CN214776647U - Automatic airport unmanned aerial vehicle take-off and landing device - Google Patents
Automatic airport unmanned aerial vehicle take-off and landing device Download PDFInfo
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- CN214776647U CN214776647U CN202120538995.2U CN202120538995U CN214776647U CN 214776647 U CN214776647 U CN 214776647U CN 202120538995 U CN202120538995 U CN 202120538995U CN 214776647 U CN214776647 U CN 214776647U
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Abstract
The utility model discloses an automatic airport unmanned aerial vehicle take off and land device, which comprises a supporting rack, a side plate, mechanism and the lift supporting mechanism of opening and shutting, through having set up the mechanism that opens and shuts on the support frame top, and set up the lift supporting mechanism bottom opening and shutting the mechanism, the buffer board through the lift supporting mechanism supports unmanned aerial vehicle, the fly leaf top of lift supporting mechanism is connected through connecting rod and the left baffle and the right baffle of mechanism that opens and shuts, open and shut between driving left baffle and the right baffle through the connecting rod when making the fly leaf reciprocate, when making the fly leaf remove downwards, it is closed between left baffle and the right baffle, shelter from the protection through left baffle and right baffle unmanned aerial vehicle on to the fly leaf, be convenient for protect unmanned aerial vehicle in sleet weather, and easy operation, high durability and convenient use.
Description
Technical Field
The utility model particularly relates to an automatic airport unmanned aerial vehicle takes off and land device relates to the relevant field of unmanned aerial vehicle technique.
Background
The unmanned plane is a non-manned plane operated by a radio remote control device and a self-contained program control device, or is completely or intermittently and autonomously operated by an onboard computer, and can be divided into military use, civil use and military use according to the application field, wherein the unmanned plane is divided into a reconnaissance plane and a target plane, and the unmanned plane and the industrial application are really just needed by the unmanned plane in the civil use.
Unmanned aerial vehicle generally takes off and land through unmanned aerial vehicle airport when taking off and land, and current unmanned aerial vehicle airport generally only supports and buffering effect, and when sleet weather, be not convenient for protect unmanned aerial vehicle, need accomodate unmanned aerial vehicle through the manual work.
SUMMERY OF THE UTILITY MODEL
Therefore, in order to solve the above insufficiency, the utility model provides an automatic airport unmanned aerial vehicle take off and land device here.
The utility model discloses a realize like this, construct an automatic airport unmanned aerial vehicle take-off and landing device, the device includes the support frame, opens and shuts mechanism and lift supporting mechanism, the support frame left and right sides is respectively through the inherent curb plate of bolt lock, the support frame top is through the bolt and the mutual lock solid of mechanism that opens and shuts, the mechanism bottom that opens and shuts is connected with lift supporting mechanism, the lift supporting mechanism outside and curb plate fixed connection, the mechanism that opens and shuts includes left baffle, right baffle, slide rail, dead lever and connection pivot, the slide rail slides along the slide rail respectively in both sides around left side baffle and the right baffle, and the slide rail outside is through the bolt and the mutual lock solid of dead lever, left side baffle and right baffle bottom front end are connected with lift supporting mechanism through connecting the pivot respectively, the dead lever bottom is through the bolt and the support frame is the lock solid each other.
Preferably, the lifting support mechanism comprises a movable plate, a buffer plate, a screw rod, a polished rod, a motor, support plates and a connecting mechanism, the middle of the top end of the movable plate is locked with the buffer plate through a bolt, the screw rod and the polished rod penetrate through the inner corners of the movable plate and are in threaded connection with the movable plate, the bottom end of the screw rod is connected with an output shaft of the motor, the support plates are connected to the upper end and the lower end of the screw rod and the polished rod, the top end of the motor is locked with the support plates through bolts, the connecting mechanism is arranged in the middle of the front end of the movable plate, the top end of the connecting mechanism is connected with a connecting rotating shaft, and the outer sides of the support plates are locked with side plates through bolts.
Preferably, coupling mechanism includes axis of rotation, screwed joint, limiting plate and connecting rod, the axis of rotation rear end is provided with screwed joint, the axis of rotation front end passes through bolt and the mutual lock solid of limiting plate, the axis of rotation outside is connected with the connecting rod rotation, the axis of rotation rear end passes through screwed joint and is connected with the fly leaf rotation, the connecting rod top is connected with being connected the pivot rotation.
Preferably, the slide rail surface is smooth form, and left baffle and right baffle inner wall all with the slide rail laminating.
Preferably, the surface of the polish rod is smooth, and the inner wall of the movable plate is attached to the polish rod.
Preferably, the screw rods and the polished rods are vertically arranged, and the number of the polished rods is three.
Preferably, the limiting plate is in a circular plate shape, and the outer diameter of the limiting plate is larger than that of the rotating shaft.
Preferably, the number of the connecting rods is two, and the top ends of the two connecting rods are respectively connected with the left baffle and the right baffle in a rotating mode through the connecting rotating shaft.
Preferably, the screw is made of hard alloy.
Preferably, the connecting rod is made of stainless steel.
The utility model has the advantages of as follows: the utility model discloses an improve and provide an automatic airport unmanned aerial vehicle take off and land device here, compare with equipment of the same type, have following improvement:
an automatic airport unmanned aerial vehicle take-off and land device, through having set up the mechanism that opens and shuts on the support frame top, and set up the lift supporting mechanism bottom opening and shutting the mechanism, the buffer board through lift supporting mechanism supports unmanned aerial vehicle, lift supporting mechanism's fly leaf top is connected with the left baffle and the right baffle of the mechanism that opens and shuts through the connecting rod, open and shut between left baffle and the right baffle of drive through the connecting rod when making the fly leaf reciprocate, when making the fly leaf move down, it is closed between left baffle and the right baffle, shelter from the protection through left baffle and right baffle unmanned aerial vehicle on to the fly leaf, be convenient for protect unmanned aerial vehicle in sleet weather, and easy operation, high durability and convenient use.
Drawings
FIG. 1 is a schematic structural view of the present invention;
fig. 2 is a front view of the structure of the present invention;
fig. 3 is a schematic structural view of the opening and closing mechanism of the present invention;
FIG. 4 is a schematic structural view of the elevating support mechanism of the present invention;
fig. 5 is a schematic view of the structure of the connection mechanism of the present invention.
Wherein: the device comprises a support frame-1, a side plate-2, an opening and closing mechanism-3, a lifting support mechanism-4, a left baffle-31, a right baffle-32, a slide rail-33, a fixed rod-34, a connecting rotating shaft-35, a movable plate-41, a buffer plate-42, a screw rod-43, a polished rod-44, a motor-45, a support plate-46, a connecting mechanism-47, a rotating shaft-471, a threaded joint-472, a limit plate-473 and a connecting rod-474.
Detailed Description
The present invention will be described in detail with reference to the accompanying fig. 1-5, and the technical solutions in the embodiments of the present invention will be clearly and completely described, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
Please refer to fig. 1 and 2, the utility model provides an automatic airport unmanned aerial vehicle device that takes off and land here through improving, including support frame 1, mechanism 3 and the lift supporting mechanism 4 that opens and shuts, the curb plate 2 is fixed through the bolt lock respectively in the support frame 1 left and right sides, 1 tops of support frame are through the bolt with mechanism 3 mutual lock solid that opens and shuts, 3 bottoms of mechanism 4 are connected with lift supporting mechanism, the 4 outsides of mechanism of lift supporting are with 2 fixed connection of curb plate.
Please refer to fig. 3, the utility model provides an automatic airport unmanned aerial vehicle takes off and land device through the improvement here, mechanism 3 that opens and shuts includes left baffle 31, right baffle 32, slide rail 33, dead lever 34 and connection pivot 35, slide rail 33 is followed respectively to both sides around left baffle 31 and the right baffle 32, and the slide rail 33 outside is through the mutual lock solid of bolt and dead lever 34, left baffle 31 and right baffle 32 bottom front end are connected with lift supporting mechanism 4 through connecting pivot 35 respectively, the mutual lock solid of bolt and support frame 1 is passed through to dead lever 34 bottom, slide rail 33 surface is the smoothness form, and left baffle 31 and right baffle 32 inner wall all laminate with slide rail 33, restrict left baffle 31 and right baffle 32's removal orbit through slide rail 33.
Referring to fig. 4, the present invention provides an automatic airport unmanned aerial vehicle take-off and landing apparatus through improvement, wherein the lifting support mechanism 4 includes a movable plate 41, a buffer plate 42, a screw 43, a polish rod 44, a motor 45, a support plate 46 and a connection mechanism 47, the middle portion of the top end of the movable plate 41 is mutually locked with the buffer plate 42 through a bolt, the screw 43 and the polish rod 44 penetrate through the corners inside the movable plate 41, the screw 43 is in threaded connection with the movable plate 41, the bottom end of the screw 43 is connected with an output shaft of the motor 45, the upper and lower ends of the screw 43 and the polish rod 44 are both connected with the support plate 46, the top end of the motor 45 is mutually locked with the support plate 46 through a bolt, the connection mechanism 47 is disposed in the middle portion of the front end of the movable plate 41, the top end of the connection mechanism 47 is connected with the connection shaft 35, the outer side of the support plate 46 is mutually locked with the side plate 2 through a bolt, the surface of the polish rod 44 is smooth, and the inner wall of the movable plate 41 is attached to the polish rod 44, the moving track of the movable plate 41 is limited, the screw rods 43 and the polished rods 44 are vertically arranged, the number of the polished rods 44 is three, the movable plate 41 is driven to vertically move along the screw rods 43 and the polished rods 44 when the screw rods 43 rotate, the screw rods 43 are made of hard alloy materials, the hardness is high, and the movable plate is not prone to abrasion.
Referring to fig. 5, the present invention provides an automatic airport unmanned aerial vehicle take-off and landing apparatus through improvement, wherein the connecting mechanism 47 includes a rotating shaft 471, a threaded joint 472, a limiting plate 473 and a connecting rod 474, the threaded joint 472 is disposed at the rear end of the rotating shaft 471, the front end of the rotating shaft 471 is mutually locked with the limiting plate 473 through a bolt, the outer side of the rotating shaft 471 is rotatably connected with the connecting rod 474, the rear end of the rotating shaft 471 is rotatably connected with the movable plate 41 through the threaded joint 472, the top end of the connecting rod 474 is rotatably connected with the connecting shaft 35, the limiting plate 473 is in a circular plate shape, the outer diameter of the limiting plate 473 is larger than that of the rotating shaft 471, the front end of the connecting rod 474 is supported through the limiting plate 473, the connecting rod 474 is provided with two connecting rods 474, and the top ends of the two connecting rods 474 are rotatably connected with the left baffle 31 and the right baffle 32 through the connecting shaft 35 respectively, so that the left baffle 31 and the right baffle 32 are outwardly pushed out through the connecting rods 474 when the movable plate 41 moves upward, the connecting rod 474 is made of stainless steel, has high hardness and is not easy to rust.
The utility model provides an automatic airport unmanned aerial vehicle taking-off and landing device through improvement, and the working principle is as follows;
firstly, before use, the device is firstly placed on a required plane position through the support frame 1, and then the power connection port of the motor 45 is connected with control equipment with an external power supply;
secondly, when the device is used, the motor 45 is controlled to generate power to drive the circle center of the bottom end of the screw 43 to rotate through the output shaft, the surface of the polished rod 44 is smooth, the inner wall of the movable plate 41 is attached to the polished rod 44, the moving track of the movable plate 41 is limited, and the movable plate 41 is driven to move upwards through the thread fit between the screw 43 and the movable plate 41 when the screw 43 rotates;
thirdly, the movable plate 41 drives the rotating shaft 471 at the front end to move upwards, because the two connecting rods 474 are arranged, the top ends of the two connecting rods 474 are respectively rotatably connected with the left baffle 31 and the right baffle 32 through the connecting rotating shaft 35, the two connecting rods 474 are inclined outwards from bottom to top, when the movable plate 41 moves upwards, the left baffle 31 and the right baffle 32 are pushed outwards through the connecting rods 474, and because the surface of the sliding rail 33 is smooth, and the inner walls of the left baffle 31 and the right baffle 32 are both attached to the sliding rail 33, the moving tracks of the left baffle 31 and the right baffle 32 are limited through the sliding rail 33, so that the left baffle 31 and the right baffle 32 slide outwards along the sliding rail 33 in parallel to open;
fourthly, then place unmanned aerial vehicle and take off and land the operation on the buffer board 42 on fly leaf 41 top, when sleet weather, through control fly leaf 41 downstream, make fly leaf 41 drive unmanned aerial vehicle move down to the support frame 1 in, and fly leaf 41 drives through connecting rod 474 and contracts between left baffle 31 and the right baffle 32, protects unmanned aerial vehicle, easy operation, convenient to use through left baffle 31 and right baffle 32.
The utility model discloses an improvement provides an automatic airport unmanned aerial vehicle take-off and landing device, through set up the mechanism 3 that opens and shuts on 1 top of support frame, and set up lift supporting mechanism 4 in mechanism 3 bottom that opens and shuts, buffer board 42 through lift supporting mechanism 4 supports unmanned aerial vehicle, connecting rod 474 and the left baffle 31 and the right baffle 32 of mechanism 3 that open and shut are passed through at the fly leaf 41 top of lift supporting mechanism 4 and are connected, open and shut between driving left baffle 31 and the right baffle 32 through connecting rod 474 when making fly leaf 41 reciprocate, when making fly leaf 41 move down, it is closed between left baffle 31 and the right baffle 32, shelter from the protection through left baffle 31 and right baffle 32 to the unmanned aerial vehicle on the fly leaf 41, be convenient for protect unmanned aerial vehicle in sleet weather, and easy operation, high durability and convenient use.
Claims (8)
1. An automatic airport unmanned aerial vehicle taking-off and landing device comprises a support frame (1), wherein side plates (2) are respectively fixed on the left side and the right side of the support frame (1) through bolts;
the method is characterized in that: the lifting support device also comprises an opening and closing mechanism (3) and a lifting support mechanism (4), the top end of the support frame (1) is mutually locked with the opening and closing mechanism (3) through a bolt, the bottom end of the opening and closing mechanism (3) is connected with a lifting support mechanism (4), the outer side of the lifting support mechanism (4) is fixedly connected with the side plate (2), the opening and closing mechanism (3) comprises a left baffle (31), a right baffle (32), a slide rail (33), a fixed rod (34) and a connecting rotating shaft (35), the front side and the rear side of the left baffle (31) and the right baffle (32) respectively slide along the slide rail (33), the outer side of the slide rail (33) is locked with a fixed rod (34) through bolts, the front ends of the bottoms of the left baffle plate (31) and the right baffle plate (32) are respectively connected with a lifting support mechanism (4) through a connecting rotating shaft (35), the bottom end of the fixed rod (34) is locked with the support frame (1) through a bolt.
2. The automated airport drone take-off and landing gear of claim 1, wherein: the lifting support mechanism (4) comprises a movable plate (41), a buffer plate (42), a screw (43), a polished rod (44), a motor (45), a support plate (46) and a connecting mechanism (47), the middle part of the top end of the movable plate (41) is mutually locked with the buffer plate (42) through a bolt, a screw rod (43) and a polish rod (44) are respectively penetrated through the inner corners of the movable plate (41), the screw rod (43) is in threaded connection with the movable plate (41), the bottom end of the screw rod (43) is connected with an output shaft of the motor (45), the upper and lower ends of the screw rod (43) and the polish rod (44) are both connected with a support plate (46), the top end of the motor (45) is locked with the support plate (46) through a bolt, the middle part of the front end of the movable plate (41) is provided with a connecting mechanism (47), the top end of the connecting mechanism (47) is connected with the connecting rotating shaft (35), and the outer side of the support plate (46) is locked with the side plate (2) through bolts.
3. The automated airport drone take-off and landing gear of claim 2, wherein: the connecting mechanism (47) comprises a rotating shaft (471), a threaded joint (472), a limiting plate (473) and a connecting rod (474), the rear end of the rotating shaft (471) is provided with the threaded joint (472), the front end of the rotating shaft (471) is locked with the limiting plate (473) through a bolt, the outer side of the rotating shaft (471) is rotatably connected with the connecting rod (474), the rear end of the rotating shaft (471) is rotatably connected with the movable plate (41) through the threaded joint (472), and the top end of the connecting rod (474) is rotatably connected with the connecting rotating shaft (35).
4. The automated airport drone take-off and landing gear of claim 1, wherein: slide rail (33) surface is smooth form, and left baffle (31) and right baffle (32) inner wall all with slide rail (33) laminating.
5. The automated airport drone take-off and landing gear of claim 2, wherein: the surface of the polish rod (44) is smooth, and the inner wall of the movable plate (41) is attached to the polish rod (44).
6. The automated airport drone take-off and landing gear of claim 2, wherein: the screw rods (43) and the polished rods (44) are vertically arranged, and the number of the polished rods (44) is three.
7. The automated airport drone take off and landing gear of claim 3, wherein: the limiting plate (473) is in a circular plate shape, and the outer diameter of the limiting plate (473) is larger than that of the rotating shaft (471).
8. The automated airport drone take off and landing gear of claim 3, wherein: the number of the connecting rods (474) is two, and the top ends of the two connecting rods (474) are respectively connected with the left baffle plate (31) and the right baffle plate (32) in a rotating manner through a connecting rotating shaft (35).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120538995.2U CN214776647U (en) | 2021-03-15 | 2021-03-15 | Automatic airport unmanned aerial vehicle take-off and landing device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120538995.2U CN214776647U (en) | 2021-03-15 | 2021-03-15 | Automatic airport unmanned aerial vehicle take-off and landing device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN214776647U true CN214776647U (en) | 2021-11-19 |
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ID=78665509
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202120538995.2U Active CN214776647U (en) | 2021-03-15 | 2021-03-15 | Automatic airport unmanned aerial vehicle take-off and landing device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN214776647U (en) |
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2021
- 2021-03-15 CN CN202120538995.2U patent/CN214776647U/en active Active
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