the rotating frame 15, the rotating frame 15 and the fixed seat 10 form a rotating structure through the bearing 7, and the fixed seat 10 and the rotating frame 15 form a clamping structure through the limiting part 11. The gear 13 can drive the rotating frame 15 to rotate through the meshing gear teeth 14, the direction of the supporting platform 16 is changed, and the limiting piece 11 can increase the stability of the supporting platform 16.

An automatic telescopic rod 18 is connected to the lower side of the supporting platform 16, a rotating structure is formed between the supporting platform 16 and the rotating frame 15 through a rotating shaft 17, a linkage structure is formed between the supporting platform 16 and the automatic telescopic rod 18, and the limiting parts 11 are symmetrically distributed about the central axis of the rotating frame 15. The support platform 16 is powered by the flexibility of the automatic telescoping pole 18 so that the support platform 16 can be tilted at different angles.

It should be noted that, the utility model relates to a radar movable stable platform for air control, when in use, the device is connected with an external power supply, the inside of the device is provided with air pressure equipment for air supply, a user utilizes the air pressure equipment to increase the air pressure in an air pressure rod 2, drives a universal wheel 3 to move out of a base 1, after pushing the platform to move to a proper position, reduces the air pressure in the air pressure rod 2, withdraws the universal wheel 3, fixes the platform, rotates a rocking wheel 4, drives a chain belt 5 to move, the chain belt 5 drives a rotating block 6 to rotate along a bearing 7, drives a threaded rod 9 to rotate, because the threaded rod 9 is connected with a supporting frame 8 by screw threads, drives the supporting frame 8 to ascend, promotes the height of a fixed seat 10, stops after the supporting platform 16 ascends to a proper height, in the use process, when the direction of the supporting platform 16 needs to be changed, the air pressure in the limiting part 11 can be reduced, the limiting part 11 is retracted, the rotating frame 15 is separated from the rotating frame, the servo motor 12 works to drive the gear 13 to rotate, the gear 13 is connected with the meshing gear teeth 14 in a meshing mode to drive the rotating frame 15 to rotate along the supporting frame 8, the angle of the supporting platform 16 is changed, after the angle is adjusted to a proper angle, the servo motor 12 stops working, the air pressure at the position of the limiting part 11 is increased, the rotating frame 15 is inserted into the rotating frame 15, the stability of the rotating frame 15 is improved, when the inclination angle of the supporting platform 16 needs to be changed, the automatic telescopic rod 18 works, the length of the automatic telescopic rod 18 is increased, the supporting platform 16 is driven to rotate along the rotating shaft 17, the inclination angle of the supporting platform 16 is changed, and the supporting platform 16 is adjusted to a proper angle.

The foregoing shows and describes the basic principles and principal features of the invention, together with the advantages thereof. It should be understood by those skilled in the art that the present invention is not limited to the above embodiments, and the above embodiments and descriptions are only illustrative of the principles of the present invention, and that various changes and modifications may be made without departing from the spirit and scope of the present invention, and all such changes and modifications fall within the scope of the present invention as claimed. The scope of the invention is defined by the appended claims and equivalents thereof.

Claims

1. The utility model provides a portable stable platform of radar for air traffic control, includes base (1) and supporting platform (16), its characterized in that: the inside outside of base (1) is provided with air pressure bar (2), the upper left side of base (1) is provided with rocking wheel (4), the inside intermediate position of base (1) is installed and is changeed piece (6), bearing (7) are installed to the bottom of changeing piece (6), the top of base (1) is provided with support frame (8), fixing base (10) are installed to the top of support frame (8), the intermediate position of fixing base (10) is provided with locating part (11), servo motor (12) are installed in the inside left side of fixing base (10), gear (13) have been cup jointed to the output of servo motor (12), the upside of fixing base (10) is connected with rotating turret (15), supporting platform (16) are installed to the upper right side of rotating turret (15), the right-hand member of supporting platform (16) is provided with pivot (17).

2. The radar movable stable platform for air traffic control according to claim 1, wherein: the universal wheel (3) is installed to the tail end of pneumatic rod (2), closely laminate between the upper surface of universal wheel (3) and the output of pneumatic rod (2), constitute extending structure between universal wheel (3) through pneumatic rod (2) and base (1).

3. The radar movable stable platform for air traffic control according to claim 1, wherein: the right side of rocking wheel (4) is connected with chain belt (5), the connected mode between chain belt (5) and commentaries on classics piece (6) is connected for the meshing, change piece (6) through chain belt (5) and rock and constitute linkage structure between wheel (4).

4. The radar movable stable platform for air control according to claim 1, wherein: threaded rod (9) are installed to the inboard of support frame (8), the connected mode between threaded rod (9) and support frame (8) is threaded connection, support frame (8) pass through between threaded rod (9) and base (1) constitute extending structure.

5. The radar movable stable platform for air control according to claim 1, wherein: the upper side of gear (13) is connected with meshing teeth of a cogwheel (14), the connected mode between meshing teeth of a cogwheel (14) and gear (13) is for the meshing connection, fixing base (10) constitute the block structure through between locating part (11) and rotating turret (15).

6. The radar movable stable platform for air traffic control according to claim 1, wherein: the downside of supporting platform (16) is connected with automatic telescopic link (18), constitute rotating-structure between supporting platform (16) through pivot (17) and rotating turret (15), constitute linkage between supporting platform (16) and automatic telescopic link (18).