An aircraft model cabin ridge structure and fuselage bonding structure
Patent Information
- Application Number
- CN202522210614.9
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2025-10-20
- Publication Date
- 2026-10-20
- Estimated Expiration
- 2035-10-20
AI Technical Summary
[0004]目前在舱脊的风动测试过程中,需要精细化研究梳理气流效果、测量对机身表面压力的分布等数据,需要在舱脊各个部分安装若干传感器,从而会将舱脊拆分为多块式结构,虽然舱脊大多为一次性物品但对其制造精度要求非常高,在粘接方面目前人工涂胶会出现共振、测试中途断裂等情况干扰测试数据
[0018]本实用新型具有以下有益效果:上脊条和下脊条的拆分能够提供更多的安装位置,安装更加便捷,省略了再次打孔等情况,而通过粘接板的设置能够进行二次连接以保证模块化规模化的普适使用。
Smart Images

Figure CN224868613U_ABST
Abstract
Description
Technical Field
[0001] This utility model relates to the field of aircraft test model technology, and in particular to an aircraft model cabin spine structure and fuselage bonding structure. Background Technology
[0002] The "cabin ridge" is a very prominent feature of the back of an aircraft fuselage. It is usually a raised structure that starts behind the cockpit and extends rearward along the back of the fuselage. It is not only part of the aircraft's shape, but also plays an important role.
[0003] The main functions of the ridge are to provide internal space, improve airflow, contribute to stability, and accommodate equipment. The internal space is used to lay out wiring and pipelines, streamline the airflow to make it smoother, reduce airflow separation, reduce flight drag, and increase the area of the fuselage dorsal fin to provide additional directional stability.
[0004] Currently, during the wind-driven testing of the ridge, it is necessary to conduct detailed research on the airflow effect and measure data such as the distribution of pressure on the fuselage surface. Several sensors need to be installed in various parts of the ridge, which will disassemble the ridge into a multi-piece structure. Although the ridge is mostly a disposable item, its manufacturing precision requirements are very high. In terms of bonding, manual gluing can cause resonance, breakage during testing, and other issues that interfere with the test data. Utility Model Content
[0005] The purpose of this invention is to overcome the shortcomings of the prior art and provide an adhesive structure for bonding the spine structure of an aircraft model to the fuselage, an adhesive structure that provides uniform testing results.
[0006] The purpose of this utility model is achieved through the following technical solution: an aircraft model cabin spine structure and fuselage bonding structure, wherein the cabin spine includes an upper spine strip, a lower spine strip and an adhesive plate for connecting the upper spine strip and the lower spine strip, the upper spine strip, the adhesive plate and the lower spine strip form a streamlined cabin spine structure, the top surface of the adhesive plate is provided with an adhesive layer for use with the upper spine strip, and the bottom surface of the adhesive plate is at least partially embedded in the lower spine strip for bonding.
[0007] The separation of the upper and lower ridge strips provides more installation positions, making installation more convenient and eliminating the need for drilling again. Furthermore, the use of adhesive plates allows for secondary connections to ensure modular and scalable universal use.
[0008] The present invention is further configured such that a strip-shaped adhesive groove is provided on the top surface of the lower ridge strip.
[0009] The strip-shaped adhesive groove can increase the bonding contact area, making it easier to apply adhesive and increasing the amount of adhesive applied.
[0010] The present invention is further configured such that: an adhesive block is provided on the bottom surface of the adhesive plate, the adhesive block is embedded in the adhesive groove, and an adhesive layer is provided between the adhesive plate and the top surface of the lower ridge strip.
[0011] The overall effect is achieved by filling the gap between the adhesive plate and the adhesive groove with an adhesive layer.
[0012] The present invention is further configured such that: an inner groove is provided on the side of the lower ridge strip, and the inner groove extends at least partially from the side of the adhesive groove toward the bottom of the lower ridge strip.
[0013] The recessed groove allows for easy side inspection after the upper and lower ridge bars are installed, enabling a final check to ensure proper installation and successful calibration.
[0014] The present invention is further configured such that a side plate capable of completely filling the inner groove is provided inside the inner groove.
[0015] The inner recess is filled by the side panels to achieve the aerodynamic shape of the complete ridge.
[0016] The present invention is further configured such that the adhesive layer is distributed in a biomimetic pattern of Victoria amazonica.
[0017] By pre-forming the adhesive into a biomimetic distribution resembling Victoria amazonica, the coverage can be effectively improved, the weight can be reduced, and the uniformity of the connection can be improved, thus avoiding resonance.
[0018] The present invention has the following advantages: the separation of the upper and lower ridge strips can provide more installation positions, making installation more convenient and eliminating the need for drilling again; and the setting of the adhesive plate enables secondary connection to ensure modular and large-scale universal use. Attached Figure Description
[0019] Figure 1 This is a perspective view of the ridge of the cabin in an embodiment of this utility model;
[0020] Figure 2 This is a schematic diagram of the ridge structure in an embodiment of this utility model;
[0021] Figure 3 This is a perspective view of the upper ridge strip in an embodiment of this utility model;
[0022] Figure 4 This is a perspective view of the adhesive plate in an embodiment of this utility model;
[0023] Figure 5 This is a second perspective view of the adhesive plate in an embodiment of this utility model;
[0024] Figure 6This is a perspective view of the lower ridge in an embodiment of this utility model;
[0025] Figure 7 This is a second perspective view of the lower ridge in an embodiment of this utility model.
[0026] In the picture:
[0027] 1. Ridge;
[0028] 2. Upper ridge;
[0029] 3. Adhesive board; 31. Adhesive block;
[0030] 4. Lower ridge strip; 41. Adhesive groove; 42. Inward groove;
[0031] 5. Side panels. Detailed Implementation
[0032] To make the objectives, technical solutions, and advantages of the embodiments of this utility model clearer, the technical solutions of the embodiments of this utility model will be clearly and completely described below with reference to the accompanying drawings. Obviously, the described embodiments are only some embodiments of this utility model, not all embodiments. The components of the embodiments of this utility model described and shown in the accompanying drawings can typically be arranged and designed in various different configurations.
[0033] 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 claimed invention, but merely to illustrate selected embodiments of the invention. All other embodiments obtained by those skilled in the art based on the embodiments of the present invention without inventive effort are within the scope of protection of the present invention.
[0034] It should be noted that, where there is no conflict, the embodiments and features in the embodiments of this utility model can be combined with each other.
[0035] It should be noted that similar labels and letters in the following figures indicate similar items. Therefore, once an item is defined in one figure, it does not need to be further defined and explained in subsequent figures.
[0036] In the description of this utility model, it should be noted that the terms "center," "upper," "lower," "left," "right," "vertical," "horizontal," "inner," and "outer," etc., indicate the orientation or positional relationship based on the orientation or positional relationship shown in the accompanying drawings, or the orientation or positional relationship commonly used when the product of this utility model is in use, or the orientation or positional relationship commonly understood by those skilled in the art. They are only used for the convenience of describing this utility model and simplifying the description, and do not indicate or imply that the device or element referred to must have a specific orientation, or be constructed and operated in a specific orientation. Therefore, they should not be construed as limitations on this utility model. In addition, the terms "first," "second," etc., are only used to distinguish descriptions and should not be construed as indicating or implying relative importance.
[0037] In the description of this utility model, it should also be noted that, unless otherwise explicitly specified and limited, the terms "set," "install," "connect," and "link" should be interpreted broadly. For example, they can refer to a fixed connection, a detachable connection, or an integral connection; they can refer to a mechanical connection or an electrical connection; they can refer to a direct connection or an indirect connection through an intermediate medium; and they can refer to the internal connection of two components. Those skilled in the art can understand the specific meaning of the above terms in this utility model based on the specific circumstances.
[0038] The following is in conjunction with the appendix Figure 1-7 The present invention will be described in further detail below, but the scope of protection of the present invention is not limited to the following description.
[0039] like Figure 1 As shown, an aircraft model cabin spine 1 structure is bonded to the fuselage. The cabin spine 1 includes an upper spine 2, a lower spine 4, and an adhesive plate 3 for connecting the upper spine 2 and the lower spine 4. The upper spine 2, the adhesive plate 3, and the lower spine 4 form a streamlined cabin spine 1 structure.
[0040] The top surface of the adhesive plate 3 is provided with an adhesive layer that works in conjunction with the upper ridge 2, and the bottom surface of the adhesive plate 3 is at least partially embedded in the lower ridge 4 for bonding.
[0041] The separation of the upper ridge strip 2 and the lower ridge strip 4 provides more installation positions, making installation more convenient and eliminating the need for drilling again. The secondary connection through the adhesive plate 3 ensures modular and large-scale universal use, while prefabrication ensures test stability.
[0042] The top surface of the lower ridge strip 4 is provided with a strip-shaped adhesive groove 41; the strip-shaped adhesive groove 41 can increase the adhesive contact surface, making it easier to apply adhesive and increasing the amount of adhesive applied.
[0043] An adhesive block 31 is provided on the bottom surface of the adhesive plate 3. The adhesive block 31 is embedded in the adhesive groove 41. An adhesive layer is provided between the top surface of the adhesive plate 3 and the lower ridge strip 4. The preparation effect is achieved by filling the gap between the adhesive plate 3 and the adhesive groove 41 with the adhesive layer.
[0044] The lower ridge 4 has an inner groove 42 on its side, which extends at least partially from the side of the adhesive groove 41 to the bottom of the lower ridge 4. The inner groove 42 allows for easy observation from the side after the upper ridge 2 and lower ridge 4 are installed to check whether the installation is neat and whether the calibration is successful.
[0045] The inner groove 42 is provided with a side plate 5 that can completely fill the inner groove 42; the inner groove 42 is filled by the side plate 5 to achieve the complete aerodynamic shape of the ridge 1.
[0046] In this embodiment, all adhesive layers are distributed in a biomimetic Victoria amazonica pattern with the adhesive. By pre-forming the adhesive into a biomimetic Victoria amazonica pattern, the coverage can be effectively improved, the weight can be reduced, and the uniformity of the connection can be improved, thus avoiding resonance.
[0047] In this embodiment, all adhesive layers are prefabricated using cloth-based adhesive. By distributing different biomimetic Victoria amazonica-shaped cloth-based adhesive sheets that are adapted to the shape of the adhesive surface, the prefabricated cloth-based adhesive can distribute the adhesive more evenly, achieving uniformity and less adhesive usage, thereby reducing weight and avoiding resonance.
[0048] In this embodiment, the biomimetic distribution of the adhesive can also provide more mounting space and prevent sensors, wires and other devices from getting too much adhesive on them.
[0049] Working principle: First, after all the sensors and wiring are set up, a pre-made fabric adhesive sheet is placed on the lower ridge 4. Then, the adhesive block 31 is embedded in the adhesive groove 41. The pre-made fabric adhesive sheet is attached to the upper ridge 2 and connected to the top surface of the adhesive plate 3. Finally, the side plate 5 is embedded in the inner groove 42. Because of the adhesive block 31, the inner groove 42 is pre-set with adhesive to complete the fixation of the ridge 1.
[0050] Although embodiments of the present invention have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and alterations can be made to these embodiments without departing from the principles and spirit of the present invention, the scope of which is defined by the appended claims and their equivalents.
Claims
1. A bonding structure between the spine structure and fuselage of an aircraft model, characterized in that: The ridge (1) includes an upper ridge strip (2), a lower ridge strip (4), and an adhesive plate (3) for connecting the upper ridge strip (2) and the lower ridge strip (4). The upper ridge strip (2), the adhesive plate (3), and the lower ridge strip (4) form a streamlined ridge (1) structure. The top surface of the adhesive plate (3) is provided with an adhesive layer that works in conjunction with the upper ridge strip (2). The bottom surface of the adhesive plate (3) is at least partially embedded in the lower ridge strip (4) for bonding.
2. The bonding structure between the spine structure and fuselage of an aircraft model according to claim 1, characterized in that: The top surface of the lower ridge strip (4) is provided with a strip-shaped adhesive groove (41).
3. The bonding structure between the spine structure and the fuselage of an aircraft model according to claim 2, characterized in that: The bottom surface of the adhesive plate (3) is provided with an adhesive block (31), the adhesive block (31) is embedded in the adhesive groove (41), and an adhesive layer is provided between the adhesive plate (3) and the top surface of the lower ridge strip (4).
4. The bonding structure between the spine structure and the fuselage of an aircraft model according to claim 2, characterized in that: The lower ridge (4) has an inner groove (42) on its side, which extends at least partially from the side of the adhesive groove (41) toward the bottom of the lower ridge (4).
5. The bonding structure between the spine structure and fuselage of an aircraft model according to claim 4, characterized in that: The inner groove (42) is provided with a side plate (5) that can completely fill the inner groove (42).
6. The bonding structure between the spine structure and the fuselage of an aircraft model according to any one of claims 1-5, characterized in that: The adhesive layer is formed by the distribution of adhesive glue in a biomimetic Victoria water lily pattern.