CN213768949U - Stable landing device for unmanned aerial vehicle navigation decoy equipment - Google Patents

Abstract

The utility model discloses a stable descending device that unmanned aerial vehicle navigation was lured and is deceived equipment is used relates to unmanned aerial vehicle descending equipment technical field, can not be applicable to environment such as slope to current unmanned aerial vehicle descending device mostly, greatly reduced unmanned aerial vehicle stabilize descending device's suitability and availability factor's problem, the following scheme of present proposition, it includes descending platform, cushion table and base, descending bench is provided with anti-skidding cushion, spring, limiting plate and gasbag, be provided with spacing groove and horizontal adjustment mechanism on the cushion table, horizontal adjustment mechanism includes horizontal pipe, metal ball, first sheetmetal, second sheetmetal and rubber pad, be provided with electric telescopic handle on the base. The utility model discloses novel structure has solved the most must setting up of common unmanned aerial vehicle descending device and has used on level and smooth ground, can not be applicable to environment such as slope, greatly reduced unmanned aerial vehicle stabilize the suitability of descending device and the problem of availability factor, suitable popularization.

Description

Stable landing device for unmanned aerial vehicle navigation decoy equipment

Technical Field

The utility model relates to an unmanned aerial vehicle descending equipment technical field especially relates to a stable descending device that unmanned aerial vehicle navigation was lured and is deceived equipment and use.

Background

An unmanned plane is called an unmanned plane for short, and is an unmanned plane operated by a radio remote control device and a self-contained program control device, and any artificial plane can stably land by means of a landing gear or a landing buffer device when landing.

Common unmanned aerial vehicle landing device must set up mostly and use on level and smooth ground, can not be applicable to environment such as slope, greatly reduced unmanned aerial vehicle stabilize the suitability and the availability factor of landing device. Therefore, in order to solve the problems, a stable landing device for the unmanned aerial vehicle navigation decoy device is provided.

SUMMERY OF THE UTILITY MODEL

The utility model provides a pair of stable descending device that unmanned aerial vehicle navigation was lured and is deceived equipment and use has solved that common unmanned aerial vehicle descending device most must set up and use on level and smooth ground, can not be applicable to environment such as slope, greatly reduced unmanned aerial vehicle stabilize descending device's suitability and availability factor's problem.

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

the utility model provides a stable descending device that unmanned aerial vehicle navigation was lured and deceives equipment usefulness, includes descending platform, cushion table and base, states the fixed anti-skidding cushion that is the annular array and distributes that is provided with in top of descending platform, just the bottom of descending platform with four springs that the structure is the same of fixedly connected with between the top of cushion table, the bottom fixedly connected with limiting plate and the gasbag of descending platform, just the spacing groove has been seted up at the top of cushion table, fixed mounting has horizontal adjustment mechanism on the lateral wall of cushion table, just the bottom of cushion table with the base is articulated, the inside fixed mounting of base has electric telescopic handle, just electric telescopic handle's one end runs through the top of base extends to the bottom of cushion table, electric telescopic handle's tip with the bottom sliding connection of cushion table.

Preferably, four springs are distributed in a rotational symmetry mode around the axis of the landing platform.

Preferably, the limiting plate is in a closed ring shape, the limiting groove is matched with the limiting plate, the bottom of the limiting plate slides and extends to the inside of the limiting groove, the airbag is located inside the limiting plate, and the bottom of the airbag is fixedly connected with the top of the buffer table.

Preferably, horizontal adjustment mechanism includes horizontal pipe, metal ball, first sheetmetal, second sheetmetal and rubber pad, just fixed mounting has the horizontal pipe that is horizontal setting on the lateral wall of cushion table, the inside slip of horizontal pipe is provided with the metal ball, just the equal fixedly connected with in top and the bottom of the circumference inner wall of horizontal pipe has the same first sheetmetal, second sheetmetal and rubber pad of structure, two first sheetmetal and two the second sheetmetal is all not the mutual contact, just the rubber pad is located the middle section body of horizontal pipe, first sheetmetal and second sheetmetal about the center of rubber pad is the symmetric distribution, and two first sheetmetal is located one side that the horizontal pipe is close to electric telescopic handle.

Preferably, the electric telescopic rod is arranged on one side of the base far away from the hinge joint position of the buffer table, and the first metal sheet and the second metal sheet are respectively and electrically connected with the electric telescopic rod.

The utility model has the advantages that:

1. through the anti-skidding cushion, a spring, the setting of limiting plate and gasbag, unmanned aerial vehicle descends when the top of descending platform, the anti-skidding cushion can effectively prevent unmanned aerial vehicle lateral sliding, unmanned aerial vehicle can make spring and gasbag adaptability compress and realize the cushioning effect to the vertical impact that the descending platform produced, limiting plate adaptability stretches into the spacing groove simultaneously, constantly reduce the deformation space of gasbag, when to the critical state, the gasbag can't produce vertical ascending effort to the descending platform again lateral deformation, produce further cushioning effect, whole effectual unmanned aerial vehicle of having realized can stabilize the effect of descending.

2. Through the arrangement of the horizontal adjusting mechanism and the electric telescopic rod, when the unmanned aerial vehicle is required to fall on a slope and other environments, the side of the electric telescopic rod of the utility model is turned to the downward direction of the slope, the power is switched on, the metal ball rolls to the end of the first metal sheet arranged in the horizontal tube due to the gravity action, the metal ball is connected with the extension control circuit of the electric telescopic rod when contacting with the two first metal sheets to control the lifting of the buffer table, the metal ball rolls to the end of the second metal sheet arranged in the horizontal tube and is connected with the contraction control circuit of the electric telescopic rod when contacting with the two second metal sheets to pull one side of the buffer table to descend, and the metal ball is repeatedly adjusted to be static on the rubber pad, electric telescopic handle's extension and contraction circuit all break off, and electric telescopic handle stop work, the cushion table is in relative horizontality this moment, realizes making things convenient for the effect that unmanned aerial vehicle stabilized descending.

To sum up, the utility model discloses not only can effectively realize unmanned aerial vehicle's stable descending, and can be applicable to environment such as slope, solve common unmanned aerial vehicle descending device and mostly must set up and use on level and smooth ground, can not be applicable to environment such as slope, greatly reduced unmanned aerial vehicle stabilize descending device's suitability and availability factor's problem, suitable popularization.

Drawings

Fig. 1 is a schematic structural view of the present invention;

fig. 2 is a front view of the present invention;

fig. 3 is a structural diagram of the present invention disposed in an environment such as a slope.

Reference numbers in the figures: 1. a landing platform; 2. a buffer table; 3. a base; 4. an anti-slip rubber pad; 5. a spring; 6. a limiting plate; 7. an air bag; 8. a limiting groove; 9. a horizontal adjustment mechanism; 10. an electric telescopic rod; 11. a horizontal tube; 12. a metal ball; 13. a first metal sheet; 14. a second metal sheet; 15. and (7) a rubber pad.

Detailed Description

The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments.

Referring to fig. 1 and 3, a stable landing device for an unmanned aerial vehicle navigation decoy device comprises a landing platform 1, a buffer platform 2 and a base 3, wherein the top of the landing platform 1 is fixedly provided with anti-skid rubber pads 4 distributed in an annular array, four springs 5 with the same structure are fixedly connected between the bottom of the landing platform 1 and the top of the buffer platform 2, the four springs 5 are rotationally and symmetrically distributed about the axis of the landing platform 1, the bottom of the landing platform 1 is fixedly connected with a limiting plate 6 and an air bag 7, the limiting plate 6 is arranged in a closed ring shape, the limiting groove 8 is matched with the limiting plate 6, the bottom of the limiting plate 6 extends to the inside of the limiting groove 8 in a sliding manner, the air bag 7 is positioned inside the limiting plate 6, the bottom of the air bag 7 is fixedly connected with the top of the buffer platform 2, the top of the buffer platform 2 is provided with the limiting groove 8, the side wall of the buffer platform 2 is fixedly provided with a horizontal adjusting mechanism 9, and the bottom of cushion table 2 is articulated with base 3, the inside fixed mounting of base 3 has electric telescopic handle 10, and the one end of electric telescopic handle 10 runs through the top of base 3 and extends to the bottom of cushion table 2, the tip of electric telescopic handle 10 and the bottom sliding connection of cushion table 2, electric telescopic handle 10 sets up in base 3 keep away from with the one side of cushion table 2 articulated position, and two first sheetmetals 13 and second sheetmetals 14 respectively with electric telescopic handle 10 electric connection.

Referring to fig. 2, horizontal adjustment mechanism 9 includes horizontal pipe 11, metal ball 12, first sheetmetal 13, second sheetmetal 14 and rubber pad 15, and fixed mounting has the horizontal pipe 11 that is horizontal setting on the lateral wall of cushion table 2, the inside slip of horizontal pipe 11 is provided with metal ball 12, and the equal fixedly connected with first sheetmetal 13 that the structure is the same in top and the bottom of the circumference inner wall of horizontal pipe 11, second sheetmetal 14 and rubber pad 15, two first sheetmetals 13 and two second sheetmetals 14 are all not mutual contact, and rubber pad 15 is located the middle section body of horizontal pipe 11, first sheetmetal 13 and second sheetmetal 14 are the symmetric distribution about the center of rubber pad 15, and two first sheetmetals 13 are located one side that horizontal pipe 11 is close to electric telescopic handle 10.

The working principle is as follows: the utility model discloses during the use, when unmanned aerial vehicle descends to landing platform 1's top, non-slip rubber mat 4 can effectively prevent unmanned aerial vehicle lateral sliding, unmanned aerial vehicle can make spring 5 and 7 adaptability of gasbag compress the realization cushioning effect to the vertical impact that landing platform 1 produced, simultaneously 6 adaptability of limiting plate stretch into spacing groove 8, constantly reduce gasbag 7's deformation space, when to the critical state, gasbag 7 can not transversely be out of shape again and will produce vertical ascending effort to landing platform 1, produce further cushioning effect, whole effectual unmanned aerial vehicle has realized can stabilize the effect of descending.

When the unmanned aerial vehicle is required to fall on an environment such as a slope, one side of the utility model provided with the electric telescopic rod 10 faces the downward direction of the slope, the power supply of the starting device is started, the metal ball 12 rolls towards one end of the horizontal tube 11 provided with the first metal sheet 13 under the action of gravity, the metal ball 12 is connected with the extension control circuit of the electric telescopic rod 10 when being contacted with the two first metal sheets 13, the rod body of the electric telescopic rod 10 extends and lifts one side of the buffer platform 2 close to the electric telescopic rod 10, when the horizontal critical state is exceeded, the metal ball 12 rolls towards one end of the second metal sheet 14 arranged in the horizontal tube 11, the metal ball 12 is connected with the contraction control circuit of the electric telescopic rod 10 when being contacted with the two second metal sheets 14, the rod body of the electric telescopic rod 10 is stored and pulls the side of the buffer platform 2 close to the electric telescopic rod 10 to descend, when the horizontal critical state tends to, the metal ball 12 rolls reversely, when the metal ball 12 is static on rubber pad 15 in the adjustment of recycling repeatedly, electric telescopic handle 10's extension and contraction circuit all break off, and electric telescopic handle 10 stop work, 2 relative horizontalities that are in of cushion table this moment make things convenient for unmanned aerial vehicle to stabilize the descending.

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 (5)

1. The utility model provides a stable descending device that unmanned aerial vehicle navigation was lured and deceives equipment usefulness, is including descending platform (1), cushion table (2) and base (3), its characterized in that, the fixed anti-skidding cushion (4) that are the annular array and distribute that is provided with in top of descending platform (1), just descend the bottom of platform (1) with four springs (5) that the structure is the same of fixedly connected with between the top of cushion table (2), the bottom fixedly connected with limiting plate (6) and gasbag (7) of descending platform (1), just spacing groove (8) have been seted up at the top of cushion table (2), fixed mounting has horizontal adjusting mechanism (9) on the lateral wall of cushion table (2), just the bottom of cushion table (2) with base (3) are articulated, the inside fixed mounting of base (3) has electric telescopic handle (10), just the one end of electric telescopic handle (10) runs through the top of base (3) extends to the bottom of cushion table (2) The end part of the electric telescopic rod (10) is connected with the bottom of the buffer table (2) in a sliding mode.

2. The stable landing device for the unmanned aerial vehicle navigation decoy equipment of claim 1, wherein four springs (5) are rotationally symmetrically distributed around the axis of the landing platform (1).

3. The stable landing device that unmanned aerial vehicle navigation lures equipment of deceiving of claim 1, characterized in that, limiting plate (6) are the setting of closed ring form, just spacing groove (8) with limiting plate (6) match, the bottom of limiting plate (6) slides and extends to the inside of spacing groove (8), just gasbag (7) are located the inside of limiting plate (6), the bottom of gasbag (7) with the top fixed connection of cushion stage (2).

4. The stable landing device for the unmanned aerial vehicle navigation decoy equipment, according to claim 1, is characterized in that the horizontal adjusting mechanism (9) comprises a horizontal pipe (11), a metal ball (12), a first metal sheet (13), a second metal sheet (14) and a rubber pad (15), the horizontal pipe (11) transversely arranged is fixedly installed on the side wall of the buffer platform (2), the metal ball (12) is slidably arranged in the horizontal pipe (11), the top and the bottom of the circumferential inner wall of the horizontal pipe (11) are fixedly connected with the first metal sheet (13), the second metal sheet (14) and the rubber pad (15) which are identical in structure, the two first metal sheets (13) and the two second metal sheets (14) are not in mutual contact, and the rubber pad (15) is located in the middle pipe body of the horizontal pipe (11), the first metal sheets (13) and the second metal sheets (14) are symmetrically distributed around the center of the rubber pad (15), and the two first metal sheets (13) are positioned on one side, close to the electric telescopic rod (10), of the horizontal pipe (11).

5. The stable landing device for the unmanned aerial vehicle navigation decoy equipment of claim 4, wherein the electric telescopic rod (10) is arranged on one side of the base (3) far away from the hinged position with the buffer table (2), and the two first metal sheets (13) and the second metal sheets (14) are respectively electrically connected with the electric telescopic rod (10).

Images