Satellite support head clamp tool for ship

Abstract

The utility model discloses a marine satellite support head clamp frock, it includes installation platform and installation device, the installation device is located on the installation platform, the installation device includes fixed post and three assembly spare, the fixed post vertical installation is fixed on the installation platform, three the assembly spare is evenly arranged in the fixed post circumference side, the assembly spare includes first fixed frame and second fixed frame, first fixed frame with second fixed frame is mutually perpendicular and is crossed and is arranged, and first fixed frame is perpendicularly arranged in the lateral wall of fixed post. The application has the effect of improving the production satellite support head qualification rate.

Description

TECHNICAL FIELD

[0001] The application relates to the technical field of clamp tooling, in particular to a marine satellite support head clamp tooling. BACKGROUND

[0002] Referring to Figure 1 The satellite support head is composed of a circular plate 20, a sleeve 21, three first support plates 22 and six second support plates 23. The sleeve 21 is welded and fixed to the upper end face of the circular plate 20, the side walls of the three first support plates 22 are uniformly welded and fixed to the circumferential side of the sleeve 21, the lower side of the first support plate 22 is welded and fixed to the upper end face of the circular plate 20, and two second support plates 23 are welded and fixed to the corresponding two side walls of the first support plate 22, and the lower side of the second support plate 23 is welded and fixed to the upper end face of the circular plate 20. According to the structure and fixing mode of the satellite support head, when the staff installs and fixes the satellite support head, the sleeve, the first support plate and the second support plate will be installed abnormally, so that the qualified rate of the satellite support head is reduced. CONTENT OF THE UTILITY MODEL

[0003] The utility model aims at the defects and deficiencies of prior art, and provides a marine satellite support head clamp tooling.

[0004] In order to realize the above-mentioned purpose, the utility model adopts the following technical scheme:

[0005] The installation device is located on the installation platform, the installation device includes a fixed column and three assembly parts, the fixed column is vertically installed and fixed on the installation platform, three assembly parts are circumferentially and uniformly arranged on the circumferential side of the fixed column, the assembly part includes a first fixed frame and a second fixed frame, the first fixed frame and the second fixed frame are arranged in perpendicular intersection, and the first fixed frame is vertically arranged on the side wall of the fixed column.

[0006] Preferably, the first fixed frame includes two first clamping plates, a first embedding groove is formed in the upper end of the first clamping plate, and the first embedding groove is used for inserting and fixing the first support plate.

[0007] Preferably, a first locking screw is rotationally connected to the side wall of the first clamping plate in a threaded manner, and one end of the first locking screw penetrates through the side wall of the first clamping plate and is inserted into the first embedding groove.

[0008] Preferably, the second fixed frame includes two second clamping plates, a second embedding groove is formed in the upper end of the second clamping plate, and the second embedding groove is used for inserting and fixing the second support plate.

[0009] Preferably, a second locking screw is rotatably connected to the inner wall of the second clamping plate, and one end of the second locking screw penetrates through the side wall of the second clamping plate and is inserted into the second embedding groove.

[0010] Preferably, the upper end surfaces of the first clamping plate and the second clamping plate are at the same horizontal level.

[0011] Preferably, a cross base is arranged at the lower end of the first fixing frame and the second fixing frame, and the two first clamping plates and the two second clamping plates are arranged at the upper end of the four corners of the cross base.

[0012] Preferably, a pressing block is arranged at the upper end of the fixing column, and a guide rod is arranged at the lower end of the pressing block, the guide rod is inserted into the fixing column in a sliding manner, and the pressing block is used to press and fix the sleeve on the fixing column.

[0013] Preferably, a pull ring is arranged at the upper end of the pressing block.

[0014] To sum up, the beneficial technical effects of the present application are as follows:

[0015] When the satellite support head needs to be assembled, first, the sleeve is sleeved and slid on the circumferential side of the fixing column until the lower end of the sleeve abuts against the mounting platform, then the three first support plates are respectively placed in the first embedding grooves of the two first clamping plates, the side of the first support plate abuts against the side wall of the sleeve, the first support plate is locked in the first embedding groove by rotating the two first locking screws, then the six second support plates are divided into three groups and are respectively placed on the corresponding two sides of the first support plate, the second support plate is placed in the second embedding groove of the second clamping plate, and the side of the second support plate abuts against the side wall of the first support plate, then the second support plate is locked in the second embedding groove by rotating the second locking screw, at this time, the contact surfaces of the sleeve, the first support plate and the second support plate can be welded and fixed by using a welding tool, then the assembled sleeve, the first support plate and the second support plate are taken out, the round plate is sleeved on the circumferential side of the fixing column until the bottom of the round plate is placed above the first clamping plate and the second clamping plate, then the assembled sleeve, the first support plate and the second support plate are placed on the round plate, finally, the contact surfaces are welded and fixed by using a welding tool. Through the above processing process, the jig tool can accurately install and fix the round plate, the sleeve, the three first support plates and the six second support plates into a satellite support head, thereby improving the qualified rate of producing the satellite support head. BRIEF DESCRIPTION OF DRAWINGS

[0016] Figure 1 is a structural schematic view of a satellite support head in the background art

[0017] Figure 2 is a structural schematic view of a jig tool in the embodiment;

[0018] Figure 3 is an explosion schematic diagram of the mounting device in the embodiment.

[0019] In the figure: 1, mounting platform; 2, mounting device; 3, mounting base; 4, fixed column; 5, assembly piece; 6, disc; 7, cross base; 8, mounting column; 9, first fixing frame; 10, second fixing frame; 11, first clamping plate; 12, second clamping plate; 13, first embedding groove; 14, second embedding groove; 15, first locking screw; 16, second locking screw; 17, pressing block; 18, guide rod; 19, pull ring; 20, round plate; 21, sleeve; 22, first support plate; 23, second support plate. DETAILED DESCRIPTION

[0020] The utility model will be further described below with reference to the drawings.

[0021] The embodiment of the application discloses a marine satellite support head clamp tool.

[0022] Reference Figure 2 and Figure 3 , comprising mounting platform 1 and mounting device 2, mounting device 2 is located on mounting platform 1, and mounting device 2 includes mounting base 3, fixed column 4 and three assembly pieces 5, mounting base 3 is fixed on mounting platform 1 by bolt, fixed column 4 and three assembly pieces 5 are located on mounting base 3, and three assembly pieces 5 are evenly placed on the circumferential side of fixed column 4.

[0023] Mounting base 3 includes disc 6 and three cross bases 7, one end of three cross bases 7 is integrally arranged on the side wall of disc 6, the upper end of disc 6 is integrally provided with mounting column 8, the lower end of fixed column 4 is sleeved on the circumferential side of mounting column 8 and is fixed by bolt, and assembly piece 5 is located on cross base 7.

[0024] Assembly piece 5 includes first fixing frame 9 and second fixing frame 10, first fixing frame 9 and second fixing frame 10 are placed perpendicularly and cross each other, first fixing frame 9 includes two first clamping plates 11, second fixing frame 10 includes two second clamping plates 12, two first clamping plates 11 and two second clamping plates 12 are integrally fixed on the upper end face of four corners of cross base 7 respectively, the upper end faces of first clamping plate 11 and second clamping plate 12 are at the same horizontal height, the upper end of first clamping plate 11 is provided with first embedding groove 13, the upper end of second clamping plate 12 is provided with second embedding groove 14, the first embedding grooves 13 of two first clamping plates 11 are correspondingly arranged, and the second embedding grooves 14 of two second clamping plates 12 are correspondingly arranged. Two first embedding grooves 13 are used for placing first support plate 22, and two second embedding grooves 14 are used for placing two second support plates 23 respectively.

[0025] The side wall of the first clamping plate 11 is threadedly connected with a first locking screw 15, one end of the first locking screw 15 is inserted into the first embedding groove 13 through the side wall of the first clamping plate 11, the side wall of the second clamping plate 12 is threadedly connected with a second locking screw 16, one end of the second locking screw 16 is inserted into the second embedding groove 14 through the side wall of the second clamping plate 12. After the first support plate 22 and the second support plate 23 are respectively placed in the first embedding groove 13 and the second embedding groove 14, the first locking screw 15 and the second locking screw 16 are respectively rotated, the inner ends of the first locking screw 15 and the second locking screw 16 are respectively tightly pressed against the first support plate 22 and the second support plate 23, so that the first support plate 22 and the second support plate 23 are respectively stably fixed in the first embedding groove 13 and the second embedding groove 14.

[0026] The upper end of the fixed column 4 is provided with a pressing block 17, the pressing block 17 is in a cylindrical shape, the diameter of the pressing block 17 is greater than the diameter of the fixed column 4, the lower end of the pressing block 17 is integrally provided with a guide rod 18, the guide rod 18 is inserted and slid in the upper end of the fixed column 4, the upper end of the pressing block 17 is welded with a pull ring 19, the pull ring 19 is in a "N" shape. The sleeve pipe 21 is sleeved and fixed on the circumferential side of the fixed column 4, then the guide rod 18 is inserted into the upper end of the fixed column 4 until the upper end of the sleeve pipe 21 abuts against the lower end of the pressing block 17, so that the sleeve pipe 21 is fixed on the circumferential side of the fixed column 4 by the pressing block 17, and the pull ring 19 drives the pressing block 17.

[0027] The implementation principle of the ship satellite support head clamp tool disclosed by the embodiment of the application is:

[0028] The sleeve pipe 21 is slidably sleeved on the circumferential side of the fixed column 4 until the lower end of the sleeve pipe 21 abuts against the installation platform 1, then the three first support plates 22 are respectively placed in the first embedding grooves 13 of the two first clamping plates 11, one side of the first support plate 22 abuts against the side wall of the sleeve pipe 21, the first support plate 22 is locked in the first embedding groove 13 by rotating the two first locking screws 15, then the six second support plates 23 are divided into three groups and placed on the corresponding two sides of the first support plate 22, and the second support plate 23 is placed in the second embedding groove 14 of the second clamping plate 12, one side of the second support plate 23 abuts against the side wall of the first support plate 22, then the second support plate 23 is locked in the second embedding groove 14 by rotating the second locking screw 16, at this time, the contact surfaces of the sleeve pipe 21, the first support plate 22 and the second support plate 23 can be welded and fixed by the welding tool, then the assembled sleeve pipe 21, first support plate 22 and second support plate 23 are taken out, the circular plate 20 is sleeved on the circumferential side of the fixed column 4 until the bottom of the circular plate 20 is placed above the first clamping plate 11 and the second clamping plate 12, then the assembled sleeve pipe 21, first support plate 22 and second support plate 23 are placed on the circular plate 20, finally the contact surfaces are welded and fixed by the welding tool.

[0029] The above merely describes preferred embodiments of the present application, and thus equivalent changes or modifications made in accordance with the structure, features and principles described in the patent application scope of the present application are included in the patent application scope of the present application.

Claims

1. A satellite support head clamp fixture for a marine vessel, characterized by: The utility model provides an installation platform (1) and installation device (2), installation device (2) is located on the installation platform (1), installation device (2) includes fixed column (4) and three assembly parts (5), fixed column (4) is vertically installed fixed on the installation platform (1), three assembly parts (5) are evenly arranged in the circumferential side of fixed column (4), and the assembly part (5) includes first fixed frame (9) and second fixed frame (10), and first fixed frame (9) and second fixed frame (10) are perpendicular and cross each other, and first fixed frame (9) is vertically arranged on the side wall of fixed column (4).

2. A satellite support head clamp tooling fixture for a marine vessel as claimed in claim 1, wherein, The first fixed frame (9) includes two first clamping plates (11), the upper end of the first clamping plate (11) is provided with a first embedding groove (13), and the first embedding groove (13) is used for inserting and fixing a first supporting plate (22).

3. A satellite support head clamp tooling fixture for a marine vessel as claimed in claim 2, wherein, The side wall of the first clamping plate (11) is screwedly and rotationally connected with a first locking screw (15), one end of the first locking screw (15) penetrates through the side wall of the first clamping plate (11) and is inserted into the first embedding groove (13).

4. A satellite support head clamp tooling fixture for a marine vessel as claimed in claim 2, wherein, The second fixed frame (10) includes two second clamping plates (12), the upper end of the second clamping plate (12) is provided with a second embedding groove (14), and the second embedding groove (14) is used for inserting and fixing a second supporting plate (23).

5. A satellite support head clamp tooling fixture for a marine vessel as claimed in claim 4, wherein, The side wall of the second clamping plate (12) is screwedly and rotationally connected with a second locking screw (16), one end of the second locking screw (16) penetrates through the side wall of the second clamping plate (12) and is inserted into the second embedding groove (14).

6. A satellite support head clamp tooling fixture for a marine vessel as defined in claim 4 wherein The upper end faces of the first clamping plate (11) and the second clamping plate (12) are at the same horizontal height.

7. A satellite support head clamp tooling fixture for a marine vessel as defined in claim 4 wherein, The lower ends of the first fixed frame (9) and the second fixed frame (10) are provided with a cross base (7), and the two first clamping plates (11) and the two second clamping plates (12) are arranged at the upper ends of four corners of the cross base (7).

8. A satellite support head clamp tooling fixture for a marine vessel as defined in claim 1, wherein The upper end of the fixed column (4) is provided with a pressing block (17), the lower end of the pressing block (17) is provided with a guide rod (18), the guide rod (18) is inserted and slid in the fixed column (4), and the pressing block (17) tightly fixes a sleeve (21) on the fixed column (4).

9. A satellite support head clamp tooling fixture for a marine vessel as claimed in claim 8, characterised in that The upper end of the pressing block (17) is provided with a pull ring (19).

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