Unmanned aerial vehicle pod hanger

Abstract

The utility model relates to the field of unmanned aerial vehicle nacelles, and discloses an unmanned aerial vehicle nacelle hanger which comprises a butt joint rod, a first riveting rod and a second riveting rod are fixedly connected to the outer portion of the butt joint rod, buffer springs are fixedly connected to the two ends of the first riveting rod and the two ends of the second riveting rod respectively, and connecting rods are arranged in inner cavities of the buffer springs. A buffer spring is fixedly connected to the bottom of the butt joint rod, a buffer cylinder is fixedly connected to the end of the buffer spring, a stretching spring is fixedly connected to the bottom of the butt joint rod, a holder rod is fixedly connected to the bottom of the stretching spring, and a holder is fixedly connected to the bottom of the holder rod. According to the unmanned aerial vehicle pod hanger, in the flight process of an unmanned aerial vehicle, when an object collides with the buffer cylinders, the buffer cylinders can compress the buffer springs at the moment, then the unmanned aerial vehicle in collision is buffered, meanwhile, damage to the unmanned aerial vehicle is reduced, the problem that an existing unmanned aerial vehicle is damaged during collision is solved, and practicability is improved.

Description

Technical Field

[0001] The utility model relates to the field of unmanned aerial vehicle pod accessories, in particular to a unmanned aerial vehicle pod rack. Background Art

[0002] The optoelectronic pod of a drone is a reconnaissance, photo and video equipment mounted on a drone, which can track, photograph and monitor distant targets around the clock. The optoelectronic pod of a drone uses a wide variety of technologies, and the types of technologies vary slightly depending on the function. The three most commonly used and representative technologies are infrared thermal imaging technology, digital image processing technology, and dynamic target tracking technology. The optoelectronic pod of a drone is an optoelectronic imaging tracking system, and its capture, tracking and aiming (ATP) functions are ultimately completed by a tracking servo system. This tracking servo system is mainly composed of three parts: an optoelectronic sensor system, a signal processing and control system, and a tracking stabilization system (image stabilization system).

[0003] Most of the existing drone pod racks are curved rods, one end of which is mounted on the drone frame, and the other end is connected to the gimbal of the pod optoelectronic equipment to achieve pod suspension installation. In this process, since the drone itself is light and the field of view is poor during night flight, it is easy to collide, which causes the pod structure and the drone to deform and affect the flight trajectory. Therefore, a drone pod rack is proposed to solve the problem that the existing drone is easily damaged by collision during flight. Utility Model Content

[0004] 1. Technical issues to be resolved

[0005] In view of the deficiencies in the prior art, the utility model provides a drone pod hanger to solve the above-mentioned problems.

[0006] (II) Technical solution

[0007] To achieve the above-mentioned purpose, the utility model provides the following technical solutions: a UAV pod bracket, including a docking rod, characterized in that: the outside of the docking rod is fixedly connected with a first riveted rod and a second riveted rod, the two ends of the first rivet rod and the second riveted rod are respectively fixedly connected with a buffer spring, the inner cavity of the buffer spring is provided with a connecting rod, the end of the buffer spring is fixedly connected with a buffer cylinder, the bottom of the docking rod is fixedly connected with a tension spring, the bottom of the tension spring is fixedly connected with a gimbal rod, and the bottom of the gimbal rod is fixedly connected with a gimbal.

[0008] Preferably, four stabilizing arms are arranged above the first riveting rod and the second riveting rod, and the four stabilizing arms are arranged on the top of the first riveting rod and the second riveting rod by means of bolts, thereby improving the stability of the overall hanger.

[0009] Preferably, a plurality of alignment holes are formed through the tops of the first riveting rod and the second riveting rod.

[0010] Preferably, the alignment holes can be respectively connected by two matching alignment rods and two fixed connecting rods through active connection, and the alignment rods and the fixed connecting rods can be adjusted and fixed on the alignment holes to adapt to the specifications of different drones.

[0011] Preferably, two alignment rods are provided below the first riveting rod, and a searchlight is provided at the bottom of the alignment rod. The position of the alignment rod at the alignment hole can be adjusted so that the light source emitted by the searchlight at the bottom will not be blocked by the equipment installed at the bottom, and the operator can observe the position of the UAV.

[0012] Preferably, ends of the first riveting rod and the second riveting rod are fixedly connected with a connecting rod.

[0013] Preferably, two fixed connecting rods are arranged below the second riveted rod, the bottom of the fixed connecting rod is fixedly connected with a bent rod, and the bottom of the bent rod is arranged with a sleeve rod.

[0014] (III) Beneficial effects

[0015] Compared with the prior art, the utility model provides a drone pod rack, which has the following beneficial effects:

[0016] 1. The drone pod bracket is installed at the bottom of the drone using a docking rod. When an object hits the buffer cylinder during the flight of the drone, the buffer cylinder will compress the buffer spring, thereby buffering the drone in collision, thereby reducing damage to the drone and solving the problem that the existing drone is easily damaged by collision during flight.

[0017] 2. When the drone pod mount collides with the drone, the pod mount will vibrate slightly, causing the gimbal at the bottom to shake. The sleeve rod bears the impact of the left and right shaking of the gimbal rod fixed to the gimbal, and the tension spring bears the up and down shaking of the gimbal, reducing the instability of the drone flight caused by the shaking.

[0018] 3. When the drone is flying at night, the position of the alignment rod in the alignment hole is adjusted according to the needs, and the searchlight at the bottom of the alignment rod is turned on to expand the night vision, avoid collision, and improve the safety of the drone during night flight. BRIEF DESCRIPTION OF THE DRAWINGS

[0019] Figure 1 It is a bottom view schematic diagram of the utility model.

[0020] Figure 2 It is a side view schematic diagram of the utility model.

[0021] Figure 3 It is a front view schematic diagram of the utility model.

[0022] In the figure: 1. docking rod; 2. first riveted rod; 3. alignment hole; 4. stabilizing arm; 5. bolt; 6. connecting rod; 7. buffer spring; 8. buffer cylinder; 9. fixed connecting rod; 10. tension spring; 11. bending rod; 12. pan / tilt rod; 13. sleeve rod; 14. pan / tilt; 15. alignment rod; 16. searchlight; 17. second riveted rod. DETAILED DESCRIPTION

[0023] The following will be combined with the drawings in the embodiments of the utility model to clarify the technical solutions in the embodiments of the utility model; it is completely described. Obviously, the described embodiments are only part of the embodiments of the utility model, not all of them. Based on the embodiments in the utility model, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the utility model.

[0024] See also Figure 1-3 A drone pod hanger includes a docking rod 1, characterized in that: the outside of the docking rod 1 is fixedly connected with a first riveted rod 2 and a second riveted rod 17, the two ends of the first rivet rod 2 and the second riveted rod 17 are respectively fixedly connected with a buffer spring 7, the inner cavity of the buffer spring 7 is provided with a connecting rod 6, the end of the buffer spring 7 is fixedly connected with a buffer tube 8, the bottom of the docking rod 1 is fixedly connected with a tension spring 10, the bottom of the tension spring 10 is fixedly connected with a pan-tilt rod 12, and the bottom of the pan-tilt rod 12 is fixedly connected with a pan-tilt 14.

[0025] Furthermore, four stabilizing arms 4 are disposed above the first riveting rod 2 and the second riveting rod 17 , and the four stabilizing arms 4 are disposed on the top of the first riveting rod 2 and the second riveting rod 17 by means of bolts 5 .

[0026] Furthermore, a plurality of alignment holes 3 are formed through the tops of the first riveting rod 2 and the second riveting rod 17 .

[0027] Furthermore, the alignment hole 3 can be respectively connected with two matching alignment rods 15 and two fixed connecting rods 9 through active connection. The alignment rods 15 and the fixed connecting rods 9 can be adjusted and fixed on the alignment hole to adapt to the specifications of different drones.

[0028] Furthermore, two alignment rods 15 are provided below the first riveted rod 2, and a searchlight 16 is provided at the bottom of the alignment rod 15. The position of the alignment rod 15 in the alignment hole 3 can be adjusted so that the light source emitted by the searchlight 16 at the bottom will not be blocked by the equipment installed at the bottom, and the position of the UAV can be observed by the operator.

[0029] Furthermore, the ends of the first riveting rod 2 and the second riveting rod 17 are fixedly connected with a connecting rod 6 .

[0030] Furthermore, two fixed connecting rods 9 are arranged below the second riveting rod 17 , the bottom of the fixed connecting rod 9 is fixedly connected with a bending rod 11 , and the bottom of the bending rod 11 is arranged with a sleeve rod 13 .

[0031] Working principle: When using this drone pod rack, install the docking rod 1 on the bottom of the drone, turn on the searchlight 16, and connect the alignment rod 15 to the alignment hole 3 according to the required field of view of the drone. The closer the alignment hole 3 is to the docking rod 1, the smaller the field of view. On the contrary, the farther the alignment hole 3 is from the docking rod 1, the larger the field of view. This solves the field of view problem of the drone operator. During the flight of the drone, when the drone collides with an object due to careless operation, the force will first act on the buffer cylinder 8. At this time, the buffer cylinder 8 fitted with the outer ring of the connecting rod 6 will compress the buffer spring 7, buffering The impact spring 7 will rebound with the help of the first riveted rod 2 and the second riveted rod 17, thereby avoiding the shaking of the entire drone caused by a hard collision, solving the problem that the existing drones are easily damaged by collisions during flight; at the same time, when a collision occurs, the gimbal 14 will shake, the gimbal rod 12 will stretch the tension spring 10, and the tension spring 10 will use elasticity to buffer slight shaking, and the gimbal rod 12 will hit the sleeve rod 13, and the sleeve rod 13 will use the collision to disperse the impact force generated by the bending rod 11 and the fixed connecting rod 9 fixed in the alignment hole 3, thereby improving the stability of the entire pod.

[0032] Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that various changes, modifications, substitutions and variations may be made to the embodiments without departing from the principles and spirit of the present invention, and that the scope of the present invention is defined by the appended claims and their equivalents.

Claims

1. A drone pod rack, comprising a docking rod (1), characterized in that: The outside of the docking rod (1) is fixedly connected to a first riveted rod (2) and a second riveted rod (17); the two ends of the first riveted rod (2) and the second riveted rod (17) are respectively fixedly connected to a buffer spring (7); the inner cavity of the buffer spring (7) is provided with a connecting rod (6); the end of the buffer spring (7) is fixedly connected to a buffer cylinder (8); the bottom of the docking rod (1) is fixedly connected to a tension spring (10); the bottom of the tension spring (10) is fixedly connected to a pan-tilt rod (12); and the bottom of the pan-tilt rod (12) is fixedly connected to a pan-tilt (14).

2. The UAV pod rack according to claim 1, characterized in that: Four stabilizing arms (4) are arranged above the first riveting rod (2) and the second riveting rod (17), and the four stabilizing arms (4) are arranged on the top of the first riveting rod (2) and the second riveting rod (17) by means of bolts (5).

3. The UAV pod rack according to claim 1, characterized in that: A plurality of alignment holes (3) are provided through the tops of the first riveting rod (2) and the second riveting rod (17).

4. The UAV pod rack according to claim 3, characterized in that: The alignment holes (3) can be respectively connected by two matching alignment rods (15) and two fixed connection rods (9) which are movably connected.

5. The UAV pod rack according to claim 1, characterized in that: Two alignment rods (15) are arranged below the first riveting rod (2), and a searchlight (16) is arranged at the bottom of the alignment rod (15).

6. The UAV pod rack according to claim 1, characterized in that: The ends of the first riveting rod (2) and the second riveting rod (17) are fixedly connected to a connecting rod (6), and the buffer cylinder (8) is sleeved on the outer ring of the connecting rod (6).

7. The UAV pod rack according to claim 1, characterized in that: Two fixed connecting rods (9) are arranged below the second riveted rod (17), the bottom of the fixed connecting rod (9) is fixedly connected to a bent rod (11), and the bottom of the bent rod (11) is arranged with a sleeve rod (13).

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