CN216468519U - Load device for large-load unmanned aerial vehicle - Google Patents
Load device for large-load unmanned aerial vehicle Download PDFInfo
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- CN216468519U CN216468519U CN202123398935.4U CN202123398935U CN216468519U CN 216468519 U CN216468519 U CN 216468519U CN 202123398935 U CN202123398935 U CN 202123398935U CN 216468519 U CN216468519 U CN 216468519U
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Abstract
The utility model discloses a big load is load device for unmanned aerial vehicle, including unmanned aerial vehicle body and heavy burden case, heavy burden case sets up in the bottom of unmanned aerial vehicle body, the bottom fixedly connected with fixed block of unmanned aerial vehicle body, the equal fixedly connected with reference column in front side and the rear side of heavy burden roof portion both sides, the constant head tank that uses with the reference column cooperation is seted up to the bottom of fixed block, the left side the movable groove has been seted up on the right side of constant head tank, the inner chamber in movable groove is provided with fixed establishment. Through setting up fixed establishment, fixed slot and stop gear cooperation use, the pulling pull rod, the pull rod drives the fixed column through the connecting rod and when the surperficial slip of locating lever and extrusion spring, takes out from the inner chamber of constant head tank, has solved current load unmanned aerial vehicle and has not been convenient for install the case that bears a burden, when installing the case that bears a burden, fixes through the screw mostly, produces smooth silk easily, influences the problem of the fixed effect of heavy case.
Description
Technical Field
The utility model belongs to the technical field of unmanned aerial vehicle, especially, relate to a loading device for big load unmanned aerial vehicle.
Background
Unmanned aerial vehicle is the unmanned vehicles who utilizes radio remote control equipment and self-contained program control device to control, to sum up, the problem that prior art exists is: the heavy burden case is inconvenient to install, and when installing the heavy burden case, fix through the screw mostly, produce smooth silk easily, influence the fixed effect of heavy burden case.
SUMMERY OF THE UTILITY MODEL
Problem to prior art exists, the utility model provides a big load is load device for unmanned aerial vehicle possesses the advantage of being convenient for install the case that bears a burden, has solved current load unmanned aerial vehicle and has not been convenient for install the case that bears a burden, when installing the case that bears a burden, fixes through the screw mostly, produces smooth silk easily, influences the problem of the fixed effect of case that bears a burden.
The utility model discloses a realize like this, a heavy load is load device for unmanned aerial vehicle, including unmanned aerial vehicle body and heavy burden case, heavy burden case sets up in the bottom of unmanned aerial vehicle body, the bottom fixedly connected with fixed block of unmanned aerial vehicle body, the equal fixedly connected with reference column in front side and the rear side of heavy burden roof portion both sides, the constant head tank that uses with the reference column cooperation is seted up to the bottom of fixed block, the left side the activity groove has been seted up on the right side of constant head tank, the inner chamber in activity groove is provided with fixed establishment, the fixed slot that uses with the fixed establishment cooperation is seted up to one side that the reference column is close to the activity groove, one side that the activity inslot inner chamber kept away from the constant head tank is provided with the stop gear who uses with the fixed establishment cooperation.
As the utility model discloses it is preferred, fixed establishment includes the fixed column, the fixed column runs through the fixed block and extends to the inner chamber of fixed slot near one side of constant head tank, the fixed column is kept away from one side of fixed slot and is seted up the spacing groove that uses with the stop gear cooperation, the fixed column is kept away from the top of fixed slot one side and the equal fixedly connected with connecting rod in bottom, one side that the fixed column was kept away from to the connecting rod runs through the fixed block and extends to the outside and the fixedly connected with pull rod of fixed block.
As the utility model discloses preferred, stop gear includes the locating lever, one side that the locating lever is close to the constant head tank runs through the fixed column and extends to the inner chamber and the fixedly connected with limiting plate of spacing groove, one side fixedly connected with spring of locating lever is kept away from to the limiting plate.
As the utility model discloses it is preferred, the reference column is close to one side of constant head tank inner wall and the inner wall contact of constant head tank, the activity groove is close to one side of constant head tank and has seted up the first through-hole that uses with the fixed column cooperation.
As the utility model discloses it is preferred, the fixed column is close to one side of fixed slot inner wall and the inner wall contact of fixed slot, the activity groove is kept away from the top and the bottom of constant head tank one side and is all seted up the second through-hole that uses with the connecting rod cooperation, the spacing groove is kept away from one side of constant head tank and is seted up the third through-hole that uses with the locating lever cooperation.
As the utility model discloses it is preferred, the limiting plate was kept away from to the locating lever one side and the inner wall fixed connection in activity groove, the limiting plate is close to one side of activity inslot wall and the inner wall contact in activity groove, the spring is kept away from the one side of limiting plate and the inner wall fixed connection in spacing groove.
Compared with the prior art, the beneficial effects of the utility model are as follows:
1. the utility model discloses a set up fixed establishment, fixed slot and stop gear cooperation and use, the pulling pull rod, the pull rod passes through the connecting rod and drives the fixed column in the surface slip of locating lever and when extruding the spring, takes out from the inner chamber of constant head tank, has solved that current load unmanned aerial vehicle is not convenient for install the case that bears a burden, when installing the case that bears a burden, fixes through the screw mostly, produces smooth silk easily, influences the problem of the fixed effect of the case that bears a burden.
2. The utility model discloses a set up fixed establishment, can play the fixed action to the reference column, the person of facilitating the use fixes the case that bears a burden.
3. The utility model discloses a set up stop gear, can play limiting displacement to fixed establishment, the person of facilitating the use uses fixed establishment.
4. The utility model discloses a set up reference column and constant head tank, can play the positioning action to the fixed block, through setting up first through-hole, can play limiting displacement to the fixed column.
5. The utility model discloses a set up fixed column and fixed slot, can play the fixed action to the reference column, through setting up the connecting rod, can drive the fixed column and take out from the inner chamber of constant head tank.
6. The utility model discloses a set up the locating lever, can play the positioning action to the limiting plate, through setting up the limiting plate, can play limiting displacement to the fixed column, through setting up the spring, can play the reset action to the fixed column.
Drawings
Fig. 1 is a schematic structural diagram provided in an embodiment of the present invention;
fig. 2 is a partial cross-sectional view of an embodiment of the invention providing a front view;
fig. 3 is a partial enlarged view of a portion a in fig. 2 according to an embodiment of the present invention.
In the figure: 1. an unmanned aerial vehicle body; 2. a load box; 3. a fixed block; 4. a positioning column; 5. positioning a groove; 6. a movable groove; 7. a fixing mechanism; 8. fixing grooves; 9. a limiting mechanism; 10. a first through hole; 11. a second through hole; 12. a third through hole; 701. fixing a column; 702. a limiting groove; 703. a connecting rod; 704. a pull rod; 901. positioning a rod; 902. a limiting plate; 903. a spring.
Detailed Description
In order to further understand the contents, features and effects of the present invention, the following embodiments are illustrated and described in detail with reference to the accompanying drawings.
The structure of the present invention will be described in detail with reference to the accompanying drawings.
As shown in fig. 1 to 3, the embodiment of the utility model provides a pair of heavy load is load device for unmanned aerial vehicle, including unmanned aerial vehicle body 1 and heavy burden case 2, heavy burden case 2 sets up in unmanned aerial vehicle body 1's bottom, unmanned aerial vehicle body 1's bottom fixedly connected with fixed block 3, the equal fixedly connected with reference column 4 in front side and the rear side of 2 top both sides of heavy burden case, constant head tank 5 with 4 cooperations of reference column uses is seted up to the bottom of fixed block 3, movable groove 6 has been seted up on the right side of left side constant head tank 5, the inner chamber of movable groove 6 is provided with fixed establishment 7, fixed slot 8 that uses with the 7 cooperations of fixed establishment is seted up to reference column 4 one side that is close to movable groove 6, one side that constant head tank 5 was kept away from to movable groove 6 inner chamber is provided with stop gear 9 that uses with the 7 cooperations of fixed establishment.
Referring to fig. 2 and 3, the fixing mechanism 7 includes a fixing column 701, one side of the fixing column 701 close to the positioning groove 5 runs through the fixing block 3 and extends to the inner cavity of the fixing groove 8, one side of the fixing column 701 far away from the fixing groove 8 is provided with a limiting groove 702 used in cooperation with the limiting mechanism 9, the fixing column 701 is far away from one side of the fixing groove 8, the top and the bottom of the fixing column 701 are both fixedly connected with a connecting rod 703, one side of the connecting rod 703 far away from the fixing column 701 runs through the fixing block 3 and extends to the outer side of the fixing block 3, and the connecting rod 704 is fixedly connected with the connecting rod.
Adopt above-mentioned scheme: through setting up fixed establishment 7, can play the fixed action to reference column 4, the person of facilitating the use is fixed case 2 that bears a burden.
Referring to fig. 2 and 3, the limiting mechanism 9 includes a positioning rod 901, one side of the positioning rod 901 close to the positioning slot 5 penetrates through the fixing column 701 and extends to the inner cavity of the limiting slot 702, and a limiting plate 902 is fixedly connected to the inner cavity of the limiting slot 702, and one side of the limiting plate 902 far away from the positioning rod 901 is fixedly connected with a spring 903.
Adopt above-mentioned scheme: through setting up stop gear 9, can play limiting displacement to fixed establishment 7, the person of facilitating the use uses fixed establishment 7.
Referring to fig. 2 and 3, one side of the positioning column 4 close to the inner wall of the positioning slot 5 contacts with the inner wall of the positioning slot 5, and one side of the movable slot 6 close to the positioning slot 5 is provided with a first through hole 10 used in cooperation with the fixing column 701.
Adopt above-mentioned scheme: through setting up reference column 4 and constant head tank 5, can play the positioning action to fixed block 3, through setting up first through-hole 10, can play limiting displacement to fixed column 701.
Referring to fig. 2 and 3, one side of the fixing column 701 close to the inner wall of the fixing groove 8 contacts with the inner wall of the fixing groove 8, the top and the bottom of one side of the movable groove 6 far from the positioning groove 5 are both provided with a second through hole 11 matched with the connecting rod 703 for use, and one side of the limiting groove 702 far from the positioning groove 5 is provided with a third through hole 12 matched with the positioning rod 901 for use.
Adopt above-mentioned scheme: through setting up fixed column 701 and fixed slot 8, can play the fixed action to reference column 4, through setting up connecting rod 703, can drive fixed column 701 and take out from the inner chamber of constant head tank 5.
Referring to fig. 2 and 3, one side of the positioning rod 901 away from the limiting plate 902 is fixedly connected with the inner wall of the movable groove 6, one side of the limiting plate 902 close to the inner wall of the movable groove 6 is in contact with the inner wall of the movable groove 6, and one side of the spring 903 away from the limiting plate 902 is fixedly connected with the inner wall of the limiting groove 702.
The scheme is adopted: through setting up locating lever 901, can play the positioning action to limiting plate 902, through setting up limiting plate 902, can play limiting displacement to fixed column 701, through setting up spring 903, can play the effect that resets to fixed column 701.
The utility model discloses a theory of operation:
when using, user pulling pull rod 704, pull rod 704 drives fixed column 701 through connecting rod 703 in the surface slip of locating lever 901 and when extrudeing spring 903, take out from the inner chamber of constant head tank 5, the user puts weight case 2 in the bottom of unmanned aerial vehicle body 1, make behind positioning column 4 inserts the inner chamber of constant head tank 5, loosen pull rod 704, the power of release pushes fixed column 701 when locating lever 901 surface reverse slip after the spring 903 extrusion, get into the inner chamber of fixed slot 8, accomplish the installation.
In summary, the following steps: this load device for big load unmanned aerial vehicle, through setting up fixed establishment 7, fixed slot 8 and stop gear 9 cooperation are used, pulling pull rod 704, pull rod 704 drives fixed column 701 through connecting rod 703 and when the surface of locating lever 901 slides and extrudees spring 903, the inner chamber from constant head tank 5 is taken out, it is inconvenient for installing the case that bears a burden to have solved current load unmanned aerial vehicle, when installing the case that bears a burden, mostly fix through the screw, produce smooth silk easily, influence the problem of the fixed effect of case that bears a burden.
It is noted that, herein, relational terms such as first and second, and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus.
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 (6)
1. The utility model provides a load device for big load unmanned aerial vehicle, includes unmanned aerial vehicle body (1) and heavy burden case (2), heavy burden case (2) set up in the bottom of unmanned aerial vehicle body (1), its characterized in that: the utility model discloses an unmanned aerial vehicle body, including unmanned aerial vehicle body (1), the bottom fixedly connected with fixed block (3) of load box (2) top both sides, the equal fixedly connected with reference column (4) in front side and rear side, constant head tank (5) that use with reference column (4) cooperation are seted up to the bottom of fixed block (3), left side activity groove (6) have been seted up on the right side of constant head tank (5), the inner chamber of activity groove (6) is provided with fixed establishment (7), fixed slot (8) that use with fixed establishment (7) cooperation are seted up to one side that reference column (4) are close to activity groove (6), one side that constant head tank (5) were kept away from to activity groove (6) inner chamber is provided with stop gear (9) that use with fixed establishment (7) cooperation.
2. A load carrying apparatus for a large load carrying unmanned aerial vehicle according to claim 1, characterized in that: fixing mechanism (7) include fixed column (701), one side that fixed column (701) are close to constant head tank (5) runs through fixed block (3) and extends to the inner chamber of fixed slot (8), fixed column (701) are kept away from one side of fixed slot (8) and are offered spacing groove (702) with stop gear (9) cooperation use, the equal fixedly connected with connecting rod (703) in top and the bottom of fixed slot (8) one side are kept away from to fixed column (701), one side that fixed column (701) were kept away from in connecting rod (703) runs through fixed block (3) and extends to the outside and fixedly connected with pull rod (704) of fixed block (3).
3. A load carrying apparatus for a large load carrying unmanned aerial vehicle according to claim 2, characterized in that: the limiting mechanism (9) comprises a positioning rod (901), one side, close to the positioning groove (5), of the positioning rod (901) penetrates through the fixing column (701) and extends to the inner cavity of the limiting groove (702), and a limiting plate (902) is fixedly connected with the limiting plate, and one side, far away from the positioning rod (901), of the limiting plate (902) is fixedly connected with a spring (903).
4. A load carrying apparatus for a large load carrying unmanned aerial vehicle according to claim 2, characterized in that: one side of the positioning column (4) close to the inner wall of the positioning groove (5) is in contact with the inner wall of the positioning groove (5), and one side of the movable groove (6) close to the positioning groove (5) is provided with a first through hole (10) matched with the fixing column (701) for use.
5. A load carrying apparatus for a large load carrying unmanned aerial vehicle according to claim 3, characterized in that: one side, close to the inner wall of the fixed groove (8), of the fixed column (701) is in contact with the inner wall of the fixed groove (8), a second through hole (11) matched with the connecting rod (703) for use is formed in the top and the bottom of one side, away from the positioning groove (5), of the movable groove (6), and a third through hole (12) matched with the positioning rod (901) for use is formed in one side, away from the positioning groove (5), of the limiting groove (702).
6. A load carrying apparatus for a large load carrying unmanned aerial vehicle according to claim 3, characterized in that: one side, away from the limiting plate (902), of the positioning rod (901) is fixedly connected with the inner wall of the movable groove (6), one side, close to the inner wall of the movable groove (6), of the limiting plate (902) is in contact with the inner wall of the movable groove (6), and one side, away from the limiting plate (902), of the spring (903) is fixedly connected with the inner wall of the limiting groove (702).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202123398935.4U CN216468519U (en) | 2021-12-30 | 2021-12-30 | Load device for large-load unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202123398935.4U CN216468519U (en) | 2021-12-30 | 2021-12-30 | Load device for large-load unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN216468519U true CN216468519U (en) | 2022-05-10 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202123398935.4U Active CN216468519U (en) | 2021-12-30 | 2021-12-30 | Load device for large-load unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN216468519U (en) |
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2021
- 2021-12-30 CN CN202123398935.4U patent/CN216468519U/en active Active
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