CN212921975U - Unmanned aerial vehicle with collapsible unmanned aerial vehicle supporting piece - Google Patents
Unmanned aerial vehicle with collapsible unmanned aerial vehicle supporting piece Download PDFInfo
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- CN212921975U CN212921975U CN202020971179.6U CN202020971179U CN212921975U CN 212921975 U CN212921975 U CN 212921975U CN 202020971179 U CN202020971179 U CN 202020971179U CN 212921975 U CN212921975 U CN 212921975U
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- unmanned aerial
- aerial vehicle
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Abstract
The utility model discloses an unmanned aerial vehicle with collapsible unmanned aerial vehicle supporting piece, including the unmanned aerial vehicle body, the symmetry is provided with folding supporting mechanism on the unmanned aerial vehicle body, both sides all are provided with storage mechanism around on the unmanned aerial vehicle body, constitute through unmanned aerial vehicle body, folding supporting mechanism and storage mechanism the utility model discloses a main body structure realizes folding accomodating and opening of unmanned aerial vehicle body support end through folding supporting mechanism, conveniently adjusts the flight and the mode of falling to the ground of unmanned aerial vehicle body, wherein when the supporting leg is accomodate, can guarantee the stability of unmanned aerial vehicle body flight state, when the supporting leg is opened, play the support fixed action to the unmanned aerial vehicle body, can accomodate the protection to the supporting leg under the flight state through storage mechanism, the utility model provides an unmanned aerial vehicle with collapsible unmanned aerial vehicle supporting piece, flight state is stable, the operation is convenient.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field, the unmanned aerial vehicle of specific field for being equipped with collapsible unmanned aerial vehicle supporting piece.
Background
Unmanned aerial vehicles are unmanned aerial vehicles operated by radio remote control equipment and self-contained program control devices, and generally, unmanned aerial vehicles can be divided into: unmanned helicopters, unmanned fixed wing aircraft, unmanned airships, unmanned umbrella wing aircraft and the like. However, current unmanned aerial vehicle's strutting arrangement can't contract, influences the air current that unmanned aerial vehicle flies, and the flight steadiness receives the influence, for this reason, we propose the unmanned aerial vehicle that is equipped with collapsible unmanned aerial vehicle bearing.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an unmanned aerial vehicle with collapsible unmanned aerial vehicle supporting piece to solve the problem of proposing in the above-mentioned background art.
In order to achieve the above object, the utility model provides a following technical scheme: the unmanned aerial vehicle provided with the foldable unmanned aerial vehicle supporting piece comprises an unmanned aerial vehicle body, wherein folding supporting mechanisms are symmetrically arranged on the unmanned aerial vehicle body, and storage mechanisms are arranged on the front side and the rear side of the unmanned aerial vehicle body;
the folding support mechanism comprises a mounting seat, the mounting seat is connected with the unmanned aerial vehicle body, a driving motor and a fixing frame are arranged on the mounting seat, a rotating shaft is arranged in the fixing frame, a driving wheel is arranged on the output end of the driving motor, a driven wheel is arranged on the rotating shaft, the driving wheel is meshed with the driven wheel, adjusting support rods are arranged at two ends of the rotating shaft, and support assemblies are arranged on the adjusting support rods;
the storage mechanism comprises an upper baffle, one end of the upper baffle is connected with the unmanned aerial vehicle body, the other end of the upper baffle is provided with a side baffle, and the left side and the right side of the side baffle are provided with side plates.
Preferably, the adjusting support rod is an arc-shaped structure taking the rotating shaft as a rotating shaft.
Preferably, the mount includes fixed frame, fixed frame with the mount pad links to each other, the inside symmetry of fixed frame is provided with the connecting plate, be provided with the bearing frame on the connecting plate, the bearing frame with pivot looks adaptation.
Preferably, the side shield with the interval of unmanned aerial vehicle body is greater than supporting component's lower terminal surface diameter, be provided with the rubber pad on receiving mechanism's the inside wall.
Preferably, the supporting assembly comprises supporting legs, one ends of the supporting legs are connected with the adjusting supporting rods, the distance between the upper end faces of the supporting legs is smaller than that between the lower end faces of the supporting legs, and supporting blocks are arranged at the other ends of the supporting legs.
Preferably, the diameter of supporting shoe is greater than the diameter of supporting leg, both sides around the interval of supporting leg is greater than the fuselage thickness of unmanned aerial vehicle body, the length of pivot is greater than the fuselage thickness of unmanned aerial vehicle body.
Preferably, the supporting component comprises an upper connecting block and a lower connecting block, the upper connecting block is connected with the adjusting support rod, a slot is formed in the upper connecting block, an inserting rod is arranged on the lower connecting block and inserted into the slot, a damping spring is arranged between the upper connecting block and the lower connecting block, a cushion block is arranged on the lower surface of the lower connecting block, and a damping pad is wrapped on the lower connecting block.
Compared with the prior art, the beneficial effects of the utility model are that: constitute through unmanned aerial vehicle body, folding supporting mechanism and storage mechanism the utility model discloses a main part structure realizes folding of unmanned aerial vehicle body support end through folding supporting mechanism and accomodates and open, conveniently adjusts the flight and the mode of falling to the ground of unmanned aerial vehicle body, and when wherein the supporting leg was accomodate, can guarantee the stability of unmanned aerial vehicle body flight state, when the supporting leg was opened, played the support fixed action to the unmanned aerial vehicle body, can accomodate the protection to the supporting leg under the flight state through storage mechanism, the utility model provides an unmanned aerial vehicle with collapsible unmanned aerial vehicle bearing spare, flight state is stable, supports firmly, and the operation is convenient.
Drawings
Fig. 1 is a schematic front view of an embodiment 1 of the unmanned aerial vehicle provided with a foldable unmanned aerial vehicle support of the present invention;
fig. 2 is a schematic view of the interior structure of an unmanned aerial vehicle embodiment 1 provided with a foldable unmanned aerial vehicle support according to the present invention;
fig. 3 is a schematic diagram of a right-view structure of an unmanned aerial vehicle storage mechanism provided with a foldable unmanned aerial vehicle support member according to the present invention;
fig. 4 is a schematic front view of an embodiment 2 of the unmanned aerial vehicle provided with a foldable unmanned aerial vehicle support of the present invention;
figure 5 is the utility model discloses unmanned aerial vehicle embodiment 2's supporting component main view inner structure schematic diagram with collapsible unmanned aerial vehicle bearing.
In the figure: the unmanned aerial vehicle comprises an unmanned aerial vehicle body 1, a mounting seat 2, a driving motor 3, a rotating shaft 4, a driving wheel 5, a driven wheel 6, an adjusting support rod 7, an upper baffle 8, a side baffle 9, a side baffle 10, a side plate 11, a fixing frame 11, a connecting plate 12, a connecting plate 13, a supporting leg 14, a supporting block 15, an upper connecting block 16, a lower connecting block 16, a slot 17, an inserting rod 18, a damping spring 19, a cushion block 20 and a damping pad 21.
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.
It should be noted that, in the description of the present invention, for the orientation words, such as the terms "center", "length", "width", "thickness", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", "clockwise", "counterclockwise", etc., the orientation and the positional relationship are indicated based on the orientation or the positional relationship shown in the drawings, and only for the convenience of describing the present invention and simplifying the description, but not for indicating or implying that the indicated device or element must have a specific orientation, be constructed and operated in a specific orientation, and should not be interpreted as limiting the specific scope of the present invention.
Example 1:
referring to fig. 1-3, the present embodiment provides a technical solution: unmanned aerial vehicle with collapsible unmanned aerial vehicle supporting piece, including unmanned aerial vehicle body 1, folding supporting mechanism is provided symmetrically on unmanned aerial vehicle body 1, both sides all are provided with storage mechanism around on unmanned aerial vehicle body 1, constitute through unmanned aerial vehicle body 1, folding supporting mechanism and storage mechanism the utility model discloses a main body structure realizes folding accomodating and opening of unmanned aerial vehicle body 1 support end through folding supporting mechanism, conveniently adjusts the flight and the mode of falling to the ground of unmanned aerial vehicle body 1, wherein when supporting leg 13 accomodates, can guarantee the stability of unmanned aerial vehicle body 1 flight state, when supporting leg 13 opens, play the support fixed action to unmanned aerial vehicle body 1, can accomodate the protection to supporting leg 13 under the flight state through storage mechanism, the utility model provides an unmanned aerial vehicle with collapsible unmanned aerial vehicle supporting piece, flight state is stable, supports firmly, the operation is convenient;
the folding support mechanism comprises a mounting seat 2, the mounting seat 2 is connected with the unmanned aerial vehicle body 1, a driving motor 3 and a fixing frame are arranged on the mounting seat 2, a rotating shaft 4 is arranged in the fixing frame, a driving wheel 5 is arranged at the output end of the driving motor 3, a driven wheel 6 is arranged on the rotating shaft 4, the driving wheel 5 is meshed with the driven wheel 6, adjusting support rods 7 are arranged at two ends of the rotating shaft 4, and support assemblies are arranged on the adjusting support rods 7;
storage mechanism includes overhead gage 8, the one end of overhead gage 8 with unmanned aerial vehicle body 1 links to each other, the other end of overhead gage 8 is provided with side shield 9, the left and right sides of side shield 9 is provided with sideboard 10.
Specifically, the adjusting support rod 7 is an arc-shaped structure using the rotating shaft 4 as a rotating shaft.
Specifically, the supporting assembly comprises supporting legs 13, one ends of the supporting legs 13 are connected with the adjusting supporting rods 7, the distance between the upper end faces of the supporting legs 13 on the left side and the right side is smaller than that between the lower end faces of the supporting legs, and supporting blocks 14 are arranged at the other ends of the supporting legs 13.
Particularly, the diameter of supporting shoe 14 is greater than the diameter of supporting leg 13, both sides around the interval of supporting leg 13 is greater than the fuselage thickness of unmanned aerial vehicle body 1, the length of pivot 4 is greater than the fuselage thickness of unmanned aerial vehicle body 1.
The working principle is as follows: the utility model provides an unmanned aerial vehicle with a foldable unmanned aerial vehicle supporting part, the unmanned aerial vehicle body is an unmanned aerial vehicle body 1 of an unmanned aerial vehicle operated by a radio remote control device and a self-contained program control device, as shown in figure 1, the folding supporting mechanism is in an open state, wherein a supporting block 14 is contacted with the ground, the supporting legs 13 at the left side and the right side are in a splayed shape and play a better supporting role for the unmanned aerial vehicle body 1, when the unmanned aerial vehicle body 1 is in a flying state, the flying state of the unmanned aerial vehicle body is influenced by the open state of the supporting legs 13, therefore, when the unmanned aerial vehicle body 1 flies, a driving motor 3 is controlled to work, a driven wheel 6 is driven by a driving wheel 5 to rotate, a rotating shaft 4 is driven to rotate along with the supporting legs, the supporting legs 13 at the left side and the right side are driven by, the driving motor 3 drives the driving wheel 5 to rotate reversely, and the state is recovered to the state shown in figure 1.
Example 2:
referring to fig. 3-5, the present embodiment provides a technical solution: the unmanned aerial vehicle provided with the foldable unmanned aerial vehicle supporting piece, the fixing frame comprises a fixing frame 11, the fixing frame 11 is connected with the mounting seat 2, connecting plates 12 are symmetrically arranged inside the fixing frame 11, bearing seats are arranged on the connecting plates 12 and are matched with the rotating shaft 4, the distance between the side baffle 9 and the unmanned aerial vehicle body 1 is larger than the diameter of the lower end face of the supporting component, rubber pads are arranged on the inner side wall of the accommodating mechanism, the supporting component comprises an upper connecting block 15 and a lower connecting block 16, the upper connecting block 15 is connected with the adjusting supporting rod 7, a slot 17 is formed in the upper connecting block 15, an inserting rod 18 is arranged on the lower connecting block 16, the inserting rod 18 is inserted into the slot 17, limit blocks are symmetrically arranged at the top of the side wall of the inserting rod 18, and limit slot bodies matched with the limit blocks are, the inserting rod 18 can be prevented from falling off from the inserting groove 17, a damping spring 19 is arranged between the upper connecting block 15 and the lower connecting block 16, a cushion block 20 is arranged on the lower surface of the lower connecting block 16, and a damping pad 21 is wrapped on the cushion block 20 and the lower connecting block 16.
The working principle is as follows: the utility model discloses in provide the unmanned aerial vehicle with collapsible unmanned aerial vehicle bearing, this embodiment provides another kind of supporting component structure, wherein go up connecting block 15 and connect through damping spring 19 between the connecting block 16 down, unmanned aerial vehicle body 1 lands and makes, and damping spring 19 can play the cushioning effect, effectively protects unmanned aerial vehicle body 1.
In the description of the present invention, unless expressly stated or limited otherwise, the terms "mounted," "connected," and "fixed" are to be construed broadly, e.g., as meaning either a fixed connection, a removable connection, or an integral part; can be mechanically or electrically connected; either directly or indirectly through intervening media, either internally or in any other relationship. The specific meaning of the above terms in the present invention can be understood in specific cases to those skilled in the art.
The utility model discloses the standard part that uses all can purchase from the market, and dysmorphism piece all can be customized according to the description with the record of drawing of description, and the concrete connected mode of each part all adopts conventional means such as ripe bolt, rivet, welding among the prior art, and machinery, part and equipment all adopt among the prior art, and conventional model, including the conventional connected mode among the circuit connection adoption prior art, and the details are not repeated here, and the content that does not make detailed description in this description belongs to the prior art that skilled person in the art knows.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (7)
1. Unmanned aerial vehicle with collapsible unmanned aerial vehicle supporting piece, including unmanned aerial vehicle body (1), its characterized in that: folding supporting mechanisms are symmetrically arranged on the unmanned aerial vehicle body (1), and storage mechanisms are arranged on the front side and the rear side of the unmanned aerial vehicle body (1);
the folding support mechanism comprises a mounting seat (2), the mounting seat (2) is connected with the unmanned aerial vehicle body (1), a driving motor (3) and a fixing frame are arranged on the mounting seat (2), a rotating shaft (4) is arranged in the fixing frame, a driving wheel (5) is arranged at the output end of the driving motor (3), a driven wheel (6) is arranged on the rotating shaft (4), the driving wheel (5) is meshed with the driven wheel (6), adjusting support rods (7) are arranged at two ends of the rotating shaft (4), and a support assembly is arranged on each adjusting support rod (7);
storage mechanism includes overhead gage (8), the one end of overhead gage (8) with unmanned aerial vehicle body (1) links to each other, the other end of overhead gage (8) is provided with side shield (9), the left and right sides of side shield (9) is provided with sideboard (10).
2. A drone provided with a foldable drone support according to claim 1, characterised in that: the adjusting support rod (7) is of an arc structure taking the rotating shaft (4) as a rotating shaft.
3. A drone provided with a foldable drone support according to claim 1, characterised in that: the mount includes fixed frame (11), fixed frame (11) with mount pad (2) link to each other, the inside symmetry of fixed frame (11) is provided with connecting plate (12), be provided with the bearing frame on connecting plate (12), the bearing frame with pivot (4) looks adaptation.
4. A drone provided with a foldable drone support according to claim 1, characterised in that: side shield (9) with the interval of unmanned aerial vehicle body (1) is greater than supporting component's lower terminal surface diameter, be provided with the rubber pad on receiving mechanism's the inside wall.
5. A drone provided with a foldable drone support according to claim 1, characterised in that: the supporting assembly comprises supporting legs (13), one ends of the supporting legs (13) are connected with the adjusting supporting rods (7), the distance between the upper end faces of the supporting legs (13) is smaller than that between the lower end faces of the supporting legs, and supporting blocks (14) are arranged at the other ends of the supporting legs (13).
6. A drone provided with a foldable drone support according to claim 5, characterised in that: the diameter of supporting shoe (14) is greater than the diameter of supporting leg (13), and both sides around the interval of supporting leg (13) is greater than the fuselage thickness of unmanned aerial vehicle body (1), the length of pivot (4) is greater than the fuselage thickness of unmanned aerial vehicle body (1).
7. A drone provided with a foldable drone support according to claim 1, characterised in that: the supporting component comprises an upper connecting block (15) and a lower connecting block (16), the upper connecting block (15) is connected with the adjusting supporting rod (7), a slot (17) is formed in the upper connecting block (15), an inserting rod (18) is arranged on the lower connecting block (16), the inserting rod (18) is inserted into the slot (17), a damping spring (19) is arranged between the upper connecting block (15) and the lower connecting block (16), a cushion block (20) is arranged on the lower surface of the lower connecting block (16), and a damping pad (21) is wrapped on the lower connecting block (16) and is arranged on the cushion block (20).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020971179.6U CN212921975U (en) | 2020-06-01 | 2020-06-01 | Unmanned aerial vehicle with collapsible unmanned aerial vehicle supporting piece |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020971179.6U CN212921975U (en) | 2020-06-01 | 2020-06-01 | Unmanned aerial vehicle with collapsible unmanned aerial vehicle supporting piece |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN212921975U true CN212921975U (en) | 2021-04-09 |
Family
ID=75319035
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202020971179.6U Expired - Fee Related CN212921975U (en) | 2020-06-01 | 2020-06-01 | Unmanned aerial vehicle with collapsible unmanned aerial vehicle supporting piece |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN212921975U (en) |
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2020
- 2020-06-01 CN CN202020971179.6U patent/CN212921975U/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20210409 |