Special clamp for aviation pipeline

Abstract

The utility model provides a special clamp for aviation pipelines, and relates to the technical field of aerospace manufacturing, the special clamp comprises a clamp body and a rubber gasket, the clamp body comprises a clamping assembly, the clamping assembly is provided with a clamping space, the inner wall surface of the clamping space is provided with a positioning groove, and the rubber gasket is arranged in the positioning groove. The face, facing the clamping space, of the rubber gasket is provided with a positioning protrusion matched with the positioning groove so that the rubber gasket can be embedded in the inner wall face of the clamping assembly, and the face, back to the clamping space, of the rubber gasket is provided with a friction protrusion. The rubber gasket is embedded in the inner wall face of the clamping assembly, the rubber gasket is made of soft materials, the buffering effect can be achieved between the hoop body and a pipeline, direct hard contact and overlarge pressure on the pipeline are reduced, deformation of the pipeline is prevented, and the service life is prolonged. And the friction protrusions are arranged on the rubber gasket, the friction force between the rubber gasket and the pipeline is increased, and the stability and reliability of the pipeline in the complex environment are improved.

Description

Technical Field

[0001] The utility model relates to the technical field of aerospace manufacturing, in particular to a special clamp for aviation pipelines. Background Art

[0002] In aircraft manufacturing, the environmental control system is responsible for maintaining a suitable ambient temperature in the cockpit, passenger cabin, cargo hold, equipment compartment and other areas by transmitting air of different temperatures through the piping system.

[0003] However, because aircraft experience a variety of complex environmental conditions during operation, such as vibrations caused by high-speed flight and airflow shock between different pressure zones, extremely high requirements are placed on the stability and reliability of the piping. If the piping is not securely fixed or easily loosens, it will affect the normal operation of the environmental control system and pose a safety hazard.

[0004] At present, most pipelines are installed and fixed using simple clamps and other methods. Although the pipeline can be fixed to a certain extent, the following technical problems still exist: the simple clamps are in hard contact with the pipeline. In order to ensure the fixing effect of the pipeline, excessive pressure is often applied to the pipeline, which will cause the pipeline to deform and thus affect its service life. In addition, under complex environmental conditions such as vibration and airflow impact, the friction between the simple clamps and the pipeline is insufficient, and the pipeline may not be able to maintain stability, posing a risk of loosening.

[0005] In view of this, the present utility model is proposed. Utility Model Content

[0006] The purpose of this utility model is to provide a clamp specifically designed for aviation piping, addressing the technical issues of existing simple clamp designs, such as hard contact with the pipeline, excessive pressure on the pipeline, and deformation, which in turn shortens its service life. The various technical advantages of the preferred technical solution among the various technical solutions provided by this utility model are detailed below.

[0007] To achieve the above objectives, the present invention provides the following technical solutions:

[0008] The utility model provides a special clamp for aviation pipelines, including a clamp body and a rubber gasket, the clamp body including a clamping assembly, the clamping assembly having a clamping space, the inner wall surface of the clamping space being provided with a positioning groove, the rubber gasket being provided with a positioning protrusion adapted to the positioning groove on a surface facing the clamping space, so that the rubber gasket is embedded in the inner wall surface of the clamping assembly, and the rubber gasket being provided with a friction protrusion on a surface facing away from the clamping space.

[0009] Preferably, the clamp body also includes a first wing plate and a second wing plate, the first wing plate and the second wing plate are respectively connected to the open end of the clamping assembly, and the first wing plate and the second wing plate are correspondingly arranged so that when the first wing plate and the second wing plate abut against each other, the clamping space is in a closed state.

[0010] Preferably, the first wing plate and the second wing plate are provided with corresponding connection holes.

[0011] Preferably, the first wing extends along the tangential direction of the clamping assembly to form a straight structure.

[0012] Preferably, avoidance grooves are formed on outer wall surfaces of connections between the first wing plate and the clamping assembly, and between the second wing plate and the clamping assembly.

[0013] Preferably, the inner wall surface of the clamping assembly transitions obliquely to the inner wall surfaces of the first wing plate and the second wing plate, respectively, to form an inclined surface.

[0014] Preferably, the rubber gasket extends onto the inclined surface.

[0015] Preferably, a weight-reducing groove is provided on the clamp body.

[0016] Preferably, there are multiple friction protrusions, which respectively extend along the circumference of the clamping space and are arranged parallel to each other.

[0017] Preferably, at least the outer edges of the two long sides of the rubber gasket are respectively provided with friction protrusions.

[0018] The preferred technical solution of the utility model can also produce at least the following technical effects:

[0019] The present invention effectively avoids the technical problems of existing simple clamp designs in the prior art, such as hard contact with the pipeline, excessive pressure on the pipeline, and deformation of the pipeline, which in turn affects its sealing and service life. The present invention provides a special clamp for aviation pipelines, comprising a clamp body and a rubber gasket. The clamp body includes a clamping assembly, the clamping assembly having a clamping space, a positioning groove provided on the inner wall surface of the clamping space, and a positioning protrusion provided on the surface of the rubber gasket facing the clamping space that matches the positioning groove, so that the rubber gasket is embedded in the inner wall surface of the clamping assembly. The rubber gasket is provided with a friction protrusion on the surface facing away from the clamping space. The present invention embeds the rubber gasket on the inner wall surface of the clamping assembly. As a soft material, the rubber gasket can act as a buffer between the clamp body and the pipeline, reducing direct hard contact and excessive pressure on the pipeline, preventing deformation of the pipeline, and extending its service life. The friction protrusion is provided on the rubber gasket to increase friction between the clamp body and the pipeline, improving the stability and reliability of the pipeline in complex environments. BRIEF DESCRIPTION OF THE DRAWINGS

[0020] In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the following briefly introduces the drawings required for use in the embodiments or the description of the prior art. Obviously, the drawings described below are only some embodiments of the present invention. For ordinary technicians in this field, other drawings can be obtained based on these drawings without paying any creative work.

[0021] Figure 1 This is a structural diagram of a special clamp for aviation pipelines provided by the utility model;

[0022] Figure 2 This is a structural diagram of a clamp body of a special clamp for aviation pipelines provided by the utility model;

[0023] Figure 3 The utility model is a structural schematic diagram of a rubber gasket for a special clamp for aviation pipelines.

[0024] In the picture:

[0025] 1. Clamping assembly; 11. Positioning groove; 2. First wing plate; 3. Second wing plate; 4. Inclined surface; 41. Large inner diameter section; 42. Small inner diameter section; 5. Rubber gasket; 51. Positioning protrusion; 52. Friction protrusion; 6. Avoidance groove; 7. Weight reduction groove; 8. Connecting hole. DETAILED DESCRIPTION

[0026] To make the purpose, technical solution, and advantages of the present invention more clear, the technical solution of the present invention will be described in detail below. Obviously, the embodiments described are only some of the embodiments of the present invention, and not all of them. Based on the embodiments of the present invention, all other implementation methods obtained by ordinary technicians in this field without making any creative efforts are within the scope of protection of the present invention.

[0027] like Figure 1-3 As shown, the utility model provides a special clamp for aviation pipelines, including a clamp body and a rubber gasket 5. The clamp body includes a clamping component 1, the clamping component 1 has a clamping space, and a positioning groove 11 is provided on the inner wall surface of the clamping space. A positioning protrusion 51 adapted to the positioning groove 11 is provided on the side of the rubber gasket 5 facing the clamping space, so that the rubber gasket 5 is embedded in the inner wall surface of the clamping component 1, and a friction protrusion 52 is provided on the side of the rubber gasket 5 facing away from the clamping space.

[0028] The present invention incorporates a rubber gasket 5 embedded within the inner wall of the clamp assembly 1. As a soft material, the rubber gasket 5 acts as a buffer between the clamp body and the pipeline, reducing direct, hard contact and excessive pressure on the pipeline, preventing deformation and extending the service life of the pipeline. Furthermore, friction protrusions 52 are provided on the rubber gasket 5 to increase friction with the pipeline, improving the stability and reliability of the pipeline in complex environments.

[0029] As an optional embodiment, the clamp body also includes a first wing plate 2 and a second wing plate 3, which are respectively connected to the open ends of the clamping assembly 1, and the first wing plate 2 and the second wing plate 3 are correspondingly arranged so that when the first wing plate 2 and the second wing plate 3 abut against each other, the clamping space is in a closed state.

[0030] The abutment between the first wing plate 2 and the second wing plate 3 increases the fastening force of the clamping assembly 1 on the pipeline, so that the pipeline remains stable in a complex environment and is not easily loosened.

[0031] As an optional embodiment, connecting holes 8 are correspondingly opened on the first wing plate 2 and the second wing plate 3 .

[0032] Fasteners such as bolts are sequentially passed through the connection holes 8 of the first wing plate 2 and the second wing plate 3 to firmly connect the first wing plate 2 and the second wing plate 3 together to ensure the closedness and fastening force of the clamping space.

[0033] As an optional embodiment, the first wing plate 2 extends along the tangential direction of the clamping assembly 1 to form a straight structure.

[0034] This arrangement allows the first wing plate 2 to provide a more stable support surface, allowing the clamp body to be evenly stressed when tightening the pipeline. It also facilitates placing the clamp body and pipeline on a horizontal surface, simplifying the operation process and improving work efficiency.

[0035] As an optional embodiment, avoidance grooves 6 are provided on the outer wall surfaces of the connection points between the first wing plate 2 and the clamping assembly 1 and between the second wing plate 3 and the clamping assembly 1 .

[0036] When carrying out the installation or adjustment of pipeline, the avoidance groove 6 provides enough operating spaces for the operator's hand and operating tools. In addition, the avoidance groove 6 also plays the effect of weight reduction.

[0037] As an optional embodiment, the inner wall surface of the clamping assembly 1 transitions obliquely to the inner wall surfaces of the first wing plate 2 and the second wing plate 3 , respectively, to form an inclined surface 4 .

[0038] Furthermore, there is a smooth transition between the inclined surface 4 and the inner wall surface of the clamping assembly 1, the inner wall surface of the first wing plate 2 and the inner wall surface of the second wing plate 3. The pipeline can slide smoothly into the clamping space along the guidance of the inclined surface 4, reducing the difficulty of installation.

[0039] When the first wing plate 2 and the second wing plate 3 are in contact, the two inclined surfaces 4 fit together, thereby completely closing the clamping space, providing stable and reliable clamping for the pipeline, so that the pipeline can operate stably in complex environments.

[0040] As an optional embodiment, the rubber gasket 5 extends onto the inclined surface 4 .

[0041] Furthermore, the inclined surface 4 has a stepped structure, which includes a small inner diameter section 42 and a large inner diameter section 41 connected in sequence from the outside to the inside, and the positioning groove 11 is set through the clamping assembly 1 so that the rubber gasket 5 extends to the large inner diameter section 41, and the outer wall surface of the rubber gasket 5 is flush with the outer wall surface of the small inner diameter section 42, so that the rubber gasket 5 can at least partially cover and fit tightly on the stepped structure of the inclined surface 4, providing a more comprehensive and effective sealing and buffering effect.

[0042] As an optional embodiment, a weight-reducing groove 7 is provided on the clamp body.

[0043] Furthermore, a weight-reducing groove 7 is provided at the connection between the first wing plate 2 and the second wing plate 3 and the clamping assembly 1 to reduce weight.

[0044] The number, specifications and positions of the weight-reducing grooves 7 can be designed according to the requirements of use, as long as they are arranged without affecting their structural strength and functionality, and the weight can be reduced while maintaining sufficient strength.

[0045] As an optional embodiment, there are multiple friction protrusions 52, which extend along the circumference of the clamping space and are arranged parallel to each other.

[0046] The multiple friction protrusions 52 can increase the contact points with the pipeline, thereby dispersing the pressure and protecting the pipeline from damage.

[0047] The friction protrusions 52 extend along the circumference of the clamping space, so that the clamp body can apply pressure evenly when tightening the pipeline, thereby preventing the pipeline from being deformed in the clamping space.

[0048] As an optional embodiment, at least the outer edges of the two long sides of the rubber gasket 5 are respectively provided with friction protrusions 52 .

[0049] This arrangement allows the rubber gasket 5 to generate greater friction with the pipe surface through the friction protrusions 52 when squeezed, thereby enhancing the fastening effect and reducing friction and collision between the pipe and the edge of the clamp body during installation.

[0050] As an optional implementation method, the rubber gasket 5 is made of silicone rubber, which has the advantages of insulation, heat insulation, wear resistance and heat insulation. The clamp body is made of 7075 aluminum, which has the advantages of good structural strength, long life and light weight, and complies with aviation design principles.

[0051] The specific specifications of the clamp body and the rubber gasket 5 can be set according to the use requirements to meet the tightening requirements of the specified pipeline.

[0052] It can be understood that the same or similar parts of the above embodiments can be referenced to each other, and the contents not described in detail in some embodiments can refer to the same or similar contents in other embodiments.

[0053] In the description of the present invention, it should be noted that, unless otherwise specified, "plurality" means two or more; the terms "upper", "lower", "left", "right", "inner", "outer", "front", "rear", "head", "tail", etc., indicating directions or positional relationships, are based on the directions or positional relationships shown in the accompanying drawings and are intended only to facilitate the description of the present invention and simplify the description. They do not indicate or imply that the devices or components referred to must have a specific direction, be constructed and operate in a specific direction, and therefore should not be construed as limiting the present invention. In addition, the terms "first", "second", "third", etc., are used for descriptive purposes only and should not be construed as indicating or implying relative importance.

[0054] It should also be noted that, in the description of this utility model, unless otherwise expressly specified or limited, the terms "mounted," "connected," and "connected" should be understood broadly. For example, they may refer to fixed, detachable, or integral connections; mechanical or electrical connections; and direct or indirect connections through an intermediary. Those skilled in the art will understand the specific meanings of these terms in this utility model depending on the specific circumstances.

[0055] Throughout this specification, references to terms such as "one embodiment," "some embodiments," "example," "specific example," or "an example" mean that the specific features, structures, materials, or characteristics described in conjunction with that embodiment or example are included in at least one embodiment or example of the present application. In this specification, schematic representations of the above terms do not necessarily refer to the same embodiment or example. Furthermore, the specific features, structures, materials, or characteristics described may be combined in any suitable manner in any one or more embodiments or examples.

[0056] The above description is merely a specific embodiment of the present invention, but the scope of protection of the present invention is not limited thereto. Any modifications or substitutions that can be easily conceived by a person skilled in the art within the technical scope disclosed in the present invention should be included within the scope of protection of the present invention. Therefore, the scope of protection of the present invention should be based on the scope of protection of the claims.

Claims

1. A special clamp for aviation pipelines, characterized in that: It includes a clamp body and a rubber gasket, the clamp body includes a clamping assembly, the clamping assembly has a clamping space, a positioning groove is provided on the inner wall surface of the clamping space, and a positioning protrusion adapted to the positioning groove is provided on the side of the rubber gasket facing the clamping space so that the rubber gasket is embedded in the inner wall surface of the clamping assembly, and a friction protrusion is provided on the side of the rubber gasket facing away from the clamping space.

2. The special clamp for aviation pipeline according to claim 1, characterized in that: The clamp body also includes a first wing plate and a second wing plate, the first wing plate and the second wing plate are respectively connected to the open end of the clamping assembly, and the first wing plate and the second wing plate are correspondingly arranged so that when the first wing plate and the second wing plate abut against each other, the clamping space is in a closed state.

3. The special clamp for aviation pipeline according to claim 2, characterized in that: The first wing plate and the second wing plate are correspondingly provided with connecting holes.

4. The special clamp for aviation pipelines according to claim 2, characterized in that: The first wing plate extends along a tangential direction of the clamping assembly to form a straight structure.

5. The special clamp for aviation pipeline according to claim 2, characterized in that: The outer wall surfaces of the connection points between the first wing plate and the clamping assembly and between the second wing plate and the clamping assembly are provided with avoidance grooves.

6. The special clamp for aviation pipelines according to claim 2, characterized in that: The inner wall surface of the clamping assembly is inclined to transition to the inner wall surfaces of the first wing plate and the second wing plate respectively, forming an inclined surface.

7. The special clamp for aviation pipeline according to claim 6, characterized in that: The rubber gasket extends to the inclined surface.

8. The special clamp for aviation pipelines according to claim 7, characterized in that: A weight-reducing groove is provided on the clamp body.

9. The special clamp for aviation pipelines according to claim 1, characterized in that: There are multiple friction protrusions, which extend along the circumference of the clamping space and are arranged parallel to each other.

10. The special clamp for aviation pipelines according to claim 9, characterized in that: At least two long side outer edges of the rubber gasket are respectively provided with friction protrusions.

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