CN214420723U - Suspension type unmanned aerial vehicle hanging cabin device - Google Patents

Suspension type unmanned aerial vehicle hanging cabin device Download PDF

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Publication number
CN214420723U
CN214420723U CN202120524184.7U CN202120524184U CN214420723U CN 214420723 U CN214420723 U CN 214420723U CN 202120524184 U CN202120524184 U CN 202120524184U CN 214420723 U CN214420723 U CN 214420723U
Authority
CN
China
Prior art keywords
aerial vehicle
unmanned aerial
gallows
sleeve
seat
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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
CN202120524184.7U
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Chinese (zh)
Inventor
曹磊
姜丝羽
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.)
Harbin Kumai Technology Co ltd
Original Assignee
Harbin Kumai 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 Harbin Kumai Technology Co ltd filed Critical Harbin Kumai Technology Co ltd
Priority to CN202120524184.7U priority Critical patent/CN214420723U/en
Application granted granted Critical
Publication of CN214420723U publication Critical patent/CN214420723U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model discloses a suspension type unmanned aerial vehicle hanging cabin device, including supporting the gallows, the inboard top of supporting the gallows is fixed to be installed and is hung the seat, the inboard of hanging the seat is installed and is kept watch on the casing, the front surface of keeping watch on the casing is installed and is made a video recording the main part, the front surface of keeping watch on the casing lies in the both sides of making a video recording the main part and sets up the guide seat of integral type, one side of guide seat is connected and is installed the round brush; when the device is when using, if the main part surface of making a video recording is infected with the dust, the clean structure of accessible is cleared up the surface of the main part of making a video recording, guarantee the definition of the picture of monitoring, facilitate the use, when the aircraft rises and falls, directly stop through supporting the gallows, if stop the speed of falling very fast, can lead to supporting the gallows and receive and collide with, it rocks and drops to probably lead to keeping watch on the casing, establish through the bottom cover at the support gallows and install the sleeve, shock-absorbing structure has been installed to telescopic bottom, stability when can guaranteeing the aircraft to rise and fall, the device's practicality has been improved.

Description

Suspension type unmanned aerial vehicle hanging cabin device
Technical Field
The utility model belongs to the technical field of the unmanned aerial vehicle hanging cabin, concretely relates to suspension type unmanned aerial vehicle hanging cabin device.
Background
The hanging cabin of the unmanned aerial vehicle is mainly divided into a missile hanging cabin and a special material transportation hanging cabin for operation according to the functions, and also comprises an onboard medium-sized or small-sized monitoring gyroscope hanging cabin which mainly starts the function of movable camera monitoring.
Present suspension type unmanned aerial vehicle hanging cabin device, when unmanned aerial vehicle used usually, suspension type hanging cabin can be installed to unmanned aerial vehicle's bottom, mainly start portable monitoring effect of making a video recording, when this hanging cabin used, there is the main part of making a video recording at the surface mounting who keeps watch on the casing, in this hanging cabin use, the aircraft is when flying, the surface of the main part of making a video recording is probably infected with debris, lead to making a video recording the unable monitoring of main part and use, influence the problem of the device's practicality, we propose a suspension type unmanned aerial vehicle hanging cabin device for this.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a suspension type unmanned aerial vehicle hanging cabin device, with the current suspension type unmanned aerial vehicle hanging cabin device who proposes in solving above-mentioned background art, when unmanned aerial vehicle uses usually, suspension type hanging cabin can be installed to unmanned aerial vehicle's bottom, mainly start portable monitoring effect of making a video recording, when this hanging cabin uses, surface mounting who keeps watch on the casing has the main part of making a video recording, in this hanging cabin use, the aircraft is when flying, the surface of the main part of making a video recording is probably infected with debris, lead to making a video recording the unable monitoring of main part and use, influence the problem of the practicality of the device.
In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides a suspension type unmanned aerial vehicle hanging cabin device, includes the support gallows, the fixed hanger that has installed in inboard top of support gallows, the inboard of hanger has installed the supervision casing, the main part of making a video recording has been installed to the front surface of supervision casing, the front surface of supervision casing is located the both sides of making a video recording the main part and has seted up the guide holder of integral type, one side of guide holder is connected and has been installed the round brush, one side the fixed servo motor of having installed of one end of guide holder, servo motor's one end is located the inboard rotation of guide holder and is connected with the lead screw, and the opposite side the inboard of guide holder is fixed and has been installed the gag lever post, the fixed nut that has installed of one end of round brush, the other end welded fastening of round brush has the cover seat.
Preferably, the bottom of the supporting hanger is sleeved with a sleeve, the bottom of the sleeve is connected with a gasket, and a damping sheet is connected between the sleeve and the gasket.
Preferably, the bottom of the supporting hanger is symmetrically provided with two sleeves, and the bottoms of the two sleeves are connected with gaskets through damping sheets.
Preferably, the damping sheet has an arc-shaped structure.
Preferably, the length of the roll brush is the same as the diameter of the imaging main body.
Preferably, one end of the rolling brush is rotatably arranged on the screw rod through a nut, and the other end of the rolling brush is sleeved on the limiting rod through a sleeve seat.
Compared with the prior art, the beneficial effects of the utility model are that:
(1) when the device is used, if the surface of the camera main body is contaminated with dust, the surface of the camera main body can be cleaned through the cleaning structure, the definition of a monitored picture is ensured, the device is convenient to use, and the practicability of the device is improved;
(2) and when the device used, when the aircraft rose and fell, directly stopped through supporting the gallows and fell, if the speed of stopping to fall is very fast, can lead to supporting the gallows to receive and collide with, probably lead to the monitoring shell to rock and drop, establish through the bottom cover at the support gallows and install the sleeve, shock-absorbing structure has been installed to telescopic bottom, stability when can guaranteeing the aircraft to rise and fall has improved the device's practicality.
Drawings
Fig. 1 is a schematic structural view of the present invention;
FIG. 2 is a schematic structural view of the guide base of the present invention;
fig. 3 is a right side view schematic structural diagram of the sleeve of the present invention;
in the figure: 1. a support hanger; 2. monitoring the housing; 3. a hanging seat; 4. a camera body; 5. a guide seat; 6. a sleeve; 7. a damping sheet; 8. a gasket; 9. a screw rod; 10. a servo motor; 11. a nut; 12. rolling and brushing; 13. a limiting rod; 14. and (4) sleeving a seat.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, 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.
Referring to fig. 1, fig. 2 and fig. 3, the present invention provides a technical solution: a suspension type unmanned aerial vehicle hanging cabin device comprises a supporting hanger 1, a hanging seat 3 is fixedly arranged at the top of the inner side of the supporting hanger 1, a monitoring shell 2 is arranged at the inner side of the hanging seat 3, a camera body 4 is arranged on the front surface of the monitoring shell 2, the front surface of the monitoring shell 2 is positioned at the two sides of the camera body 4 and is provided with an integrated guide seat 5, one side of the guide seat 5 is connected with a rolling brush 12, one end of the guide seat 5 at one side is fixedly provided with a servo motor 10, one end of the servo motor 10 is positioned at the inner side of the guide seat 5 and is rotatably connected with a screw rod 9, the inner side of the guide seat 5 at the other side is fixedly provided with a limiting rod 13, one end of the rolling brush 12 is fixedly provided with a nut 11, the other end of the rolling brush 12 is fixedly welded with a sleeve seat 14, when the device is used, if the surface of the camera body 4 is stained with dust, the surface of the camera body 4 can be cleaned through a cleaning structure, and the definition of a monitored picture can be ensured, in order to ensure the stability of the rolling brush 12, in this embodiment, preferably, one end of the rolling brush 12 is screwed on the screw rod 9 through a nut 11, and the other end of the rolling brush 12 is sleeved on the limiting rod 13 through a sleeve seat 14, so as to facilitate the rolling cleaning of the rolling brush 12.
For better buffering, in this embodiment, preferably, the shock absorbing plate 7 is an arc-shaped structure, the arc-shaped structure is convenient for deformation to generate a reaction force, for better cleaning, in this embodiment, preferably, the length of the rolling brush 12 is the same as the diameter of the main body 4 for image pickup, and the main body 4 for image pickup is convenient for the rolling brush 12 to clean, for better lifting, in this embodiment, preferably, the bottom of the support hanger 1 is sleeved with the sleeve 6, the bottom of the sleeve 6 is connected with the gasket 8, the shock absorbing plate 7 is connected between the sleeve 6 and the gasket 8, and the support hanger 1 is prevented from colliding with, in order to ensure the stability of the support hanger 1, in this embodiment, preferably, the bottom of the support hanger 1 is symmetrically provided with the two sleeves 6, and the bottoms of the two sleeves 6 are connected with the gasket 8 through the shock absorbing plate 7.
The utility model discloses a theory of operation and use flow: when the device is used, if the surface of the main camera body 4 is contaminated with dust, the surface of the main camera body 4 can be cleaned through a cleaning structure, a servo motor 10 converts electric energy into kinetic energy to drive a screw rod 9 to rotate during operation, a nut 11 screwed on the screw rod 9 moves to drive the roller brush 12 to move, the other end of the roller brush 12 is limited and mounted on a limiting rod 13 through a sleeve seat 14 to ensure the stability of the roller brush 12 in the use process, the main camera body 4 can be cleaned through the roller brush 12 to ensure the definition of a monitored picture, the use is convenient, and when the device is used, the airplane directly stops through the supporting hanger 1 when rising and falling, if stop the speed of falling very fast, can lead to supporting gallows 1 to receive to collide with, probably lead to hanger 3 to rock and drop, establish through the bottom cover that supports gallows 1 and install sleeve 6, gasket 8 has been installed through shock attenuation piece 7 in the bottom of sleeve 6, and when supporting gallows 1 atress, the crooked deformation of shock attenuation piece 7 produces certain reaction force, stability when guaranteeing the aircraft and rise and fall has improved the device's practicality.
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 suspension type unmanned aerial vehicle hanging cabin device, includes support gallows (1), the inboard top of supporting gallows (1) is fixed to be installed hanger (3), monitor casing (2) have been installed to the inboard of hanger (3), the front surface of monitoring casing (2) has been installed and has been made a video recording main part (4), its characterized in that: the front surface of the monitoring shell (2) is located on two sides of the camera main body (4) and is provided with an integrated guide seat (5), one side of the guide seat (5) is connected with a rolling brush (12), one side of the guide seat (5) is fixedly provided with a servo motor (10), one end of the servo motor (10) is located on the inner side of the guide seat (5) and is rotatably connected with a lead screw (9), the other side of the guide seat (5) is fixedly provided with a limiting rod (13), one end of the rolling brush (12) is fixedly provided with a nut (11), and the other end of the rolling brush (12) is fixedly welded with a sleeve seat (14).
2. A suspended unmanned aerial vehicle hangar apparatus as claimed in claim 1, wherein: the bottom of the supporting hanger (1) is sleeved with a sleeve (6), the bottom of the sleeve (6) is connected with a gasket (8), and a damping sheet (7) is connected between the sleeve (6) and the gasket (8).
3. A suspended unmanned aerial vehicle hangar apparatus as claimed in claim 2, wherein: the bottom of the supporting hanger (1) is symmetrically provided with two sleeves (6), and the bottoms of the two sleeves (6) are connected with gaskets (8) through damping sheets (7).
4. A suspended unmanned aerial vehicle hangar apparatus as claimed in claim 2, wherein: the shock absorption sheet (7) is of an arc-shaped structure.
5. A suspended unmanned aerial vehicle hangar apparatus as claimed in claim 1, wherein: the length of the rolling brush (12) is the same as the diameter of the camera body (4).
6. A suspended unmanned aerial vehicle hangar apparatus as claimed in claim 1, wherein: one end of the rolling brush (12) is rotatably arranged on the screw rod (9) through a nut (11), and the other end of the rolling brush (12) is sleeved on the limiting rod (13) through a sleeve seat (14).
CN202120524184.7U 2021-03-11 2021-03-11 Suspension type unmanned aerial vehicle hanging cabin device Expired - Fee Related CN214420723U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202120524184.7U CN214420723U (en) 2021-03-11 2021-03-11 Suspension type unmanned aerial vehicle hanging cabin device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202120524184.7U CN214420723U (en) 2021-03-11 2021-03-11 Suspension type unmanned aerial vehicle hanging cabin device

Publications (1)

Publication Number Publication Date
CN214420723U true CN214420723U (en) 2021-10-19

Family

ID=78073043

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202120524184.7U Expired - Fee Related CN214420723U (en) 2021-03-11 2021-03-11 Suspension type unmanned aerial vehicle hanging cabin device

Country Status (1)

Country Link
CN (1) CN214420723U (en)

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CF01 Termination of patent right due to non-payment of annual fee
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Granted publication date: 20211019