CN211943716U - Portable outdoor undercarriage for military unmanned aerial vehicle - Google Patents
Portable outdoor undercarriage for military unmanned aerial vehicle Download PDFInfo
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- CN211943716U CN211943716U CN202020577923.4U CN202020577923U CN211943716U CN 211943716 U CN211943716 U CN 211943716U CN 202020577923 U CN202020577923 U CN 202020577923U CN 211943716 U CN211943716 U CN 211943716U
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- aerial vehicle
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- 206010020649 Hyperkeratosis Diseases 0.000 claims abstract description 4
- 238000013016 damping Methods 0.000 claims description 6
- 239000000463 material Substances 0.000 claims description 3
- 239000000853 adhesive Substances 0.000 claims description 2
- 230000001070 adhesive effect Effects 0.000 claims description 2
- 230000035939 shock Effects 0.000 abstract description 5
- 230000003139 buffering effect Effects 0.000 abstract description 4
- 238000012545 processing Methods 0.000 abstract description 2
- 238000010521 absorption reaction Methods 0.000 description 2
- 238000005452 bending Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
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Abstract
The utility model discloses a for military use unmanned aerial vehicle is with portable outdoor undercarriage, including the undercarriage main part, be equipped with mounting platform in the undercarriage main part, undercarriage main part both sides are equipped with the support frame, and the pot head is equipped with wear-resisting callus on the sole under the support frame to be connected with the head rod between support frame and the mounting platform, be connected with the second connecting rod between the support frame, and second connecting rod lower extreme is equipped with the spliced pole, and the cover is equipped with the spring on the spliced pole, still be equipped with balanced leg between the support frame. This for military use unmanned aerial vehicle makes unmanned aerial vehicle can carry out shock attenuation buffering and balanced processing through balanced leg and spring damper when descending for unmanned aerial vehicle descending stability obtains guaranteeing, reduces the unmanned aerial vehicle descending and receives the possibility of damage.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field specifically is a for military use unmanned aerial vehicle uses portable outdoor undercarriage.
Background
Military drones are unmanned aircraft that are controlled by remote control devices or self-contained programs. The control modes are mainly divided into three types, namely radio remote control, automatic program control and comprehensive control. With the wide application of high and new technologies to weaponry, the development of unmanned aerial vehicles makes breakthrough progress, and the unmanned aerial vehicles frequently turn on in local wars and frequently stand on battle works, and are highly praised by people in the military field of various countries. Military unmanned aerial vehicle can be divided into reconnaissance unmanned aerial vehicle, bait unmanned aerial vehicle, electronic countermeasure unmanned aerial vehicle, communication relay unmanned aerial vehicle, unmanned fighter and target drone etc. can carry out tasks such as information reconnaissance, military striking, information countermeasure, information relay and logistics support. When small-size for military use unmanned aerial vehicle plays and falls in the open air, can lead to roller type undercarriage not convenient to use because of outdoor topography reason, consequently the portable posture undercarriage of accessible carries out safety and rises and falls when playing unmanned aerial vehicle in the open air.
The current outdoor landing gear that for military use unmanned aerial vehicle used when carrying out the use, through the bolt fastening at unmanned aerial vehicle lower extreme or both sides, the support frame of undercarriage generally is the oblique bending structure, can cushion when unmanned aerial vehicle rises and falls, protect unmanned aerial vehicle, but current landing gear is when carrying out unmanned aerial vehicle's descending, stability when control that can not be convenient descends, it is crooked when the ground that if descends is unstable leads to unmanned aerial vehicle to descend easily, produced huge impact force can cause the damage of unmanned aerial vehicle internals during the descending, be unfavorable for unmanned aerial vehicle's protection.
SUMMERY OF THE UTILITY MODEL
The utility model aims at providing: the utility model provides a for military use unmanned aerial vehicle is with portable outdoor undercarriage to solve the portable outdoor undercarriage for military use unmanned aerial vehicle on the existing market that above-mentioned background art provided and set up when carrying out unmanned aerial vehicle's descending, stability when control that can not be convenient descends, if it is crooked when descending ground unstability leads to unmanned aerial vehicle to descend easily, the huge impact force that produces during descending can cause the damage of unmanned aerial vehicle internals, is unfavorable for the problem of unmanned aerial vehicle protection.
The technical scheme of the utility model: the utility model provides a for military use unmanned aerial vehicle is with portable outdoor undercarriage, includes undercarriage main part, be equipped with mounting platform in the undercarriage main part, undercarriage main part both sides are equipped with the support frame, and the pot head is equipped with wear-resisting callus on the sole under the support frame to be connected with the head rod between support frame and the mounting platform, be connected with the second connecting rod between the support frame, and second connecting rod lower extreme is equipped with the spliced pole to the cover is equipped with the spring on the spliced pole, still be equipped with balanced leg between the support frame.
Preferably, a circular through hole is formed in the mounting platform, the support frame is fixedly connected with the mounting platform through the circular through hole of the mounting platform, and a triangular structure is formed among the mounting platform, the support frame and the first connecting rod.
Preferably, the lower end of the support frame is in a 'n' -shaped structure and inclines outwards, and the support frame is fixedly connected with the wear-resistant foot pad through an adhesive.
Preferably, the two ends of the balance leg are of inclined structures, the balance leg is provided with a through hole matched with the shape of the support frame, and the lower end of the balance leg is of a pointed structure.
Preferably, the lower end of the spring is fixedly connected with a damping rubber pad through a bolt, and the damping rubber pad and the wear-resistant foot pad are made of rubber materials.
Preferably, a first connecting rod is uniformly connected and fixed between the second connecting rod and the mounting platform through a bolt, and a triangular structure is formed among the first connecting rod, the second connecting rod and the mounting platform.
Compared with the prior art, the beneficial effects of the utility model are that: this for military use unmanned aerial vehicle makes unmanned aerial vehicle can carry out shock attenuation buffering and balanced processing through balanced leg and spring damper when descending for unmanned aerial vehicle descending stability obtains guaranteeing, reduces the unmanned aerial vehicle descending and receives the possibility of damage. This for military use unmanned aerial vehicle fixes on the support frame with the balanced leg installation of portable outdoor undercarriage, and the support frame can make whole unmanned aerial vehicle obtain the support, and when unmanned aerial vehicle descends, the support frame inclines to the direction of difference respectively with balanced leg, makes the stability of undercarriage obtain the guarantee, even descend in the outdoor unstable place and can not cause the slope of undercarriage yet, has reduced the descending damage probability of unmanned aerial vehicle.
Drawings
FIG. 1 is a schematic view of the portable outdoor landing gear for military unmanned aerial vehicles according to the present invention;
FIG. 2 is a side view of a portable outdoor landing gear for a military unmanned aerial vehicle according to the present invention;
FIG. 3 is a schematic view of a three-dimensional structure of a balance leg of a portable outdoor landing gear for a military unmanned aerial vehicle according to the present invention;
fig. 4 is the utility model relates to a mounting platform and support frame connection structure sketch map of portable outdoor undercarriage for military use unmanned aerial vehicle.
In the figure: 1. undercarriage main part, 2, mounting platform, 3, head rod, 4, support frame, 5, balanced leg, 6, shock attenuation cushion, 7, spring, 8, spliced pole, 9, wear-resisting callus on the sole, 10, second connecting rod.
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. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
Referring to fig. 1-4, the present invention provides a technical solution: a portable outdoor landing gear for a military unmanned aerial vehicle comprises a landing gear body 1, wherein a mounting platform 2 is arranged on the landing gear body 1, a circular through hole is formed in the mounting platform 2, a support frame 4 is fixedly connected with the mounting platform 2 through the circular through hole of the mounting platform 2, a triangular structure is formed among the mounting platform 2, the support frame 4 and a first connecting rod 3, the support frame 4 is fixedly connected with the mounting platform 2 through the circular through hole of the mounting platform 2, the triangular structure is formed among the mounting platform 2, the support frame 4 and the first connecting rod 3, so that the stability of the support frame 4 relative to the military unmanned aerial vehicle can be ensured, the landing of the military unmanned aerial vehicle is ensured, the support frames 4 are arranged on two sides of the landing gear body 1, the lower end of the support frame 4 is outwards inclined in a ' n ' shaped ' structure, and, the support frame 4 with the structure of a 'n' -shaped structure and inclining outwards can have a buffering effect, when a military unmanned aerial vehicle descends through the landing gear main body 1, the support frame 4 can buffer, meanwhile, the support frame 4 enables the military unmanned aerial vehicle to be balanced and stable left and right, the lower end of the support frame 4 is sleeved with the wear-resistant foot pad 9, the first connecting rod 3 is connected between the support frame 4 and the mounting platform 2, the second connecting rod 10 is connected between the support frame 4, the first connecting rod 3 is uniformly connected and fixed between the second connecting rod 10 and the mounting platform 2 through bolts, a triangular structure is formed among the first connecting rod 3, the second connecting rod 10 and the mounting platform 2, the stability of the landing gear main body 1 is enhanced, and the landing gear main body 1 can conveniently realize the landing buffering effect of the military unmanned aerial vehicle through the balancing legs 5 and the support frame 4, the lower end of the second connecting rod 10 is provided with a connecting column 8, the connecting column 8 is sleeved with a spring 7, the lower end of the spring 7 is fixedly connected with a damping rubber pad 6 through a bolt, the damping rubber pad 6 and a wear-resistant foot pad 9 are both made of rubber materials, the upper end of the structural spring 7 is fixedly connected with the connecting column 8, when the undercarriage main body 1 is in contact with the ground, even if the outdoor terrain is unstable, the undercarriage main body 1 can be supported through the elasticity of the spring 7, the stability of the undercarriage main body 1 is ensured, so that the military unmanned aerial vehicle can be stably lifted through the undercarriage main body 1, the military unmanned aerial vehicle is prevented from being skewed and damaged, a balance leg 5 is further arranged between the supporting frames 4, two ends of the balance leg 5 are of an inclined structure, a through hole matched with the shape of the supporting frame 4 is formed in the balance leg 5, the lower end of the balance leg 5, make balance leg 5 can insert and establish on support frame 4, and can stabilize fixedly between the support frame 4, the slope structure at 5 both ends of balance leg can guarantee for military use unmanned aerial vehicle through the stationarity when undercarriage main part 1 descends.
The working principle is as follows: when the portable outdoor landing gear for the military unmanned aerial vehicle is used, firstly, the landing gear main body 1 is fixedly connected with the military unmanned aerial vehicle through the mounting platform 2, the mounting platform 2 is stably connected with the support frame 4 through the first connecting rod 3, the support frame 4 is stably connected through the second connecting rod 10, when the military unmanned aerial vehicle is used, the military unmanned aerial vehicle is placed on the ground through the landing gear main body 1, the spring 7 can perform compression and shock absorption, the military unmanned aerial vehicle is stably placed under the combined action of the spring 7 and the shock absorption rubber mat 6 and the connecting column 8, the military unmanned aerial vehicle can stably take off conveniently, when the military unmanned aerial vehicle lands, the support frame 4 is firstly contacted with the ground, the support frame 4 which is respectively inclined outwards can ensure that the military unmanned aerial vehicle is balanced leftwards and rightwards and buffered, the wear-resistant foot pad 9 at the lower, 5 for military use unmanned aerial vehicle forward-backward slopes of 5 both sides of balance leg relatively, can guarantee for military use unmanned aerial vehicle front and back balance and cushion, the sharp form of 5 lower extremes of balance leg simultaneously can reduce the resistance of descending, the impact force that for military use unmanned aerial vehicle descends is when the support frame 4 that bends, spring 7 through the spliced pole 8 connection can the auxiliary stay frame 4 cushion, realize undercarriage main part 1 in the purpose that the outdoor supplementary for military use unmanned aerial vehicle reaches steady take off and land, thereby accomplish a series of works.
Although the present invention has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that modifications may be made to the embodiments or portions thereof without departing from the spirit and scope of the invention.
Claims (6)
1. The utility model provides a military use unmanned aerial vehicle is with portable outdoor undercarriage, includes undercarriage main part (1), be equipped with mounting platform (2) on undercarriage main part (1), its characterized in that: undercarriage main part (1) both sides are equipped with support frame (4), and the pot head is equipped with wear-resisting callus on the sole (9) under support frame (4) to be connected with head rod (3) between support frame (4) and mounting platform (2), be connected with second connecting rod (10) between support frame (4), and second connecting rod (10) lower extreme is equipped with spliced pole (8), and the cover is equipped with spring (7) on spliced pole (8), still be equipped with between support frame (4) balanced leg (5).
2. The portable outdoor landing gear for military unmanned aerial vehicles of claim 1, wherein: circular through holes are formed in the mounting platform (2), the support frame (4) is fixedly connected with the mounting platform (2) through the circular through holes of the mounting platform (2), and a triangular structure is formed among the mounting platform (2), the support frame (4) and the first connecting rod (3).
3. The portable outdoor landing gear for military unmanned aerial vehicles of claim 1, wherein: the lower end of the support frame (4) is of a 'n' -shaped structure and inclines outwards, and the support frame (4) is fixedly connected with the wear-resistant foot pad (9) through an adhesive.
4. The portable outdoor landing gear for military unmanned aerial vehicles of claim 1, wherein: the two ends of the balance leg (5) are of inclined structures, a through hole matched with the shape of the support frame (4) is formed in the balance leg (5), and the lower end of the balance leg (5) is of a pointed structure.
5. The portable outdoor landing gear for military unmanned aerial vehicles of claim 1, wherein: the lower end of the spring (7) is fixedly connected with a damping rubber pad (6) through a bolt, and the damping rubber pad (6) and the wear-resistant foot pad (9) are made of rubber materials.
6. The portable outdoor landing gear for military unmanned aerial vehicles of claim 1, wherein: and a first connecting rod (3) is also uniformly connected and fixed between the second connecting rod (10) and the mounting platform (2) through bolts, and a triangular structure is also formed between the first connecting rod (3) and the second connecting rod (10) as well as between the first connecting rod and the mounting platform (2).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020577923.4U CN211943716U (en) | 2020-04-17 | 2020-04-17 | Portable outdoor undercarriage for military unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020577923.4U CN211943716U (en) | 2020-04-17 | 2020-04-17 | Portable outdoor undercarriage for military unmanned aerial vehicle |
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| Publication Number | Publication Date |
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| CN211943716U true CN211943716U (en) | 2020-11-17 |
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| CN202020577923.4U Active CN211943716U (en) | 2020-04-17 | 2020-04-17 | Portable outdoor undercarriage for military unmanned aerial vehicle |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114426105A (en) * | 2022-03-02 | 2022-05-03 | 河南省地质环境规划设计院有限公司 | Multi-functional unmanned aerial vehicle of portable that adjustable is balanced plays platform |
-
2020
- 2020-04-17 CN CN202020577923.4U patent/CN211943716U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114426105A (en) * | 2022-03-02 | 2022-05-03 | 河南省地质环境规划设计院有限公司 | Multi-functional unmanned aerial vehicle of portable that adjustable is balanced plays platform |
| CN114426105B (en) * | 2022-03-02 | 2022-10-04 | 河南省地质环境规划设计院有限公司 | Multi-functional unmanned aerial vehicle of portable that adjustable is balanced plays platform |
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