CN217060720U - Shutter assembly for unmanned aerial vehicle cradle head - Google Patents
Shutter assembly for unmanned aerial vehicle cradle head Download PDFInfo
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- CN217060720U CN217060720U CN202220577275.1U CN202220577275U CN217060720U CN 217060720 U CN217060720 U CN 217060720U CN 202220577275 U CN202220577275 U CN 202220577275U CN 217060720 U CN217060720 U CN 217060720U
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Abstract
The application provides unmanned aerial vehicle is shutter assembly for cloud platform relates to shutter equipment technical field. Unmanned aerial vehicle is shutter subassembly for cloud platform, including fixing base and blade, seted up fast door and window in the fixing base, be equipped with constant head tank and power unit in the fixing base, be equipped with on the power unit and pass the blade stretches into the reference column of constant head tank, the blade can move down under power unit's the drive and open and close fast door and window. Compared with the prior art, this application simple structure, practical convenient drive the blade through power unit and remove and open and close fast door and window, realize the accurate of blade and remove and stop, make shutter subassembly during operation remain stable, avoid taking place the condition of shake because of the striking, improve unmanned aerial vehicle and shoot the definition.
Description
[ technical field ] A
The application relates to shutter equipment technical field, especially relates to unmanned aerial vehicle is shutter assembly for cloud platform.
[ background ] A method for producing a semiconductor device
Along with the rapid development of unmanned aerial vehicle technique, more and more occasions all can use the shadow of seeing unmanned aerial vehicle.
Current unmanned aerial vehicle, the shutter structure that conventional used drives the blade and removes and go on for solenoid valve direct drive, and the stop position relies on striking the stopper to stop. The product can shake due to impact force at the moment of impact, and slight shake can influence the shake of a shot imaging picture, so that the image is unclear, fuzzy and the like.
[ summary of the invention ]
The utility model provides an aim at provides unmanned aerial vehicle is shutter assembly for cloud platform can be at shutter structure during operation remain stable.
The application is realized by the following technical scheme:
unmanned aerial vehicle is shutter subassembly for cloud platform, including fixing base and blade, fast door and window has been seted up on the fixing base, be equipped with constant head tank and power unit in the fixing base, be equipped with on the power unit and pass the blade stretches into the reference column of constant head tank, the blade can move down under power unit's the drive and open and close fast door and window.
As above shutter assembly for unmanned aerial vehicle cloud platform, power unit is including locating drive arrangement and drive gear in the fixing base to and with this drive gear meshing driven gear train, the reference column is located the gear train is kept away from drive gear one end.
As above-mentioned unmanned aerial vehicle is shutter assembly for cloud platform, drive arrangement is step motor formula solenoid valve.
As above unmanned aerial vehicle is shutter assembly for cloud platform, the blade the constant head tank and power unit all is equipped with two, and respectively corresponding locating fast door and window relative both sides, drive arrangement's quantity is 4, and two liang of correspondences locate fast door and window relative two corners department.
As above shutter assembly for unmanned aerial vehicle cloud platform, the blade the constant head tank and power unit all is equipped with two, just the constant head tank with the reference column is located shutter window one side, drive arrangement's quantity is 2, and correspondingly locates the both sides limit department that the fast door window is adjacent.
As above unmanned aerial vehicle is shutter assembly for cloud platform, the fixing base is including having seted up fast door and window's base and locating in proper order the base rear end and with inner cup and back lid that the shutter window is relative.
As above-mentioned shutter assembly for unmanned aerial vehicle cloud platform, the relative both sides of inner cup and back lid all are equipped with the constant head tank, two the reference column passes respectively corresponding the blade and stretches into correspondingly in the constant head tank.
According to the shutter assembly for the unmanned aerial vehicle holder, the two blades are respectively arranged between the inner cover and the rear cover in a stacked mode and located on two opposite sides of the shutter window, and the two power mechanisms are respectively arranged between the inner cover and the base and located on two opposite sides of the shutter window.
As above shutter assembly for unmanned aerial vehicle cloud platform, seted up on the blade and dodged the groove, the reference column passes dodge the groove and remove in it.
As above unmanned aerial vehicle is shutter assembly for cloud platform, be equipped with on the blade and make its removal when it moves to open position the breach of fast door and window.
Compared with the prior art, the method has the following advantages: this application simple structure, practical convenient drive the blade through power unit and remove and open and close fast door and window, realize the accurate removal and the stop of blade, make shutter assembly during operation remain stable, avoid taking place the condition of shake because of the striking, improve unmanned aerial vehicle and shoot the definition.
[ description of the drawings ]
In order to more clearly illustrate the technical solutions in the embodiments of the present application, the drawings needed to be used in the description of the embodiments are briefly introduced below, and it is obvious that the drawings in the following description are only some embodiments of the present application, and it is obvious for those skilled in the art to obtain other drawings based on these drawings without creative efforts.
Fig. 1 is a schematic structural diagram of an embodiment of the present application when being turned on.
Fig. 2 is a second schematic structural diagram of the first embodiment of the present application when being opened.
Fig. 3 is an exploded view of the first embodiment of the present application.
Fig. 4 is an exploded view of the second embodiment of the present application.
Fig. 5 is a schematic structural diagram of a closing operation according to an embodiment of the present application.
Fig. 6 is a second schematic structural diagram of the first embodiment of the present application when closed.
Fig. 7 is an enlarged schematic view of the embodiment of the present application at a in fig. 3.
Fig. 8 is a schematic structural diagram of the second embodiment of the present application when opened.
Fig. 9 is an exploded view of the second embodiment of the present application when opened.
Fig. 10 is a second exploded view of the second embodiment of the present application when opened.
FIG. 11 is an enlarged view of FIG. 9 at B.
Fig. 12 is a schematic structural diagram of the second embodiment of the present application when closed.
[ detailed description ] embodiments
In order to make the technical problems, technical solutions and advantageous effects solved by the present application more clear and obvious, the present application is further described in detail below with reference to the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are merely illustrative of the present application and are not intended to limit the present application.
As shown in fig. 1 to 7, this application embodiment provides a shutter assembly for unmanned aerial vehicle cloud platform, including fixing base 1 and blade 2, quick door and window 11 has been seted up on fixing base 1, fixing base 1 is equipped with constant head tank 12 and power unit 3, be equipped with on the power unit 3 and pass blade 2 stretches into the reference column 4 of constant head tank 12, blade 2 can move under power unit 3's the drive and open and close quick door and window 11. The power mechanism 3 drives the blades 2 to move to open and close the shutter door and window 11, so that the blades 2 can move and stop accurately, the shutter assembly can keep stable during working, and the shaking caused by impact is avoided.
Furthermore, the power mechanism 3 includes a driving device and a driving gear 311 disposed in the fixing base 1, and a gear set 32 in meshing transmission with the driving gear 311, and the positioning column 4 is disposed at one end of the gear set 32 far away from the driving gear 311. Specifically, the blade 2 the constant head tank 12 and power unit 3 all is equipped with two, and respectively corresponding locates 11 relative both sides of fast door and window, drive arrangement's quantity is 4, and two liang of correspondences locate 11 relative two corners department of fast door and window. The driving means is a stepping motor type electromagnetic valve 31. Through step motor formula solenoid valve 31 output control signal drive gear 311 rotates, gear train 32 meshing transmission drives reference column 4 with blade 2 removes, and the stop position uses drive signal control equally, realizes not having the unsettled stopping of striking, reaches the shutter subassembly and does not take place the shake effect, improves unmanned aerial vehicle and shoots the definition.
Specifically, the number of the blades 2, the positioning grooves 12 and the power mechanism 3 is two, and the two are respectively and correspondingly arranged on two opposite sides of the fast door and window 11.
Further, the fixing seat 1 includes a base 13 provided with the fast door and window 11, and an inner cover 14 and a rear cover 15 which are sequentially provided at the rear end of the base 13 and are opposite to the fast door and window 11. Specifically, the two blades 2 are respectively stacked between the inner cover 14 and the rear cover 15 and located on two opposite sides of the fast door/window 11, and the two power mechanisms 3 are respectively located between the inner cover 14 and the base 13 and located on two opposite sides of the fast door/window 11. The blade 2 is prevented from contacting with the power mechanism 3 and the external environment, the working stability of the shutter assembly is kept, and the service life is prolonged.
Specifically, the positioning grooves 12 are formed in two opposite sides of the inner cover 14 and the rear cover 15, and the two positioning pillars 4 respectively penetrate through the corresponding blades 2 and extend into the corresponding positioning grooves 12. The positioning groove 12 extends in the moving direction of the vane 2.
Specifically, avoidance grooves 21 are formed in the blades 2, and the two positioning columns 4 penetrate through the corresponding avoidance grooves 21 respectively and move in the avoidance grooves. Both blades 2 are provided with notches 22 for moving the blades away from the door/window 11 when the blades are moved to the opening position.
In embodiment 2, this embodiment is basically the same as embodiment 1, and for the sake of convenience, only the difference in the main structure from embodiment 1 will be described. The parts not described in this example are the same as example 1, except that:
as shown in fig. 8 to 12, the number of the blades 2 and the number of the positioning grooves 12 are two, the power mechanism 3, the number of the positioning grooves 12 and the number of the positioning columns 4 are two, the positioning grooves 12 and the positioning columns 4 are all arranged on one side of the fast door window 11, the number of the driving devices is 2, and the driving devices are correspondingly arranged on two adjacent side edges of the fast door window 11.
To better understand the technical solution of the present embodiment, the working principle is as follows:
when shooting: step motor formula solenoid valve 31 starts, drive gear 311 with gear train 32 meshing transmission drives gear train 32 rotates, thereby drives reference column 4 with blade 2 removes, realizes the start-up or the closing of fast door and window 11, and the stop position uses drive signal control, realizes the unsettled stopping of no striking, reaches the shutter subassembly and does not take place the shake effect, improves unmanned aerial vehicle and shoots the definition.
It should be understood that the terms "first", "second", etc. are used herein to describe various information but such information should not be limited to these terms, which are only used to distinguish one type of information from another. For example, "first" information may also be referred to as "second" information, and similarly, "second" information may also be referred to as "first" information, without departing from the scope of the present application. Furthermore, the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer", and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience in describing the present application and simplifying the description, but do not indicate or imply that the referred devices or elements must have a specific orientation, be constructed in a specific orientation, and be operated, and thus, should not be construed as limiting the present application.
The foregoing is illustrative of one or more embodiments provided in connection with the detailed description and is not intended to limit the disclosure to the particular forms disclosed. Similar or identical methods, structures, etc. as used herein, or several technical inferences or substitutions made on the concept of the present application should be considered as the scope of the present application.
Claims (10)
1. Unmanned aerial vehicle is shutter assembly for cloud platform, its characterized in that, including fixing base (1) and blade (2), fast door and window (11) have been seted up on fixing base (1), be equipped with constant head tank (12) and power unit (3) in fixing base (1), be equipped with on power unit (3) and pass blade (2) and stretch into reference column (4) of constant head tank (12), blade (2) can remove under the drive of power unit (3) and open and close fast door and window (11).
2. The shutter assembly for the pan/tilt head of the unmanned aerial vehicle according to claim 1, wherein the power mechanism (3) comprises a driving device and a driving gear (311) which are arranged in the fixing base (1), and a gear set (32) which is in meshing transmission with the driving gear (311), and the positioning column (4) is arranged at one end of the gear set (32) far away from the driving gear (311).
3. The shutter assembly for an unmanned aerial vehicle pan-tilt according to claim 2, wherein said driving means is a stepping motor type solenoid valve (31).
4. The shutter assembly for the tripod head of the unmanned aerial vehicle according to claim 3, wherein the number of the blades (2), the positioning grooves (12) and the power mechanism (3) is two, and the two corresponding positioning grooves are respectively arranged on two opposite sides of the fast door window (11), the number of the driving devices is 4, and two corresponding positioning grooves are respectively arranged on two opposite corners of the fast door window (11).
5. The shutter assembly for the tripod head of the unmanned aerial vehicle according to claim 3, wherein the number of the blades (2) and the positioning grooves (12) is two, the power mechanism (3), the two positioning grooves (12) and the two positioning columns (4) are arranged on one side of the fast door window (11), the number of the driving devices is 2, and the driving devices are correspondingly arranged on two adjacent side edges of the fast door window (11).
6. The shutter assembly for the tripod head of the unmanned aerial vehicle according to claim 4, wherein the fixing base (1) comprises a base (13) provided with the fast door and window (11), and an inner cover (14) and a rear cover (15) which are sequentially arranged at the rear end of the base (13) and are opposite to the fast door and window (11).
7. The shutter assembly for the tripod head of the unmanned aerial vehicle according to claim 6, wherein the two blades (2) are respectively stacked between the inner cover (14) and the rear cover (15) and located on two opposite sides of the fast door window (11), and the two power mechanisms (3) are respectively located between the inner cover (14) and the base (13) and located on two opposite sides of the fast door window (11).
8. The shutter assembly for an unmanned aerial vehicle pan-tilt according to claim 6, wherein said positioning slots (12) are provided on opposite sides of said inner cover (14) and said rear cover (15), and said positioning posts (4) respectively penetrate through said corresponding blades (2) and extend into said corresponding positioning slots (12).
9. The shutter assembly for the tripod head of the unmanned aerial vehicle according to any one of claims 1 to 8, wherein an avoiding groove (21) is formed on the blade (2), and the positioning column (4) passes through the avoiding groove (21) and moves in the avoiding groove.
10. The shutter assembly for an unmanned aerial vehicle pan-tilt-head according to claim 9, wherein said blade (2) is provided with a notch (22) for moving it away from said shutter window (11) when it is moved to the open position.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN202220577275.1U CN217060720U (en) | 2022-03-16 | 2022-03-16 | Shutter assembly for unmanned aerial vehicle cradle head |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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CN202220577275.1U CN217060720U (en) | 2022-03-16 | 2022-03-16 | Shutter assembly for unmanned aerial vehicle cradle head |
Publications (1)
Publication Number | Publication Date |
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CN217060720U true CN217060720U (en) | 2022-07-26 |
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Family Applications (1)
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CN202220577275.1U Active CN217060720U (en) | 2022-03-16 | 2022-03-16 | Shutter assembly for unmanned aerial vehicle cradle head |
Country Status (1)
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CN (1) | CN217060720U (en) |
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2022
- 2022-03-16 CN CN202220577275.1U patent/CN217060720U/en active Active
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