Waterborne aircraft carrier platform

The design of retracting and stacking the main platform and the secondary platform solves the problem that large surface carrier platforms cannot pass through narrow waterways, thus enhancing their versatility.

CN122232818APending Publication Date: 2026-06-19AUTOFLIGHT (KUNSHAN) CO LTD

Patent Information

Authority / Receiving Office
CN · China
Patent Type
Applications(China)
Current Assignee / Owner
AUTOFLIGHT (KUNSHAN) CO LTD
Filing Date
2024-12-18
Publication Date
2026-06-19

AI Technical Summary

Technical Problem

Large surface aircraft carrier platforms are limited in their versatility because their width prevents them from passing through narrow waterways.

Method used

By retracting parts of the platform, including rotating the main platform and auxiliary platforms, stacking them, or shrinking them into a hollow cavity, the width of the surface carrier platform can be reduced to adapt to narrow waterways.

Benefits of technology

It has improved the adaptability of the surface-based aircraft carrier platform to pass through narrow waterways, enhancing its versatility.

✦ Generated by Eureka AI based on patent content.

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Abstract

This application relates to the field of naval vessel technology and discloses a surface-to-water aircraft carrier platform. The surface-to-water aircraft carrier platform includes a main body, a main platform, and a secondary platform. During operation, the main platform and secondary platform are mounted on the same plane as the main body. The secondary platform is connected to the main platform and can retract to the main platform, thereby reducing the width of the surface-to-water aircraft carrier platform and enabling it to pass through narrow waterways. This application allows for free control of the surface-to-water aircraft carrier's width by retracting a portion of the platform, adapting to navigation in various waterways.
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Description

Technical Field

[0001] This application relates to the field of ship technology, and in particular to a seaborne aircraft carrier platform. Background Technology

[0002] For some large surface carrier platforms, their versatility is often limited because their width prevents them from passing through narrow waterways. Summary of the Invention

[0003] The purpose of this application is to provide a surface carrier platform. This surface carrier platform can freely control the width of the surface carrier by retracting part of the platform, so as to adapt to navigation in various waterways.

[0004] To address the aforementioned technical problems, this application provides a seaborne aircraft carrier platform, comprising: a platform body, a main platform, and a secondary platform. The main platform and the secondary platform are mounted on the same plane of the platform body during operation. The secondary platform is connected to the main platform and can retract to the main platform, thereby reducing the width of the seaborne aircraft carrier platform and enabling it to pass through narrow waterways.

[0005] Optionally, the main platform and the sub-platform are rotatably connected, and the sub-platform can be rotatably stacked on the main platform, thereby reducing the width of the seaborne aircraft carrier platform.

[0006] Optionally, the main platform includes a hollow cavity, and the auxiliary platform can retract into the hollow cavity of the main platform, thereby reducing the width of the seaplane carrier platform.

[0007] Optionally, the main platform and the secondary platform are rotatably connected, and the secondary platform is rotatably vertically oriented, thereby reducing the width of the surface carrier platform.

[0008] Optionally, the main platform is erected above the main body of the platform, and the secondary platform is suspended on both sides of the main body of the platform.

[0009] Optionally, the platform body includes a platform section and a control platform section, with the main platform and the sub-platform disposed on the platform section, and the width of the platform section and the control platform section being the same when the sub-platform is retracted.

[0010] Optionally, when the main platform and the auxiliary platform are mounted on the same plane of the platform body during operation, the auxiliary platform is supported by a hydraulic rod and can be retracted vertically downwards by the hydraulic rod.

[0011] This application proposes a surface-to-water aircraft carrier platform that allows for free control of the carrier's width by retracting a portion of the platform, thus adapting to navigation in various waterways. Attached Figure Description

[0012] Figure 1 The image shown is a top view of the seaborne aircraft carrier platform according to an embodiment of this application;

[0013] Figure 2 Shown is a rear view of the seaborne aircraft carrier platform according to an embodiment of this application;

[0014] Figure 3 The diagram shows the left sub-platform folded up in an embodiment of this application.

[0015] Figure 4 This is a schematic diagram showing the state of the left sub-platform stacked on the main platform in an embodiment of this application;

[0016] Figure 5 This is a schematic diagram showing the state in which the left and right sub-platforms of this application embodiment are stacked on the main platform;

[0017] Figure 6 The diagram shows a top view of the embodiments of this application, where the left and right sub-platforms are stacked on the main platform.

[0018] Figure 7 The diagram shown is a structural schematic of the hollow chamber inside the main platform in an embodiment of this application.

[0019] Figure 8 The diagram shown is a structural schematic of the hollow chamber inside the main platform of the sub-platform in an embodiment of this application.

[0020] Figure 9 The diagram shown is a structural schematic of a sub-platform vertically mounted via a hydraulic rod, as described in an embodiment of this application.

[0021] Figure 10 The diagram shown is a structural schematic of an embodiment of this application, in which the sub-platform is supported on the same plane as the main platform by hydraulic rods. Detailed Implementation

[0022] The following embodiments further illustrate the technical solutions of this application. It should be understood that the specific embodiments described herein are merely for explaining this application. Furthermore, it should be noted that, for ease of description, only the parts relevant to this application are shown in the accompanying drawings, not all of them.

[0023] In the description of this application, it should be noted that, unless otherwise expressly specified and limited, the terms "installation," "connection," and "linking" should be interpreted broadly. For example, they can refer to fixed connections or detachable connections; mechanical connections or electrical connections; direct connections or indirect connections through an intermediate medium; and internal connections between two components. Those skilled in the art can understand the specific meaning of the above terms in this application based on the specific circumstances.

[0024] In this application, unless otherwise expressly specified and limited, "above" or "below" the second feature can include direct contact between the first and second features, or contact between the first and second features through another feature between them. Furthermore, "above," "over," and "on top" of the second feature includes the first feature being directly above or diagonally above the second feature, or simply indicates that the first feature is at a higher horizontal level than the second feature. "Below," "below," and "under" the second feature includes the first feature being directly below or diagonally below the second feature, or simply indicates that the first feature is at a lower horizontal level than the second feature.

[0025] Embodiments of this application are described below with reference to the accompanying drawings, such as Figure 1 and Figure 2 As shown in the figure, the seaborne aircraft carrier platform of this application embodiment includes: a platform body 10, a main platform 11, and a secondary platform 12. The main platform 11 and the secondary platform 12 are mounted on the same plane above the platform body 10 during operation. The platform body 10 includes a platform section 101 and a control platform section 102. The main platform 11 and the secondary platform 12 are disposed on the platform section 101. The secondary platform 12 is connected to the main platform 11 and can retract to the main platform 11, thereby reducing the width of the seaborne aircraft carrier platform and enabling it to pass through narrow waterways.

[0026] Specifically, in one embodiment, such as Figures 3 to 6 As shown, the main platform 11 is erected above the platform body 10, and the auxiliary platform 12 is suspended on both sides of the platform body 10. The main platform 11 and the auxiliary platform 12 are rotatably connected, and the auxiliary platform 12 can be rotatably stacked on the main platform 11, thereby reducing the width of the floating aircraft carrier platform. Figure 3 The left auxiliary platform 12 is shown in a rotated state. In one embodiment, the auxiliary platform 12 can be pushed up by a lower thrust device. In another embodiment, the auxiliary platform 12 can also be pulled up by a pulling device. Figure 4 The left sub-platform 12 is stacked on top of the main platform 11. Figure 5 and Figure 6 The left and right sub-platforms 12 are stacked on the main platform 11. Figure 6 The left and right sub-platforms 12 are not connected. Of course, in another embodiment, the left and right sub-platforms 12 can be connected. After the sub-platforms 12 are retracted, the width of the platform part 101 is the same as that of the control platform part 102.

[0027] Specifically, in one embodiment, such as Figure 7 and Figure 8As shown, the main platform 11 includes a hollow cavity 110, and the auxiliary platform 12 can retract into the hollow cavity 110 of the main platform, thereby reducing the width of the seaplane carrier platform. In one embodiment, a slide rail can be arranged in the hollow cavity 110, the auxiliary platform 12 can be mounted on the slide rail, and the slide rail can be moved by an actuation device. In addition, the hollow cavity 110 can be designed to open from above to facilitate installation, maintenance, and replacement.

[0028] In one embodiment, such as Figure 9 and Figure 10 As shown, the main platform 11 and the auxiliary platform 12 are rotatably connected. The auxiliary platform 12 can be rotatably set vertically downwards, thereby reducing the width of the surface carrier platform. The auxiliary platform 12 is supported on the same plane as the main platform 11 by hydraulic rods 13. When it is necessary to adjust the auxiliary platform 12 vertically downwards, this can also be accomplished by hydraulic rods 13.

[0029] This application proposes a surface-to-water aircraft carrier platform that allows for free control of the carrier's width by retracting a portion of the platform, thus adapting to navigation in various waterways.

[0030] The above embodiments are merely illustrative of the principles and effects of this application. Any person skilled in the art can modify or alter the above embodiments without departing from the purpose of this application. Therefore, all equivalent modifications or alterations made by those skilled in the art without departing from the purpose disclosed in this application should still be covered by the claims of this application.

Claims

1. A seaborne aircraft carrier platform, characterised in that, include: The platform consists of a main body (10), a main platform (11), and a secondary platform (12). The main platform (11) and the secondary platform (12) are mounted on the same plane of the main body (10) during operation. The secondary platform (12) is connected to the main platform (11) and can be retracted to the main platform (11) to reduce the width of the aircraft carrier platform and thus pass through narrow waterways.

2. The sea-based aircraft carrier platform of claim 1, wherein, The main platform (11) and the sub-platform (12) are rotatably connected, and the sub-platform (12) can be rotatably stacked on the main platform (11), thereby reducing the width of the seaplane carrier platform.

3. The sea-based aircraft carrier platform of claim 1, wherein, The main platform (11) includes a hollow cavity (110), and the sub-platform (12) can be retracted into the hollow cavity (110) of the main platform, thereby reducing the width of the seaplane carrier platform.

4. The sea-based aircraft carrier platform of claim 1, wherein, The main platform (11) and the sub-platform (12) are rotatably connected. The sub-platform (12) is rotatably set vertically downward, thereby reducing the width of the seaplane carrier platform.

5. The surface carrier platform according to claim 1, characterized in that, The main platform (11) is erected above the platform body (10), and the secondary platform (12) is suspended on both sides of the platform body (10).

6. The surface carrier platform according to claim 1, characterized in that, The platform body (10) includes a platform section (101) and a control platform section (102). The main platform (11) and the sub-platform (12) are disposed on the platform section (101). When the sub-platform (12) is retracted, the width of the platform section (101) and the width of the control platform section (102) are the same.

7. The surface carrier platform according to claim 1, characterized in that, When the main platform (11) and the secondary platform (12) are mounted on the same plane of the platform body (10) during operation, the secondary platform (12) is supported by a hydraulic rod (13) and can be retracted vertically downwards by the hydraulic rod (13).