CN216834256U - Small-size intelligent unmanned vehicles is with stabilizing component - Google Patents
Small-size intelligent unmanned vehicles is with stabilizing component Download PDFInfo
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- CN216834256U CN216834256U CN202220504602.0U CN202220504602U CN216834256U CN 216834256 U CN216834256 U CN 216834256U CN 202220504602 U CN202220504602 U CN 202220504602U CN 216834256 U CN216834256 U CN 216834256U
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Abstract
The utility model provides a stabilizing component for a small intelligent unmanned aerial vehicle, which comprises an aircraft main body and a stabilizing device, wherein at least one propeller is arranged on the aircraft main body; at least one group of stabilizing devices; the stabilizing device at least comprises a mounting block; the stabilizing device at least comprises a first telescopic rod which is used for improving the stability of the aircraft body when the aircraft body descends; the stabilizing device at least comprises a connecting block, and the connecting block is used for connecting the first telescopic rod with the mounting block and the sliding block; the stabilizing device comprises a fixed block; the stabilizing device at least comprises a spring which is used for adjusting the position of the sliding block; the stabilizing device at least comprises a cross bar which is used for improving the stability of the spring; the stabilizing device at least comprises a second telescopic rod; and the landing leg is arranged at the bottom of the aircraft body. This unmanned aerial vehicle of small-size intelligence is with stabilizing component, rational in infrastructure, easy operation uses the flexibility strong, is favorable to using widely.
Description
Technical Field
The utility model belongs to the technical field of unmanned vehicles, concretely relates to small-size intelligent unmanned vehicles is with stabilizing component.
Background
An aircraft is an instrumental flying object made by humans, capable of flying off the ground, flying in space and controlled by humans, flying in the atmosphere or in the extraterrestrial space (space). Flying in the atmosphere is called aircraft and flying in space is called spacecraft.
Along with the progress of science and technology, unmanned vehicles's application is more and more extensive, and the most single structure of present unmanned vehicles's landing leg does not have stabilising arrangement, and unmanned vehicles takes place to turn on one's side because of the relief influence easily when descending, consequently, need design a stabilising arrangement to the not good problem of stability when improving unmanned vehicles and descending.
SUMMERY OF THE UTILITY MODEL
The utility model aims at providing a small-size intelligent unmanned vehicles uses stabilizes component
A stabilizing member for a small intelligent unmanned aerial vehicle, comprising: an aircraft body and a stabilizing device, at least one propeller on the aircraft body for the aircraft body to fly;
at least one group of stabilizing devices;
the stabilizing device comprises at least one mounting block for connection of the stabilizing device to the aircraft body;
the stabilizing device at least comprises a first telescopic rod which is used for improving the stability of the aircraft body when the aircraft body descends;
the stabilizing device at least comprises a connecting block, and the connecting block is used for connecting the first telescopic rod with the mounting block and the sliding block;
the stabilizing device comprises a fixed block;
the stabilizing device at least comprises a spring which is used for adjusting the position of the sliding block;
the stabilizing device at least comprises a cross bar which is used for improving the stability of the spring;
the stabilizing device at least comprises a second telescopic rod;
the landing leg is used for landing of the aircraft body.
Preferably, the stabilizing devices are oppositely distributed with two groups, the mounting blocks are connected with the bottom of the aircraft main body, the mounting blocks are connected with first telescopic rods through connecting blocks, and the first telescopic rods are connected with the sliding blocks through the connecting blocks.
Preferably, two opposite ends of the fixing block are respectively connected with a cross rod, the other end of the cross rod is connected with a baffle, and the cross rod is sleeved with a sliding block.
Preferably, the two ends of the sliding block are respectively connected with a spring, the springs are sleeved with the cross rod, the bottom of the sliding block is connected with a second telescopic rod, and the telescopic end of the second telescopic rod is connected with a first rubber pad.
Preferably, the landing leg has four at least, and distribute respectively in the edge of aircraft main part bottom, the bottom of landing leg is connected with the connecting plate, the bottom of connecting plate is connected with the connecting rod, the bottom of connecting rod is connected with the joint ball, the joint has the bottom plate on the joint ball.
Preferably, the number of the supporting legs is at least four, the supporting legs are respectively distributed at the corners of the bottom of the aircraft main body, the bottom of each supporting leg is connected with a third telescopic rod, and the bottom of each third telescopic rod is connected with a second rubber pad.
The utility model has the advantages that: according to the stabilizing component for the small intelligent unmanned aerial vehicle, the clamping balls and the bottom plate are additionally arranged on the supporting legs, and the angle of the bottom plate can be adjusted according to the height of the terrain when the unmanned aerial vehicle lands by virtue of movable clamping between the clamping balls and the bottom plate, so that the bottom plate is convenient to contact with the ground, and the possibility of side turning is reduced; in addition, rely on the elastic action of spring and the flexible position of adjusting the slider that comes of first telescopic link, be favorable to further improving the descending stability of aircraft main part. This unmanned aerial vehicle of small-size intelligence is with stabilizing component, rational in infrastructure, easy operation uses the flexibility strong, is favorable to using widely.
Drawings
The accompanying drawings are included to provide a further understanding of the invention, and are incorporated in and constitute a part of this specification, illustrate embodiments of the invention, and together with the description serve to explain the invention and not to limit the invention. In the drawings:
fig. 1 is a schematic structural diagram of the present invention;
FIG. 2 is a schematic view of the structure of the stabilizing device of the present invention;
fig. 3 is an enlarged view of a point a in the schematic structural diagram 1 of the present invention;
fig. 4 is another schematic structural diagram of the leg of the present invention.
Labeled as: 1. an aircraft body; 2. a propeller; 3. a stabilizing device; 301. mounting blocks; 302. a first telescopic rod; 303. connecting blocks; 304. a spring; 305. a slider; 306. a fixed block; 307. a cross bar; 308. a first rubber pad; 309. a second telescopic rod; 310. a baffle plate; 4. a support leg; 5. a connecting plate; 6. a connecting rod; 7. clamping the ball; 8. a base plate; 9. a third telescopic rod; 10. and a second rubber pad.
Detailed Description
Example one
As shown in fig. 1 to 3, a stabilizing member for a small intelligent unmanned aerial vehicle comprises an aircraft body 1 and a stabilizing device 3, wherein at least one propeller 2 is arranged on the aircraft body 1 and is used for flying the aircraft body 1;
at least one group of the stabilizing devices 3;
the stabilizing device 3 comprises at least one mounting block 301 for the connection of the stabilizing device 3 to the aircraft body 1;
the stabilizing device 3 comprises at least one first telescopic rod 302 for improving the stability of the aircraft body 1 during descent;
the stabilizing device 3 at least comprises a connecting block 303, which is used for connecting the first telescopic rod 302 with the mounting block 301 and the sliding block 305;
the stabilizing device 3 comprises a fixing block 306;
the stabilizing device 3 comprises at least one spring 304 for adjusting the position of the slide 305;
the stabilizing device 3 comprises at least one cross bar 307 for improving the stability of the spring 304;
the stabilizing device 3 comprises at least one second telescopic rod 309;
Further, the stabilizing devices 3 are distributed in two groups, the mounting blocks 301 are connected with the bottom of the aircraft main body 1, the mounting blocks 301 are connected with the first telescopic rods 302 through the connecting blocks 303, and the first telescopic rods 302 are connected with the sliding blocks 305 through the connecting blocks 303.
Furthermore, the two opposite ends of the fixed block 306 are respectively connected with a cross bar 307, the other end of the cross bar 307 is connected with a baffle 310, the cross bar 307 is sleeved with a sliding block 305, and the baffle 310 plays a limiting role to prevent the sliding block 305 from falling off from the cross bar 307.
Further, the both ends of slider 305 are connected with spring 304 respectively, just spring 304 cup joints with horizontal pole 307, the bottom of slider 305 is connected with second telescopic link 309, when aircraft main part 1 descends, accomplishes the landing through landing leg 4 and third telescopic link 9's cooperation, and at this moment, rely on the telescopic action of first telescopic link 302, the position that slider 305 was used for to the elastic action of spring 304 to support aircraft main part 1, can improve the stability when aircraft main part 1 descends, the flexible end of second telescopic link 309 is connected with first rubber pad 308, and first rubber pad 308 is used for improving frictional force, is favorable to improving the stability when aircraft main part 1 descends.
Further, landing leg 4 has four at least, and distribute respectively in the edge of 1 bottom of aircraft main part, the bottom of landing leg 4 is connected with connecting plate 5, the bottom of connecting plate 5 is connected with connecting rod 6, the bottom of connecting rod 6 is connected with joint ball 7, the joint has bottom plate 8 on the joint ball 7, sets up the joint groove that supplies joint ball 7 to hold on the bottom plate 8, and guarantees that joint ball 7 can not drop, and joint ball 7 is convenient for bottom plate 8 adjustment dispatch with 8 movable joints of bottom plate, is favorable to bottom plate 8 and ground contact, can effectively reduce the possibility that aircraft main part 1 turned on one's side when descending.
Example two
As shown in fig. 4, the difference between the first embodiment and the second embodiment is that, in the present embodiment, at least four support legs 4 are respectively distributed at the corners of the bottom of the aircraft body 1, the bottom of each support leg 4 is connected with a third telescopic rod 9, the length of each third telescopic rod 9 can be adjusted according to different terrain, so as to improve the flexibility of the aircraft body 1 when landing, the bottom of each third telescopic rod 9 is connected with a second rubber pad 10, and each second rubber pad 10 is used for improving the friction force.
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 described in the foregoing embodiments, or equivalents may be substituted for elements thereof. Any modification, equivalent replacement, or improvement made within the spirit and principle of the present invention should be included in the protection scope of the present invention.
Claims (6)
1. A stabilizing component for a small intelligent unmanned aerial vehicle comprises an aircraft body (1) and stabilizing devices (3), and is characterized in that at least one propeller (2) is installed on the aircraft body (1), and at least one group of stabilizing devices (3) is arranged;
each set of stabilizing means (3) comprises,
at least one mounting block (301) for connecting the stabilization device (3) to the aircraft body (1);
at least one first telescopic rod (302), wherein two ends of the first telescopic rod (302) are respectively connected with a connecting block (303)
The stabilizing device (3) comprises a fixing block (306), two ends of the fixing block (306) are respectively connected with a cross rod (307), a sliding block (305) is sleeved on the cross rod (307), one end of the sliding block (305) is connected with a connecting block (303), the other end of the sliding block is connected with a second telescopic rod (309), and the telescopic end of the second telescopic rod (309) is connected with a first rubber pad (308);
at least one supporting leg (4) is installed at the bottom of the aircraft main body (1).
2. The stabilizing member for the small intelligent Unmanned Aerial Vehicle (UAV) according to claim 1, wherein the stabilizing devices (3) are distributed in two groups, the mounting blocks (301) are connected with the bottom of the main body (1) of the aircraft, the mounting blocks (301) are connected with the first telescopic rods (302) through the connecting blocks (303), and the first telescopic rods (302) are connected with the sliding blocks (305) through the connecting blocks (303).
3. The stabilizing member for a small intelligent unmanned aerial vehicle according to claim 1, wherein a baffle (310) is connected to an end of the cross bar (307) away from the fixed block (306).
4. The stabilizing member for the small intelligent unmanned aerial vehicle of claim 1, wherein springs (304) are respectively connected to two ends of the sliding block (305), and the springs (304) are sleeved with the cross bar (307).
5. The stabilizing member for the small intelligent unmanned aerial vehicle according to claim 1, wherein the number of the supporting legs (4) is at least four, and the supporting legs are respectively distributed at the corners of the bottom of the aircraft body (1), a connecting plate (5) is connected to the bottom of the supporting legs (4), a connecting rod (6) is connected to the bottom of the connecting plate (5), a clamping ball (7) is connected to the bottom of the connecting rod (6), and a bottom plate (8) is clamped on the clamping ball (7).
6. The stabilizing member for the small intelligent unmanned aerial vehicle according to claim 1, wherein the number of the supporting legs (4) is at least four, and the supporting legs are respectively distributed at the corners of the bottom of the aircraft body (1), the bottom of each supporting leg (4) is connected with a third telescopic rod (9), and the bottom of each third telescopic rod (9) is connected with a second rubber pad (10).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202220504602.0U CN216834256U (en) | 2022-03-09 | 2022-03-09 | Small-size intelligent unmanned vehicles is with stabilizing component |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202220504602.0U CN216834256U (en) | 2022-03-09 | 2022-03-09 | Small-size intelligent unmanned vehicles is with stabilizing component |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN216834256U true CN216834256U (en) | 2022-06-28 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202220504602.0U Active CN216834256U (en) | 2022-03-09 | 2022-03-09 | Small-size intelligent unmanned vehicles is with stabilizing component |
Country Status (1)
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|---|---|
| CN (1) | CN216834256U (en) |
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- 2022-03-09 CN CN202220504602.0U patent/CN216834256U/en active Active
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