CN212766766U - Carry mechanism suitable for unmanned aerial vehicle installs multiple load - Google Patents
Carry mechanism suitable for unmanned aerial vehicle installs multiple load Download PDFInfo
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- CN212766766U CN212766766U CN202021227305.3U CN202021227305U CN212766766U CN 212766766 U CN212766766 U CN 212766766U CN 202021227305 U CN202021227305 U CN 202021227305U CN 212766766 U CN212766766 U CN 212766766U
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Abstract
The utility model discloses a carry mechanism suitable for unmanned aerial vehicle installs multiple load, include: fuselage, a plurality of equipment accessory, supporting component and installation component, the supporting component is installed in fuselage top both sides, the installation component matches and installs on the supporting component, just installation component matches the installation with the fuselage, a plurality of groups the assembly part matches and installs on the installation component. The utility model has the advantages of simple whole structure, the degree of matching is high, and the staff of being convenient for operates the use, and the device is applicable to the carry mechanism of multiple load, supports equipment such as installation radar, camera and cloud platform, has reached a tractor serves several purposes's good effect, and many degrees reduce unmanned aerial vehicle use cost, improve unmanned aerial vehicle availability factor.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle equipment field specifically is a carry mechanism suitable for multiple load of unmanned aerial vehicle installation.
Background
The application range of the vertical take-off and landing fixed wing unmanned aerial vehicle comprises: aerial photography surveying and mapping, agricultural plant protection, news reporting, electric power inspection, disaster relief and rescue, traffic command, movie and television shooting and the like. Because of the different application ranges, various loads need to be carried to carry out operation, and a carrying mechanism suitable for various loads is needed according to actual operation requirements.
The prior art has the following defects: traditional unmanned aerial vehicle is when assembling different loads, and whole result of use is not good, and the installation that can't be synchronous carries out synchronization to multiple load is handled, has increased unmanned aerial vehicle integral erection's limitation, and the unable effect that reaches a tractor serves several purposes that is good has improved unmanned aerial vehicle's use cost, has reduced the availability factor of unmanned aerial vehicle body.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a carry mechanism suitable for unmanned aerial vehicle installs multiple load to solve traditional unmanned aerial vehicle and when assembling different loads, whole result of use is not good, and unable synchronous carries out synchronous installation to multiple load and handles, has increased unmanned aerial vehicle integral erection's limitation, and the unable effect that reaches a tractor serves several purposes that is good has improved unmanned aerial vehicle's use cost scheduling problem.
In order to achieve the above object, the utility model provides a following technical scheme: a carry mechanism suitable for unmanned aerial vehicle installs multiple load, includes: fuselage, a plurality of equipment accessory, supporting component and installation component, the supporting component is installed in fuselage top both sides, the installation component matches and installs on the supporting component, just installation component matches the installation with the fuselage, a plurality of groups the assembly part matches and installs on the installation component.
Preferably, the supporting component comprises a left stringer, a right stringer, a plurality of groups of supporting pieces, a plurality of groups of first rubber dampers and a plurality of groups of first pan head screws, the left stringer is installed on one side of the top end of the machine body, the right stringer is installed on the other side of the top end of the machine body, the plurality of groups of supporting pieces are uniformly distributed on the inner sides of the left stringer and the right stringer, the plurality of groups of first rubber dampers are installed on the plurality of groups of supporting pieces in a matching mode, the plurality of groups of first pan head screws are installed on the plurality of groups of first rubber dampers in a locking mode, supporting processing on the left side and the right side can be synchronously performed on the device under the matching use of the left stringer and the right stringer, then installation positions can be synchronously provided for assembly pieces, the stability of subsequent integral supporting is guaranteed, the strength of the integral supporting is further strengthened under the matching use of the plurality of groups of, and with the assistance of a plurality of groups of the first rubber shock absorbers, the rigid contact between the upper bottom plate and the supporting piece is avoided, and the overall service life of the device is prolonged.
Preferably, the left stringer and the right stringer are the same in size and are installed in parallel, so that the installation stability is guaranteed, and the overall support strength is high.
Preferably, the mounting assembly comprises an upper base plate, a support plate, a plurality of groups of second pan head screws, a plurality of groups of second rubber shock absorbers, a shock absorption support and a plurality of groups of third pan head screws, the upper base plate is mounted across a left stringer and a right stringer, the plurality of groups of second pan head screws penetrate through the upper base plate and are respectively connected with a plurality of groups of supporting pieces in a locking manner, the support plate is mounted at the top end of the upper base plate, the plurality of groups of second rubber shock absorbers are uniformly distributed between the upper base plate and the support plate, the plurality of groups of third pan head screws penetrate through the support plate and are connected with the upper base plate in a locking manner, the shock absorption support is mounted on the support plate, the plurality of groups of assembly parts are mounted on the shock absorption support in a matching manner, the upper base plate is firstly mounted on the left stringer and the right stringer, then the upper base plate is connected with the supporting pieces in a locking manner by the second pan head screws, install No. two rubber shock absorbers of a plurality of groups simultaneously through between upper plate, the mounting panel, further strengthened whole shock attenuation effect, can be synchronous protect the assembly part, install the assembly part afterwards and use on shock absorber support, guaranteed the whole result of use of assembly part.
Preferably, the installation is matchd to upper plate, mounting panel, just the size of upper plate is greater than the mounting panel size, has improved device stability in use.
Preferably, the assembling parts in several groups are respectively a tripod head, a camera and a radar device.
The utility model provides a carry mechanism suitable for unmanned aerial vehicle installs multiple load possesses following beneficial effect:
(1) the utility model discloses a be equipped with supporting component, utilize left stringer, under the cooperation of right stringer is used, can be synchronous carry out the support of the left and right sides to the device and handle, and then can be synchronous provide the mounted position to the assembly part, the stability of follow-up whole support has been guaranteed, and under a plurality of groups support piece's cooperation is used, the intensity of whole support has further been strengthened, whole result of use has been improved, and under a plurality of groups rubber shock absorber's assistance, upper plate and support piece's rigid contact has been avoided, the whole life of device has been improved.
(2) The utility model discloses a be equipped with the installation component, install the upper plate at first on left stringer, right stringer, later utilize No. two pan head screws to be connected upper plate and support piece closure, utilize No. two pan head screws to install the mounting panel closure on the upper plate afterwards, simultaneously through the upper plate, install No. two rubber shock absorbers of a plurality of groups between the mounting panel, whole shock attenuation effect has further been strengthened, can be synchronous protect the assembly part, install the assembly part on shock absorber support and use afterwards, the whole result of use of assembly part has been guaranteed.
Drawings
Fig. 1 is a schematic overall structure diagram of the present invention;
FIG. 2 is a schematic structural view of the support assembly of the present invention;
FIG. 3 is a schematic side view of the body of the present invention;
FIG. 4 is a schematic view of the connection between the upper plate and the supporting plate of the present invention;
FIG. 5 is a schematic structural view of the mounting assembly of the present invention;
fig. 6 is an overall side view of the mounting assembly of the present invention.
In the figure: 1. a body; 2. an assembly member; 3. a left stringer; 4. a right stringer; 5. a support member; 6. a first rubber damper; 7. a pan head screw; 8. an upper base plate; 9. a mounting plate; 10. a second pan head screw; 11. a second rubber damper; 12. a shock-absorbing support; 13. no. three pan head screws.
Detailed Description
The technical solution in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention.
As shown in fig. 1-6, the utility model provides a technical solution: a carry mechanism suitable for unmanned aerial vehicle installs multiple load, includes: fuselage 1, a plurality of equipment accessory 2, supporting component and installation component, the supporting component is installed in 1 top both sides of fuselage, the installation component matches and installs on the supporting component, just installation component matches the installation with fuselage 1, a plurality of groups assembly part 2 matches and installs on the installation component.
Further, the supporting component comprises a left stringer 3, a right stringer 4, a plurality of groups of supporting pieces 5, a plurality of groups of first rubber dampers 6 and a plurality of groups of first pan head screws 7, the left stringer 3 is installed on one side of the top end of the machine body 1, the right stringer 4 is installed on the other side of the top end of the machine body 1, the plurality of groups of supporting pieces 5 are evenly distributed on the inner sides of the left stringer 3 and the right stringer 4, the plurality of groups of first rubber dampers 6 are installed on the plurality of groups of supporting pieces 5 in a matching mode, the plurality of groups of first pan head screws 7 are installed on the plurality of groups of first rubber dampers 6 in a locking mode, supporting treatment can be synchronously carried out on the left side and the right side of the device under the matching use of the left stringer 3 and the right stringer 4, further, installation positions can be synchronously provided for the assembly part 2, the stability of subsequent integral supporting is ensured, and, the strength of the integral support is further enhanced, the integral use effect is improved, rigid contact between the upper bottom plate 8 and the support piece 5 is avoided under the assistance of a plurality of groups of the first rubber shock absorbers 6, and the integral service life of the device is prolonged;
furthermore, the left stringer 3 and the right stringer 4 are the same in size, and the left stringer 3 and the right stringer 4 are installed in parallel, so that the installation stability is ensured, and the overall support strength is high;
further, the mounting assembly comprises an upper base plate 8, a support plate 9, a plurality of groups of second pan head screws 10, a plurality of groups of second rubber shock absorbers 11, a shock absorption support 12 and a plurality of groups of third pan head screws 13, the upper base plate 8 is mounted across a left stringer 3 and a right stringer 4, the plurality of groups of second pan head screws 10 penetrate through the upper base plate 8 and are respectively connected with the plurality of groups of support members 5 in a locking manner, the support plate 9 is mounted at the top end of the upper base plate 8, the plurality of groups of second rubber shock absorbers 11 are uniformly distributed between the upper base plate 8 and the support plate 9, the plurality of groups of third pan head screws 13 penetrate through the support plate 9 and are connected with the upper base plate 8 in a locking manner, the shock absorption support 12 is mounted on the support plate 9, the plurality of groups of assembly parts 2 are mounted on the shock absorption support 12 in a matching manner, the upper base plate 8 is firstly mounted on the left stringer 3 and the right stringer 4, and then the upper base plate 8 is, then, a second pan head screw 10 is used for installing the support plate 9 on the upper bottom plate 8 in a locking mode, meanwhile, a plurality of groups of second rubber shock absorbers 11 are installed between the upper bottom plate 8 and the support plate 9, the overall shock absorption effect is further enhanced, the assembly part 2 can be protected synchronously, and then the assembly part 2 is installed on a shock absorption support 12 for use, so that the overall use effect of the assembly part 2 is guaranteed;
furthermore, the upper bottom plate 8 and the support plate 9 are installed in a matching mode, and the size of the upper bottom plate 8 is larger than that of the support plate 9, so that the use stability of the device is improved;
further, the assembling parts 2 are a holder, a camera and a radar device respectively.
The working principle is as follows: when the device is used, the supporting components are arranged, the left stringer 3 and the right stringer 4 are matched for use, the supporting processing of the left side and the right side of the device can be synchronously carried out, the assembly parts 2 can be synchronously provided with mounting positions, the stability of subsequent overall supporting is ensured, the strength of overall supporting is further enhanced under the matched use of a plurality of groups of supporting parts 5, the overall using effect is improved, the rigid contact between the upper base plate 8 and the supporting parts 5 is avoided under the assistance of a plurality of groups of first rubber shock absorbers 6, the overall service life of the device is prolonged, meanwhile, the upper base plate 8 is firstly mounted on the left stringer 3 and the right stringer 4, then the upper base plate 8 is connected with the supporting parts 5 in a locking manner through a second pan head screw 10, the support plate 9 is mounted on the upper base plate 8 in a locking manner through a second pan head screw 10, and meanwhile, the upper base plate 8, Install a plurality of groups No. two rubber shock absorbers 11 between the mounting panel 9, further strengthened whole shock attenuation effect, can be synchronous protect assembly part 2, install assembly part 2 and use on shock absorber support 12 afterwards, guaranteed the whole result of use of assembly part 2.
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 carry mechanism suitable for unmanned aerial vehicle installs multiple load which characterized in that includes: fuselage (1), a plurality of equipment accessory (2), supporting component and installation component, the supporting component is installed in fuselage (1) top both sides, the installation component matches and installs on the supporting component, just installation component matches the installation with fuselage (1), a plurality of groups assembly part (2) match and install on the installation component.
2. The mounting mechanism of claim 1, wherein the mounting mechanism is adapted for mounting a plurality of loads on the drone, and comprises: the supporting component comprises a left stringer (3), a right stringer (4), a plurality of groups of supporting pieces (5), a plurality of groups of rubber shock absorbers (6) and a plurality of groups of pan head screws (7), the left stringer (3) is installed on one side of the top end of the machine body (1), the right stringer (4) is installed on the other side of the top end of the machine body (1), and the supporting pieces (5) are evenly distributed on the inner sides of the left stringer (3) and the right stringer (4), the rubber shock absorbers (6) are installed on the supporting pieces (5) in a matching mode, and the pan head screws (7) are installed on the rubber shock absorbers (6) in the groups in a locking mode.
3. The mounting mechanism of claim 2, wherein the mounting mechanism is adapted for mounting a plurality of loads on the drone, and comprises: the left stringer (3) and the right stringer (4) are the same in size, and the left stringer (3) and the right stringer (4) are installed in parallel.
4. The mounting mechanism of claim 1, wherein the mounting mechanism is adapted for mounting a plurality of loads on the drone, and comprises: the mounting component comprises an upper bottom plate (8), a support plate (9), a plurality of groups of second pan head screws (10), a plurality of groups of second rubber shock absorbers (11), a shock absorption support (12) and a plurality of groups of third pan head screws (13), the upper bottom plate (8) is installed across the left stringer (3) and the right stringer (4), and a plurality of groups of second pan head screws (10) pass through the upper bottom plate (8) and are respectively connected with a plurality of groups of supporting pieces (5) in a locking way, the support plate (9) is arranged at the top end of the upper bottom plate (8), a plurality of groups of second rubber shock absorbers (11) are uniformly distributed between the upper bottom plate (8) and the support plate (9), a plurality of groups of third pan head screws (13) penetrate through the bracket plate (9) to be connected with the upper bottom plate (8) in a locking way, the damping bracket (12) is arranged on the bracket plate (9), and a plurality of groups of the assembly parts (2) are matched and installed on the shock absorption bracket (12).
5. The mounting mechanism of claim 4, wherein the mounting mechanism is adapted for mounting a plurality of loads on the unmanned aerial vehicle, and comprises: the upper base plate (8) and the support plate (9) are installed in a matched mode, and the size of the upper base plate (8) is larger than that of the support plate (9).
6. The mounting mechanism of claim 1, wherein the mounting mechanism is adapted for mounting a plurality of loads on the drone, and comprises: the assembling parts (2) are respectively a tripod head, a camera and radar equipment.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021227305.3U CN212766766U (en) | 2020-06-29 | 2020-06-29 | Carry mechanism suitable for unmanned aerial vehicle installs multiple load |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021227305.3U CN212766766U (en) | 2020-06-29 | 2020-06-29 | Carry mechanism suitable for unmanned aerial vehicle installs multiple load |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN212766766U true CN212766766U (en) | 2021-03-23 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202021227305.3U Active CN212766766U (en) | 2020-06-29 | 2020-06-29 | Carry mechanism suitable for unmanned aerial vehicle installs multiple load |
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| Country | Link |
|---|---|
| CN (1) | CN212766766U (en) |
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2020
- 2020-06-29 CN CN202021227305.3U patent/CN212766766U/en active Active
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