Aircraft parking frame capable of flying on water

Abstract

The aircraft parking frame capable of flying on the water comprises a floating platform and further comprises a supporting platform, a stabilizing mechanism and a buffering supporting mechanism, the supporting platform is movably connected to the upper portion of the floating platform through the buffering supporting mechanism, and the buffering supporting mechanism is located between the floating platform and the supporting platform and extends towards the outer circumferential side of the floating platform. The stabilizing mechanism is movably connected to the bottom of the supporting platform, penetrates through the floating platform, extends downwards and is used for keeping the stability of the floating platform. The utility model belongs to the technical field of water parking platforms, and particularly relates to an aircraft parking frame capable of flying on water, which aims at improving the stability and the reliability of the aircraft parking frame, improving the supporting stability of the parking frame and reducing the influence caused by waves and water flow.

Description

TECHNICAL FIELD

[0001] The utility model belongs to water parking platform technical field, especially relate to a kind of aircraft parking stand for water flight. BACKGROUND

[0002] Water aircraft can include seaplane, ground effect vehicle, amphibious drone and the like.

[0003] Common parking stand is floating pontoon type parking platform, it is easy to sway when wind and wave are larger, it is greatly influenced by wave and current, its stability and reliability can still be improved, simultaneously, aircraft is parked and it is easy to cause floating pontoon to incline due to uneven weight distribution. UTILITY MODEL CONTENT

[0004] The utility model solves the technical problem to the stability and reliability promotion of aircraft parking stand, improve the support stability of parking stand, reduce the influence brought by wave and current.

[0005] To solve the above technical problem, the utility model adopts the following technical scheme: a kind of aircraft parking stand for water flight, including floating platform, further including support platform, stabilizing mechanism and buffer support mechanism, the support platform is movably connected on the upper portion of floating platform by buffer support mechanism, the buffer support mechanism is located between floating platform and support platform, and extend to the outer circumferential side of floating platform, the stabilizing mechanism is movably connected to the bottom of support platform, and extend downward and pass through floating platform, for keeping the stability of floating platform.

[0006] Further, the buffer support mechanism includes air bag column one, air bag column two and extension rod, the air bag column one is fixedly connected between floating platform and support platform, one end of the extension rod is fixedly connected to the outer circumferential side of floating platform, the air bag column two is fixedly connected to the other end of extension rod, and pipeline connection is carried out between the air bag column one and air bag column two.

[0007] Further, the air bag column one is arranged in ring shape and evenly spaced around the center axis of floating platform, and the position of the air bag column one corresponds to the extension rod.

[0008] Further, the stabilizing mechanism includes connecting cylinder, universal joint assembly and counterweight column, the connecting cylinder is fixedly connected to the bottom wall of floating platform, the counterweight column is movably connected in the connecting cylinder by universal joint assembly, and the universal joint assembly is fixedly connected to the center of the bottom wall of support platform.

[0009] Further, the universal joint assembly includes connecting rod one, universal joint coupling and connecting rod two, the connecting rod one is fixedly connected to the center of the bottom wall of support platform, one end of the universal joint coupling is fixedly connected to the bottom end of the connecting rod one, the connecting rod two is fixedly connected to the other end of the universal joint coupling, and the connecting rod two is fixedly connected to the upper end of the counterweight column.

[0010] Further, the counterweight column is arranged in an inverted circular table type.

[0011] With the above structure, the utility model has the beneficial effects as follows: for the stable support of the water aircraft, the floating platform is floated on the water surface by using the self buoyancy, supports the upper support platform, the buffer support mechanism between the floating platform and the support platform provides the buffer force for the support platform, and extends to the outer circumferential side of the floating platform, expands the support on the water surface;

[0012] The stable mechanism at the bottom of the floating platform increases the floating stability of the floating platform, the connecting barrel extends downward into the water, the counterweight column connected by the universal connecting assembly is lowered by using the gravity, so that the floating platform is not affected by the inclination of the waves and the water flow, and maintains the vertical state with the water surface. BRIEF DESCRIPTION OF DRAWINGS

[0013] The accompanying drawings are included to provide a further understanding of the utility model, and constitute a part of the specification, and are used together with the embodiments of the utility model to explain the utility model, and do not constitute the limitation to the utility model.

[0014] Figure 1 It is an overall structure schematic view of the aircraft parking stand for water flight proposed by the utility model;

[0015] Figure 2 It is an internal structure schematic view of the aircraft parking stand for water flight proposed by the utility model;

[0016] Figure 3 It is a connecting barrel structure schematic view of the aircraft parking stand for water flight proposed by the utility model;

[0017] Figure 4 It is a half sectional view of the aircraft parking stand for water flight proposed by the utility model.

[0018] In the drawings: 1, floating platform, 2, support platform, 3, stable mechanism, 4, buffer support mechanism, 5, air bag column one, 6, air bag column two, 7, extension rod, 8, connecting barrel, 9, universal connecting assembly, 10, counterweight column, 11, connecting rod one, 12, universal joint coupling, 13, connecting rod two. DETAILED DESCRIPTION

[0019] As Figures 1-4As shown in the figure, a kind of aircraft parking stand for water flight, it includes floating platform 1, it further includes support platform 2, stabilizing mechanism 3 and buffer support mechanism 4, support platform 2 is movably connected to the upper portion of floating platform 1 by buffer support mechanism 4, buffer support mechanism 4 is located between floating platform 1 and support platform 2, and extends to the outer circumferential side of floating platform 1, stabilizing mechanism 3 is movably connected to the bottom of support platform 2, and extends downwardly through floating platform 1, for keeping the stability of floating platform 1, floating platform 1 can adopt air bag structure, floats on water surface, support platform 2 is arranged above floating platform 1 by buffer support mechanism 4, and extends to the outer circumferential side of floating platform 1, floats on water surface, expands support surface, improves floating stability, and bottom stabilizing mechanism 3 extends downwardly into water, further increases the stability of floating platform 1 and support platform 2.

[0020] As shown in the figure, Figure 1 , Figure 2 and Figure 4 As shown in the figure, in order to realize the buffer of support platform 2 and reduce the inclination of support platform 2, buffer support mechanism 4 includes air bag column one 5, air bag column two 6 and extension rod 7, air bag column one 5 is fixedly connected between floating platform 1 and support platform 2, one end of extension rod 7 is fixedly connected to the outer circumferential side of floating platform 1, air bag column two 6 is fixedly connected to the other end of extension rod 7, air bag column one 5 and air bag column two 6 are connected by pipeline, air bag column one 5 is arranged in ring shape and uniformly spaced around the center axis of floating platform 1, air bag column one 5 corresponds to the position of extension rod 7, a plurality of air bag column one 5 are connected between floating platform 1 and support platform 2 to support support platform 2, when support platform 2 is stressed, air bag column one 5 in the stress direction is extruded, gas is transported to air bag column two 6 in the corresponding direction through the pipeline, air bag column two 6 expands, increases buoyancy, and provides counter-support force, so that support platform 2 remains stable, and air bag column two 6 extends outwardly through extension rod 7, expands the support surface of floating platform 1.

[0021] As shown in the figure, Figures 2-4 As shown in the figure, in order to further increase the stability of floating platform 1, stabilizing mechanism 3 includes connecting cylinder 8, universal connecting assembly 9 and counterweight column 10, connecting cylinder 8 is fixedly connected to the bottom wall of floating platform 1, counterweight column 10 is movably connected to the inside of connecting cylinder 8 through universal connecting assembly 9, universal connecting assembly 9 is fixedly connected to the center of the bottom wall of support platform 2, counterweight column 10 is movably connected below support platform 2 through universal connecting assembly 9, and vertically downwardly counterweights, increases the stability of floating platform 1 and support platform 2, while connecting cylinder 8 is outside counterweight column 10, reduces the influence of water flow and wave on counterweight column 10;

[0022] In order to realize the activity adjustment of the counterweight column 10, the universal connecting assembly 9 comprises a connecting rod one 11, a universal joint coupling 12 and a connecting rod two 13, the connecting rod one 11 is fixedly connected at the center of the bottom wall of the support platform 2, one end of the universal joint coupling 12 is fixedly connected to the bottom end of the connecting rod one 11, the connecting rod two 13 is fixedly connected to the other end of the universal joint coupling 12, the connecting rod two 13 is fixedly connected to the upper end of the counterweight column 10, the universal joint coupling 12 is movably connected between the counterweight column 10 and the bottom of the support platform 2, so that the counterweight column 10 can be flexibly adjusted, when the support platform 2 is inclined, the counterweight column 10 keeps the downward pulling force, so that the support platform 2 is slowed down in the inclination, the counterweight column 10 is in the shape of an inverted circular truncated cone, the diameter of the bottom of the counterweight column 10 is smaller, so that the water flow resistance is reduced.

[0023] In specific use, the operator places the device on the water surface, the floating plate floats on the water surface due to the material characteristics, the air bag column two 6 expands the support surface of the floating platform 1 outside the floating platform 1, and the counterweight column 10 keeps the downward state;

[0024] When the support platform 2 bears the load, the air bag column one 5 in the stress direction is extruded, the gas is transported to the air bag column two 6 in the corresponding direction through the pipeline, the air bag column two 6 is inflated, the buoyancy is increased, and the counteracting support force is provided, so that the support platform 2 is kept stable, and the air bag column two 6 is extended outward through the extension rod 7, so that the support surface of the floating platform 1 is expanded;

[0025] When the device is impacted by waves or water flow, the connecting cylinder 8 is integrated with the floating platform 1, the connecting cylinder 8 protects the internal counterweight column 10 from the impact, keeps the counterweight column 10 in the vertical downward state, stably pulls down the support platform 2, and keeps the stability of the support platform 2, so that the fluctuation of the support platform 2 is slowed down.

[0026] Although the embodiments of the present application have been shown and described, it should be understood by those skilled in the art that various changes, modifications, replacements and variations can be made to the embodiments without departing from the principles and spirits of the present application, the scope of the present application is defined by the appended claims and their equivalents. In general, if the ordinary skilled in the art is inspired by the present application, without departing from the creative purpose of the present application, the similar structure modes and embodiments are not creatively designed, which should belong to the protection scope of the present application.

Claims

1. A seaplane parking stand, usable for waterborne flight, comprising a floating platform (1), characterized in that: It also includes a support platform (2), a stabilizing mechanism (3) and a buffer support mechanism (4), the support platform (2) is movably connected to the upper part of the floating platform (1) through the buffer support mechanism (4), the buffer support mechanism (4) is located between the floating platform (1) and the support platform (2), and extends to the outer circumferential side of the floating platform (1), the stabilizing mechanism (3) is movably connected to the bottom of the support platform (2) and extends downward through the floating platform (1), used for maintaining the stability of the floating platform (1).

2. A watercraft according to claim 1, wherein: The buffer support mechanism (4) includes a gas bag column one (5), a gas bag column two (6) and an extension rod (7), the gas bag column one (5) is fixedly connected between the floating platform (1) and the support platform (2), one end of the extension rod (7) is fixedly connected to the outer circumferential side of the floating platform (1), the gas bag column two (6) is fixedly connected to the other end of the extension rod (7), and the gas bag column one (5) and the gas bag column two (6) are connected by pipelines.

3. A watercraft according to claim 2, wherein: The gas bag column one (5) is arranged in a ring shape around the center axis of the floating platform (1), and the positions of the gas bag column one (5) and the extension rod (7) correspond to each other.

4. A watercraft according to claim 1, wherein: The stabilizing mechanism (3) includes a connecting cylinder (8), a universal connecting assembly (9) and a counterweight column (10), the connecting cylinder (8) is fixedly connected to the bottom wall of the floating platform (1), the counterweight column (10) is movably connected to the inside of the connecting cylinder (8) through the universal connecting assembly (9), and the universal connecting assembly (9) is fixedly connected to the center of the bottom wall of the support platform (2).

5. A watercraft according to claim 4, wherein: The universal connecting assembly (9) includes a connecting rod one (11), a universal joint coupling (12) and a connecting rod two (13), the connecting rod one (11) is fixedly connected to the center of the bottom wall of the support platform (2), one end of the universal joint coupling (12) is fixedly connected to the bottom end of the connecting rod one (11), the connecting rod two (13) is fixedly connected to the other end of the universal joint coupling (12), and the connecting rod two (13) is fixedly connected to the upper end of the counterweight column (10).

6. A watercraft according to claim 4, wherein: The counterweight column (10) is arranged in an inverted circular table type.

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