Drawer type unmanned aerial vehicle field suspension cable supporting device

Abstract

The utility model relates to the technical field of unmanned aerial vehicles, and discloses a drawer type unmanned aerial vehicle field suspension cable supporting device which comprises a main body assembly, a protection shell, a wind power sensor, a rainfall sensor and a heat dissipation shell, the wind power sensor is fixed to the top of the protection shell, and the rainfall sensor is fixed to the top of the protection shell. The heat dissipation shell is fixed in the protection shell; the fixing assembly is arranged in the protective shell and comprises a sliding part and a limiting part, the sliding part is arranged in the protective shell, and the limiting part is located on one side of the sliding part. The unmanned aerial vehicle landing platform has the advantages that by arranging the fixing assembly, when an unmanned aerial vehicle lands on the platform, the landing platform cannot shake and is in a stable state through mutual cooperation of the sliding piece and the limiting piece, and therefore the situation that the landing platform inclines due to inertia when the unmanned aerial vehicle lands is avoided.

Description

Technical Field

[0001] The utility model relates to the technical field of unmanned aerial vehicles, in particular to a drawer-type unmanned aerial vehicle airport suspension cable support device. Background Art

[0002] In recent years, drone technology has received widespread attention and application, especially in aerial photography, agriculture, logistics, rescue and other fields. With the continuous expansion of drone applications, higher requirements are placed on the flexibility and convenience of take-off and landing sites. The design of the drawer-type drone site opening and closing device is precisely to meet this demand. Through the drawer-type structural design, the drone site can be easily stored and unfolded. The current drawer-type structural design is usually used in a suspended state. Long-term use or when the drone lands on the platform, due to the inertia of gravity when the drone descends, the landing platform will tilt for a long time, so the drone will be unstable and shake. Utility Model Content

[0003] The purpose of this section is to summarize some aspects of the embodiments of the utility model and briefly introduce some preferred embodiments. Some simplifications or omissions may be made in this section and the specification abstract and utility model name of this application to avoid blurring the purpose of this section, specification abstract and utility model name, and such simplifications or omissions cannot be used to limit the scope of the utility model.

[0004] In view of the above problems and / or the problems existing in the existing drawer-type UAV airport suspension cable support device, the present utility model is proposed.

[0005] Therefore, the problem to be solved by the utility model is that the current drawer-type structural design is usually used in a suspended state. When used for a long time or when a drone lands on a platform, due to the inertia of gravity when the drone descends, the landing platform will tilt over a long period of time, thus making the drone land unsteadily and shake.

[0006] In order to solve the above technical problems, the utility model provides the following technical solutions: a drawer-type UAV airport suspension cable support device, which includes a main body component, including a protective shell, a wind sensor, a rain sensor and a heat dissipation shell, the wind sensor is fixed to the top of the protective shell, the rain sensor is fixed to the top of the protective shell, and the heat dissipation shell is fixed inside the protective shell; and,

[0007] The fixing assembly is arranged in the protective shell and comprises a sliding member and a limiting member. The sliding member is arranged in the protective shell, and the limiting member is located at one side of the sliding member.

[0008] As a preferred solution of the drawer-type unmanned aerial vehicle airport suspension cable support device of the utility model, the sliding member includes a positioning plate and a first support plate, the positioning plate is fixed in the protective shell, and the first support plate is fixed to one side of the positioning plate.

[0009] As a preferred solution of the drawer-type unmanned aerial vehicle airport suspension support device of the utility model, wherein: the sliding part also includes a first sliding plate, a second support plate and a limit plate, the first sliding plate slides on the top of the first support plate, the second support plate is fixed to one side of the first sliding plate, the limit plate is fixed to one side of the first support plate, and the limit plate is used to limit the sliding distance of the first sliding plate.

[0010] As a preferred solution of the drawer-type unmanned aerial vehicle airport suspension cable support device of the utility model, the sliding member also includes a fixed plate and a second sliding plate, the fixed plate is fixed to one side of the second support plate, and the second sliding plate slides on the top of the fixed plate.

[0011] As a preferred solution of the drawer-type unmanned aerial vehicle airport suspension cable support device of the utility model, the sliding part also includes a support plate and a connecting plate, the support plate is fixed to one side of the fixed plate, the connecting plate is fixed to one side of the second sliding plate, and the connecting plate slides on the top of the support plate.

[0012] As a preferred solution of the drawer-type UAV airport suspension cable support device of the utility model, the sliding member also includes a support frame and a UAV platform, the support frame is fixed to one side of the connecting plate, and the UAV platform is fixed to the top of the support frame.

[0013] As a preferred solution of the drawer-type unmanned aerial vehicle airport suspension cable support device of the utility model, the limiting member includes a positioning block and a moving rod, the positioning block is fixed to one side of the first sliding plate, and the moving rod is rotatably connected to the surface of the positioning block through a bearing.

[0014] As a preferred solution of the drawer-type unmanned aerial vehicle airport suspension cable support device of the utility model, the limiting member also includes a fixed block and a limiting rod, the fixed block is fixed to the bottom of the heat dissipation shell, and the limiting rod is rotatably connected to the surface of the fixed block through a bearing.

[0015] As a preferred solution of the drawer-type unmanned aerial vehicle airport suspension cable support device of the utility model, the limiting member also includes a limiting block, the limiting block is fixed in the limiting rod, a movable groove is opened on the surface of the movable rod, and the limiting block slides in the movable groove.

[0016] The beneficial effect of the utility model is that by setting a fixed component, when the UAV lands on the platform, the sliding part and the limit part can cooperate with each other to prevent the landing platform from shaking and being in a stable state, thereby avoiding the landing platform from tilting due to the inertia of the UAV when landing. BRIEF DESCRIPTION OF THE DRAWINGS

[0017] In order to more clearly illustrate the technical solutions of the embodiments of the present utility model, the following briefly introduces the drawings required for the description of the embodiments. Obviously, the drawings described below are only some embodiments of the present utility model. For ordinary technicians in this field, other drawings can be obtained based on these drawings without creative labor. Among them:

[0018] Figure 1 This is a structural diagram of the drawer-type UAV airport cable support device.

[0019] Figure 2 This is a cross-sectional structural diagram of the protective shell of the drawer-type UAV airport suspension support device.

[0020] Figure 3 This is a cross-sectional structural diagram of the protective shell of the drawer-type UAV airport suspension support device.

[0021] Figure 4 This is a structural diagram of the connection between the first sliding plate and the positioning block of a drawer-type UAV airport suspension cable support device.

[0022] Figure 5 This is a structural diagram of the connection plate and support frame of the drawer-type UAV airport suspension support device.

[0023] Figure 6 For the drawer type UAV airport cable support device Figure 5 A in the enlarged structure diagram. DETAILED DESCRIPTION

[0024] In order to make the above-mentioned purposes, features and advantages of the present invention more obvious and easy to understand, the specific implementation methods of the present invention are described in detail below in conjunction with the accompanying drawings.

[0025] In the following description, many specific details are set forth to facilitate a full understanding of the present invention, but the present invention may also be implemented in other ways different from those described herein, and those skilled in the art may make similar generalizations without violating the connotation of the present invention. Therefore, the present invention is not limited to the specific embodiments disclosed below.

[0026] Secondly, the term "one embodiment" or "embodiment" as used herein refers to a specific feature, structure or characteristic that may be included in at least one implementation of the present invention. The term "in one embodiment" that appears in different places in this specification does not necessarily refer to the same embodiment, nor does it refer to a separate or selective embodiment that is mutually exclusive with other embodiments.

[0027] Example 1

[0028] Reference Figure 1 to Figure 6 , which is the first embodiment of the utility model, and this embodiment provides a drawer-type UAV airport suspension cable support device. The drawer-type UAV airport suspension cable support device includes a main component 100 and a fixing component 200. Through the cooperation of the two, when the UAV lands on the platform, the sliding member 201 and the limiting member 202 can cooperate with each other to prevent the landing platform from shaking and being in a stable state, thereby avoiding the landing platform from tilting due to the inertia of the UAV when landing.

[0029] Specifically, the main component 100 includes a protective shell 101, a wind sensor 102, a rain sensor 103 and a heat dissipation shell 104. The wind sensor 102 is fixed to the top of the protective shell 101, the rain sensor 103 is fixed to the top of the protective shell 101, and the heat dissipation shell 104 is fixed inside the protective shell 101.

[0030] The protective shell 101 is used to protect the internal equipment and to protect the drone. The wind sensor 102 is used to detect the wind force to see if it is sufficient for the drone to fly normally, ensuring that the drone will not encounter air currents during flight. The rain sensor 103 is used to detect the amount of rainfall, thereby ensuring that the drone can take off normally. The wind sensor 102 and the rain sensor 103 are prior art and will not be described in detail herein. The heat dissipation shell 104 is used to ensure that the temperature inside the protective shell 101 is moderate, preventing the drone equipment from overheating inside the protective shell 101, and ensuring that the drone can be used normally.

[0031] The fixing assembly 200 is disposed in the protective shell 101 , and includes a sliding member 201 and a limiting member 202 . The sliding member 201 is disposed in the protective shell 101 , and the limiting member 202 is located at one side of the sliding member 201 .

[0032] The sliding member 201 is used to move the drone lifting platform out of the protective shell 101 to provide a take-off or landing platform for the drone. The limiting member 202 can cooperate with the sliding member 201 to provide support for the drone platform so that the inertia of the drone will not cause the landing platform to tilt when landing.

[0033] Specifically, the sliding member 201 includes a positioning plate 201 a and a first supporting plate 201 b . The positioning plate 201 a is fixed in the protective shell 101 , and the first supporting plate 201 b is fixed to one side of the positioning plate 201 a .

[0034] The positioning plate 201a is used to fix the position of the sliding member 201 so that the sliding member 201 can cooperate with the limiting member 202 to ensure that the lifting platform will not tilt. The first supporting plate 201b is used to support the sliding member 201 to slide normally without deviation.

[0035] Specifically, the sliding member 201 also includes a first sliding plate 201c, a second supporting plate 201d and a limiting plate 201e. The first sliding plate 201c slides on the top of the first supporting plate 201b, the second supporting plate 201d is fixed to one side of the first sliding plate 201c, and the limiting plate 201e is fixed to one side of the first supporting plate 201b. The limiting plate 201e is used to limit the sliding distance of the first sliding plate 201c.

[0036] The first sliding plate 201c is used to drive the second supporting plate 201d to slide, so as to ensure that the second supporting plate 201d can drive the sliding member 201 to slide, so that the lifting platform can slide outside the protective shell 101 to facilitate the landing or take-off of the drone. The limiting plate 201e is used to limit the position of the first sliding plate 201c, so that the first sliding plate 201c is fixed after sliding a certain distance and will not slide autonomously.

[0037] Specifically, the sliding member 201 further includes a fixed plate 201f and a second sliding plate 201g. The fixed plate 201f is fixed to one side of the second supporting plate 201d, and the second sliding plate 201g slides on the top of the fixed plate 201f.

[0038] When the second support plate 201d moves, the second support plate 201d can drive the fixed plate 201f to slide in the second sliding plate 201g, thereby extending the moving distance of the lifting platform, so that the drone will not contact the protective shell 101 when lifting.

[0039] Example 2

[0040] Reference Figure 2 to Figure 5 , which is the second embodiment of the utility model, and this embodiment is based on the previous embodiment.

[0041] Specifically, the sliding member 201 further includes a supporting plate 201h and a connecting plate 201i. The supporting plate 201h is fixed to one side of the fixing plate 201f, and the connecting plate 201i is fixed to one side of the second sliding plate 201g. The connecting plate 201i slides on the top of the supporting plate 201h.

[0042] When the second sliding plate 201g moves, the supporting plate 201h can be driven to move at the same time. The connecting plate 201i is used to ensure that the supporting plate 201h will not deviate when moving, thereby ensuring that the sliding member 201 will not shake.

[0043] Specifically, the sliding member 201 also includes a support frame 201j and a UAV platform 201k. The support frame 201j is fixed to one side of the connecting plate 201i, and the UAV platform 201k is fixed to the top of the support frame 201j.

[0044] There are two support frames 201j, both fixed on one side of the connecting plate 201i, and used to fix the position of the UAV platform 201k, so that the UAV can land on the UAV platform 201k smoothly and accurately when it is lifted or lowered, which is convenient for the subsequent recovery or use of the UAV.

[0045] Specifically, the limiting member 202 includes a positioning block 202a and a moving rod 202b. The positioning block 202a is fixed to one side of the first sliding plate 201c, and the moving rod 202b is rotatably connected to the surface of the positioning block 202a through a bearing.

[0046] The positioning block 202a is used to fix the position of the limit member 202 so that the limit member 202 can cooperate with the sliding member 201 to ensure that the lifting platform will not tilt due to inertia when the drone lands after being extended. The moving rod 202b is used to limit the distance of the limit member 202 to ensure that the limit member 202 can limit the position of the sliding member 201.

[0047] Example 3

[0048] Reference Figure 2 to Figure 6 , which is the third embodiment of the utility model, and this embodiment is based on the first two embodiments.

[0049] Specifically, the limiting member 202 further includes a fixing block 202c and a limiting rod 202d. The fixing block 202c is fixed to the bottom of the heat dissipation shell 104, and the limiting rod 202d is rotatably connected to the surface of the fixing block 202c through a bearing.

[0050] The fixing block 202c is used to fix the position of the limiting rod 202d so that the limiting rod 202d can cooperate with the moving rod 202b, so that the moving rod 202b can support the extended first sliding plate 201c and prevent the first sliding plate 201c from tilting.

[0051] Specifically, the limiting member 202 further includes a limiting block 202e, which is fixed in the limiting rod 202d. A moving groove V is provided on the surface of the moving rod 202b, and the limiting block 202e slides in the moving groove V.

[0052] There are two limit blocks 202e, both fixed in the limit rod 202d. The limit block 202e slides in the movable slide groove V to limit the position of the movable rod 202b so that the movable rod 202b will not slide out of the limit rod 202d, and the movable rod 202b is limited by the limit block 202e, so that the first sliding plate 201c will not tilt, thereby ensuring that the sliding part 201 will not contact the protective shell 101 when the drone platform is recovered.

[0053] During use, when it is necessary to support the suspension cable of the drone airport, the drone lifting platform is first pushed out of the protective shell 101 through the first sliding plate 201c, and then the connecting plate 201i is driven to move through the second sliding plate 201g to extend the drone lifting platform. When the first sliding plate 201c moves, the moving rod 202b can also be driven to slide at the same time. When the first sliding plate 201c moves, the moving rod 202b moves on the limit rod 202d, so that after the second sliding plate 201g moves, the moving rod 202b can support the first sliding plate 201c, so that the first sliding plate 201c can support the second sliding plate 201g, so that the drone lifting platform will not tilt, ensuring that the drone lifting platform can be used normally.

[0054] It should be noted that the above embodiments are only used to illustrate the technical solution of the utility model rather than to limit it. Although the utility model has been described in detail with reference to the preferred embodiments, ordinary technicians in the field should understand that the technical solution of the utility model can be modified or replaced by equivalents without departing from the spirit and scope of the technical solution of the utility model, which should be included in the scope of the claims of the utility model.

Claims

1. A drawer-type UAV airport suspension cable support device, characterized in that: include, A main body component (100) comprises a protective shell (101), a wind sensor (102), a rain sensor (103) and a heat dissipation shell (104), wherein the wind sensor (102) is fixed to the top of the protective shell (101), the rain sensor (103) is fixed to the top of the protective shell (101), and the heat dissipation shell (104) is fixed inside the protective shell (101); and The fixing assembly (200) is arranged in the protective shell (101), and comprises a sliding member (201) and a limiting member (202); the sliding member (201) is arranged in the protective shell (101), and the limiting member (202) is located on one side of the sliding member (201).

2. The drawer-type UAV airport suspension cable support device according to claim 1, characterized in that: The sliding member (201) comprises a positioning plate (201a) and a first supporting plate (201b); the positioning plate (201a) is fixed in the protective shell (101); and the first supporting plate (201b) is fixed to one side of the positioning plate (201a).

3. The drawer-type UAV airport suspension cable support device according to claim 2, characterized in that: The sliding member (201) further comprises a first sliding plate (201c), a second supporting plate (201d) and a limiting plate (201e), wherein the first sliding plate (201c) slides on the top of the first supporting plate (201b), the second supporting plate (201d) is fixed to one side of the first sliding plate (201c), and the limiting plate (201e) is fixed to one side of the first supporting plate (201b), and the limiting plate (201e) is used to limit the sliding distance of the first sliding plate (201c).

4. The drawer-type UAV airport suspension cable support device according to claim 3, characterized in that: The sliding member (201) further comprises a fixed plate (201f) and a second sliding plate (201g), wherein the fixed plate (201f) is fixed to one side of the second supporting plate (201d), and the second sliding plate (201g) slides on the top of the fixed plate (201f).

5. The drawer-type UAV airport suspension cable support device according to claim 4, characterized in that: The sliding member (201) further comprises a supporting plate (201h) and a connecting plate (201i), wherein the supporting plate (201h) is fixed to one side of the fixing plate (201f), the connecting plate (201i) is fixed to one side of the second sliding plate (201g), and the connecting plate (201i) slides on the top of the supporting plate (201h).

6. The drawer-type UAV airport suspension cable support device according to claim 5, characterized in that: The sliding member (201) further comprises a support frame (201j) and an unmanned aerial vehicle platform (201k), wherein the support frame (201j) is fixed to one side of the connecting plate (201i), and the unmanned aerial vehicle platform (201k) is fixed to the top of the support frame (201j).

7. The drawer-type UAV airport suspension cable support device according to claim 5 or 6, characterized in that: The limiting member (202) comprises a positioning block (202a) and a moving rod (202b); the positioning block (202a) is fixed to one side of the first sliding plate (201c); and the moving rod (202b) is rotatably connected to the surface of the positioning block (202a) via a bearing.

8. The drawer-type UAV airport suspension cable support device according to claim 7, characterized in that: The limiting member (202) further comprises a fixing block (202c) and a limiting rod (202d); the fixing block (202c) is fixed to the bottom of the heat dissipation shell (104); and the limiting rod (202d) is rotatably connected to the surface of the fixing block (202c) via a bearing.

9. The drawer-type UAV airport suspension cable support device according to claim 8, characterized in that: The limiting member (202) further comprises a limiting block (202e), wherein the limiting block (202e) is fixed inside the limiting rod (202d), a movable slide groove (V) is provided on the surface of the movable rod (202b), and the limiting block (202e) slides inside the movable slide groove (V).

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