Suspension bracket for aviation teaching
By designing a suspension system for aviation education that integrates the simulated wing and engine, the problem of inefficiency caused by the separate setup of existing equipment is solved, thereby improving training efficiency and enabling trainees to fully master the skills.
Patent Information
- Application Number
- CN202520147742.0
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2025-01-21
- Publication Date
- 2026-01-27
- Estimated Expiration
- 2035-01-21
AI Technical Summary
In existing aircraft maintenance training equipment, the wings and engines are set up with separate support or hoisting equipment, which affects the efficiency of training and is not conducive to trainees fully mastering the training content.
Design a suspension system for aviation teaching. The system is stably connected to a simulated wing via a support section and to a simulated engine via a suspension section. The simulated wing and engine are integrated into one unit. Both the support section and the suspension section are detachable for easy disassembly and replacement.
It improves the efficiency of teaching and training, helps trainees fully grasp the training content, and facilitates the disassembly, assembly, and replacement of the simulated wings and engines.
Smart Images
Figure CN223836947U_ABST
Abstract
Description
Technical Field
[0001] This application relates to the field of aviation teaching equipment, and in particular to a suspension system for aviation teaching. Background Technology
[0002] In existing aviation maintenance training, the identification, disassembly, assembly, and troubleshooting of wing and engine components are key training contents. In particular, the training content of wings and engines is related to each other. However, in the existing training equipment, wings and engines are set up in different places by independent support equipment or hoisting equipment. This will affect the efficiency of training and will not be conducive to trainees' comprehensive mastery of the training content. Utility Model Content
[0003] In view of this, the purpose of this application is to provide a suspension system for aviation teaching, in order to solve the problem that the existing method of connecting the wings and engines separately through two sets of support equipment or hoisting equipment affects the efficiency of training and is not conducive to trainees' comprehensive mastery of the training content.
[0004] In accordance with the above objectives, this utility model provides a suspension frame for aviation teaching, wherein the suspension frame for aviation teaching comprises:
[0005] A support section, the top of which is detachably provided with a simulated wing;
[0006] The suspension unit is detachably connected to the simulated engine; the suspension unit includes a first suspension point and a second suspension point, the first suspension point and the second suspension point being located at a first end and a second end in the extension direction of the simulated wing, respectively.
[0007] Preferably, the support includes two support members, which are distributed on both sides of the extension direction of the simulated wing.
[0008] Preferably, the extension direction of the support member is perpendicular to the bottom end of the simulated wing; along the extension direction of the support member, the top end of the support member is screwed to the simulated wing, and the bottom end of the support member is screwed to the moving component.
[0009] Preferably, the movable component includes a connecting plate screwed to the support member, and the movable component also includes a plurality of movable wheels located at the bottom end of the connecting plate away from the support member.
[0010] Preferably, along the extension direction of the simulated wing, the two end faces of the support member are respectively formed with arc-shaped recesses.
[0011] Preferably, the first suspension point has a first fixing part and a first connecting part, the first fixing part is screwed to the simulated wing, and the first connecting part is screwed to the simulated engine.
[0012] Preferably, the second suspension point has a second fixing part and a second connecting part, the second fixing part is screwed to the simulated wing, and the second connecting part is screwed to the simulated engine.
[0013] Preferably, the suspension frame for aviation teaching further includes a receiving component, the housing of which has a recessed portion corresponding to the simulated wing, and the receiving component is fitted to the first end of the simulated wing in the extension direction through the recessed portion.
[0014] Preferably, the interior of the housing is formed with a cavity for housing the piping assembly of the simulated engine.
[0015] Preferably, the housing of the receiving component is further provided with an inspection port cover.
[0016] According to this utility model, the suspension frame for aviation teaching can stably connect to the simulated wing through the support part and stably connect to the simulated engine through the suspension part. That is, the suspension frame can integrate the simulated wing and the simulated engine into one unit, which facilitates teaching and training, effectively improves the efficiency of teaching and training, and helps students fully master the training content. In addition, the support part of this suspension frame is detachably connected to the simulated wing, and the suspension part is also detachably connected to the simulated engine, which makes it easier to disassemble and replace the simulated wing and the simulated engine.
[0017] To make the above-mentioned objectives, features and advantages of this application more apparent and understandable, preferred embodiments are described below in detail with reference to the accompanying drawings. Attached Figure Description
[0018] To more clearly illustrate the technical solutions of the embodiments of this application, the accompanying drawings used in the embodiments will be briefly introduced below. It should be understood that the following drawings only show some embodiments of this application and should not be regarded as a limitation of the scope. For those skilled in the art, other related drawings can be obtained based on these drawings without creative effort.
[0019] Figure 1 This is a schematic diagram of a suspension frame for aviation teaching according to an embodiment of the present invention;
[0020] Figure 2 This is another schematic diagram of a suspension frame for aviation teaching, which is an embodiment of this utility model.
[0021] Icons: 10-Simulated wing; 20-Support component; 200-Arched recess; 21-Connecting plate; 22-Moving wheel; 30-First lifting point; 300-First fixing part; 301-First connecting part; 31-Second lifting point; 310-Second fixing part; 311-Second connecting part; 40-Accommodating component. Detailed Implementation
[0022] The following detailed embodiments are provided to help the reader gain a comprehensive understanding of the methods, apparatus, and / or systems described herein. However, various changes, modifications, and equivalents of the methods, apparatus, and / or systems described herein will be apparent after understanding the disclosure of this application. For example, the order of operations described herein is merely illustrative and is not limited to the order set forth herein; changes that will be apparent after understanding the disclosure of this application are possible, except for operations that must occur in a specific order. Furthermore, for clarity and brevity, descriptions of features known in the art may be omitted.
[0023] The features described herein may be implemented in different forms and should not be construed as being limited to the examples described herein. Rather, the examples described herein have been provided merely to illustrate some of the many feasible ways of implementing the methods, apparatus, and / or systems described herein that will be apparent upon understanding the disclosure of this application.
[0024] Throughout the specification, when an element (such as a layer, region, or substrate) is described as being "on" another element, "connected to" another element, "bonded to" another element, "on" another element, or "covering" another element, it may be directly "on" another element, "connected to" another element, "bonded to" another element, "on" another element, or "covering" another element, or there may be one or more other elements in between. In contrast, when an element is described as being "directly on" another element, "directly connected to" another element, "directly bonded to" another element, "directly on" another element, or "directly covering" another element, there may be no other elements in between.
[0025] As used herein, the term “and / or” includes any one of the relevant items listed and any combination of any two or more items.
[0026] Although terms such as “first,” “second,” and “third” may be used herein to describe individual components, assemblies, regions, layers, or parts, these components, assemblies, regions, layers, or parts are not limited by these terms. Rather, these terms are used only to distinguish one component, assembly, region, layer, or part from another. Therefore, without departing from the teachings of the examples described herein, the first component, assembly, region, layer, or part referred to as the second component, assembly, region, layer, or part may also be referred to as the second component, assembly, region, layer, or part.
[0027] For ease of description, spatial relation terms such as “above,” “upper,” “below,” and “lower” are used herein to describe the relationship between one element and another, as shown in the accompanying drawings. Such spatial relation terms are intended to include not only the orientation depicted in the drawings but also different orientations of the device during use or operation. For example, if the device in the drawings is flipped, an element described as being “above” or “upper” relative to another element will subsequently be “below” or “lower” relative to that other element. Therefore, the term “above” includes both “above” and “below” orientations depending on the spatial orientation of the device. The device may also be positioned in other ways (e.g., rotated 90 degrees or in other orientations), and the spatial relation terms used herein will be interpreted accordingly.
[0028] The terminology used herein is for the purpose of describing various examples only and is not intended to limit this disclosure. Unless the context clearly indicates otherwise, the singular form is also intended to include the plural form. The terms “comprising,” “including,” and “having” enumerate the stated features, quantities, operations, components, elements, and / or combinations thereof, but do not exclude the presence or addition of one or more other features, quantities, operations, components, elements, and / or combinations thereof.
[0029] Variations in the shapes shown in the accompanying drawings may occur due to manufacturing techniques and / or tolerances. Therefore, the examples described herein are not limited to the specific shapes shown in the accompanying drawings, but include changes in shape that may occur during manufacturing.
[0030] The features of the examples described herein can be combined in various ways that will be apparent upon understanding the disclosure of this application. Furthermore, although the examples described herein have a wide variety of constructions, other constructions are possible, as will be apparent upon understanding the disclosure of this application.
[0031] This utility model provides a suspension frame for aviation teaching, such as... Figures 1 to 2As shown, the suspension frame for aviation teaching in this embodiment includes a support part and a suspension part, which can be stably connected to the simulated wing 10 and the simulated engine, respectively. Thus, the simulated wing 10 and the simulated engine can be integrated into one unit through this suspension frame, thereby improving the efficiency of teaching and training. The specific structure of each of the above-mentioned parts of the suspension frame for aviation teaching according to this utility model will be described in detail below.
[0032] In this embodiment, as Figures 1 to 2 As shown, the support includes two support members 20, each of which is perpendicular to the bottom end (plane) of the simulated wing 10 to improve the stability of the simulated wing 10 assembly; along the extension direction of the support member 20, the top end of the support member 20 is screwed to the simulated wing 10, and the bottom end of the support member 20 is screwed to the moving component; furthermore, in order to improve the stability of the connection of the support member 20, the cross-sections at both ends of the extension direction of the support member 20 are formed into a trapezoidal shape structure, that is, the thickness at both ends of the extension direction of the support member 20 is increased.
[0033] Furthermore, in this embodiment, the two support members 20 are distributed on both sides of the extension direction of the simulated wing 10 (the extension direction of the simulated wing 10 is the width direction of the support member 20); further, along the extension direction of the simulated wing 10, the two end faces of the support member 20 are respectively formed with arc-shaped recesses 200, that is, along the extension direction of the support member 20, the support member 20 is formed with a structure that is "narrow in the middle and wide at both ends" to avoid occupying too much space, thereby facilitating the passage of personnel or other equipment, so as to facilitate operations such as equipment maintenance.
[0034] In this embodiment, as Figures 1 to 2 As shown, the above-mentioned moving component includes a connecting plate 21 that is screwed to the support member 20. The moving component also includes a plurality of moving wheels 22 located at the bottom end of the connecting plate 21 away from the support member 20. In this embodiment, the moving wheels 22 are configured as a fuma wheel mechanism, which can realize the flexible movement of the suspension frame and self-locking after moving to the preset position, which is more conducive to the flexible development of teaching and training.
[0035] It should be noted that in this embodiment, the detachable connection between the support and the simulated wing 10 is achieved through screwing. However, there are no specific limitations on the specifications, quantity, or placement of the bolts, as long as the aforementioned technical effect can be achieved. However, this is not the only limitation; the support can also be detachably connected to the simulated wing 10 through other connection methods, such as snap-fit or pin connection.
[0036] In this embodiment, the suspension frame stably connects the simulated engine via the suspension unit, such as... Figures 1 to 2As shown, the suspension includes a first suspension point 30 and a second suspension point 31, located at a first end and a second end respectively along the extension direction of the simulated wing 10. Specifically, the first suspension point 30 has a first fixing part 300 and a first connecting part 301. The first fixing part 300 is screwed to the bottom of the first end along the extension direction of the simulated wing 10, and the first connecting part 301 is screwed to the simulated engine. Similarly, the second suspension point 31 has a second fixing part 310 and a second connecting part 311. The second fixing part 310 is screwed to the bottom of the second end along the extension direction of the simulated wing 10, and the second connecting part 311 is screwed to the simulated engine.
[0037] It should be noted that there are no specific limitations on the specific structure of the first lifting point 30 and the second lifting point 31. For example, in this embodiment, the first fixing part 300 of the first lifting point 30 is formed with a plate-like structure, while the second fixing part 310 of the second lifting point 31 is formed with a column-like structure; or, as... Figure 2 As shown, the structures of the first connecting part 301 and the second connecting part 311 also differ significantly. That is, the structural specifications of the first lifting point 30 and the second lifting point 31 should be determined comprehensively based on actual conditions, such as the engine's outline structure, as long as the technical effect of a stable connection to the simulated engine can be achieved. Furthermore, in this embodiment, the detachable connection between the suspension part and the simulated engine and simulated wing 10 is achieved through bolting, but there are no specific restrictions on the specifications, quantity, or placement of the bolts, as long as the aforementioned technical effect can be achieved. However, this is not the only limitation; the suspension part can also achieve detachable connection with the simulated wing 10 and simulated engine through other connection methods, such as snap-fit or pin connection.
[0038] In this embodiment, to avoid the clutter of piping after the simulated engine and simulated wing 10 are assembled, the suspension frame is also provided with a receiving component 40. For example... Figures 1 to 2 As shown, the housing 40 has a recessed portion corresponding to the simulated wing 10, allowing the housing 40 to be fitted onto the first end of the simulated wing 10 in its extending direction via the recessed portion. To increase the stability of the connection of the housing 40, after the housing 40 and the simulated wing 10 are snapped together, they can be further connected by screws. The housing 40 has an internal cavity for housing the piping and wiring components of the simulated engine, thus preventing cluttered piping from affecting teaching and training.
[0039] Furthermore, the housing of the housing 40 is also provided with an inspection port cover. By removing the inspection port cover, the cavity can be connected to the external space, so as to facilitate the maintenance of the pipes and lines inside the housing 40.
[0040] According to the above-described suspension frame for aviation teaching based on this utility model, the simulated wing 10 can be stably connected through the support part, and the simulated engine can be stably connected through the suspension part. That is, the simulated wing 10 and the simulated engine can be integrated into one unit through this suspension frame, which facilitates the conduct of teaching and training, effectively improves the efficiency of teaching and training, and helps students to fully master the training content. In addition, the support part of this suspension frame is detachably connected to the simulated wing 10, and the suspension part is also detachably connected to the simulated engine, which makes it easier to disassemble and replace the simulated wing 10 and the simulated engine.
[0041] Finally, it should be noted that the above-described embodiments are merely specific implementations of this application, used to illustrate the technical solutions of this application, and not to limit them. The protection scope of this application is not limited thereto. Although this application has been described in detail with reference to the foregoing embodiments, those skilled in the art should understand that any person skilled in the art can still modify or easily conceive of changes to the technical solutions described in the foregoing embodiments, or make equivalent substitutions for some of the technical features, within the technical scope disclosed in this application. Such modifications, changes, or substitutions do not cause the essence of the corresponding technical solutions to deviate from the spirit and scope of the technical solutions of the embodiments of this application, and should all be covered within the protection scope of this application. Therefore, the protection scope of this application should be determined by the protection scope of the claims.
Claims
1. A suspension frame for aviation teaching, characterized in that, The suspension system used for aviation teaching includes: A support section, the top of which is detachably provided with a simulated wing; The suspension unit is detachably connected to the simulated engine; the suspension unit includes a first suspension point and a second suspension point, the first suspension point and the second suspension point being located at a first end and a second end in the extension direction of the simulated wing, respectively.
2. The suspension frame for aviation teaching according to claim 1, characterized in that, The support includes two support members, which are distributed on both sides of the extension direction of the simulated wing.
3. The suspension frame for aviation teaching according to claim 2, characterized in that, The extension direction of the support member is perpendicular to the bottom end of the simulated wing; along the extension direction of the support member, the top end of the support member is screwed to the simulated wing, and the bottom end of the support member is screwed to the moving component.
4. The suspension frame for aviation teaching according to claim 3, characterized in that, The movable component includes a connecting plate screwed to the support member, and the movable component also includes a plurality of movable wheels located at the bottom end of the connecting plate away from the support member.
5. The suspension frame for aviation teaching according to claim 3, characterized in that, Along the extension direction of the simulated wing, the two end faces of the support member are respectively formed with arc-shaped recesses.
6. The suspension frame for aviation teaching according to claim 1, characterized in that, The first suspension point has a first fixing part and a first connecting part. The first fixing part is screwed to the simulated wing, and the first connecting part is screwed to the simulated engine.
7. The suspension frame for aviation teaching according to claim 1, characterized in that, The second suspension point has a second fixing part and a second connecting part. The second fixing part is screwed to the simulated wing, and the second connecting part is screwed to the simulated engine.
8. The suspension frame for aviation teaching according to claim 1, characterized in that, The suspension frame used for aviation teaching also includes a receiving component, the housing of which has a recessed portion corresponding to the simulated wing, and the receiving component is fitted to the first end of the simulated wing in the extension direction through the recessed portion.
9. The suspension frame for aviation teaching according to claim 8, characterized in that, The interior of the housing has a cavity for housing the piping assembly of the simulated engine.
10. The suspension frame for aviation teaching according to claim 8, characterized in that, The housing of the container is also provided with an inspection port cover.