CN210653581U

CN210653581U - Unmanned aerial vehicle lifting platform for scientific investigation ship

Info

Publication number: CN210653581U
Application number: CN201921848541.4U
Authority: CN
Inventors: 李旦; 俞李明; 任善林
Original assignee: Zhejiang Zhoushan Bost Ship Design And Research Institute Co Ltd
Current assignee: Zhejiang Zhoushan Bost Ship Design And Research Institute Co Ltd
Priority date: 2019-10-30
Filing date: 2019-10-30
Publication date: 2020-06-02
Anticipated expiration: 2029-10-30

Abstract

The utility model discloses an unmanned aerial vehicle lift platform for scientific investigation ship, the on-line screen storage device comprises a base, the equal fixedly connected with inserted bar in both sides at base top, and the top of two inserted bars has all to peg graft and has to insert a section of thick bamboo, two the equal fixedly connected with spring of inner wall at an inserted section of thick bamboo top, and two same platforms of top fixedly connected with of inserting a section of thick bamboo, the intermediate position fixedly connected with electro-magnet of platform bottom, and the intermediate position fixedly connected with bracing piece at base top, the top fixedly connected with steel cap of bracing piece. The utility model discloses during the use, the unmanned aerial vehicle descending is in the platform top, and the downward compression spring of platform atress cushions the offend that unmanned aerial vehicle whereabouts produced, avoids unmanned aerial vehicle impaired, along with platform downstream, travel switch collision base switches on being connected of electro-magnet and power, adsorbs the steel cap after the electro-magnet circular telegram, locks the platform, prevents that the spring upwards resets, ensures that unmanned aerial vehicle stably stops.

Description

Unmanned aerial vehicle lifting platform for scientific investigation ship

Technical Field

The utility model relates to an unmanned air vehicle technique field especially relates to an unmanned aerial vehicle lift platform for scientific investigation ship.

Background

At present, scientific research ships are applied to exploring oceanic science, and a series of major scientific problems such as oceanic circulation systems and climate change, oceanic power processes and disasters, deep-sea organisms, gene resources and biodiversity, oceanic ecosystem and carbon circulation, oceanic ridge and continental edge hydrothermal systems and earth deep processes, deep sea seabed oil and gas resource formation mechanisms and the like are solved; unmanned aerial vehicles have wide application in research work of scientific research ships.

The dedicated lift platform of unmanned aerial vehicle does not possess to current scientific research ship, and unmanned aerial vehicle take off and descend and can only go on the deck, and unmanned aerial vehicle can produce the striking when descending and between the deck, can cause the injury to unmanned aerial vehicle under the long-time use, needs a design for the unmanned aerial vehicle lift platform of scientific research ship to solve above-mentioned problem urgently.

SUMMERY OF THE UTILITY MODEL

The utility model aims at solving the shortcoming that exists among the prior art, and the unmanned aerial vehicle lift platform who provides for scientific investigation ship.

In order to achieve the above purpose, the utility model adopts the following technical scheme:

the utility model provides an unmanned aerial vehicle lift platform for scientific investigation ship, includes the base, the equal fixedly connected with inserted bar in both sides at base top, and the top of two inserted bars has all to peg graft and has an inserted section of thick bamboo, two the equal fixedly connected with spring of inner wall at inserted section of thick bamboo top, and two same platforms of top fixedly connected with of inserting a section of thick bamboo, the intermediate position fixedly connected with electro-magnet of platform bottom, and the intermediate position fixedly connected with bracing piece at base top, the top fixedly connected with steel cap of bracing piece, and there is travel switch bottom one side of the platform through bolted connection.

As a further aspect of the present invention: the electromagnet is connected with the travel switch through a lead, and the travel switch is connected with a power supply through a lead.

As a further aspect of the present invention: two push plates are welded at the tops of the inserting rods, and the tops of the two push plates are respectively contacted with the two springs.

As a further aspect of the present invention: the top welding of bracing piece has the supporting shoe, and the outer wall at supporting shoe top is cup jointed to the steel cap.

As a further aspect of the present invention: the edge at platform top has solid fixed ring through bolted connection, and solid fixed ring's inner wall bonds there is the rubber pad.

As a further aspect of the present invention: the middle position of the top of the platform is provided with a groove, and the bottom of the rubber pad is clamped in the groove.

As a further aspect of the present invention: the supporting rod is replaced by an electric push rod, the bottom of the electric push rod is connected with the base through a bolt, and the supporting block is fixedly connected to the top of the electric push rod.

The utility model has the advantages that:

1. by arranging the electromagnet, the travel switch, the inserted rod and the spring, the unmanned aerial vehicle lands above the platform, the force of the platform downwards compresses the spring, collision generated by falling of the unmanned aerial vehicle is buffered, the unmanned aerial vehicle is prevented from being damaged, the travel switch collides with the base along with downward movement of the platform, the electromagnet is conducted to be connected with a power supply, the electromagnet is electrified to adsorb the steel cap, the platform is locked, the spring is prevented from upwards resetting, and the unmanned aerial vehicle is guaranteed to stably stay;

2. by arranging the fixing ring and the rubber pad, the bottom of the unmanned aerial vehicle is protected by the rubber pad, and the rubber pad is arranged on the platform through the fixing ring, so that the rubber pad is convenient to replace after being worn due to long-term use;

3. through setting up electric putter, after the platform was locked by the electro-magnet, can adjust the height of platform through electric putter, make the device have more extensive suitability.

Drawings

Fig. 1 is a structural sectional view of an unmanned aerial vehicle lifting platform for a scientific investigation ship, which is provided in embodiment 1;

fig. 2 is a schematic structural view of a fixing ring of the unmanned aerial vehicle lifting platform for a scientific investigation ship provided in embodiment 1;

fig. 3 is a structural sectional view of the unmanned aerial vehicle lifting platform for a scientific investigation ship provided in embodiment 2.

In the figure: the device comprises a base 1, an inserted rod 2, a push plate 3, an inserted cylinder 4, a spring 5, a fixing ring 6, a rubber pad 7, a steel cap 8, a supporting block 9, an electromagnet 10, a travel switch 11, a platform 12, a supporting rod 13 and an electric push rod 14.

Detailed Description

The technical solution of the present patent will be described in further detail with reference to the following embodiments.

Reference will now be made in detail to embodiments of the present patent, examples of which are illustrated in the accompanying drawings, wherein like or similar reference numerals refer to the same or similar elements or elements having the same or similar function throughout. The embodiments described below with reference to the drawings are exemplary only for the purpose of explaining the present patent and are not to be construed as limiting the present patent.

In the description of this patent, it is to be understood that the terms "center," "upper," "lower," "front," "rear," "left," "right," "vertical," "horizontal," "top," "bottom," "inner," "outer," and the like are used in the orientations and positional relationships indicated in the drawings for the convenience of describing the patent and for the simplicity of description, and are not intended to indicate or imply that the referenced devices or elements must have a particular orientation, be constructed and operated in a particular orientation, and are not to be considered limiting of the patent.

In the description of this patent, it is noted that unless otherwise specifically stated or limited, the terms "mounted," "connected," and "disposed" are to be construed broadly and can include, for example, fixedly connected, disposed, detachably connected, disposed, or integrally connected and disposed. The specific meaning of the above terms in this patent may be understood by those of ordinary skill in the art as appropriate.

Example 1

Referring to fig. 1-2, an unmanned aerial vehicle lift platform for scientific investigation ship, including base 1, the equal fixedly connected with inserted bar 2 in both sides at base 1 top, and there is an inserted section of thick bamboo 4 at the top of two inserted bars 2 all pegged graft, the equal fixedly connected with spring 5 of inner wall at two inserted section of thick bamboo 4 tops, and the same platform 12 of the top fixedly connected with of two inserted section of thick bamboo 4, the intermediate position fixedly connected with electro-magnet 10 of platform 12 bottom, and the intermediate position fixedly connected with bracing piece 13 at base 1 top, the top fixedly connected with steel cap 8 of bracing piece 13, and there is travel switch 11 bottom one side of platform 12 through bolted connection, unmanned aerial vehicle descends in platform 12 top, platform 12 atress compresses spring 5 downwards, bump that produces unmanned aerial vehicle whereabouts is cushioned, avoid unmanned aerial vehicle impaired.

Wherein, electro-magnet 10 is connected with travel switch 11 through the wire, and travel switch 11 is connected with the power through the wire, and along with platform 12 downstream, travel switch 11 collides base 1, switches on being connected of electro-magnet 10 and power, adsorbs steel cap 8 after electro-magnet 10 circular telegram, locks platform 12, prevents spring 5 upwards to reset, and guarantee unmanned aerial vehicle stably stops.

Wherein, push pedal 3 has all been welded at the top of two inserted bar 2, and the top of two push pedal 3 contacts with two springs 5 respectively, and inserted bar 2 presses each other with spring 5 through push pedal 3.

Wherein, the top welding of bracing piece 13 has supporting shoe 9, and steel cap 8 cup joints the outer wall at supporting shoe 9 top.

Wherein, there is solid fixed ring 6 at the edge at platform 12 top through bolted connection, and the inner wall of solid fixed ring 6 bonds and has rubber pad 7, protects unmanned aerial vehicle's bottom through rubber pad 7, and rubber pad 7 is installed on platform 12 through solid fixed ring 6.

Wherein, the middle position at platform 12 top is seted up flutedly, and the inside in the recess is blocked to the bottom of rubber pad 7.

The working principle is as follows: unmanned aerial vehicle descending is in platform 12 top, platform 12 atress back is through push pedal 3 compression spring 5 downwards, clash to unmanned aerial vehicle whereabouts production cushions, it is impaired to avoid unmanned aerial vehicle, along with platform 12 downstream, travel switch 11 collides base 1, switch on being connected of electro-magnet 10 and power, adsorb steel cap 8 after electro-magnet 10 circular telegram, lock platform 12, prevent spring 5 upwards to reset, guarantee unmanned aerial vehicle stably stops, protect unmanned aerial vehicle's bottom through rubber pad 7, rubber pad 7 is installed on platform 12 through solid fixed ring 6, after the rubber pad 7 appears wearing and tearing because of long-time the use, be convenient for change rubber pad 7.

Example 2

Referring to fig. 3, an unmanned aerial vehicle lift platform for scientific research ship, this embodiment compares in embodiment 1, and bracing piece 13 is replaced by electric putter 14, and electric putter 14's bottom is connected with base 1 through the bolt, and supporting shoe 9 fixed connection is in electric putter 14's top.

The working principle is as follows: after the platform 12 is locked by the electromagnet 10, the height of the platform 12 can be adjusted by the electric push rod 14, so that the device has wider applicability.

The above, only be the concrete implementation of the preferred embodiment of the present invention, but the protection scope of the present invention is not limited thereto, and any person skilled in the art is in the technical scope of the present invention, according to the technical solution of the present invention and the utility model, the concept of which is equivalent to replace or change, should be covered within the protection scope of the present invention.

Claims

1. The utility model provides an unmanned aerial vehicle lift platform for scientific investigation ship, includes base (1), its characterized in that, the equal fixedly connected with inserted bar (2) in both sides at base (1) top, and the top of two inserted bar (2) have all to peg graft and have to insert a section of thick bamboo (4), two the equal fixedly connected with spring (5) of inner wall at an inserted section of thick bamboo (4) top, and two same platform (12) of top fixedly connected with of inserting a section of thick bamboo (4), intermediate position fixedly connected with electro-magnet (10) of platform (12) bottom, and intermediate position fixedly connected with bracing piece (13) at base (1) top, the top fixedly connected with steel cap (8) of bracing piece (13), and there is travel switch (11) bottom on one side of platform (12) through bolted connection.

2. The unmanned aerial vehicle lifting platform for scientific investigation ship of claim 1, characterized in that the electromagnet (10) is connected with the travel switch (11) through a wire, and the travel switch (11) is connected with a power supply through a wire.

3. The unmanned aerial vehicle lifting platform for scientific investigation ship of any one of claims 1-2, characterized in that push plates (3) are welded on the tops of two said inserted rods (2), and the tops of two push plates (3) are respectively contacted with two springs (5).

4. The unmanned aerial vehicle lifting platform for scientific investigation ship of claim 1, characterized in that the supporting block (9) is welded on the top of the supporting rod (13), and the steel cap (8) is sleeved on the outer wall of the top of the supporting block (9).

5. The unmanned aerial vehicle lifting platform for scientific investigation ship of claim 1, characterized in that the edge of the top of the platform (12) is connected with a fixed ring (6) through bolts, and the inner wall of the fixed ring (6) is bonded with a rubber pad (7).

6. The unmanned aerial vehicle lifting platform for scientific investigation ship of claim 5, wherein the middle position of the top of the platform (12) is provided with a groove, and the bottom of the rubber pad (7) is clamped in the groove.

7. The unmanned aerial vehicle lifting platform for scientific investigation ship of claim 4, characterized in that the support rod (13) is replaced by an electric push rod (14), the bottom of the electric push rod (14) is connected with the base (1) through a bolt, and the support block (9) is fixedly connected to the top of the electric push rod (14).