CN218489894U - Folded cascade unmanned aerial vehicle rack construction - Google Patents
Folded cascade unmanned aerial vehicle rack construction Download PDFInfo
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- CN218489894U CN218489894U CN202223105842.2U CN202223105842U CN218489894U CN 218489894 U CN218489894 U CN 218489894U CN 202223105842 U CN202223105842 U CN 202223105842U CN 218489894 U CN218489894 U CN 218489894U
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- unmanned aerial
- aerial vehicle
- locking
- bracing piece
- main part
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
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Abstract
The utility model relates to a folded cascade unmanned aerial vehicle rack construction, including the unmanned aerial vehicle main part, instrument group case and folding box, be provided with the instrument group case in the unmanned aerial vehicle main part, be provided with the handle on the instrument group case, the bottom of unmanned aerial vehicle main part is provided with the folding box, first support frame is articulated with the rotor mounting bracket in the outside, the one end that the unmanned aerial vehicle main part was kept away from to the rotor mounting bracket is provided with the rotor, be provided with locking mechanism between first support frame and the rotor mounting bracket, the bottom of folding box is provided with a plurality of bracing piece, the top of bracing piece is articulated with the second support frame of setting in the folding box, be provided with locking mechanism between second support frame and the bracing piece. The utility model discloses a rotor mounting bracket and bracing piece can carry out folding processing, make things convenient for unmanned aerial vehicle to accomodate when not using, save occupation space.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle correlation technique field especially relates to a folded cascade unmanned aerial vehicle rack construction.
Background
Unmanned aerial vehicles are unmanned aerial vehicles that operate using radio remote control devices and self-contained program control devices, and unmanned aerial vehicles are a collective term for unmanned aerial vehicles in practice.
Through magnanimity retrieval, discovery prior art is No. CN211033008U, a rack construction for unmanned aerial vehicle is disclosed, including the rotor mounting bracket, the unmanned aerial vehicle main part, instrument box group, battery box and camera unit, both ends all are provided with the rotor mounting bracket about the unmanned aerial vehicle main part, the one end that the unmanned aerial vehicle main part was kept away from to the rotor mounting bracket is provided with the rotor, instrument box group sets up the top in the unmanned aerial vehicle main part, battery box and camera unit set gradually in the below of unmanned aerial vehicle main part, camera unit passes through the fixed bottom that sets up at the battery box of camera unit base, the bottom of the unmanned aerial vehicle main part at battery box both ends all is provided with the bracing piece, be provided with the strengthening rib between bracing piece and the rotor mounting bracket, the bottom of bracing piece is provided with damping device. The utility model discloses a rotor mounting bracket, unmanned aerial vehicle main part, instrument box group, battery box and camera unit structure set up to and the strengthening rib that sets up between bracing piece and the rotor mounting bracket, the overall structure nature of frame is firm, and the design is simple, and the cost is lower.
To sum up, the rotor mounting bracket and the bracing piece etc. of current unmanned aerial vehicle frame are longer for its occupation space is great, and inconvenient the use of accomodating.
In view of the above-mentioned defects, the present designer is actively making research and innovation to create a foldable unmanned aerial vehicle frame structure, so that the foldable unmanned aerial vehicle frame structure has more industrial utility value.
SUMMERY OF THE UTILITY MODEL
In order to solve the technical problem, the utility model aims at providing a folded cascade unmanned aerial vehicle rack construction.
In order to achieve the above purpose, the utility model adopts the following technical scheme:
the utility model provides a folded cascade unmanned aerial vehicle rack construction, including the unmanned aerial vehicle main part, instrument group case and folding box, be provided with the instrument group case in the unmanned aerial vehicle main part, be provided with the handle in the instrument group case, the bottom of unmanned aerial vehicle main part is provided with the folding box, the left and right sides of unmanned aerial vehicle main part all is provided with first support frame, first support frame is articulated with the rotor mounting bracket in the outside, the one end that the unmanned aerial vehicle main part was kept away from to the rotor mounting bracket is provided with the rotor, be provided with locking mechanism between first support frame and the rotor mounting bracket, the bottom of folding box is provided with a plurality of bracing piece, the top of bracing piece is articulated with the second support frame of setting in the folding box, be provided with locking mechanism between second support frame and the bracing piece.
As a further improvement, the bottom of the supporting rod is provided with a supporting sleeve, the bottom of the supporting rod is embedded into the supporting sleeve and is in contact with the spring column arranged in the supporting sleeve, and the bottom of the supporting sleeve is provided with a supporting leg.
As a further improvement of the utility model, the supporting rod and the supporting sleeve are connected together through the locking piece, and the locking piece is a bolt-nut component.
As a further improvement, the locking mechanism includes a first locking block, a locking rod and a second locking block, the first locking block is disposed on the first support frame or the second support frame, the second locking block is disposed on the rotor wing mounting frame or the support rod, and the locking rod is connected with the second locking block after passing through the first locking block.
As a further improvement of the utility model, a thread groove is arranged in the second locking block, and the locking rod is connected with the thread groove in a threaded manner.
As a further improvement of the utility model, the locking rod between the first locking block and the second locking block is sleeved with a spring.
Borrow by above-mentioned scheme, the utility model discloses at least, have following advantage:
the utility model discloses a rotor mounting bracket and bracing piece can carry out folding processing, make things convenient for unmanned aerial vehicle to accomodate when not using, save occupation space; can realize the expansion of rotor mounting bracket and bracing piece fixedly through the lock solid mechanism, remove the lock solid simultaneously and can realize rotor mounting bracket and bracing piece folding processing, convenient and fast.
The above description is only an overview of the technical solution of the present invention, and in order to make the technical means of the present invention clearer and can be implemented according to the content of the description, the following detailed description is made with reference to the preferred embodiments of the present invention and accompanying drawings.
Drawings
In order to more clearly illustrate the technical solutions of the embodiments of the present invention, the drawings that are required to be used in the embodiments will be briefly described below, it should be understood that the following drawings only illustrate some embodiments of the present invention, and therefore should not be considered as limiting the scope, and for those skilled in the art, other related drawings can be obtained according to the drawings without inventive efforts.
Fig. 1 is a schematic structural view of a foldable unmanned aerial vehicle frame structure of the present invention;
FIG. 2 is a schematic view of the locking mechanism shown in FIG. 1;
fig. 3 is a schematic structural view of a second usage state of the present invention.
Wherein the meanings of each reference numeral in the figures are as follows.
1 unmanned aerial vehicle main part 2 instrument group case
3 handle 4 locking mechanism
5 rotor mounting rack 6 rotors
7 first support 8 folding box
9 second support rack 10 support bar
11 support sleeve 12 support callus on sole
13 spring post 14 locking piece
15 first locking block 16 locking rod
17 second locking block 18 spring
19 thread groove
Detailed Description
The following detailed description of the embodiments of the present invention is made with reference to the accompanying drawings and examples. The following examples are intended to illustrate the invention, but are not intended to limit the scope of the invention.
In order to make the technical solution of the present invention better understood, the technical solution in the embodiments of the present invention will be clearly and completely described below with reference to the 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. The components of embodiments of the present invention, as generally described and illustrated in the figures herein, may be arranged and designed in a wide variety of different configurations. Thus, the following detailed description of the embodiments of the invention, as presented in the figures, is not intended to limit the scope of the invention, as claimed, but is merely representative of selected embodiments of the invention. Based on the embodiment of the present invention, all other embodiments obtained by those skilled in the art without creative efforts belong to the protection scope of the present invention.
Examples
As shown in figures 1 to 3 of the drawings,
the utility model provides a folded cascade unmanned aerial vehicle rack construction, including unmanned aerial vehicle main part 1, instrument cluster case 2 and folding box 8, be provided with instrument cluster case 2 in the unmanned aerial vehicle main part 1, be provided with handle 3 on the instrument cluster case 2, the bottom of unmanned aerial vehicle main part 1 is provided with folding box 8, the left and right sides of unmanned aerial vehicle main part 1 all is provided with first support frame 7, first support frame 7 is articulated with the rotor mounting bracket 5 in the outside, the one end that unmanned aerial vehicle main part 1 was kept away from to rotor mounting bracket 5 is provided with rotor 6, be provided with locking mechanism 4 between first support frame 7 and the rotor mounting bracket 5, folding box 13's bottom is provided with a plurality of bracing piece 10, bracing piece 10's top is articulated with the second support frame 9 that sets up in folding box 8, be provided with locking mechanism 4 between second support frame 9 and the bracing piece 10.
Description of the specific structure of the support pole 10: the bottom of the support rod 10 is provided with a support sleeve 11, the bottom of the support rod 10 is embedded into the support sleeve 11 and is arranged in contact with a spring column 13 arranged in the support sleeve 11, and the bottom of the support sleeve 11 is provided with a support leg 11. The support bar 10 and the support sleeve 11 are connected together through a locking member 14, and the locking member 14 is a bolt-nut assembly. Through the structure setting of bracing piece 10, can effectively reduce the impact force of unmanned aerial vehicle when descending in the high altitude, reduce the destruction to unmanned aerial vehicle internal machine or other equipment.
Description of the structure of the locking mechanism 4: the locking mechanism 4 comprises a first locking block 15, a locking rod 16 and a second locking block 17, the first locking block 15 is arranged on the first support frame 7 or the second support frame 9, the second locking block 17 is arranged on the rotor wing mounting frame 5 or the support rod 10, and the locking rod 16 penetrates through the first locking block 15 and then is connected with the second locking block 17. A thread groove 19 is formed in the second locking block 17, and the locking rod 16 is in threaded connection with the thread groove 19. A spring 18 is sleeved on the locking rod 16 between the first locking block 15 and the second locking block 17.
Fig. 1 is a schematic view of a first state of the present invention, at this time, the rotor mounting rack 5 is in the horizontal expansion state, the supporting rod 10 is in the vertical expansion state, and both are equally divided into two sections to be respectively locked by the locking mechanism 4, so that the state can be maintained.
Fig. 2 is a schematic view of a first state of the present invention, at this time, the rotor mounting bracket 5 is vertically contracted relative to the first support frame 7, the support rod 10 is vertically contracted relative to the second support frame 9 in the folding box 8, both of them are released from the locked state, and the locking rod 16 on the locking mechanism 4 is removed.
In the description of the present invention, it is to be understood that the terms "center", "longitudinal", "lateral", "up", "down", "front", "back", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", and the like, indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are used only for convenience of description and simplicity of description, and do not indicate or imply that the device or element being referred to must have a particular orientation, be constructed and operated in a particular orientation, and therefore, should not be construed as limiting the present invention. Furthermore, the terms "first", "second", etc. are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or implicitly referring to the number of technical features being indicated. Thus, a feature defined as "first," "second," etc. may explicitly or implicitly include one or more of that feature. In the description of the present invention, "a plurality" means two or more unless otherwise specified.
In the description of the present invention, it is to be noted that, unless otherwise explicitly specified or limited, the terms "mounted", "connected" and "connected" are to be interpreted broadly, and may be, for example, fixedly connected, detachably connected, or integrally connected: either mechanically or electrically: the terms may be directly connected or indirectly connected through an intermediate member, or may be a communication between two elements.
The above description is only a preferred embodiment of the present invention, and should not be used to limit the present invention, it should be noted that, for those skilled in the art, without departing from the technical principle of the present invention, a plurality of improvements and modifications can be made, and these improvements and modifications should also be regarded as the protection scope of the present invention.
Claims (6)
1. The utility model provides a folded cascade unmanned aerial vehicle rack construction, includes unmanned aerial vehicle main part (1), instrument group case (2) and folding box (8), be provided with instrument group case (2) in unmanned aerial vehicle main part (1), be provided with handle (3) on instrument group case (2), the bottom of unmanned aerial vehicle main part (1) is provided with folding box (8), its characterized in that, the left and right sides of unmanned aerial vehicle main part (1) all is provided with first support frame (7), first support frame (7) are articulated with rotor mounting bracket (5) in the outside, the one end that unmanned aerial vehicle main part (1) was kept away from in rotor mounting bracket (5) is provided with rotor (6), be provided with lock solid mechanism (4) between first support frame (7) and rotor mounting bracket (5), the bottom of folding box (8) is provided with a plurality of bracing piece (10), the top of bracing piece (10) is articulated with second support frame (9) that sets up in folding box (8), be provided with lock solid mechanism (4) between second support frame (9) and bracing piece (10).
2. Foldable unmanned aerial vehicle frame structure of claim 1, characterized in that the bottom of bracing piece (10) is provided with support sleeve (11), the bottom of bracing piece (10) is embedded into support sleeve (11) and is set up with spring post (13) contact that sets up in support sleeve (11), the bottom of support sleeve (11) is provided with support callus on the sole (12).
3. Foldable unmanned aerial vehicle frame structure of claim 1, characterized in that, the bracing piece (10) and support sleeve (11) are connected together through retaining member (14), the retaining member (14) is a bolt-nut assembly.
4. Foldable unmanned aerial vehicle frame structure of claim 1, characterized in that locking mechanism (4) includes first locking piece (15), locking pole (16) and second locking piece (17), first locking piece (15) set up on first support frame (7) or second support frame (9), second locking piece (17) set up on rotor mounting bracket (5) or bracing piece (10), be connected with second locking piece (17) after locking pole (16) passes first locking piece (15).
5. Foldable unmanned aerial vehicle frame structure of claim 4, characterized in that threaded groove (19) is provided in said second locking piece (17), said locking bar (16) being in threaded connection with threaded groove (19).
6. Foldable unmanned aerial vehicle frame structure of claim 4, characterized in that the locking bar (16) between the first locking block (15) and the second locking block (17) is sleeved with a spring (18).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202223105842.2U CN218489894U (en) | 2022-11-23 | 2022-11-23 | Folded cascade unmanned aerial vehicle rack construction |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202223105842.2U CN218489894U (en) | 2022-11-23 | 2022-11-23 | Folded cascade unmanned aerial vehicle rack construction |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN218489894U true CN218489894U (en) | 2023-02-17 |
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ID=85197850
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202223105842.2U Active CN218489894U (en) | 2022-11-23 | 2022-11-23 | Folded cascade unmanned aerial vehicle rack construction |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN218489894U (en) |
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2022
- 2022-11-23 CN CN202223105842.2U patent/CN218489894U/en active Active
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