阅读说明：本技术 一种用于无人机降落至海面船艇的降落装置 (Landing device for unmanned aerial vehicle to land on sea surface boat ) 是由 贺军 房佳琦 张秋豪 肖宽容 熊灿松 邓登宝 于 2021-08-25 设计创作，主要内容包括：本发明提供的用于无人机降落至海面船艇的降落装置包括主垫件、承接件、连接件、第一定位件与第二定位件,承接件铺设于主垫件的上端面,连接件的第一端连接于承接件,连接件的第二端连接于船艇的船体,第一定位件固定于承接件的顶面,第二定位件固定于无人机的底部,第一定位件连接第二定位件以使无人机降落于降落装置。承接件铺设于主垫件的上端面,第一定位件固定于承接件的顶面,第二定位件固定于无人机的底部,无人机降落时,第一定位件连接第二定位件以使无人机降落于降落装置,从而避免无人机因船体晃动而无法降落,保证无人机安全、快捷的降落,防止无人机因船体晃动而受损。(The landing device for the unmanned aerial vehicle to land on the sea surface boat comprises a main cushion piece, a bearing piece, a connecting piece, a first positioning piece and a second positioning piece, wherein the bearing piece is laid on the upper end face of the main cushion piece, the first end of the connecting piece is connected to the bearing piece, the second end of the connecting piece is connected to the boat body of the boat, the first positioning piece is fixed to the top face of the bearing piece, the second positioning piece is fixed to the bottom of the unmanned aerial vehicle, and the first positioning piece is connected with the second positioning piece so that the unmanned aerial vehicle lands on the landing device. The up end of main backing spare is laid to the adapting piece, and first setting element is fixed in the top surface of adapting piece, and the second setting element is fixed in unmanned aerial vehicle's bottom, and when unmanned aerial vehicle descended, the second setting element was connected to first setting element so that unmanned aerial vehicle descended in the descending device to avoid unmanned aerial vehicle to rock unable descending because of the hull, guarantee unmanned aerial vehicle safety, swift descending, prevent that unmanned aerial vehicle from rocking because of the hull and impaired.)

1. The utility model provides a descending device that is used for unmanned aerial vehicle to descend to sea ship which characterized in that:

the landing device comprises a main cushion part, a receiving part, a connecting part, a first positioning part and a second positioning part, the receiving part is laid on the upper end surface of the main cushion part, the first end of the connecting part is connected with the receiving part, the second end of the connecting part is connected with the hull of the boat,

the first positioning piece is fixed to the top surface of the bearing piece, the second positioning piece is fixed to the bottom of the unmanned aerial vehicle, and the first positioning piece is connected with the second positioning piece so that the unmanned aerial vehicle can land on the landing device;

the area of the first positioning piece is not less than 80% of the area of the bearing piece and not more than 100% of the area of the bearing piece.

2. A landing assembly for a drone to land on a surface vessel, according to claim 1, wherein:

the main cushion piece is an air cushion, the receiving piece is square canvas, and the connecting piece is a rope.

3. A landing assembly for a drone to land on a surface vessel, according to claim 2, wherein:

the first positioning piece is a hook face sticker, and the second positioning piece is a hair face sticker.

4. A landing assembly for a drone to land on a surface vessel as claimed in claim 3, wherein:

the first locating piece bonds in the top surface of accepting the piece, the second locating piece bonds in unmanned aerial vehicle's bottom.

5. A landing assembly for a drone to land on a surface vessel, according to claim 4, wherein:

the first positioning piece is arranged in a square shape.

6. A landing assembly for a drone to land on a surface vessel, according to claim 2, wherein:

first locating piece with the second locating piece is the magnet piece, first locating piece with the mutual magnetism of second locating piece is inhaled mutually so that unmanned aerial vehicle descend in descending device.

7. A landing assembly for a drone to land on a surface vessel, according to claim 6, wherein:

the first locating piece bonds in the top surface of accepting the piece, the second locating piece bonds in unmanned aerial vehicle's bottom.

8. A landing assembly for a drone to land on a surface vessel according to any one of claims 1 to 7, wherein:

the number of the connecting pieces is four.

Technical Field

The invention belongs to the technical field of aircrafts, and particularly relates to a landing device for an unmanned aerial vehicle to land on a sea surface boat.

Background

Along with the development of economy, aviation flight utensil, especially unmanned aerial vehicle's application is more and more extensive, and unmanned aerial vehicle both can regard as private utensil of shooing, more can be used to the marine operation. Sea patrol inspection is as one of them important work of ocean operation, uses the sea surface ships including ships as the sea patrol inspection ship in order to carry out the sea task of patrolling and examining more, and the sea patrol inspection ship extremely consumes manpower, material resources, and the cost is higher and inefficiency, consequently, along with the development of unmanned aerial vehicle technique, unmanned aerial vehicle also can be applied to sea and patrol inspection. However, when the seasurface boat is on the sea surface, no matter the boat is in the driving process or stops driving, the boat can shake along with sea waves, the landing of the unmanned aerial vehicle is not facilitated, the offshore operation of the unmanned aerial vehicle is mostly taken off and landed on the land, and the voyage of the offshore operation of the unmanned aerial vehicle is shortened.

Disclosure of Invention

The invention mainly aims to provide a landing device for an unmanned aerial vehicle to land on a sea surface boat.

In order to achieve the main purpose, the landing device for the unmanned aerial vehicle to land on the sea surface boat provided by the invention comprises a main cushion part, a bearing part, a connecting part, a first positioning part and a second positioning part, wherein the bearing part is laid on the upper end surface of the main cushion part, the first end of the connecting part is connected to the bearing part, the second end of the connecting part is connected to the hull of the boat, the first positioning part is fixed on the top surface of the bearing part, the second positioning part is fixed on the bottom of the unmanned aerial vehicle, and the first positioning part is connected with the second positioning part so that the unmanned aerial vehicle lands on the landing device; the area of the first positioning piece is not less than 80% of the area of the bearing piece and not more than 100% of the area of the bearing piece.

According to the scheme, the bearing piece is laid on the upper end face of the main cushion piece, the first positioning piece is fixed on the top face of the bearing piece, the second positioning piece is fixed at the bottom of the unmanned aerial vehicle, when the unmanned aerial vehicle lands, the first positioning piece is connected with the second positioning piece so that the unmanned aerial vehicle lands on the landing device, thereby avoiding the unmanned aerial vehicle from being unable to land due to the shaking of the ship body, ensuring the safe and rapid landing of the unmanned aerial vehicle, preventing the unmanned aerial vehicle from being damaged due to the shaking of the ship body, in addition, the area of the first positioning piece is not less than 80% of the area of the adapting piece and not more than 100% of the area of the adapting piece, the area of the bearing part is not less than 80 percent to ensure a sufficient landing area for the unmanned aerial vehicle to land stably, through not exceeding 100% of accepting the piece area and avoiding unmanned aerial vehicle can't descend to accepting the piece top, prevent that unmanned aerial vehicle from falling the skew accepting of point, can obtain abundant descending face support when making unmanned aerial vehicle descend.

Preferably, the main cushion part is an air cushion, the receiving part is square canvas, and the connecting part is a rope.

Furthermore, the first positioning piece is a hook surface patch, and the second positioning piece is a hair surface patch.

Further, first setting element bonds in the top surface of accepting the piece, and the second setting element bonds in unmanned aerial vehicle's bottom.

Further, the first positioning piece is arranged in a square shape.

Preferably, first setting element is magnet spare with the second setting element, and first setting element attracts so that unmanned aerial vehicle descends in the landing device with the mutual magnetism of second setting element mutually.

Further, first setting element bonds in the top surface of accepting the piece, and the second setting element bonds in unmanned aerial vehicle's bottom.

Further, the number of the connecting pieces is four.

Drawings

The invention is further illustrated by means of the attached drawings, but the embodiments in the drawings do not constitute any limitation to the invention, and for a person skilled in the art, other drawings can be derived on the basis of the following drawings without inventive effort.

Figure 1 is an exploded view of an embodiment of a descent apparatus of the invention.

Fig. 2 is a structural view of a landing gear according to an embodiment of the present invention in a use state.

Detailed Description

In order to make the objects, technical solutions and advantages of the present invention more apparent, the present invention is described in further detail below with reference to the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are merely illustrative of the invention and are not intended to limit the invention.

First embodiment

Referring to fig. 1 and fig. 2, the descending device 100 that is used for unmanned aerial vehicle to descend to sea surface ships and light boats that this embodiment provided includes main backing member 1, receiving member 2, connecting piece 3, first setting element 4 and second setting element 5, receiving member 2 lays in the up end of main backing member 1, the first end of connecting piece 3 is connected in receiving member 2, the second end of connecting piece 3 is connected in the hull of ships and light boats, first setting element 4 is fixed in the top surface of receiving member 2, second setting element 5 is fixed in unmanned aerial vehicle's bottom, first setting element 4 is connected second setting element 5 so that unmanned aerial vehicle descends in descending device 100.

The main cushion part 1 is an air cushion, the bearing part 2 is a square canvas, the connecting part 3 is a rope, and the connecting part 3 can be a synthetic fiber rope or a steel rope.

The number of the connecting pieces 3 is four, and one connecting piece 3 is connected to each angle of the square bearing pieces 2.

In this embodiment, the connecting member 3 may be a nylon rope, a first end of the connecting member 3 may be stitched to the bearing member 2, and a second end of the connecting member 3 may be connected to the hull by a knot.

The first positioning piece 4 is a hook face sticker, and the second positioning piece 5 is a hair face sticker.

First setting element 4 bonds in the top surface of accepting 2, and second setting element 5 bonds in unmanned aerial vehicle's bottom, and is specific, and first setting element 4 bonds in the top surface of accepting 2 through the double faced adhesive tape, and second setting element 5 bonds in unmanned aerial vehicle's bottom through the double faced adhesive tape.

The first positioning piece 4 is arranged in a square mode, the area of the first positioning piece 4 is not less than 80% of the area of the bearing piece 2 and not more than 100% of the area of the bearing piece 2, and the area of the first positioning piece 4 and the area of the bearing piece 2 are the projection area of the projection to the horizontal plane.

Receiving piece 2 lays in the up end of main backing member 1, first setting element 4 is fixed in receiving piece 2's top surface, second setting element 5 is fixed in unmanned aerial vehicle 6's bottom, when unmanned aerial vehicle 6 descends, can collude the face subsides of colluding as first setting element 4 and connect the matte subsides as second setting element 5, when unmanned aerial vehicle 6 descends to the descending device, first setting element 4 can collude immediately and connect second setting element 5 so that unmanned aerial vehicle descends in descending device 100, thereby avoid unmanned aerial vehicle to lead to taking place to empty or the unable descending of inflation because of the hull rocks, guarantee unmanned aerial vehicle 6 safety, swift descending, prevent that unmanned aerial vehicle from rocking because of the hull and impaired. In addition, landing device 100 more can locate sea ships and light boats with unmanned aerial vehicle 6's the point of taking off and land, makes the scope of patrolling and examining on the sea increase, and the replenishment of unmanned aerial vehicle fuel can all directly go on the ship, has improved unmanned aerial vehicle's work efficiency, reduces the frequency that personnel went out to the sea and patrol and examine.

When the receiving member 2 is laid on the upper end surface of the main cushion member 1, the bottom surface of the receiving member 2 is connected to the upper end surface of the main cushion member 1, and the receiving member 2 may also be hooked to the main cushion member 1.

With the area of first locating piece 4 be no less than the 2 area of receiving 80% and be no longer than the 100% of 2 area of receiving, through being no less than the 80% of 2 area of receiving and guarantee sufficient descending region in order to supply unmanned aerial vehicle steady to descend, moreover, through not being no less than the 2 area of receiving 100% and avoid unmanned aerial vehicle can't descend to receiving 2 top, prevent that unmanned aerial vehicle from falling the skew receiving 2 of point, can obtain abundant descending face when making unmanned aerial vehicle descend and support.

Second embodiment

First setting element 4 is the magnet piece with second setting element 5, and first setting element 4 attracts so that unmanned aerial vehicle descends in descending device 100 with second setting element 5 mutual magnetism mutually, and first setting element 4 bonds in the top surface of accepting 2, and second setting element 5 bonds in unmanned aerial vehicle's bottom.

When 6 descends to the descending device of unmanned aerial vehicle, first setting element 4 magnetism is inhaled mutually immediately and is connected second setting element 5 so that make unmanned aerial vehicle descend in descending device 100 to avoid unmanned aerial vehicle to rock because of the hull and lead to taking place to empty or the inflation can't descend, guarantee 6 safe, swift descending of unmanned aerial vehicle, prevent that unmanned aerial vehicle from rocking because of the hull and impaired. In addition, landing device 100 more can locate sea ships and light boats with unmanned aerial vehicle 6's the point of taking off and land, makes the scope of patrolling and examining on the sea increase, and the replenishment of unmanned aerial vehicle fuel can all directly go on the ship, has improved unmanned aerial vehicle's work efficiency, reduces the frequency that personnel went out to the sea and patrol and examine.

The rest of the structure is the same as the first embodiment, and is not described herein again.

Finally, it should be emphasized that the present invention is not limited to the above-described embodiments, but only the preferred embodiments of the invention have been described above, and the present invention is not limited to the above-described embodiments, and any modifications, equivalent substitutions, improvements, etc. within the spirit and principle of the present invention should be included in the protection scope of the present invention.