CN219008639U - Unmanned aerial vehicle storage rack - Google Patents
Unmanned aerial vehicle storage rack Download PDFInfo
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- CN219008639U CN219008639U CN202223439052.8U CN202223439052U CN219008639U CN 219008639 U CN219008639 U CN 219008639U CN 202223439052 U CN202223439052 U CN 202223439052U CN 219008639 U CN219008639 U CN 219008639U
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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
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Abstract
The utility model relates to the technical field of unmanned aerial vehicle equipment storage, and particularly discloses an unmanned aerial vehicle storage rack which is used for storing a fuselage or a wing and comprises a movable bracket support, a vertical support which is arranged on the bracket support and is arranged along the Y-axis direction, and at least two groups of storage components which are arranged on the vertical support in parallel and on the same horizontal plane; each group of storage components comprises a plurality of groups of storage lugs which are arranged in parallel along the Y-axis direction and connecting sheets for connecting the storage lugs with the vertical support. The utility model is suitable for storing wings or fuselages with different height and sizes and different forms, can realize one frame for multiple purposes, and has strong universality and wide application range.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicle storage, in particular to an unmanned aerial vehicle storage rack.
Background
The storage bracket belongs to top support equipment and is mainly used for storing wings or fuselages of the unmanned aerial vehicle; when the wing storage rack is used as a wing storage rack, the wing storage rack has the main functions of storing and transporting the unmanned aerial vehicle wings, and the unmanned aerial vehicle needs to store the wings on site for a long time and conveniently and rapidly move in the general assembly and transportation process.
When it is as fuselage storage rack, its main role is to support unmanned aerial vehicle fuselage, unmanned aerial vehicle at installation and maintenance debugging in-process, need carry out long-time support and convenient and fast's removal to the fuselage.
The existing unmanned aerial vehicle storage rack adopts an integral structure, cannot be suitable for unmanned aerial vehicles of various types, cannot be disassembled, and has poor adjustability and maintainability; the storage rack of each model is customized, and the application range is small.
Disclosure of Invention
The utility model aims to solve the technical problem of providing the unmanned aerial vehicle storage rack, which can adjust the relative position relation according to different machine types, realize the storage of wings of different machine types, and has simple structure and strong practicability.
The utility model solves the technical problems by adopting the following solution:
an unmanned aerial vehicle storage rack is used for storing a fuselage or a wing and comprises a movable bracket support, a vertical support which is arranged on the bracket support and is arranged along the Y-axis direction, and at least two groups of storage components which are arranged on the vertical support in parallel and are on the same horizontal plane;
each group of storage components comprises a plurality of groups of storage lugs which are arranged in parallel along the Y-axis direction and connecting sheets for connecting the storage lugs with the vertical support.
When the device is used, firstly, according to the height dimension of the stored wings or the airframe along the Y-axis direction, the positions of two groups of vertically adjacent storage brackets along the Y-axis direction are adjusted, so that the device can effectively support the airframe or the wings according to the heights of the airframes or the wings, realize the storage of the airframes or the wings of unmanned aerial vehicles of different models, then place the airframes or the wings on a storage assembly, transport the airframes or the wings to a designated position through a movable bracket, and then perform subsequent operation;
in some possible embodiments, in order to ensure that the wing or the fuselage can be effectively stored, damage to the fuselage or the wing when present and slipping after storage are avoided;
the storage support comprises a support body connected with the vertical support, rubber pads which are adhered to the support body and are arranged vertically symmetrically, and binding belts which are arranged on the support body.
In some possible embodiments, storage of the fuselage is to be effected efficiently;
the support body is of a tubular structure, and the long direction is arranged along the Z-axis direction; the connecting sheet is positioned between the two groups of rubber mats and is connected with the vertical support.
In some possible embodiments, in order to avoid slipping of the fuselage;
the top of the rubber pad is provided with a U-shaped open slot.
In some possible embodiments, in order to effectively store the wing, and avoid the wing from slipping off;
the support body is two groups and is symmetrically arranged along the Y axis, the two groups of support bodies are connected through connecting sheets to form a Y-shaped structure, and an included angle formed by the support body and the vertical support is A, and 45 degrees is less than or equal to 90 degrees.
In some possible embodiments, to effectively achieve adjustment of the position between vertically adjacent supporting bodies;
the two groups of support bodies are symmetrically arranged along the Y axis and are connected through the two groups of connecting lugs;
the connecting piece is of a Y-shaped structure and comprises connecting lug seats respectively connected with the two groups of support bodies and connecting pieces arranged along the Y-axis direction and positioned between the two groups of connecting lug seats;
two groups of support bodies are close to one end of each other, and two groups of connecting pieces are close to one side of each other to form a slot.
In some possible embodiments, to effectively enable the installation of the storage assembly;
the vertical support comprises a plurality of groups of Y-direction rods which are arranged along the Y-axis direction and are arranged in parallel along the X-axis direction, and X-direction rods which are used for connecting the Y-direction rods and are arranged along the X-axis direction.
In some possible embodiments, to effect transport;
the bracket support comprises a bracket platform, universal casters arranged at the bottom of the bracket platform, and lifting supporting feet which are arranged in one-to-one correspondence with the universal casters and are arranged on the bracket platform.
In some possible embodiments, to effectively achieve storage stability of the device;
the lifting supporting leg comprises a screw rod in threaded connection with the bracket platform, a supporting seat connected with the bottom of the screw rod and a rotary table connected with the top of the screw rod.
Compared with the prior art, the utility model has the beneficial effects that:
the utility model can effectively adjust the height of the fuselage or the wing in the vertical direction, so that the storage requirements of the fuselage or the wing in unmanned aerial vehicles of different models can be met, and the utility model has simple structure and strong practicability;
the utility model effectively avoids the problem that the airframe or the wing is damaged when being stored by limiting the storage bracket, and simultaneously can effectively avoid the problem that the airframe or the wing is damaged due to sliding in the transportation process;
according to the utility model, the lifting supporting legs are matched with the universal casters, so that the support and fixation are more stable;
the utility model has simple structure and strong practicability.
Drawings
FIG. 1 is a schematic structural diagram of embodiment 1 of the present utility model;
FIG. 2 is a side view of FIG. 1;
FIG. 3 is a schematic structural diagram of embodiment 2 of the present utility model;
FIG. 4 is a side view of FIG. 3;
wherein: 1. a bracket support; 2. a vertical bracket; 3. a storage assembly; 31. a storage bracket; 311. a support body; 312. rubber cushion; 3121. u-shaped open slot; 4. lifting the supporting feet.
Detailed Description
In the present utility model, unless explicitly specified and limited otherwise, the terms "mounted," "connected," "secured," and the like are to be construed broadly, and may be, for example, fixedly connected, detachably connected, or integrally formed; can be directly connected or indirectly connected through an intermediate medium, and can be communicated with the inside of two elements or the interaction relationship of the two elements. Reference to "first," "second," and similar terms in this application does not denote any order, quantity, or importance, but rather are used to distinguish one element from another. Likewise, the terms "a" or "an" and the like do not denote a limitation of quantity, but rather denote the presence of at least one. In the implementation of the present application, "and/or" describes an association relationship of an association object, which means that there may be three relationships, for example, a and/or B may mean: a exists alone, A and B exist together, and B exists alone. In the description of the embodiments of the present application, unless otherwise indicated, the meaning of "a plurality" means two or more. For example, a plurality of positioning posts refers to two or more positioning posts. The specific meaning of the above terms in the present utility model can be understood by those of ordinary skill in the art according to the specific circumstances.
The present utility model will be described in detail below.
Example 1:
an unmanned aerial vehicle storage rack is used for storing a fuselage and comprises a movable bracket support 1, a vertical support 2 which is arranged on the bracket support 1 along the Y-axis direction and at least two groups of storage components 3 which are arranged on the vertical support 2 in parallel and on the same horizontal plane;
each group of the storage assemblies 3 comprises a plurality of groups of storage lugs 31 which are arranged in parallel along the Y-axis direction, and connecting pieces 32 for connecting the storage lugs 31 and the vertical supports 2.
When the robot is used, firstly, the height dimension of the robot body along the Y-axis direction is stored according to the requirement, and the positions of two groups of vertically adjacent storage brackets 31 along the Y-axis direction are adjusted, so that the robot body can be effectively supported and stored according to the height of the robot body, the robot bodies of different models can be stored, then the robot body is placed on the storage assembly 3, and the robot body is transported to a designated position through the movable bracket support 1, so that the subsequent operation can be performed;
in some possible embodiments, in order to ensure an effective storage of the fuselage, damage to the fuselage when present and slipping after storage are avoided;
the storage support 31 comprises a support body 311 connected with the vertical support, a rubber pad 312 adhered to the support body and arranged vertically symmetrically, and a binding belt arranged on the support body 311.
Two groups of rubber pads 312 are arranged on the support body, the machine body is placed on the rubber pads 312, and is fixed with the support body through a binding belt to form a whole, so that the machine body is prevented from moving in the transportation process;
the arrangement of the rubber pad 312 can also effectively avoid the hard contact between the machine body and the support body, and avoid damage;
in some possible embodiments, storage of the fuselage is to be effected efficiently;
the support body is of a tubular structure, and the long direction is arranged along the Z-axis direction; the connecting piece 32 is located between the two groups of rubber pads 312 and is connected with the vertical support 2.
The two groups of rubber pads 312 are positioned at two sides of the vertical bracket and are symmetrically arranged, and the bracket body divides the vertical bracket into two parts with the same size for supporting and storing the two groups of machine bodies;
in some possible embodiments, in order to avoid slipping of the fuselage;
the top of the rubber pad 312 is provided with a U-shaped opening slot 3121. The machine body is placed at the bottom of the U-shaped open slot when being stored, and the two side surfaces are limited to move, so that the machine body is prevented from sliding off.
Preferably, the rubber pad 312 is a rubber pad 312 or a silica gel pad 312.
In some possible embodiments, the mounting of the storage assembly 3 is to be effected;
the vertical support 2 comprises a plurality of groups of Y-direction rods which are arranged along the Y-axis direction and are arranged in parallel along the X-axis direction, and X-direction rods which are used for connecting the Y-direction rods and are arranged along the X-axis direction.
As shown in fig. 2, when the storage assemblies 3 on the same horizontal plane are three groups, the Y-direction rods for the storage assemblies 3 are also three groups, and the Y-direction rods are arranged in one-to-one correspondence with the storage assemblies 3 and are used for installing and fixing the storage assemblies 3;
the storage support brackets 31 are detachably arranged on the Y-direction rod through the connecting sheets 32, when the Y-direction rod is used, the distance between two groups of storage support brackets 31 which are arranged in parallel along the vertical direction at the storage position can be adjusted according to the height dimension of the machine body along the Y-axis direction, so that the storage height requirement of the machine body can be met, and then the connecting sheets 32 and the Y-direction rod are fixed, so that the storage support brackets 31 and the Y-direction rod can be fixed; thereby allowing storage for fuselages of different height dimensions.
The storage assemblies 3 are arranged into a plurality of groups along the Y-axis direction, so that the unmanned aerial vehicle bodies with different models can be stored in the device; realizing multiple purposes.
In some possible embodiments, to effect transport;
the bracket support 1 comprises a bracket platform, universal casters arranged at the bottom of the bracket platform and lifting supporting feet 4 which are arranged in one-to-one correspondence with the universal casters and are arranged on the bracket platform.
Preferably, the bracket platform is in a square frame structure, wherein the storage component 3 close to the bracket platform can be directly arranged on the bracket platform and connected with the Y-direction rod;
in some possible embodiments, to effectively achieve the support stability of the present device;
the lifting supporting leg 4 comprises a screw rod in threaded connection with the bracket platform, a supporting seat connected with the bottom of the screw rod and a rotary table connected with the top of the screw rod.
When the universal roller is transported to a designated position, the universal roller is braked, the whole device is not moved any more, and then the turntable is rotated to enable the support seat to move to the side close to the bottom surface and to be abutted against the ground; when the supporting seats are abutted against the bottom surface, the whole support seat is effectively supported and fixed and cannot move;
furthermore, in order to ensure the stability of the vertical support 2, a diagonal brace may be further provided to connect the Y-direction rod and the X-direction rod, so as to form a stable whole.
Example 2:
an unmanned aerial vehicle storage rack is used for storing wings and comprises a movable bracket support 1, a vertical support 2 which is arranged on the bracket support 1 and is arranged along the Y-axis direction, and two groups of storage components 3 which are arranged on the vertical support 2 in parallel and are on the same horizontal plane;
each group of the storage assemblies 3 comprises a plurality of groups of storage lugs 31 which are arranged in parallel along the Y-axis direction, and connecting pieces 32 for connecting the storage lugs 31 and the vertical supports 2.
When the wing storage device is used, firstly, according to the height dimension of the stored wings along the Y-axis direction, the positions of two groups of storage brackets 31 which are vertically adjacent along the Y-axis direction are adjusted, so that the wings can be effectively supported according to the heights or the forms of the wings, the wings of unmanned aerial vehicles of different types can be stored, then, the wings are placed on the storage assembly 3, and transported to the designated positions through the movable bracket support 1, and the subsequent operation can be performed;
in some possible embodiments, in order to ensure that the wing can be effectively stored, damage to the wing when present and slipping after storage are avoided;
the storage support 31 comprises a support body 311 connected with the vertical support, a rubber pad 312 adhered to the support body and arranged vertically symmetrically, and a binding belt arranged on the support body 311.
In some possible embodiments, in order to effectively realize storage of wings with different height sizes or different forms, and avoid sliding of the wings;
the two groups of support bodies 311 are symmetrically arranged along the Y axis, the two groups of support bodies 311 are connected through the connecting sheet 32 to form a Y-shaped structure, and an included angle formed by the support bodies 311 and the vertical support 2 is A, and 45 degrees is less than or equal to 90 degrees.
The projection of the holder body 311 onto the horizontal plane will be set along the Z-axis direction.
The arrangement of the included angle enables the support body 311 to be inclined, so that the wing will not want to move the free end of the support body 311;
in some possible embodiments, to effectively achieve adjustment of the position between vertically adjacent support bodies 311;
two groups of support bodies 311 which are symmetrically arranged along the Y axis are connected through two groups of connecting lugs;
the connecting piece 32 has a Y-shaped structure and comprises connecting lugs connected with the two groups of support bodies 311 respectively and connecting pieces arranged along the Y-axis direction and positioned between the two groups of connecting lugs;
two groups of support bodies 311 are close to one another, and two groups of connecting pieces are close to one another to form a slot.
The slot is sleeved on the outer side of the Y-direction rod, and the adjustment of the position relation between the two groups of storage assemblies 3 along the Y-axis direction is realized according to the shape or the height of the wing through detachable connection, so that the storage of different wings is realized;
in some possible embodiments, the mounting of the storage assembly 3 is to be effected;
the vertical support 2 comprises a plurality of groups of Y-direction rods which are arranged along the Y-axis direction and are arranged in parallel along the X-axis direction, and X-direction rods which are used for connecting the Y-direction rods and are arranged along the X-axis direction.
In some possible embodiments, to effect transport;
the bracket support 1 comprises a bracket platform, universal casters arranged at the bottom of the bracket platform and lifting supporting feet 4 which are arranged in one-to-one correspondence with the universal casters and are arranged on the bracket platform.
In some possible embodiments, the support of the device is more stable and reliable for effectiveness;
the lifting supporting leg 4 comprises a screw rod in threaded connection with the bracket platform, a supporting seat connected with the bottom of the screw rod and a rotary table connected with the top of the screw rod.
The utility model is not limited to the specific embodiments described above. The utility model extends to any novel one, or any novel combination, of the features disclosed in this specification, as well as to any novel one, or any novel combination, of the steps of the method or process disclosed.
Claims (9)
1. An unmanned aerial vehicle storage rack is used for storing a fuselage or a wing and is characterized by comprising a movable bracket support, a vertical support which is arranged on the bracket support and is arranged along the Y-axis direction, and at least two groups of storage components which are arranged on the vertical support in parallel and are on the same horizontal plane;
each group of storage components comprises a plurality of groups of storage lugs which are arranged in parallel along the Y-axis direction and connecting sheets for connecting the storage lugs with the vertical support.
2. The unmanned aerial vehicle storage rack of claim 1, wherein the storage bracket comprises a bracket body connected with the vertical bracket, a rubber pad adhered to the bracket body and arranged along the vertical symmetry, and a binding belt arranged on the bracket body.
3. The unmanned aerial vehicle storage rack of claim 2, wherein the bracket body is of a tubular structure, and the long direction is along the Z-axis direction; the connecting sheet is positioned between the two groups of rubber mats and is connected with the vertical support.
4. A storage rack for an unmanned aerial vehicle according to claim 3, wherein the top of the rubber mat is provided with a U-shaped open slot.
5. The unmanned aerial vehicle storage rack of claim 2, wherein the two groups of support bodies are symmetrically arranged along the Y axis, the two groups of support bodies are connected through connecting sheets to form a Y-shaped structure, and an included angle formed by the support bodies and the vertical support is A, and 45 degrees is less than A and less than 90 degrees.
6. The unmanned aerial vehicle storage rack of claim 5, wherein two sets of bracket bodies symmetrically arranged along the Y-axis are connected by two sets of connecting lugs;
the connecting piece is of a Y-shaped structure and comprises connecting lug seats respectively connected with the two groups of support bodies and connecting pieces arranged along the Y-axis direction and positioned between the two groups of connecting lug seats;
two groups of support bodies are close to one end of each other, and two groups of connecting pieces are close to one side of each other to form a slot.
7. The unmanned aerial vehicle storage rack of any of claims 1-6, wherein the vertical support comprises a plurality of sets of Y-bars arranged in the Y-axis direction and parallel to the X-axis direction, and X-bars for connecting the Y-bars and arranged in the X-axis direction.
8. The unmanned aerial vehicle storage rack of claim 7, wherein the bracket comprises a bracket platform, universal casters arranged at the bottom of the bracket platform, and lifting supporting feet which are arranged in one-to-one correspondence with the universal casters and are arranged on the bracket platform.
9. The unmanned aerial vehicle storage rack of claim 8, wherein the lifting support feet comprise a screw rod in threaded connection with the bracket platform, a support base connected with the bottom of the screw rod, and a turntable connected with the top of the screw rod.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202223439052.8U CN219008639U (en) | 2022-12-21 | 2022-12-21 | Unmanned aerial vehicle storage rack |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202223439052.8U CN219008639U (en) | 2022-12-21 | 2022-12-21 | Unmanned aerial vehicle storage rack |
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| Publication Number | Publication Date |
|---|---|
| CN219008639U true CN219008639U (en) | 2023-05-12 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202223439052.8U Active CN219008639U (en) | 2022-12-21 | 2022-12-21 | Unmanned aerial vehicle storage rack |
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| Country | Link |
|---|---|
| CN (1) | CN219008639U (en) |
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2022
- 2022-12-21 CN CN202223439052.8U patent/CN219008639U/en active Active
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