CN217199444U - Storage device for unmanned aerial vehicle based on coaxial double-paddle - Google Patents

Storage device for unmanned aerial vehicle based on coaxial double-paddle Download PDF

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Publication number
CN217199444U
CN217199444U CN202123401336.3U CN202123401336U CN217199444U CN 217199444 U CN217199444 U CN 217199444U CN 202123401336 U CN202123401336 U CN 202123401336U CN 217199444 U CN217199444 U CN 217199444U
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China
Prior art keywords
aerial vehicle
unmanned aerial
locating
coaxial double
groove
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CN202123401336.3U
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Chinese (zh)
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黄兴睿
杨卓
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Wuhan Yinci Innovation Uav Technology Co ltd
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Nanjing Yinci Huilai Aviation Technology Co ltd
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Abstract

The utility model discloses a storage device for unmanned aerial vehicle based on coaxial double-oar, be used for fixed unmanned aerial vehicle's fixed part on including the body and locating the body, fixed part is including locating the first unmanned aerial vehicle groove on the body, locating a plurality of first elastic poles in the first unmanned aerial vehicle inslot, locating the first stationary blade on the first elastic pole, locating the top cap of body top, locating the second unmanned aerial vehicle groove on the top cap, locating a plurality of second elastic poles in the second unmanned aerial vehicle inslot and locating the second stationary blade on the second elastic pole, the utility model discloses a set up body, fixed part, can carry out fixed protection to unmanned aerial vehicle to have the shockproof function, solved current unmanned aerial vehicle storage device and can't fixed unmanned aerial vehicle make unmanned aerial vehicle carry when accomodating unmanned aerial vehicle, cause the damage easily in the memory process.

Description

Storage device for unmanned aerial vehicle based on coaxial double-paddle
Technical Field
The utility model belongs to the technical field of storage device, especially, relate to a based on coaxial double-oar storage device for unmanned aerial vehicle.
Background
Unmanned aerial vehicle is called "unmanned aerial vehicle" for short, and the unmanned aerial vehicle application is extensive, goes up to civilian shooting under for military use investigation, and live now simultaneously, from media trade unmanned aerial vehicle more be indispensable equipment, unmanned aerial vehicle storage device is the device that is used for accomodating unmanned aerial vehicle, and the problem that prior art exists is: neglected the protection to unmanned aerial vehicle, unable fixed unmanned aerial vehicle makes unmanned aerial vehicle cause the damage easily carrying, the storage in-process.
SUMMERY OF THE UTILITY MODEL
Problem to prior art exists, the utility model provides a based on coaxial double-oar storage device for unmanned aerial vehicle possesses fixed unmanned aerial vehicle, takes precautions against earthquakes, prevents the advantage that falls, has solved current unmanned aerial vehicle and has caused the problem of damage easily in carrying, the storage process.
The utility model discloses a realize like this, a based on storage device for coaxial double-oar unmanned aerial vehicle, be used for fixed unmanned aerial vehicle's fixed part on including the body and locating the body, fixed part is including locating the first unmanned aerial vehicle groove on the body, locating a plurality of first elastic poles in the first unmanned aerial vehicle inslot, locating the first stationary blade on the first elastic pole, locating the top cap of body top, locating the second unmanned aerial vehicle groove on the top cap, locating a plurality of second elastic poles in the second unmanned aerial vehicle inslot and locating the second stationary blade on the second elastic pole.
As the utility model discloses preferred, be equipped with the bounce-off part on the body, the bounce-off part is including locating a plurality of bounce-off posts on the body, locating the inside first spring of bounce-off post, locating the gas storage post of first spring bottom and locating the air vent on gas storage post top, gas storage post and bounce-off post sliding connection.
As the utility model discloses it is preferred, be equipped with a plurality of fixed lift flip parts on the body, fixed lift flip part is including locating the lifter plate of body one side, locating a plurality of columns of revolution of lifter plate upper end, locating a plurality of lift grooves on the lifter plate, locating first limiting plate on the lift groove, locating a plurality of spacing of lifter plate lower part and locating the second limiting plate on the spacing.
As the utility model discloses preferred, be equipped with a plurality of automatic parts of locking on the body, the automatic part of locking is including locating the lock post of lifter plate lower extreme, locating the lock tooth on the lock post, locating the lock hole of lock tooth below, locating the lock core at lock hole middle part, locating the second spring of lock core one side, locating the push pedal of lock core opposite side, locating the inside third spring of push pedal, locating the baffle of push pedal one side, locating the push rod on the baffle and locating the traveller of push rod one side, the push rod runs through the baffle both sides and is connected in the push pedal traveller respectively.
As the utility model discloses preferred, be equipped with the supporting component on the body, the supporting component is including locating the support ring on body one side, locating the double-layered hook of support ring top, locating the support stock on the double-layered hook and locating the solid fixed ring of support stock upper end, gu fixed ring links firmly with the top cap.
As the utility model discloses it is preferred, all be equipped with a plurality of anti-falling feet that are used for preventing unmanned aerial vehicle damage on the turning of body and top cap.
Compared with the prior art, the beneficial effects of the utility model are as follows:
1. the utility model discloses a set up fixed part, can fix the protection to unmanned aerial vehicle to have shockproof function.
2. The utility model discloses a set up the part of bounceing, earlier upwards bounce avoids causing the damage to unmanned aerial vehicle when can making the top cap open.
3. The utility model discloses a set up fixed lift flip part, can make the top cap upwards rise and can open, can protect unmanned aerial vehicle to receive the damage.
4. The utility model discloses a set up a plurality of automatic parts of locking, can make the top cap lock automatically when carrying out the closure, avoid kick-backing to cause the damage to unmanned aerial vehicle.
5. The utility model discloses a set up the supporting component, support when can making the top cap open, avoid the top cap whereabouts to cause the damage to unmanned aerial vehicle.
6. The utility model discloses a setting prevents falling the foot, can make storage device protect unmanned aerial vehicle when receiving the collision, avoids unmanned aerial vehicle to cause the damage.
Drawings
Fig. 1 is a schematic structural diagram provided in an embodiment of the present invention;
fig. 2 is a top view provided by an embodiment of the present invention;
fig. 3 is a cross-sectional view taken at a-a in accordance with an embodiment of the present invention;
fig. 4 is an enlarged view of F in fig. 3 according to an embodiment of the present invention;
fig. 5 is a left side view provided by an embodiment of the present invention;
fig. 6 is an enlarged view of Q in fig. 5 provided by the embodiment of the present invention;
fig. 7 is a cross-sectional view at C-C provided by an embodiment of the present invention;
fig. 8 is an enlarged view of B in fig. 6 according to an embodiment of the present invention.
In the figure: 1. a body; 2. a first drone sink; 3. a first resilient lever; 4. a first fixing sheet; 5. a top cover; 6. a second drone sink; 7. a second elastic rod; 8. a second fixing sheet; 21. ejecting the column; 22. a first spring; 23. a gas storage column; 24. a vent hole; 31. a lifting plate; 32. a spin column; 33. a lifting groove; 34. a first limit plate; 35. a limiting strip; 36. a second limiting plate; 41. a lock cylinder; 42. locking teeth; 43. locking holes; 44. a lock cylinder; 45. a second spring; 46. pushing the plate; 47. a third spring; 48. a baffle plate; 49. a push rod; 50. a traveler; 51. a support ring; 52. clamping a hook; 53. a long support rod; 54. a fixing ring; 61. prevent falling the foot.
Detailed Description
For further understanding the contents, features and effects of the present invention, the following embodiments will be illustrated in detail with reference to the accompanying drawings.
The structure of the present invention will be described in detail with reference to the accompanying drawings.
As shown in fig. 1 to 8, the embodiment of the utility model provides a based on storage device for coaxial double-oar unmanned aerial vehicle, include body 1 and locate the fixed part that is used for fixed unmanned aerial vehicle on the body 1, the fixed part is including locating first unmanned aerial vehicle groove 2 on the body 1, locating a plurality of first elastic rods 3 in first unmanned aerial vehicle groove 2, locating first stationary blade 4 on first elastic rod 3, locating top cap 5 above body 1, locating second unmanned aerial vehicle groove 6 on top cap 5, locating a plurality of second elastic rods 7 in second unmanned aerial vehicle groove 6 and locating second stationary blade 8 on second elastic rods 7.
Referring to fig. 4, the body 1 is provided with a bounce component, the bounce component includes a plurality of bounce columns 21 arranged on the body 1, a first spring 22 arranged inside the bounce column 21, an air storage column 23 arranged at the bottom end of the first spring 22, and an air vent 24 arranged at the top end of the air storage column 23, and the air storage column 23 is connected with the bounce columns 21 in a sliding manner.
Adopt above-mentioned scheme: through setting up the part of bounceing, earlier upwards bounce avoids causing the damage to unmanned aerial vehicle when can making top cap 5 open.
Referring to fig. 6, a plurality of fixed flip-up components are disposed on the body 1, and the fixed flip-up components include a lifting plate 31 disposed on one side of the body 1, a plurality of rotating posts 32 disposed on an upper end of the lifting plate 31, a plurality of lifting grooves 33 disposed on the lifting plate 31, a first limiting plate 34 disposed on the lifting grooves 33, a plurality of limiting strips 35 disposed on a lower portion of the lifting plate 31, and a second limiting plate 36 disposed on the limiting strips 35.
The scheme is adopted: through setting up fixed lift flip part, can make top cap 5 upwards rise and can open, can protect unmanned aerial vehicle to receive the damage.
Referring to fig. 8, the body 1 is provided with a plurality of automatic locking components, the automatic locking components include a lock cylinder 41 arranged at the lower end of the lifting plate 31, a lock tooth 42 arranged on the lock cylinder 41, a lock hole 43 arranged below the lock tooth 42, a lock core 44 arranged in the middle of the lock hole 43, a second spring 45 arranged at one side of the lock core 44, a push plate 46 arranged at the other side of the lock core 44, a third spring 47 arranged inside the push plate 46, a baffle plate 48 arranged at one side of the push plate 46, a push rod 49 arranged on the baffle plate 48, and a sliding column 50 arranged at one side of the push rod 49, wherein the push rod 49 penetrates through two sides of the baffle plate 48 and is respectively connected with the sliding column 50 of the push plate 46.
Adopt above-mentioned scheme: set up a plurality of automatic parts of locking, can make top cap 5 automatic locking when carrying out the closure, avoid kick-backing to cause the damage to unmanned aerial vehicle.
Referring to fig. 7, the body 1 is provided with a support member, the support member includes a support ring 51 disposed on one side of the body 1, a clamp hook 52 disposed above the support ring 51, a long support rod 53 disposed on the clamp hook 52, and a fixing ring 54 disposed at an upper end of the long support rod 53, and the fixing ring 54 is fixedly connected to the top cover 5.
Adopt above-mentioned scheme: through setting up the supporting component, support when can making top cap 5 open, avoid top cap 5 whereabouts to cause the damage to unmanned aerial vehicle.
Referring to fig. 1, a plurality of falling-preventing legs 61 for preventing the damage of the unmanned aerial vehicle are provided on corners of the body 1 and the top cover 5.
Adopt above-mentioned scheme: set up and prevent falling foot 61, can make storage device protect unmanned aerial vehicle when receiving the collision, avoid unmanned aerial vehicle to cause the damage.
The utility model discloses a theory of operation:
when the unmanned aerial vehicle locking device is used, the unmanned aerial vehicle is firstly placed into the first unmanned aerial vehicle slot 2 to enable the first fixing piece 4 to be in contact with the unmanned aerial vehicle, then the clamping hook 52 is removed from the support ring 51, the top cover 5 is turned over by 90 degrees to enable the top cover 5 to be matched with the bouncing post 21, then the top cover 5 is slightly pressed to enable the top cover 5 to descend with the bouncing post 21, the lifting plate 31 is driven to descend, the lifting plate 31 drives the locking post 41 and the locking tooth 42 to descend, the locking tooth 42 is contacted with the lock core 44 when descending to a certain height, the locking tooth 42 continues to descend to push the lock core 44 to one side, when the locking tooth 42 completely descends to the bottom, the lock core 44 is automatically locked due to rebounding of the second spring 45, the first fixing piece 4 and the second fixing piece 8 can be in contact with the side wall of the unmanned aerial vehicle, and the unmanned aerial vehicle can have a shockproof effect due to the existence of the first elastic rod 3 and the second elastic rod 7.
In conclusion: this be based on coaxial double-oar storage device for unmanned aerial vehicle is through setting up body 1 and locating the fixed part that is used for fixed unmanned aerial vehicle on the body 1, has solved unable fixed unmanned aerial vehicle and has made unmanned aerial vehicle carry, the storage in-process causes the problem of damage easily.
It is noted that, herein, relational terms such as first and second, and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus.
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 based on coaxial double-oar storage device for unmanned aerial vehicle, includes body (1) and locates the fixed part that is used for fixed unmanned aerial vehicle on body (1), its characterized in that: the fixing part comprises a first unmanned aerial vehicle groove (2) arranged on the body (1), a plurality of first elastic rods (3) arranged in the first unmanned aerial vehicle groove (2), a first fixing piece (4) arranged on the first elastic rods (3), a top cover (5) arranged above the body (1), a second unmanned aerial vehicle groove (6) arranged on the top cover (5), a plurality of second elastic rods (7) arranged in the second unmanned aerial vehicle groove (6) and a second fixing piece (8) arranged on the second elastic rods (7).
2. The containing device based on the coaxial double-paddle unmanned aerial vehicle as claimed in claim 1, wherein: be equipped with the part of bounceing on body (1), the part of bounceing is including locating a plurality of posts of bounceing (21) on body (1), locating the inside first spring (22) of the post of bounceing (21), locating gas storage post (23) of first spring (22) bottom and locating air vent (24) on gas storage post (23) top, gas storage post (23) and the post of bounceing (21) sliding connection.
3. The containing device based on the coaxial double-paddle unmanned aerial vehicle as claimed in claim 1, wherein: be equipped with a plurality of fixed lift flip parts on body (1), fixed lift flip part is including locating lifter plate (31) of body (1) one side, locating a plurality of column spinner (32) of lifter plate (31) upper end, locating a plurality of lift groove (33) on lifter plate (31), locating first limiting plate (34) on lift groove (33), locating a plurality of spacing (35) of lifter plate (31) lower part and locating second limiting plate (36) on spacing (35).
4. The containing device based on coaxial double-oar for unmanned aerial vehicle of claim 1, characterized in that: the automatic locking device is characterized in that the body (1) is provided with a plurality of automatic locking components, the automatic locking components comprise a lock cylinder (41) arranged at the lower end of the lifting plate (31), locking teeth (42) arranged on the lock cylinder (41), a lock hole (43) arranged below the locking teeth (42), a lock cylinder (44) arranged in the middle of the lock hole (43), a second spring (45) arranged on one side of the lock cylinder (44), a push plate (46) arranged on the other side of the lock cylinder (44), a third spring (47) arranged inside the push plate (46), a baffle (48) arranged on one side of the push plate (46), a push rod (49) arranged on the baffle (48) and a sliding column (50) arranged on one side of the push rod (49), and the push rod (49) penetrates through the two sides of the baffle (48) and is connected with the sliding column (50) of the push plate (46) respectively.
5. The containing device based on the coaxial double-paddle unmanned aerial vehicle as claimed in claim 1, wherein: the support device is characterized in that a support component is arranged on the body (1), the support component comprises a support ring (51) arranged on one side of the body (1), a clamp hook (52) arranged above the support ring (51), a support long rod (53) arranged on the clamp hook (52) and a fixing ring (54) arranged at the upper end of the support long rod (53), and the fixing ring (54) is fixedly connected with the top cover (5).
6. The containing device based on the coaxial double-paddle unmanned aerial vehicle as claimed in claim 1, wherein: all be equipped with a plurality of anti-falling feet (61) that are used for preventing unmanned aerial vehicle damage on the corner of body (1) and top cap (5).
CN202123401336.3U 2021-12-30 2021-12-30 Storage device for unmanned aerial vehicle based on coaxial double-paddle Active CN217199444U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202123401336.3U CN217199444U (en) 2021-12-30 2021-12-30 Storage device for unmanned aerial vehicle based on coaxial double-paddle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202123401336.3U CN217199444U (en) 2021-12-30 2021-12-30 Storage device for unmanned aerial vehicle based on coaxial double-paddle

Publications (1)

Publication Number Publication Date
CN217199444U true CN217199444U (en) 2022-08-16

Family

ID=82788552

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202123401336.3U Active CN217199444U (en) 2021-12-30 2021-12-30 Storage device for unmanned aerial vehicle based on coaxial double-paddle

Country Status (1)

Country Link
CN (1) CN217199444U (en)

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GR01 Patent grant
GR01 Patent grant
TR01 Transfer of patent right

Effective date of registration: 20221128

Address after: 430000 South taizihu innovation Valley Qidi Xiexin science and Technology Innovation Park, Wuhan Economic and Technological Development Zone, Hubei Province (qdxx-q20138)

Patentee after: Wuhan yinci innovation UAV Technology Co.,Ltd.

Address before: Room 309-26, building A10, No. 9, Kechuang Avenue, intelligent manufacturing Industrial Park (Zhihe Park), Jiangbei new area, Nanjing, Jiangsu 210000

Patentee before: Nanjing yinci Huilai Aviation Technology Co.,Ltd.

TR01 Transfer of patent right