CN208897339U - A kind of unmanned plane quick despatch structure - Google Patents

A kind of unmanned plane quick despatch structure Download PDF

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Publication number
CN208897339U
CN208897339U CN201821591748.3U CN201821591748U CN208897339U CN 208897339 U CN208897339 U CN 208897339U CN 201821591748 U CN201821591748 U CN 201821591748U CN 208897339 U CN208897339 U CN 208897339U
Authority
CN
China
Prior art keywords
fixedly connected
plate
wall
unmanned plane
spring
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
CN201821591748.3U
Other languages
Chinese (zh)
Inventor
吴岳逢
许楚辉
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Shenzhen Junhua Uav Technology Co Ltd
Original Assignee
Shenzhen Junhua Uav Technology Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Shenzhen Junhua Uav Technology Co Ltd filed Critical Shenzhen Junhua Uav Technology Co Ltd
Priority to CN201821591748.3U priority Critical patent/CN208897339U/en
Application granted granted Critical
Publication of CN208897339U publication Critical patent/CN208897339U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model discloses a kind of unmanned plane quick despatch structures, including drone body, the lower end of the drone body is equipped with device slot, described device slot is fixedly connected by two fixed mechanisms and camera, the lower end of the drone body is fixedly connected with multiple stabilizer blades, and the lower end of the stabilizer blade is fixedly connected with mounting plate.The structure design of the utility model is reasonable, can be rapidly performed by disassembly installation, and can reduce decline bring impact force.

Description

A kind of unmanned plane quick despatch structure
Technical field
The utility model relates to rapid handling technique field more particularly to a kind of unmanned plane quick despatch structures.
Background technique
Referred to as " unmanned plane ", english abbreviation is " UAV " to UAV, is using radio robot and to provide for oneself The not manned aircraft of presetting apparatus manipulation, or fully or intermittently automatically operated by car-mounted computer.
For existing unmanned plane in installation camera, process is complex, when needing to disassemble in camera, causes to tear open Difficulty is unloaded, quickly it can not be dismantled, while the impact force of unmanned plane decline is larger, is easily damaged camera.
Utility model content
Purpose of the utility model is to solve disadvantages existing in the prior art, and a kind of unmanned plane proposed is quick Construct for handling can be rapidly performed by disassembly installation, and can reduce decline bring impact force.
To achieve the goals above, the utility model adopts the technical scheme that
The lower end of a kind of unmanned plane quick despatch structure, including drone body, the drone body is equipped with device slot, Described device slot is fixedly connected by two fixed mechanisms and camera, and the lower end of the drone body is fixedly connected with multiple Foot, the lower end of the stabilizer blade are fixedly connected with mounting plate, and the lower end of the mounting plate is equipped with damping.
Preferably, the fixed mechanism includes the lock chamber being arranged in drone body, on the inner wall of the lock chamber Push plate is slidably connected, the lower end of the push plate runs through the inner wall of lock chamber and extends to outside, the push plate and unmanned plane sheet Body is slidably connected, and the side wall of the push plate is fixedly connected with spacer pin, and the spacer pin runs through lock chamber far from one end of push plate Inner wall and extend in device slot, the inner wall of the lock chamber is fixedly connected with the first spring, and first spring is far from solid The one end for determining cavity wall is fixedly connected on the side wall of push plate.
Preferably, the damping includes the bottom plate that mounting plate lower end is arranged in, and the upper end of the bottom plate is equipped with groove, It is equipped with sliding slot on the opposite inner wall of the groove, is slidably connected in the sliding slot there are two slide plate, two slide plates are opposite Side wall be fixedly connected with third spring, the third spring is fixedly connected on the inner wall of groove far from one end of slide plate, two The opposite side wall of a slide plate is rotatably connected to rotor plate, and the rotor plate is rotatably connected on installation far from one end of slide plate The lower end of plate, the interior bottom of the groove are fixedly connected with telescopic rod, and the telescopic end of the telescopic rod is fixedly connected on mounting plate Lower end, be arranged with second spring on the telescopic rod, the both ends of the second spring are respectively fixedly connected under mounting plate On end and the interior bottom of groove.
Preferably, the side wall of the camera is equipped with the limiting slot matched with spacer pin.
Preferably, the camera is equipped with shield.
Preferably, the lower end of the bottom plate is equipped with rubber pad.
The utility model has the beneficial effects that
1, pull two push plates to be moved in the opposite direction, push plate is mobile to drive spacer pin mobile, keeps spacer pin de- From in limiting slot, camera can quickly be disassembled;
2, when drone body is landed, downward impact force is generated, second spring and third spring-compressed are made, it is carried out Buffering, is then resetted, and impact force is reduced, and prevents camera impaired.
Detailed description of the invention
Fig. 1 be the utility model proposes a kind of unmanned plane quick despatch structure structural schematic diagram;
Fig. 2 be the utility model proposes a kind of unmanned plane quick despatch structure A at enlarged drawing.
In figure: 1 drone body, 2 first springs, 3 stabilizer blades, 4 mounting plates, 5 cameras, 6 spacer pins, 7 push plates, 8 rotor plates, 9 second springs, 10 telescopic rods, 11 sliding slots, 12 grooves, 13 slide plates, 14 third springs.
Specific embodiment
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole Embodiment.
Referring to Fig.1-2, a kind of unmanned plane quick despatch structure, including drone body 1, the lower end of drone body 1 are set Have a device slot, device slot by two fixed mechanisms be fixedly connected with camera 5, pull two push plates 7 to carry out in the opposite direction Mobile, push plate 7 is mobile to drive spacer pin 6 mobile, is detached from spacer pin 6 in limiting slot, camera can quickly be disassembled, The lower end of drone body 1 is fixedly connected with multiple stabilizer blades 3, and the lower end of stabilizer blade 3 is fixedly connected with mounting plate 4, under mounting plate 4 End is equipped with damping and generates downward impact force when drone body 1 is landed, and presses second spring 9 and third spring 14 Contracting, buffers it, is then resetted, and reduces impact force, prevents camera 5 impaired.
Fixed mechanism includes the lock chamber being arranged in drone body 1, slidably connects push plate on the inner wall of lock chamber 7, the width of 7 lower section of push plate is less than the width of upper section, and the lower end of push plate 7 runs through the inner wall of lock chamber and extends to outside, push plate 7 It is slidably connected with drone body 1, the side wall of push plate 7 is fixedly connected with spacer pin 6, and spacer pin 6 runs through far from one end of push plate 7 The inner wall of lock chamber simultaneously extends in device slot, and the inner wall of lock chamber is fixedly connected with the first spring 2, and the first spring 2 is far from solid The one end for determining cavity wall is fixedly connected on the side wall of push plate 7, can quickly be dismantled to it, and damping includes setting Bottom plate in 4 lower end of mounting plate, the upper end of bottom plate are equipped with groove 12, are equipped with sliding slot 11, sliding slot on the opposite inner wall of groove 12 It is slidably connected in 11 there are two slide plate 13, two opposite side walls of slide plate 13 are fixedly connected with third spring 14, third spring 14 One end far from slide plate 13 is fixedly connected on the inner wall of groove, and two opposite side walls of slide plate 13 are rotatably connected to rotor plate 8, rotor plate 8 is rotatably connected on the lower end of mounting plate 4 far from one end of slide plate 13, and the interior bottom of groove 12 is fixedly connected with flexible Bar 10, the telescopic end of telescopic rod 10 are fixedly connected on the lower end of mounting plate 4, and second spring 9, the second bullet are arranged on telescopic rod 10 The both ends of spring 9 are respectively fixedly connected on the lower end of mounting plate 4 and the interior bottom of groove 12, are reduced downward impact force, are prevented Camera 5 is impaired, and the side wall of camera 5 is equipped with the limiting slot matched with spacer pin 6, plays fixed effect, and camera 5 is equipped with anti- Shield plays the role of protecting camera 5, and the lower end of bottom plate is equipped with rubber pad, has the function of buffering.
In the utility model, two push plates 7 is pulled to be moved in the opposite direction, push plate 7 is mobile to drive spacer pin 6 to move It is dynamic, it is detached from spacer pin 6 in limiting slot, camera can be disassembled, when drone body 1 is landed, generate downward impact Power compresses second spring 9 and third spring 14, buffers to it, then resetted, reduces impact force, prevent camera 5 It is impaired.
More than, the only preferable specific embodiment of the utility model, but the protection scope of the utility model is not limited to In this, anyone skilled in the art within the technical scope disclosed by the utility model, according to the utility model Technical solution and its utility model design be subject to equivalent substitution or change, should all cover the protection scope of the utility model it It is interior.

Claims (6)

1. a kind of unmanned plane quick despatch structure, including drone body (1), which is characterized in that the drone body (1) Lower end is equipped with device slot, and described device slot is fixedly connected and camera (5), the drone body (1) by two fixed mechanisms Lower end be fixedly connected with multiple stabilizer blades (3), the lower end of the stabilizer blade (3) is fixedly connected with mounting plate (4), the mounting plate (4) lower end is equipped with damping.
2. a kind of unmanned plane quick despatch structure according to claim 1, which is characterized in that the fixed mechanism includes setting The lock chamber on drone body (1) is set, is slidably connected on the inner wall of the lock chamber push plate (7), the push plate (7) Lower end runs through the inner wall of lock chamber and extends to outside, and the push plate (7) is slidably connected with drone body (1), the push plate (7) side wall is fixedly connected with spacer pin (6), and the spacer pin (6) runs through the inner wall of lock chamber simultaneously far from the one end of push plate (7) It extends in device slot, the inner wall of the lock chamber is fixedly connected with the first spring (2), and first spring (2) is far from fixed One end of cavity wall is fixedly connected on the side wall of push plate (7).
3. a kind of unmanned plane quick despatch structure according to claim 1, which is characterized in that the damping includes setting The bottom plate in mounting plate (4) lower end is set, the upper end of the bottom plate is equipped with groove (12), on the opposite inner wall of the groove (12) Equipped with sliding slot (11), being slidably connected in the sliding slot (11), there are two slide plate (13), the opposite side walls of two slide plates (13) It is fixedly connected with third spring (14), the third spring (14) is fixedly connected on the inner wall of groove far from the one end of slide plate (13) On, two opposite side walls of the slide plate (13) are rotatably connected to rotor plate (8), and the rotor plate (8) is far from slide plate (13) One end be rotatably connected on the lower ends of mounting plate (4), the interior bottom of the groove (12) is fixedly connected with telescopic rod (10), described The telescopic end of telescopic rod (10) is fixedly connected on the lower end of mounting plate (4), is arranged with second spring on the telescopic rod (10) (9), the both ends of the second spring (9) are respectively fixedly connected on the lower end of mounting plate (4) and the interior bottom of groove (12).
4. a kind of unmanned plane quick despatch structure according to claim 1, which is characterized in that the side wall of the camera (5) Equipped with the limiting slot matched with spacer pin (6).
5. a kind of unmanned plane quick despatch structure according to claim 1, which is characterized in that the camera (5) is equipped with Shield.
6. a kind of unmanned plane quick despatch structure according to claim 3, which is characterized in that the lower end of the bottom plate is equipped with Rubber pad.
CN201821591748.3U 2018-09-28 2018-09-28 A kind of unmanned plane quick despatch structure Expired - Fee Related CN208897339U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201821591748.3U CN208897339U (en) 2018-09-28 2018-09-28 A kind of unmanned plane quick despatch structure

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201821591748.3U CN208897339U (en) 2018-09-28 2018-09-28 A kind of unmanned plane quick despatch structure

Publications (1)

Publication Number Publication Date
CN208897339U true CN208897339U (en) 2019-05-24

Family

ID=66574120

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201821591748.3U Expired - Fee Related CN208897339U (en) 2018-09-28 2018-09-28 A kind of unmanned plane quick despatch structure

Country Status (1)

Country Link
CN (1) CN208897339U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110963032A (en) * 2019-11-29 2020-04-07 江苏金猫机器人科技有限公司 Robot capable of collecting information at multiple angles

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110963032A (en) * 2019-11-29 2020-04-07 江苏金猫机器人科技有限公司 Robot capable of collecting information at multiple angles

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GR01 Patent grant
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20190524

Termination date: 20190928

CF01 Termination of patent right due to non-payment of annual fee