Novel airplane support supporting system

Abstract

The utility model relates to the technical field of constructional engineering, in particular to a novel aircraft support supporting system. The novel aircraft support supporting system comprises a base, a vertical rod, a supporting table and a matching block. The vertical rod is detachably arranged on the base; the supporting table is movably arranged on the vertical rod so as to move to a preset position in the height direction of the vertical rod. The supporting table is configured to be fixedly connected and matched with the vertical rod after reaching a preset position, so that stress on the supporting table is transmitted to the base through the vertical rod; the matching block is movably arranged on the vertical rod, and a hooking part is arranged on the matching block and used for being connected with a binding iron wire. In this way, the height can be flexibly adjusted to support the steel pipe to the preset position, and meanwhile connection is more stable.

Description

Technical Field

[0001] The utility model relates to the technical field of construction engineering, in particular to a novel aircraft support system. Background Art

[0002] When setting up various types of formwork in construction projects, such as floor construction and large building foundations, support frames, commonly known as "aircraft supports", are often needed. The "aircraft support" support frames are used to support steel pipes and play an important role in the installation of steel pipes.

[0003] However, the aircraft support in the prior art has a single function and can only support the steel pipe. At the same time, it is inconvenient to adjust the support height, thus affecting the construction efficiency. Utility Model Content

[0004] The purpose of the utility model includes, for example, providing a novel aircraft support system, which can flexibly adjust the height to support the steel pipe to a preset position, and at the same time the connection is more stable.

[0005] The embodiments of the present invention can be implemented as follows:

[0006] In a first aspect, the utility model provides a novel aircraft support system, comprising:

[0007] Base, vertical rods, support platform and matching blocks;

[0008] The vertical rod is detachably arranged on the base; the support platform is movably arranged on the vertical rod to move to a preset position along the height direction of the vertical rod; and the support platform is configured to be able to be fixedly matched with the vertical rod after reaching the preset position, so as to transmit the force on the support platform to the base through the vertical rod;

[0009] The matching block can be movably arranged on the vertical rod, and a hook portion is arranged on the matching block, and the hook portion is used to connect the binding wire.

[0010] In an optional embodiment, the support platform is threadedly connected to the vertical rod to achieve movement along the height direction of the vertical rod.

[0011] In an optional embodiment, the vertical rod has an external thread on its outer circumference along its height direction; a penetrating connecting hole with an internal thread is provided in the middle of the support platform; the vertical rod is threadedly connected to the connecting hole so that the vertical rod and the connecting hole can be rotatably matched.

[0012] In an optional embodiment, it further includes a first anti-slip nut, which is threadedly connected to the vertical rod; and the first anti-slip nut can be abutted against the bottom of the support platform to achieve anti-slip support for the support platform.

[0013] In an optional embodiment, a through fitting hole is provided in the middle of the fitting block, an inner wall of the fitting hole is provided with an internal thread, and the fitting hole passes through the vertical rod so that the fitting block is threadedly connected to the vertical rod.

[0014] In an optional embodiment, a second anti-slip nut is further included, wherein the second anti-slip nut is threadedly connected to the vertical rod; and the second anti-slip nut can be abutted against the bottom of the matching block to provide anti-slip support for the matching block.

[0015] In an optional embodiment, a scale unit is further included; the scale unit is arranged on the vertical rod along the height direction of the vertical rod, and the scale unit can indicate the distance between a preset position on the vertical rod and the bottom of the base.

[0016] In an optional embodiment, when the support platform moves to a preset position on the vertical rod, the support platform is configured to be welded and fixed to the vertical rod;

[0017] When the matching block moves to a preset position on the vertical rod, the matching block is configured to be welded and fixed to the vertical rod.

[0018] In an optional embodiment, a connecting column is further included, and the bottom of the connecting column is connected to the top of the base through a plane bearing; a mounting through hole is provided at the bottom of the vertical rod, and the connecting column is inserted into the mounting through hole.

[0019] In an optional embodiment, a ball head is further included; the top of the ball head is spherical, and the bottom of the ball head is connected to the top of the vertical rod.

[0020] The beneficial effects of the embodiments of the present utility model include, for example:

[0021] The new aircraft support system of this scheme includes a base, a vertical rod, a support platform and a matching block. The support platform can be moved to a preset position along the height direction of the vertical rod. After the support platform reaches the preset position, it can be fixedly matched with the vertical rod to transfer the force on the support platform to the base through the vertical rod. When in use, the pipe mouth at the bottom of the steel pipe is against the support platform, and the force from the steel pipe is transmitted to the installation ground through the support platform, the vertical rod and the base, so that the steel pipe can be stably supported on the installation ground. At the same time, because the height of the support platform can be adjusted, the steel pipe can be adjusted to a preset height, thereby meeting the support of steel pipes at different heights. The hook part on the matching block can make the fixed points around the vertical rod tightly connected to the matching block through binding wire, thereby ensuring the stable matching of the new aircraft support system with the surrounding area. For example, when the new aircraft support system is set in a steel cage, the fixed point around the vertical rod is any steel bar, and the surrounding steel bars are connected to the hook part by bundling wires, so that the new aircraft support system can be stably set in the steel cage, which ensures the stable support of the steel pipe on the one hand, and ensures the structural stability during the casting of the steel cage on the other hand. At the same time, the matching block can also move along the vertical rod, so that the hook part can be more easily connected to the surrounding fixed points through the bundling wire. In summary, such a new aircraft support system has a simple structure, easy operation, convenient adjustment of the support height, and can ensure the support of the steel pipe while increasing the tightness of the connection with the surrounding fixed points. BRIEF DESCRIPTION OF THE DRAWINGS

[0022] In order to more clearly illustrate the technical solutions of the embodiments of the utility model, the drawings required for use in the embodiments will be briefly introduced below. It should be understood that the following drawings only show certain embodiments of the utility model and therefore should not be regarded as limiting the scope. For ordinary technicians in this field, other relevant drawings can be obtained based on these drawings without paying creative work.

[0023] Figure 1 It is a structural schematic diagram of a novel aircraft support system according to an embodiment of the utility model.

[0024] Icon: 100-base; 200-vertical rod; 201-mounting through hole; 300-support platform; 301-connecting hole; 311-first anti-slip nut; 400-matching block; 401-matching hole; 422-second anti-slip nut; 433-hook part; 500-scale unit; 600-connecting column; 610-plane bearing; 700-ball head. DETAILED DESCRIPTION

[0025] In order to make the purpose, technical scheme and advantages of the embodiments of the utility model clearer, the technical scheme in the embodiments of the utility model will be clearly and completely described below in conjunction with the drawings in the embodiments of the utility model. Obviously, the described embodiments are part of the embodiments of the utility model, not all of the embodiments. Generally, the components of the embodiments of the utility model described and shown in the drawings here can be arranged and designed in various different configurations.

[0026] Therefore, the following detailed description of the embodiments of the present invention provided in the accompanying drawings is not intended to limit the scope of the present invention to be protected, but merely represents selected embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the present invention.

[0027] It should be noted that similar reference numerals and letters denote similar items in the following drawings, and therefore, once an item is defined in one drawing, further definition and explanation thereof is not required in subsequent drawings.

[0028] In the description of the present utility model, it should be noted that if the terms "upper", "lower", "inside", "outside", etc. appear, the orientation or position relationship indicated is based on the orientation or position relationship shown in the accompanying drawings, or is the orientation or position relationship in which the utility model product is usually placed when used. It is only for the convenience of describing the utility model and simplifying the description, and does not indicate or imply that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation. Therefore, it cannot be understood as a limitation on the present utility model.

[0029] In addition, the terms “first”, “second”, etc., if used, are merely used to distinguish between the descriptions and should not be understood as indicating or implying relative importance.

[0030] It should be noted that, in the absence of conflict, the features in the embodiments of the present invention may be combined with each other.

[0031] Please refer to Figure 1 This embodiment provides a novel aircraft support system, including a base 100, a vertical rod 200, a support platform 300 and a matching block 400.

[0032] The vertical rod 200 is detachably disposed on the base 100; the support platform 300 is movably disposed on the vertical rod 200 to move to a preset position along the height direction of the vertical rod 200; and the support platform 300 is configured to be able to be fixedly matched with the vertical rod 200 after reaching the preset position, so as to transmit the force on the support platform 300 to the base 100 through the vertical rod 200;

[0033] The matching block 400 is movably disposed on the vertical rod 200 . A hook portion 433 is disposed on the matching block 400 . The hook portion 433 is used to connect the binding wire.

[0034] The support platform 300 of this solution can be moved to a preset position along the height direction of the vertical rod 200. After the support platform 300 reaches the preset position, it can be fixedly matched with the vertical rod 200 to transfer the force on the support platform 300 to the base 100 through the vertical rod 200. When in use, the pipe mouth at the bottom of the steel pipe is against the support platform 300, and the force from the steel pipe is transmitted to the installation ground through the support platform 300, the vertical rod 200, and the base 100, so that the steel pipe can be stably supported on the installation ground. At the same time, because the height of the support platform 300 can be adjusted, it can meet the requirements of adjusting the steel pipe to a preset height, thereby meeting the support of steel pipes at different height positions. The hooking part 433 on the matching block 400 can make the fixed points around the vertical rod 200 tightly connected to the matching block 400 through the binding wire, thereby ensuring the stable matching of the new aircraft support system with the surrounding area. For example, when the new aircraft support system is set in a steel cage, the fixed point around the vertical rod 200 is any steel bar, and the surrounding steel bars are connected to the hook part 433 by binding wires, so that the new aircraft support system can be stably set in the steel cage, which ensures the stable support of the steel pipe on the one hand, and ensures the structural stability of the steel cage during casting on the other hand. At the same time, the matching block 400 can also move along the vertical rod 200, so that the hook part 433 can be more easily connected to the surrounding fixed points through the binding wire. In summary, such a new aircraft support system has a simple structure, easy operation, convenient adjustment of the support height, and can ensure the support of the steel pipe while increasing the tightness of the connection with the surrounding fixed points.

[0035] As a usage scenario, in existing wind power generation, the construction of building steel bars and support formwork is required in the foundation of large wind turbines. In the prior art, the support steel pipe is directly inserted into the steel cage in the wind turbine foundation, and the support steel pipe is used to support other components of the wind turbine foundation. The part of the support steel pipe that penetrates into the steel cage is cast together with the steel cage to form an integrated foundation slab. After the casting is completed, the part of the steel pipe located above the foundation slab is cut off. However, the diameter of the support steel pipe is large, and there are many and large holes formed after cutting, which will have an adverse effect on the structural stability of the entire wind turbine foundation. At the same time, the method of cutting the support steel pipe will cause technical problems such as waste of steel pipes and inconvenience in construction.

[0036] The base 100 and the vertical rod 200 of the novel aircraft support system of this solution can be inserted into the above-mentioned steel cage, and the support platform 300 can adjust the height to meet the support of the steel pipe, so that the steel cage can be above the foundation bottom plate after casting. In this way, only the aircraft support of a smaller volume needs to be cut, avoiding the operation of cutting the steel pipe; the matching block 400 can also ensure the stable connection between the aircraft support and the surrounding steel cage. Optionally, the vertical rod 200 can be a vertical steel bar or a threaded rod, and the support platform 300 can be an iron block or a nut, which can reduce the space occupancy rate of the aircraft support. At the same time, because the vertical rod 200 is solid and no holes are formed after cutting, it can also ensure the structural force stability of the wind turbine foundation.

[0037] Optionally, in this embodiment of the utility model, the novel aircraft support system further includes a connecting column 600, the bottom of which is connected to the top of the base 100 via a plane bearing 610; a mounting through hole 201 is provided at the bottom of the vertical rod 200, and the connecting column 600 is inserted into the mounting through hole 201. The provision of the connecting column 600 enables the vertical rod 200 and the base 100 to be connected more flexibly, thereby improving the overall stability of the aircraft support.

[0038] The novel aircraft support system further includes a ball head 700; the top of the ball head 700 is spherical, and the bottom of the ball head 700 is connected to the top of the vertical rod 200. The ball head 700 can more easily allow the vertical rod 200 to pass through the bottom opening of the steel pipe, so that the bottom of the steel pipe can be smoothly supported on the support platform 300.

[0039] Furthermore, in this embodiment of the utility model, the support platform 300 is threadedly connected to the vertical rod 200 to achieve movement along the height direction of the vertical rod 200. The threaded connection can not only adjust the height position of the support platform 300 relative to the vertical rod 200, but also ensure the stability of the support platform 300 and the vertical rod 200 through the self-locking feature of the thread.

[0040] Optionally, the outer circumference of the vertical rod 200 is provided with external threads along the height direction of the vertical rod 200; a connecting hole 301 with internal threads is provided in the middle of the support platform 300; the vertical rod 200 is threadedly connected with the connecting hole 301, so that the vertical rod 200 and the connecting hole 301 can be rotatably matched. It should be noted that the external threads of the vertical rod 200 can be formed by machining alone, or a screw rod can be directly selected as the vertical rod 200; similarly, a nut can be directly selected for the support platform 300.

[0041] In this embodiment of the utility model, a first anti-slip nut 311 is also included, and the first anti-slip nut 311 is threadedly connected to the vertical rod 200; and the first anti-slip nut 311 can be abutted against the bottom of the support platform 300 to achieve anti-slip support for the support platform 300. The first anti-slip nut 311 and the support platform 300 are both threadedly matched with the vertical rod 200, and the two form an anti-slip design to ensure that the support platform 300 can be stably fixed to the vertical rod 200, thereby ensuring good support of the steel pipe by the support platform 300. It should be noted that in order to ensure the force reliability of the support platform 300 and the vertical rod 200, the support platform 300 can also be stably connected to the vertical rod 200 by welding after the support platform 300 is adjusted to a preset height.

[0042] Furthermore, in this embodiment of the utility model, a through-hole 401 is provided in the middle of the mating block 400, and an inner wall of the mating hole 401 is provided with an internal thread, and the mating hole 401 is penetrated by the vertical rod 200 so that the mating block 400 is threadedly connected with the vertical rod 200. It should be noted that the internal thread of the mating block 400 can be formed by machining alone, or a nut can be directly used as the mating block 400.

[0043] The present embodiment also includes a second anti-slip nut 422, which is threadedly connected to the vertical rod 200; and the second anti-slip nut 422 can be abutted against the bottom of the matching block 400 to achieve anti-slip support for the matching block 400. The second anti-slip nut 422 and the matching block 400 are both threadedly matched with the vertical rod 200, and the two form an anti-slip design to ensure that the matching block 400 can be stably fixed to the vertical rod 200, thereby ensuring the stable connection between the aircraft support and the surrounding fixed points. It should be noted that in order to ensure the stable connection between the matching block 400 and the vertical rod 200, the matching block 400 can also be stably connected to the vertical rod 200 by welding after the matching block 400 is adjusted to a preset height.

[0044] That is, when the support platform 300 moves to the preset position on the vertical rod 200, the support platform 300 is configured to be welded and fixed to the vertical rod 200; when the matching block 400 moves to the preset position on the vertical rod 200, the matching block 400 is configured to be welded and fixed to the vertical rod 200. The advantage of this is that the support platform 300 (matching block 400) is threadedly connected with the vertical rod 200 to form a first-level fixed connection, the first anti-detachment nut 311 (second anti-detachment nut 422) is threadedly connected with the vertical rod 200 to form a second-level fixed connection, and the support platform 300 (matching block 400) is welded with the vertical rod 200 to form a third-level fixed connection. This multiple fixing method can ensure that the aircraft support has good supporting effect and structural stability.

[0045] It can also be seen from the figure that the present embodiment further includes a scale unit 500; the scale unit 500 is arranged on the vertical rod 200 along the height direction of the vertical rod 200, and the scale unit 500 can indicate the distance between the preset position on the vertical rod 200 and the bottom of the base 100. The scale unit 500 facilitates smooth adjustment of the position of the support platform 300 relative to the vertical rod 200, thereby meeting the support requirements for the steel pipe at different height positions.

[0046] In summary, the embodiment of the utility model provides a novel aircraft support system, which has at least the following advantages:

[0047] This new aircraft support system has a simple structure, is easy to operate, and is convenient to adjust the support height. It can not only ensure the support of the steel pipe but also increase the tightness of the connection with the surrounding fixed points.

[0048] The above are only specific implementations of the utility model, but the protection scope of the utility model is not limited thereto. Any changes or substitutions that can be easily thought of by a person skilled in the art within the technical scope disclosed by the utility model should be included in the protection scope of the utility model. Therefore, the protection scope of the utility model should be based on the protection scope of the claims.

Claims

1. A novel aircraft support system, characterized in that: include: A base (100), a vertical rod (200), a support platform (300) and a matching block (400); The vertical rod (200) is detachably arranged on the base (100); the support platform (300) is movably arranged on the vertical rod (200) so as to be moved to a preset position along the height direction of the vertical rod (200); and the support platform (300) is configured to be fixedly matched with the vertical rod (200) after reaching the preset position so as to transmit the force on the support platform (300) to the base (100) through the vertical rod (200); The matching block (400) is movably arranged on the vertical rod (200), and a hook portion (433) is arranged on the matching block (400), and the hook portion (433) is used to connect the binding wire.

2. The novel aircraft support system according to claim 1 is characterized in that: The support platform (300) is threadedly connected to the vertical rod (200) to achieve movement along the height direction of the vertical rod (200).

3. The novel aircraft support system according to claim 2 is characterized in that: The vertical rod (200) has an external thread on its outer circumference along the height direction of the vertical rod (200); a connecting hole (301) with an internal thread is provided in the middle of the support platform (300); the vertical rod (200) is threadedly connected to the connecting hole (301) so that the vertical rod (200) and the connecting hole (301) can be rotatably matched.

4. The novel aircraft support system according to claim 3 is characterized in that: It also includes a first anti-slip nut (311), which is threadedly connected to the vertical rod (200); and the first anti-slip nut (311) can be abutted against the bottom of the support platform (300) to achieve anti-slip support for the support platform (300).

5. The novel aircraft support system according to claim 3 is characterized in that: A through-going matching hole (401) is provided in the middle of the matching block (400), and an inner wall of the matching hole (401) is provided with an internal thread. After the matching hole (401) passes through the vertical rod (200), the matching block (400) is threadedly connected to the vertical rod (200).

6. The novel aircraft support system according to claim 5 is characterized in that: It also includes a second anti-slip nut (422), which is threadedly connected to the vertical rod (200); and the second anti-slip nut (422) can be abutted against the bottom of the matching block (400) to achieve anti-slip support for the matching block (400).

7. The novel aircraft support system according to claim 1 is characterized in that: It also comprises a scale unit (500); the scale unit (500) is arranged on the vertical rod (200) along the height direction of the vertical rod (200), and the scale unit (500) can mark the distance between a preset position on the vertical rod (200) and the bottom of the base (100).

8. The novel aircraft support system according to claim 1 is characterized in that: When the support platform (300) moves to a preset position on the vertical rod (200), the support platform (300) is configured to be welded and fixed to the vertical rod (200); When the matching block (400) moves to a preset position on the vertical rod (200), the matching block (400) is configured to be welded and fixed to the vertical rod (200).

9. The novel aircraft support system according to claim 1 is characterized in that: It also includes a connecting column (600), the bottom of which is connected to the top of the base (100) via a plane bearing (610); a mounting through hole (201) is provided at the bottom of the vertical rod (200), and the connecting column (600) is inserted into the mounting through hole (201).

10. The novel aircraft support system according to claim 1 is characterized in that: It also includes a ball head (700); the top of the ball head (700) is spherical, and the bottom of the ball head (700) is connected to the top of the vertical rod (200).

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