CN215680938U

CN215680938U - High-stability satellite antenna

Info

Publication number: CN215680938U
Application number: CN202121798859.3U
Authority: CN
Inventors: 申展; 戴宜兴; 戴顺岐
Original assignee: Hebei Chaowei Communication Equipment Co ltd
Current assignee: Hebei Chaowei Communication Equipment Co ltd
Priority date: 2021-08-03
Filing date: 2021-08-03
Publication date: 2022-01-28
Anticipated expiration: 2031-08-03

Abstract

The application relates to a high-stability satellite antenna, which comprises a satellite antenna panel, wherein a panel bracket is arranged outside the satellite antenna panel, the bottom of the panel bracket is fixedly connected with a base, and the base is connected with a supporting frame; the bottom fixedly connected with axis of rotation of satellite antenna panel, the axis of rotation is arranged in the base and is rotated relatively the base and is connected, is equipped with the fixing device who fixes the satellite antenna panel on the panel support. This application has the effect that whether convenient detection satellite antenna panel warp.

Description

High-stability satellite antenna

Technical Field

The present application relates to the field of satellite antenna panels, and more particularly, to a highly stable satellite antenna.

Background

Satellite antenna panel can appear leading to the unstable condition of satellite antenna panel received signal because of satellite antenna panel warp in the use, often need dismantle satellite antenna panel, finds the problem, then processes the part that satellite antenna panel warp, and the testing process can produce a large amount of work load.

In view of the above-mentioned related art, the inventor believes that there is a defect that it is inconvenient for a consumer to detect a satellite antenna panel in a case where a signal received by the satellite antenna panel is unstable.

SUMMERY OF THE UTILITY MODEL

In order to solve the problem that the satellite antenna panel is inconvenient to detect, the application provides a high stable satellite antenna.

The application provides a high stable satellite antenna adopts following technical scheme:

a high-stability satellite antenna comprises a satellite antenna panel, wherein a panel bracket is arranged outside the satellite antenna panel, the bottom of the panel bracket is fixedly connected with a base, and the base is connected with a supporting frame; the bottom fixedly connected with axis of rotation of satellite antenna panel, the axis of rotation is arranged in the base and is rotated relatively the base and is connected, is equipped with the fixing device who fixes the satellite antenna panel on the panel support.

Through adopting above-mentioned technical scheme, rotate the satellite antenna panel, through fixing device, fix the satellite antenna panel on the panel support, through measuring the distance between satellite antenna panel unit and the panel support, learn whether the satellite antenna panel takes place to warp, this device has and need not to dismantle the satellite antenna panel, alright in order to have the advantage that warp and detect to the satellite antenna panel.

Optionally, the fixing device comprises a first fixing clamp, a support body which is staggered transversely and vertically is arranged on the back face of the satellite antenna panel, the first fixing clamp is rotatably connected with the panel support, two opposite first round holes are formed in the two sides of the first fixing clamp respectively, a first bolt is connected in each round hole in a threaded mode, and the first bolt can penetrate through the first round holes to be inconsistent with the support body.

Through adopting above-mentioned technical scheme, the both sides threaded connection of the first fixation clamp on the panel support has first bolt, offsets first bolt and support body, realizes that satellite antenna panel is fixed relative to the panel support.

Optionally, the support body includes a plurality of crossbearers and erects the frame, and panel support fixedly connected with has the locating lever that parallels with erecting the frame, sliding connection has adjusting part on the locating lever.

By adopting the technical scheme, the deformed part of the satellite antenna panel can be restored through the adjusting component.

Optionally, the adjusting part includes the sliding block, sliding block and locating lever sliding connection, and sliding block female connection has the pivot, rotates in the pivot to be connected with the second fixation clamp, and the both sides of second fixation clamp are equipped with two relative second round holes, and the equal threaded connection in the second round hole has the second bolt, and the second bolt can pass the second round hole and support body inconsistent.

Through adopting above-mentioned technical scheme, satellite antenna panel rotates and the sliding block can slide relative positioning lever relative to the panel support, and the second bolt and the support body of second fixation clamp both sides are inconsistent, through rotatory pivot, can restore the part that satellite antenna panel warp.

Optionally, a handle is fixedly connected to an end of the rotating shaft far away from the second fixing clamp.

By adopting the technical scheme, when the rotating shaft restores the deformed part of the satellite antenna panel, the rotating shaft can be operated more conveniently by the handle.

Optionally, the inner ends of the first bolt and the second bolt are fixedly connected with rubber pads.

Through adopting above-mentioned technical scheme, first bolt and second bolt contradict when the support body, and the rubber pad can prevent that first bolt and second bolt from causing wearing and tearing to the support body, reaches the effect of the lateral wall of protection support body.

Optionally, the bottom of the base is fixedly connected with a first support and a second support, the first support and the second support are both rotatably connected with the support frame, and a driving assembly for driving the satellite antenna panel to rotate relative to the support frame is arranged outside a connecting line of the first support and the second support.

Through adopting above-mentioned technical scheme, through first support, second support and drive assembly, the support frame rotation relatively of base.

Optionally, the driving assembly comprises a fixing seat, a screw rod is rotatably connected to the fixing seat, a sleeve is sleeved outside the screw rod, nuts are connected to the screw rods on two sides of the sleeve in a threaded mode, and the sleeve can rotate relative to the supporting frame.

Through adopting above-mentioned technical scheme, adjust the distance of base and support frame, and the nut that will be located the sleeve both sides is inconsistent with the sleeve, and when the sleeve was located the different positions of screw rod, the base all can be fixed relative to the support frame.

In summary, the present application includes at least one of the following beneficial technical effects:

1. the satellite antenna panel is rotated, the satellite antenna panel is fixed on the panel bracket through the fixing device, and whether the satellite antenna panel is deformed or not is known through measuring the distance between the satellite antenna panel unit and the panel bracket;

2. two sides of a first fixing clamp on the panel bracket are in threaded connection with first bolts, and the first bolts are abutted against the frame body, so that the satellite antenna panel is fixed relative to the panel bracket;

3. the satellite antenna panel rotates and the sliding block can slide relative to the positioning rod relative to the panel support, the second bolts on the two sides of the second fixing clamp are abutted to the frame body, and the deformed part of the satellite antenna panel can be restored through the rotating shaft.

Drawings

Fig. 1 is a schematic overall structure diagram of an embodiment of the present application.

Fig. 2 is a schematic view showing the structure of a satellite antenna panel.

FIG. 3 is a schematic view showing the structure of the fixture.

FIG. 4 is a schematic view of the highlighting adjustment assembly.

FIG. 5 is a schematic view showing the structure of the driving assembly.

Description of reference numerals: 1. a satellite antenna panel; 11. a rotating shaft; 12. a frame body; 121. a cross frame; 122. erecting; 2. a panel bracket; 3. a base; 31. a first bracket; 32. a second bracket; 33. a drive assembly; 331. a fixed seat; 332. a screw; 333. a sleeve; 334. a nut; 4. a support frame; 5. a fixing device; 51. a first fixing clip; 52. a first circular hole; 53. a first bolt; 6. Positioning a rod; 7. an adjustment assembly; 71. a slider; 72. a rotating shaft; 73. a handle; 74. a second fixing clip; 741. a second circular hole; 742. a second bolt; 8. and (7) a rubber pad.

Detailed Description

The present application is described in further detail below with reference to figures 1-5.

The embodiment of the application discloses a high-stability satellite antenna.

Referring to fig. 1 and 2, a highly stable satellite antenna includes a satellite antenna panel 1, a frame body 12 which is staggered horizontally and vertically is fixedly connected to the back of the satellite antenna panel 1, the frame body 12 includes a plurality of horizontal frames 121 and a plurality of vertical frames 122, the horizontal frames 121 have the same shape as the opening of the satellite antenna panel 1, the outer diameter of the horizontal frames 121 is smaller than the outer diameter of the opening of the satellite antenna panel 1, and the vertical frames 122 are perpendicular to the horizontal frames 121; a panel bracket 2 which has the same shape as the satellite antenna panel 1 is arranged outside the satellite antenna panel 1, and the bottom of the panel bracket 2 is fixedly connected with a base 3; the bottom fixedly connected with axis of rotation 11 of satellite antenna panel 1, axis of rotation 11 arrange in base 3 and relative base 3 rotates, when satellite antenna panel 1 rotates relative panel support 2, compares a plurality of positions of satellite antenna panel 1 with the same position of panel support 2, can detect whether satellite antenna panel 1 takes place to warp.

Referring to fig. 1 and 3, a fixing device 5 for fixing the satellite antenna panel 1 is disposed on the panel support 2, the fixing device 5 includes a first fixing clip 51, the first fixing clip 51 is rotatably connected to the panel support 2, two first circular holes 52 which are identical in size and opposite to each other are disposed on two sides of the first support 31, a first bolt 53 is screwed into each first circular hole 52, a rubber pad 8 is disposed at an inner end of each first bolt 53, and when the first bolt 53 penetrates through the first circular hole 52 and the rubber pad 8 to be abutted to the cross frame 121 of the support 12, the first fixing clip 51 can fix the panel support 2 to the satellite antenna panel 1.

Referring to fig. 1 and 4, a positioning rod 6 parallel to the vertical frame 122 is fixedly connected to the panel bracket 2, one end of the positioning rod 6 is located at the outermost edge of the panel bracket 2, and the other end of the positioning rod 6 is fixedly connected to the inner edge of the panel bracket 2; sliding connection has adjusting part 7 on locating lever 6, adjusting part 7 includes sliding block 71, sliding block 71 can slide relative to locating lever 6, sliding block 71 threaded connection has pivot 72, rotating connection has second fixation clamp 74 on pivot 72, the both sides of second fixation clamp 74 are equipped with two the same and relative second round holes 741 of size, equal threaded connection has second bolt 742 in the second round hole 741, the tip also is equipped with rubber pad 8 in second bolt 742, the tip fixedly connected with handle 73 of pivot 72 of keeping away from second fixation clamp 74, after satellite antenna panel 1 takes place to warp, through handle 73 on the rotatory pivot 72, second bolt 742 passes second round hole 741 and rubber pad 8 and support body 12's erects 122 when inconsistent, adjusting part 7 can realize restoreing the satellite antenna panel 1 of warping.

Referring to fig. 1 and 5, a first bracket 31 and a second bracket 32 are fixedly connected to the bottom of the base 3, the first bracket 31 and the second bracket 32 are both rotatably connected to the support frame 4, and a driving assembly 33 for driving the satellite antenna panel 1 to rotate relative to the support frame 4 is arranged outside a connection line between the first bracket 31 and the second bracket 32; the driving component 33 includes a fixing seat 331, the fixing seat 331 is fixedly connected with the base 3, the fixing seat 331 is rotatably connected with a screw rod 332, a sleeve 333 is sleeved outside the screw rod 332, nuts 334 are connected to the screw rods 332 on two sides of the sleeve 333 in a threaded manner, the two nuts 334 are respectively located on two sides of the sleeve 333 and are abutted to the sleeve 333, the sleeve 333 can rotate relative to the support frame 4, and by adjusting the distance between the base 3 and the sleeve 333 on the screw rod 332, the satellite antenna panel 1 can rotate relative to the support frame 4 and fix the satellite antenna panel 1 relative to the support frame 4.

The implementation principle of the high-stability satellite antenna in the embodiment of the application is as follows: the satellite antenna panel 1 can rotate relative to the panel support 2, the distances between a plurality of positions of the satellite antenna panel 1 and the same position of the panel support 2 are compared, the satellite antenna panel 1 is fixed relative to the panel support 2 through the fixing device 5, and whether the satellite antenna panel 1 deforms or not can be known; when the satellite antenna panel 1 is deformed, the deformed portion of the satellite antenna panel 1 can be repaired by the sliding block 71 sliding with respect to the positioning rod 6 and the satellite antenna panel 1 rotating with respect to the panel holder 2.

The above embodiments are preferred embodiments of the present application, and the protection scope of the present application is not limited by the above embodiments, so: all equivalent changes made according to the structure, shape and principle of the present application shall be covered by the protection scope of the present application.

Claims

1. A highly stable satellite antenna comprising a satellite antenna panel (1), characterized in that: a panel support (2) is arranged outside the satellite antenna panel (1), the bottom of the panel support (2) is fixedly connected with a base (3), and the base (3) is connected with a support frame (4); the bottom of satellite antenna panel (1) is fixedly connected with axis of rotation (11), and axis of rotation (11) are arranged in base (3) and rotate relative base (3) and are connected, are equipped with on panel support (2) with fixed fixing device (5) of satellite antenna panel (1).

2. A highly stable satellite antenna as claimed in claim 1, wherein: fixing device (5) are equipped with a crisscross support body (12) anyhow including first fixation clamp (51), the back of satellite antenna panel (1), and first fixation clamp (51) rotate with panel support (2) and be connected just the both sides of first fixation clamp (51) and be equipped with two relative first round holes (52) respectively, and equal threaded connection has first bolt (53) in first round hole (52), and first round hole (52) can be passed in first bolt (53) and support body (12) are inconsistent.

3. A highly stable satellite antenna as claimed in claim 2, wherein: the frame body (12) comprises a plurality of transverse frames (121) and vertical frames (122), the panel bracket (2) is fixedly connected with a positioning rod (6) parallel to the vertical frames (122), and the positioning rod (6) is connected with an adjusting component (7) in a sliding mode.

4. A highly stable satellite antenna as claimed in claim 3, wherein: adjusting part (7) include sliding block (71), sliding block (71) and locating lever (6) sliding connection, sliding block (71) internal thread connection has pivot (72), it is connected with second fixation clamp (74) to rotate on pivot (72), the both sides of second fixation clamp (74) are equipped with two relative second round holes (741), equal threaded connection has second bolt (742) in second round hole (741), second bolt (742) can pass second round hole (741) and support body (12) inconsistent.

5. A highly stable satellite antenna as claimed in claim 4, wherein: the end part of the rotating shaft (72) far away from the second fixing clamp (74) is fixedly connected with a handle (73).

6. A highly stable satellite antenna as claimed in claim 4, wherein: the inner ends of the first bolt (53) and the second bolt (742) are fixedly connected with rubber pads (8).

7. A highly stable satellite antenna as claimed in claim 1, wherein: the bottom fixedly connected with first support (31) and second support (32) of base (3), first support (31) and second support (32) all rotate with support frame (4) and are connected, and first support (31) and the line of second support (32) are equipped with drive satellite antenna panel (1) relative support frame (4) pivoted drive assembly (33) outward.

8. A highly stable satellite antenna as claimed in claim 7, wherein: the driving assembly (33) comprises a fixed seat (331), a screw rod (332) is connected to the fixed seat (331) in a rotating mode, a sleeve (333) is sleeved outside the screw rod (332), nuts (334) are connected to the screw rods (332) on two sides of the sleeve (333) in a threaded mode, and the sleeve (333) can rotate relative to the support frame (4).