A support structure for a ship fuel tank

By designing a clamping mechanism and a sliding adjustment mechanism for rotatable clamping arm and telescopic cylinder, the multi-size and length adaptation problems of the existing fuel tank fixed structure are solved, and the convenient installation and disassembly of the fuel tank is achieved.

CN119975647BActive Publication Date: 2025-07-04SHANGHAI KAIREN GAS ENG CO LTD
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Patent Information

Application Number
CN202510472512.6
Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
Filing Date
2025-04-16
Publication Date
2025-07-04
Estimated Expiration
2045-04-16

AI Technical Summary

Technical Problem

The existing fixed structure of the ship fuel tank does not have the functions of removable multi-size clamping and multi-length adjustment, which makes the installation and disassembly of fuel tanks cumbersome, and is inconvenient for the adaptation of different sizes and lengths.

Method used

A bracket structure including a base, a clamping mechanism and a sliding adjustment mechanism is designed. Multi-size clamping and fixing of the fuel tank is achieved through the rotatable clamping arm of the clamping mechanism and the telescopic cylinder. The clamping distance is adjusted by the sliding adjustment mechanism to accommodate fuel tanks of different lengths.

Benefits of technology

It realizes convenient clamping and fixing of fuel tanks of different sizes and lengths, simplifies the installation and disassembly process, and improves the removability and adaptability of fuel tanks.

✦ Generated by Eureka AI based on patent content.

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Abstract

The present invention relates to the technical field of fixing ship fuel tanks, and a bracket structure for a ship fuel tank, including a base. A chute is provided on the upper surface of the base. Above the base, there is a clamping mechanism that facilitates clamping and fixing fuel tanks of different sizes. On the upper surface of the base, there is a sliding adjustment mechanism that facilitates adjusting the distance between two sets of clamping mechanisms to adapt to clamping and fixing fuel tanks of different lengths. A support is fixedly connected to the upper surface of the sliding adjustment mechanism. The first rotating shaft is inserted through both ends of the support. In this bracket structure for a ship fuel tank, anti-slip pads are provided on the inner sides of the first clamping arm and the second clamping arm that are successively connected through the first rotating shaft and the second rotating shaft on the support. A first telescopic cylinder and a second telescopic cylinder are respectively connected to the first clamping arm and the second rotating shaft, so as to control the first clamping arm and the second clamping arm to rotate inwards and retract or expand to clamp and fix fuel tanks of different sizes.
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Description

Technical Field

[0001] The present invention relates to the technical field of ship fuel tank fixing, and specifically relates to a support structure for a ship fuel tank. Background Art

[0002] A ship fuel tank is a key component of a ship's power system. Its main function is to store fuels such as liquefied natural gas (LNG) and supply energy to equipment such as the ship's engine and generator.

[0003] The prior art does not have a structure for detachable multi-size clamping and fixing and multi-length adjustable fixing of the fuel tank when in use. When the existing fuel tank is in use, the installation of the fuel tank mostly relies on the brackets welded by itself for fixing. Although it has a good fixing effect, when disassembling, assembling, inspecting or replacing the fuel tank, only welding and cutting are used, which is rather cumbersome. Moreover, since the lengths of the fuel tanks are different, when installing the fuel tank, it is necessary to use a support frame that matches it to adjust the support spacing and then perform welding and fixing installation, which is not convenient to use. Based on the deficiencies of the existing technology, the present invention designs a support structure for a ship fuel tank. Summary of the Invention

[0004] The present invention provides a support structure for a ship fuel tank, which has the advantages of detachable multi-size clamping and fixing and multi-length adjustable fixing of the fuel tank.

[0005] The present invention provides the following technical solution: A support structure for a ship fuel tank, including a base. A chute is provided on the upper surface of the base. Above the base, there is a clamping mechanism for facilitating clamping and fixing of fuel tanks of different sizes, and a sliding adjustment mechanism for facilitating adjustment of the distance between two sets of clamping mechanisms to adapt to clamping and fixing of fuel tanks of different lengths is provided on the upper surface of the base;

[0006] Clamping mechanism, the clamping mechanism includes a support base, a first rotating shaft, a first clamping arm, a second rotating shaft, a second clamping arm, an anti-slip gasket, a first lower hinge seat, a first upper hinge seat, a first telescopic cylinder, a second lower hinge seat, a second upper hinge seat and a second telescopic cylinder. The support base is fixedly connected to the upper surface of the sliding adjustment mechanism. The first rotating shaft is inserted through both ends of the support base. The first clamping arm is hinged at both ends of the support base. The second rotating shaft is inserted through the top end of the first clamping arm. The second clamping arm is hinged at the top end of the first clamping arm. The anti-slip gasket is arranged on the inner sides of the support base, the first clamping arm and the second clamping arm. The first lower hinge seat is fixedly connected to the sliding adjustment mechanism. The first upper hinge seat is fixedly connected to the side wall of the first clamping arm. The upper and lower ends of the first telescopic cylinder are respectively rotatably connected in the first lower hinge seat and the first upper hinge seat. The second lower hinge seat is fixedly connected to the outer surface of the first clamping arm. The second upper hinge seat is fixedly connected to the outer surface of the second clamping arm. The upper and lower ends of the second telescopic cylinder are respectively rotatably connected in the second lower hinge seat and the second upper hinge seat.

[0007] As a preferred technical solution of the present invention, the sliding adjustment mechanism includes a sliding seat, an adjustment seat, side clamping frames, rotating grooves, rotating rods, rotating wheels, a top cover, telescopic top rods, anti-slip clamping plates, locking plates and threaded grooves. The sliding seat is slidably connected to the upper surface of the base. The adjustment seat is fixedly connected to the lower surface of the sliding seat. The side clamping frames are fixedly connected to both ends of the sliding seat. The rotating grooves are penetrated and opened at both ends of the sliding seat. The rotating rods are fixedly connected inside the rotating grooves. The rotating wheels are rotatably connected to the rotating rods. The top cover is arranged above the rotating grooves. The telescopic top rods are arranged at the bottoms of the side clamping frames. The anti-slip clamping plates are fixedly connected to the top ends of the telescopic top rods. The locking plates are fixedly connected to the lower surface at the edge of the top of the base. The threaded grooves are penetrated and opened on the adjustment seat.

[0008] As a preferred technical solution of the present invention, a fixing plate is fixedly connected to the bottom of the base. A fixing block is fixedly connected to the fixing plate. An installation hole is penetrated and opened in the fixing block.

[0009] As a preferred technical solution of the present invention, an inner groove is opened at the bottom of the sliding groove. A threaded rod is rotatably connected inside the inner groove. A motor is fixedly connected to one side of the base.

[0010] As a preferred technical solution of the present invention, the first rotating shaft is inserted through the rotational hinge joint of the support base and the first clamping arm. The second rotating shaft is arranged at the rotational hinge joint of the first clamping arm and the second clamping arm.

[0011] As a preferred technical solution of the present invention, the support base is fixedly connected to the upper surface of the sliding seat. The first lower hinge seat is fixedly connected to the upper surface of the sliding seat.

[0012] As a preferred technical solution of the present invention, the adjusting seat is slidably connected inside the chute and the inner groove, and the top cover is fixedly connected to the upper surfaces at both ends of the sliding seat.

[0013] As a preferred technical solution of the present invention, the side clamping frames are slidably clamped on both sides of the base. The telescopic end of the telescopic top rod passes through the bottom of the side clamping frame and is connected to the anti-slip clamping plate. The anti-slip clamping plate is arranged below the locking plate and the anti-slip clamping plate is clamped with the locking plate.

[0014] As a preferred technical solution of the present invention, the threaded rod is rotationally connected to the inside of the threaded groove by threads, and the thread directions of the left and right groups of threaded grooves are arranged in opposite directions.

[0015] As a preferred technical solution of the present invention, one end of the threaded rod passes through the base and is connected to the output end of the motor.

[0016] Compared with the prior art, the present invention has the following beneficial effects:

[0017] 1. For the bracket structure of a ship fuel tank, through the contraction of the first telescopic cylinder and the second telescopic cylinder to pull and expand the first clamping arm and the second clamping arm outwardly, and then hoist the fuel tank onto the two brackets and fit and fix it with the anti-slip gasket. At this time, first start the first telescopic cylinder to extend. The extended first telescopic cylinder, under the support and limit of the first lower hinge seat, pushes the first clamping arm and the first upper hinge seat to rotate inwardly around the first rotating shaft, so that the two first clamping arms retract inwardly to contact and clamp the fuel tank. Then start the second telescopic cylinder. Under the support and limit of the second lower hinge seat, it pushes the second clamping arm and the second upper hinge seat to rotate inwardly around the second rotating shaft, so that the second clamping arm gradually moves inwardly to contact the outer wall of the fuel tank for clamping and fixing. At this time, the two ends of the fuel tank are in a semi-wrapped clamping state to complete the fixing. This device is convenient for clamping and fixing fuel tanks of different sizes.

[0018] 2. For the bracket structure of a ship fuel tank, by measuring the distance between the clamping and fixing points at the left and right ends of the fuel tank, and then starting the telescopic top rod to contract and pull the anti-slip clamping plate out from the bottom of the locking plate to release the lock. At this time, the motor drives the threaded rod to rotate and uses the threaded groove to push the two adjusting seats and the sliding seat to move inwardly or outwardly to both ends of the base under the sliding support of the rotating wheels and drive the clamping mechanism to move accordingly to adjust the distance. Until the distance between the two clamping mechanisms is the same as the pre-measured distance of the fixed points. After the adjustment is completed, the telescopic top rod extends to push the anti-slip clamping plate into the locking plate to lock the positions of the sliding seat and the clamping mechanism. This device is convenient for clamping and fixing fuel tanks of different lengths. Description of the Drawings

[0019] Figure 1 It is a schematic diagram of the overall structure of the present invention;

[0020] Figure 2 Schematic diagram of the installation and fixing frame structure of the fuel tank of the present invention;

[0021] Figure 3 Schematic diagram of the internal sectional structure of the base of the present invention;

[0022] Figure 4 Schematic diagram of the exploded structure of the chute and the sliding adjustment mechanism of the present invention;

[0023] Figure 5 Schematic diagram of the exploded structure of the sliding adjustment mechanism and the base of the present invention;

[0024] Figure 6 Schematic diagram of the main structure of the sliding adjustment mechanism of the present invention;

[0025] Figure 7 Schematic diagram of the connection structure between the clamping mechanism and the sliding seat of the present invention;

[0026] Figure 8 Schematic diagram of the main structure of the clamping mechanism of the present invention.

[0027] In the figure: 1. Base; 101. Fixed plate; 102. Fixed block; 103. Mounting hole; 2. Chute; 201. Inner groove; 202. Threaded rod; 203. Motor; 3. Sliding adjustment mechanism; 301. Sliding seat; 302. Adjusting seat; 303. Side clamping frame; 304. Rotating groove; 305. Rotating rod; 306. Rotating wheel; 307. Top cover; 308. Telescopic ejector rod; 309. Anti-slip clamping plate; 310. Locking plate; 311. Threaded groove; 4. Clamping mechanism; 401. Support seat; 402. First rotating shaft; 403. First clamping arm; 404. Second rotating shaft; 405. Second clamping arm; 406. Anti-slip gasket; 407. First lower hinge seat; 408. First upper hinge seat; 409. First telescopic cylinder; 410. Second lower hinge seat; 411. Second upper hinge seat; 412. Second telescopic cylinder. Detailed implementation manners

[0028] Next, the technical solutions in the embodiments of the present invention will be clearly and completely described in conjunction with the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only a part of the embodiments of the present invention, rather than all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art without making creative efforts shall fall within the protection scope of the present invention.

[0029] Please refer to Figures 1 - 8, A support structure for a ship fuel tank, including a base 1. A chute 2 is opened on the upper surface of the base 1. Above the base 1, there is a clamping mechanism 4 that facilitates clamping and fixing fuel tanks of different sizes. On the upper surface of the base 1, there is a sliding adjustment mechanism 3 that facilitates adjusting the distance between the two groups of clamping mechanisms 4 to adapt to clamping and fixing fuel tanks of different lengths. The bottom of the base 1 is fixedly connected with a fixing plate 101, and a fixing block 102 is fixedly connected to the fixing plate 101. An installation hole 103 is penetrated and opened on the fixing block 102.

[0030] Please refer to Figures 3 - 4 , An inner groove 201 is opened at the bottom of the chute 2. A threaded rod 202 is rotatably connected inside the inner groove 201. One side of the base 1 is fixedly connected with a motor 203. The threaded rod 202 is threadedly rotatably connected inside the threaded groove 311, and the thread directions of the left and right two groups of threaded grooves 311 are arranged in opposite directions. One end of the threaded rod 202 penetrates the base 1 and is connected to the output end of the motor 203.

[0031] Please refer to Figures 7 - 8 , The clamping mechanism 4 includes a support 401, a first rotating shaft 402, a first clamping arm 403, a second rotating shaft 404, a second clamping arm 405, an anti-slip gasket 406, a first lower hinge seat 407, a first upper hinge seat 408, a first telescopic cylinder 409, a second lower hinge seat 410, a second upper hinge seat 411, and a second telescopic cylinder 412. The support 401 is fixedly connected to the upper surface of the sliding adjustment mechanism 3. The first rotating shaft 402 is inserted through both ends of the support 401. The first clamping arm 403 is hinged at both ends of the support 401. The second rotating shaft 404 is inserted through the top end of the first clamping arm 403. The second clamping arm 405 is hinged at the top end of the first clamping arm 403. The anti-slip gasket 406 is arranged on the inner sides of the support 401, the first clamping arm 403, and the second clamping arm 405. The first lower hinge seat 407 is fixedly connected to the sliding adjustment mechanism 3. The first upper hinge seat 408 is fixedly connected to the side wall of the first clamping arm 403. The upper and lower ends of the first telescopic cylinder 409 are respectively rotatably connected inside the first lower hinge seat 407 and the first upper hinge seat 408. The second lower hinge seat 410 is fixedly connected to the outer surface of the first clamping arm 403. The second upper hinge seat 411 is fixedly connected to the outer surface of the second clamping arm 405. The upper and lower ends of the second telescopic cylinder 412 are respectively rotatably connected inside the second lower hinge seat 410 and the second upper hinge seat 411. The first rotating shaft 402 is inserted through the rotational hinge between the support 401 and the first clamping arm 403. The second rotating shaft 404 is arranged at the rotational hinge between the first clamping arm 403 and the second clamping arm 405. The support 401 is fixedly connected to the upper surface of the sliding seat 301. The first lower hinge seat 407 is fixedly connected to the upper surface of the sliding seat 301.

[0032] By providing a support base 401, a first rotating shaft 402, a first clamping arm 403, a second rotating shaft 404, and a second clamping arm 405, it is convenient to clamp and fix fuel tanks of different sizes. By providing an anti-slip gasket 406, it is convenient to assist in anti-slip fixing of the fuel tank clamped and fixed within the support base 401, the first clamping arm 403, and the second clamping arm 405. By providing a first lower hinge seat 407, a first upper hinge seat 408, and a first telescopic cylinder 409, it is convenient to push the first clamping arms 403 at both ends of the support base 401 to rotate inwards to fit and fix the bottom of the outer surface of fuel tanks of different sizes. By providing a second lower hinge seat 410, a second upper hinge seat 411, and a second telescopic cylinder 412, it is convenient to push the second clamping arm 405 to rotate inwards to clamp and fix the upper middle part of the outer surface of fuel tanks of different sizes.

[0033] Please refer to Figures 4 - 6 As shown in Figures 4 - 6 , the sliding adjustment mechanism 3 includes a sliding seat 301, an adjustment seat 302, side clamping frames 303, rotating grooves 304, rotating rods 305, rotating wheels 306, top covers 307, telescopic top rods 308, anti-slip clamping plates 309, locking plates 310, and threaded grooves 311. The sliding seat 301 is slidably connected to the upper surface of the base 1. The adjustment seat 302 is fixedly connected to the lower surface of the sliding seat 301. The side clamping frames 303 are fixedly connected to both ends of the sliding seat 301. The rotating grooves 304 are penetrated and opened at both ends of the sliding seat 301. The rotating rods 305 are fixedly connected to the inside of the rotating grooves 304. The rotating wheels 306 are rotatably connected to the rotating rods 305. The top covers 307 are arranged above the rotating grooves 304. The telescopic top rods 308 are arranged at the bottom of the side clamping frames 303. The anti-slip clamping plates 309 are fixedly connected to the top ends of the telescopic top rods 308. The locking plates 310 are fixedly connected to the lower surface at the edge of the top of the base 1. The threaded grooves 311 are penetrated and opened on the adjustment seat 302. The adjustment seat 302 is slidably connected to the inside of the sliding groove 2 and the inner groove 201. The top covers 307 are fixedly connected to the upper surfaces at both ends of the sliding seat 301. The side clamping frames 303 are slidably clamped to both sides of the base 1. The telescopic ends of the telescopic top rods 308 penetrate through the bottom of the side clamping frames 303 and are connected to the anti-slip clamping plates 309. The anti-slip clamping plates 309 are arranged below the locking plates 310 and the anti-slip clamping plates 309 are clamped with the locking plates 310.

[0034] By providing the sliding seat 301, the adjustment seat 302, the rotating grooves 304, the rotating rods 305, the rotating wheels 306, and the threaded grooves 311, and the threaded grooves 311 are threadedly connected to the threaded rod 202, it is convenient to move and adjust the sliding seat 301, the adjustment seat 302, i.e., the clamping mechanism 4 at the top, by using the threaded rod 202. Furthermore, the clamping mechanism 4 can clamp and fix fuel tanks of different lengths. By providing the side clamping frames 303, the telescopic top rods 308, the anti-slip clamping plates 309, and the locking plates 310, it is convenient to lock the positions of the sliding seat 301, the adjustment seat 302, and the clamping mechanism 4.

[0035] Working principle: When a support structure of a ship fuel tank is in use, in the initial state, the fixing plate 101 is fixed at the bottom of the base 1. The fixing block 102 installed on the fixing plate 101 is provided with an installation hole 103 for fixing the base 1. A threaded rod 202 is rotatably connected in the chute 2 and the inner groove 201 opened on the base 1 through a motor 203. The threaded rod 202 is connected to an adjusting seat 302 slidably connected in the inner groove 201. A side clamping frame 303 is connected to the top of the adjusting seat 302. Both ends of the side clamping frame 303 are supported by rollers 306 and a clamping mechanism 4 is also connected to the upper surface, so as to adjust the distance between the two clamping mechanisms 4 to realize the clamping and fixing of fuel tanks of different lengths. Anti-slip pads 406 are arranged on the inner sides of the first clamping arm 403 and the second clamping arm 405 which are sequentially connected through the first rotating shaft 402 and the second rotating shaft 404 on the support 401. A first telescopic cylinder 409 and a second telescopic cylinder 412 are respectively connected to the first clamping arm 403 and the second rotating shaft 404, so as to control the first clamping arm 403 and the second clamping arm 405 to rotate inwards or expand to clamp and fix fuel tanks of different sizes;

[0036] When it is necessary to clamp and fix fuel tanks of different sizes, first, the first telescopic cylinder 409 and the second telescopic cylinder 412 contract to pull the first clamping arm 403 and the second clamping arm 405 to rotate and expand outwards. Then, the fuel tank is hoisted onto the two supports 401 and fixed in contact with the anti-slip pads 406. At this time, first start the first telescopic cylinder 409 to extend. The extended first telescopic cylinder 409 pushes the first clamping arm 403 and the first upper hinge seat 408 to rotate inwards around the first rotating shaft 402 under the support and limit of the first lower hinge seat 407, so that the first clamping arms 403 on both sides move inwards to contact and clamp the fuel tank. Then start the second telescopic cylinder 412 to push the second clamping arm 405 and the second upper hinge seat 411 to rotate inwards around the second rotating shaft 404 under the support and limit of the second lower hinge seat 410, so that the second clamping arm 405 moves inwards gradually to contact the outer wall of the fuel tank for clamping and fixing. At this time, both ends of the fuel tank are in a semi-wrapped clamping state to complete the fixing. This device is convenient for clamping and fixing fuel tanks of different sizes.

[0037] When it is necessary to clamp and fix fuel tanks of different lengths, first measure the distance between the clamping and fixing points at the left and right ends of the fuel tank, and then start the telescopic ejector rod 308 to contract and pull the anti-slip clamping plate 309 out from the bottom of the lock plate 310 to release the lock. At this time, the motor 203 drives the threaded rod 202 to rotate, and uses the thread groove 311 to push the two sets of adjusting seats 302 and the sliding seat 301 to move inward or outward to the inner sides of both ends of the base 1 under the sliding support of the runner 306, and drives the clamping mechanism 4 to move accordingly to adjust the distance. It is okay until the distance between the two sets of clamping mechanisms 4 is the same as the pre-measured distance between the fixed points. After the adjustment is completed, the telescopic ejector rod 308 extends to push the anti-slip clamping plate 309 into the lock plate 310 to lock the positions of the sliding seat 301 and the clamping mechanism 4. This device is convenient for clamping and fixing fuel tanks of different lengths.

[0038] It should be noted that in this article, relational terms such as first and second are only used to distinguish one entity or operation from another entity or operation, and do not necessarily require or imply any actual relationship or order between these entities or operations. Moreover, the term "comprises", "comprising" or any other variation thereof is intended to cover a non-exclusive inclusion, so that a process, method, article or device comprising a series of elements not only includes those elements, but also includes other elements not expressly listed, or further includes elements inherent to such process, method, article or device.

[0039] Although the embodiments of the present invention have been shown and described, for those of ordinary skill in the art, it can be understood that various changes, modifications, substitutions and variations can be made to these embodiments without departing from the principle and spirit of the present invention. The scope of the present invention is defined by the appended claims and their equivalents.

Claims

1. A support structure for a ship fuel tank, comprising a base (1), characterized in that: A chute (2) is provided on the upper surface of the base (1). A clamping mechanism (4) is arranged above the base (1) for clamping and fixing fuel tanks of different sizes. A sliding adjustment mechanism (3) is arranged on the upper surface of the base (1) for adjusting the distance between two groups of clamping mechanisms (4) to adapt to the clamping and fixing of fuel tanks of different lengths. The clamping mechanism (4) includes a support base (401), a first rotating shaft (402), a first clamping arm (403), a second rotating shaft (404), a second clamping arm (405), an anti-slip gasket (406), a first lower hinge seat (407), a first upper hinge seat (408), a first telescopic cylinder (409), a second lower hinge seat (410), a second upper hinge seat (411) and a second telescopic cylinder (412). The support base (401) is fixedly connected to the upper surface of the sliding adjustment mechanism (3). The first rotating shaft (402) is inserted through both ends of the support base (401). The first clamping arm (403) is hinged to both ends of the support base (401). The second rotating shaft (404) is inserted through the top end of the first clamping arm (403). The second clamping arm (405) is hinged to the top end of the first clamping arm (403). The anti-slip gasket (406) is arranged on the inner sides of the support base (401), the first clamping arm (403) and the second clamping arm (405). The first lower hinge seat (407) is fixedly connected to the sliding adjustment mechanism (3). The first upper hinge seat (408) is fixedly connected to the side wall of the first clamping arm (403). The upper and lower ends of the first telescopic cylinder (409) are respectively rotatably connected in the first lower hinge seat (407) and the first upper hinge seat (408). The second lower hinge seat (410) is fixedly connected to the outer surface of the first clamping arm (403). The second upper hinge seat (411) is fixedly connected to the outer surface of the second clamping arm (405). The upper and lower ends of the second telescopic cylinder (412) are respectively rotatably connected in the second lower hinge seat (410) and the second upper hinge seat (411).

2. The support structure of a ship fuel tank according to claim 1, characterized in that: The sliding adjustment mechanism (3) comprises a sliding seat (301), an adjustment seat (302), a side clamp (303), a rotating groove (304), a rotating rod (305), a rotating wheel (306), a top cover (307), a telescopic top rod (308), an anti-slip splint (309), a locking plate (310) and a threaded groove (311); the sliding seat (301) is slidably connected to the upper surface of the base (1); the adjustment seat (302) is fixedly connected to the lower surface of the sliding seat (301); the side clamp (303) is fixedly connected to both ends of the sliding seat (301); and the rotating groove (304) is connected to the bottom surface of the sliding seat (301). The rotating rod (305) is fixedly connected to the inside of the rotating groove (304), the rotating wheel (306) is rotatably connected to the rotating rod (305), the top cover (307) is arranged above the rotating groove (304), the telescopic top rod (308) is arranged at the bottom of the side bracket (303), the anti-slip clamping plate (309) is fixedly connected to the top of the telescopic top rod (308), the locking plate (310) is fixedly connected to the lower surface at the top edge of the base (1), and the threaded groove (311) is penetrated and opened on the adjustment seat (302).

3. The bracket structure of a ship fuel tank according to claim 1, characterized in that: A fixing plate (101) is fixedly connected to the bottom of the base (1), a fixing block (102) is fixedly connected to the fixing plate (101), and a mounting hole (103) is formed through the fixing block (102).

4. The support structure of a ship fuel tank according to claim 1, characterized in that: An inner groove (201) is provided at the bottom of the slide groove (2), a threaded rod (202) is rotatably connected inside the inner groove (201), and a motor (203) is fixedly connected to one side of the base (1).

5. The support structure of a ship fuel tank according to claim 1, characterized in that: The first rotating shaft (402) is inserted through and arranged at the rotating hinge between the bracket (401) and the first clamping arm (403), and the second rotating shaft (404) is arranged at the rotating hinge between the first clamping arm (403) and the second clamping arm (405).

6. The support structure of a ship fuel tank according to claim 1, characterized in that: The support seat (401) is fixedly connected to the upper surface of the slide seat (301), and the first lower hinge seat (407) is fixedly connected to the upper surface of the slide seat (301).

7. The bracket structure of a ship fuel tank according to claim 2, characterized in that: The adjustment seat (302) is slidably connected inside the slide groove (2) and the inner groove (201), and the top cover (307) is fixedly connected to the upper surfaces of both ends of the slide seat (301).

8. The support structure of a ship fuel tank according to claim 2, characterized in that: The side clamping frame (303) is slidably clamped on both sides of the base (1); the telescopic end of the telescopic top rod (308) passes through the bottom of the side clamping frame (303) and is connected to the anti-skid clamping plate (309); the anti-skid clamping plate (309) is arranged below the locking plate (310) and the anti-skid clamping plate (309) is clamped with the locking plate (310).

9. The support structure of a ship fuel tank according to claim 4, characterized in that: The threaded rod (202) is threadably connected to the inside of the thread groove (311), and the thread directions of the left and right sets of thread grooves (311) are opposite.

10. The bracket structure of a ship fuel tank according to claim 4, characterized in that: One end of the threaded rod (202) passes through the base (1) and is connected to the output end of the motor (203).

Citation Information

Patent Citations

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