CN208325628U - A kind of mapping unmanned plane of self-protection - Google Patents

A kind of mapping unmanned plane of self-protection Download PDF

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Publication number
CN208325628U
CN208325628U CN201820494448.7U CN201820494448U CN208325628U CN 208325628 U CN208325628 U CN 208325628U CN 201820494448 U CN201820494448 U CN 201820494448U CN 208325628 U CN208325628 U CN 208325628U
Authority
CN
China
Prior art keywords
drone body
fixed link
wing
fixedly connected
support frame
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
CN201820494448.7U
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Chinese (zh)
Inventor
黄汕
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.)
Qingyuan Jujin Technology Co Ltd
Original Assignee
Qingyuan Jujin 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 Qingyuan Jujin Technology Co Ltd filed Critical Qingyuan Jujin Technology Co Ltd
Priority to CN201820494448.7U priority Critical patent/CN208325628U/en
Application granted granted Critical
Publication of CN208325628U publication Critical patent/CN208325628U/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 mapping unmanned planes of self-protection; including casing assembly and guard assembly; the casing assembly includes drone body, propeller, connection shell, support frame, fixed link and wing; the wing is located at the right surface of the drone body; and it is fixedly connected with the drone body; the connection shell is located at the right end of the wing, and is fixedly connected with the wing;Sound equipment plays the cry of eagle by external USB flash disk to drive the birds around drone body; birds are avoided to contact drone body; achieve the effect that protect drone body; drone body is when from raked floor or from airborne to ground; vibration and drone body self weight when propeller rotates can cause to impact to drone body; drone body buffers above-mentioned vibration by piston and spring clip and achievees the effect that protect drone body, brings convenience to staff.

Description

A kind of mapping unmanned plane of self-protection
Technical field
The utility model belongs to air vehicle technique field, and in particular to a kind of mapping unmanned plane of self-protection.
Background technique
Mapping unmanned plane is the not manned aircraft manipulated using radio robot and the presetting apparatus provided for oneself, or Person fully or is intermittently automatically operated by car-mounted computer, and mapping unmanned plane will be at information by flying shooting in space Reason is sent to computer, effectively accurately carries out mapping operations.
Unmanned plane during flying to it is aerial when, be easy to receive the attack of the animal with flight performance such as birds, unmanned plane cost The damage of valuableness, unmanned plane causes influence to the economy of staff and job schedule.
Utility model content
The purpose of this utility model is to provide a kind of mapping unmanned planes of self-protection, to solve in above-mentioned background technique The unmanned plane during flying of proposition to it is aerial when, be easy to receive the attack of the animal with flight performance such as birds, unmanned plane cost is high It is expensive, the problem of damage of unmanned plane causes influence to the economy of staff and job schedule.
To achieve the above object, the utility model provides the following technical solutions: a kind of mapping unmanned plane of self-protection, Be characterized in that: including casing assembly and guard assembly, the casing assembly includes drone body, propeller, connection shell, support Frame, fixed link and wing, the wing is located at the right surface of the drone body, and fixes and connect with the drone body It connects, the connection shell is located at the right end of the wing, and is fixedly connected with the wing, and the propeller is located at the connection shell Upper end, and be sequentially connected with the connection shell, the fixed link is located at the bottom end of the drone body, and with it is described nobody Machine ontology is fixedly connected, and support frame as described above is located at the lower section of the fixed link, and is fixedly connected with the fixed link, it is described nobody Machine ontology and external power supply are electrically connected, and guard assembly includes sound equipment, spring(-supported) mount, connection frame and rubber sleeve, and the sound equipment is located at The upper surface of the drone body, and be fixedly connected with the drone body, the rubber sleeve is located at support frame as described above Lateral wall, and be adhesively fixed with support frame as described above, the spring(-supported) mount is located at the lower end of the fixed link, and solid with the fixed link Fixed connection, the connection frame is located at the lateral wall of support frame as described above, and is fixedly connected with the fixed link, support frame as described above and institute It states fixed link to be fixedly connected by described, the sound equipment and external power supply are electrically connected.
Preferably, the quantity of the wing is four, and four wings are symmetrically distributed in the drone body Outer surface.
Preferably, the quantity of the fixed link is two, and two fixed links are symmetrically distributed in the unmanned plane The bottom end of ontology.
Preferably, the first cavity is offered inside the connection frame, is fixedly installed piston inside first cavity, institute It states support frame and the connection frame is slidably connected by the piston.
Preferably, the second cavity is offered inside the connection shell, is fixedly installed motor inside second cavity, institute It states and is provided with rotation axis on motor, the motor and the propeller are sequentially connected by the rotation axis.
Preferably, there is USB interface on the sound equipment.
Compared with prior art, the utility model has the beneficial effects that sound equipment is fixedly installed in drone body, sound It rings and the cry of eagle is played to drive the birds around drone body by external USB flash disk, birds is avoided to contact drone body, Achieve the effect that protect drone body, be fixedly installed spring(-supported) mount in drone body, drone body is from ground It rises or when from airborne to ground, vibration and drone body self weight when propeller rotates can make drone body At impact, drone body buffers above-mentioned vibration by piston and spring clip and achievees the effect that protect drone body, gives work Personnel bring convenience.
Detailed description of the invention
Fig. 1 is the structural schematic diagram of the utility model;
Fig. 2 is the landing gear structure schematic diagram in the utility model;
Fig. 3 is the shock absorber structure schematic diagram in the utility model;
In figure: 10- casing assembly, 11- drone body, 12- propeller, 13- connection shell, 14- support frame, 15- are fixed Bar, 16- wing, 20- guard assembly, 21- sound equipment, 22- spring(-supported) mount, 23- connection frame, 24- rubber sleeve.
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.Based on the embodiments of the present invention, those of ordinary skill in the art are without making creative work Every other embodiment obtained, fall within the protection scope of the utility model.
Fig. 1-3 is please referred to, the utility model provides a kind of technical solution: a kind of mapping unmanned plane of self-protection, including Casing assembly 10 and guard assembly 20, casing assembly 10 include drone body 11, propeller 12, connection shell 13, support frame 14, Fixed link 15 and wing 16, wing 16 is located at the right surface of drone body 11, and is fixedly connected with drone body 11, connection Shell 13 is located at the right end of wing 16, and is fixedly connected with wing 16, propeller 12 be located at connection shell 13 upper end, and with connect shell 13 transmission connections, fixed link 15 is located at the bottom end of drone body 11, and is fixedly connected with drone body 11, and support frame 14 It is fixedly connected in the lower section of fixed link 15, and with fixed link 15, drone body 11 and external power supply are electrically connected, guard assembly 20 include sound equipment 21, spring(-supported) mount 22, connection frame 23 and rubber sleeve 24, and sound equipment 21 is located at the upper surface of drone body 11, and with Drone body 11 is fixedly connected, and rubber sleeve 24 is located at the lateral wall of support frame 14, and is adhesively fixed with support frame 14, spring(-supported) mount 22 are located at the lower end of fixed link 15, and are fixedly connected with fixed link 15, and connection frame 23 is located at the lateral wall of support frame 14, and with consolidate Fixed pole 15 is fixedly connected, and support frame 14 is fixedly connected with fixed link 15 by 23, and sound equipment 21 and external power supply are electrically connected.
In the present embodiment, it is internally provided with motor in connection shell 13, motor rotation drives the rotation axis rotation of motor in turn Propeller 12 is driven to rotate, the model kv950 of motor.
In the present embodiment, drone body 11 is placed on job site by staff, and staff inserts external USB flash disk Enter sound equipment 21, open sound equipment 21, manipulation drone body 11 is taken off, and spring(-supported) mount 22 and connection are provided in drone body 11 Frame 23 is provided with piston in connection frame 23, and drone body 11 is by piston and spring clip 22 come 12 bring of damping coil paddle Vibration has the function that protection drone body 11, drone body 11 clap space environment by the camera of lower section It takes the photograph and handles, after drone body 11 is surveyed and drawn, staff manipulates drone body 11 and declines, in drone body 11 Rubber sleeve 24 is set, and drone body 11 is buffered self weight when drone body 11 drop to ground by rubber sleeve 24, reached To the effect protected to drone body 11.
Further, the quantity of wing 16 is four, and four wings 16 are symmetrically distributed in the outer of drone body 11 Surface.
In the present embodiment, wing 16 is uniformly distributed the outer surface with drone body 11, when running drone body 11 Center of gravity does not deviate by, and keeps the operation of drone body 11 more stable.
Further, the quantity of fixed link 15 is two, and two fixed links 15 are symmetrically distributed in drone body 11 Bottom end.
In the present embodiment, spring(-supported) mount 23 is fixedly installed in fixed link 15, drone body 11 is buffered by spring clip 22 Vibration when drone body 11 is run, reaches the protective effect to drone body 11.
Further, the first cavity is offered inside connection frame 23, and piston, support frame are fixedly installed inside the first cavity 14 and connection frame 23 be slidably connected by piston.
In the present embodiment, piston can buffer speed bring pressure when being self-possessed and decline when drone body 11 is landed Power reaches the protective effect to drone body 11.
Further, it connects inside shell 13 and offers the second cavity, be fixedly installed motor inside the second cavity, on motor Rotation axis, motor and propeller 12 is provided with to be sequentially connected by rotation axis.
In the present embodiment, staff, which manipulates drone body 11, rotates propeller 12 respectively, realizes drone body The function of 11 lifting, steering and hovering.
Further, there is USB interface on sound equipment 21.
In the present embodiment, work people will be copied outside sound source into external USB flash disk, and USB flash disk is inserted into sound equipment, make sound equipment can be with It plays outside sound source and drives birds, avoid birds from contacting drone body 11, reach the protective effect to drone body 11.
The working principle and process for using of the utility model: after the utility model installs, staff is by unmanned plane Ontology 11 is placed on job site, and relatively smoothly external USB flash disk is inserted into sound equipment 21 by place, staff, opens sound equipment 21, manipulation Drone body 11 is taken off, and spring(-supported) mount 22 and connection frame 23 are provided in drone body 11, is provided with work in connection frame 23 Plug, drone body 11 are shaken by piston and 22 damping coil paddle of spring clip, 12 bring, reach protection drone body 11 Effect, drone body 11 shot and handled to space environment by the camera of lower section, when drone body 11 is surveyed After drawing, staff manipulates drone body 11 and declines, and rubber sleeve 24, drone body are arranged in drone body 11 11 buffer self weight when drone body 11 drop to ground by rubber sleeve 24, reach the effect protected to drone body 11 Fruit, rubber sleeve 24 can avoid 14 corrosion of support frame by stopping outside air, after mapping operations, staff External signal is cut off, the storage of drone body 11 is suitably local to safety, facilitate staff to use next time.
While there has been shown and described that the embodiments of the present invention, for the ordinary skill in the art, It is understood that these embodiments can be carried out with a variety of variations in the case where not departing from the principles of the present invention and spirit, repaired Change, replacement and variant, the scope of the utility model is defined by the appended claims and the equivalents thereof.

Claims (6)

1. a kind of mapping unmanned plane of self-protection, it is characterised in that: described including casing assembly (10) and guard assembly (20) Casing assembly (10) include drone body (11), propeller (12), connection shell (13), support frame (14), fixed link (15) and Wing (16), the wing (16) are located at the right surface of the drone body (11), and solid with the drone body (11) Fixed connection, connection shell (13) is located at the right end of the wing (16), and is fixedly connected with the wing (16), the spiral Paddle (12) is located at the upper end of connection shell (13), and is sequentially connected with the connection shell (13), and the fixed link (15) is located at The bottom end of the drone body (11), and be fixedly connected with the drone body (11), support frame as described above (14) is located at institute The lower section of fixed link (15) is stated, and is fixedly connected with the fixed link (15), the drone body (11) and external power supply electricity Property connection, guard assembly (20) includes sound equipment (21), spring(-supported) mount (22), connection frame (23) and rubber sleeve (24), the sound equipment (21) it is located at the upper surface of the drone body (11), and is fixedly connected with the drone body (11), the rubber sleeve (24) it is located at the lateral wall of support frame as described above (14), and is adhesively fixed with support frame as described above (14), the spring(-supported) mount (22) is located at The lower end of the fixed link (15), and be fixedly connected with the fixed link (15), the connection frame (23) is located at support frame as described above (14) lateral wall, and be fixedly connected with the fixed link (15), support frame as described above (14) and the fixed link (15) pass through institute It states (23) to be fixedly connected, the sound equipment (21) and external power supply are electrically connected.
2. a kind of mapping unmanned plane of self-protection according to claim 1, it is characterised in that: the number of the wing (16) Amount is four, and four wings (16) are symmetrically distributed in the outer surface of the drone body (11).
3. a kind of mapping unmanned plane of self-protection according to claim 1, it is characterised in that: the fixed link (15) Quantity is two, and two fixed links (15) are symmetrically distributed in the bottom end of the drone body (11).
4. a kind of mapping unmanned plane of self-protection according to claim 1, it is characterised in that: in the connection frame (23) Portion offers the first cavity, and piston, support frame as described above (14) and the connection frame are fixedly installed inside first cavity (23) it is slidably connected by the piston.
5. a kind of mapping unmanned plane of self-protection according to claim 1, it is characterised in that: in the connection shell (13) Portion offers the second cavity, and motor is fixedly installed inside second cavity, and rotation axis, the electricity are provided on the motor Machine and the propeller (12) are sequentially connected by the rotation axis.
6. a kind of mapping unmanned plane of self-protection according to claim 1, it is characterised in that: have on the sound equipment (21) There is USB interface.
CN201820494448.7U 2018-04-09 2018-04-09 A kind of mapping unmanned plane of self-protection Expired - Fee Related CN208325628U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201820494448.7U CN208325628U (en) 2018-04-09 2018-04-09 A kind of mapping unmanned plane of self-protection

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201820494448.7U CN208325628U (en) 2018-04-09 2018-04-09 A kind of mapping unmanned plane of self-protection

Publications (1)

Publication Number Publication Date
CN208325628U true CN208325628U (en) 2019-01-04

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Country Status (1)

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110203393A (en) * 2019-06-19 2019-09-06 山西大学 A kind of quickly mapping multi-rotor unmanned aerial vehicle and its mapping method

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110203393A (en) * 2019-06-19 2019-09-06 山西大学 A kind of quickly mapping multi-rotor unmanned aerial vehicle and its mapping method

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

Granted publication date: 20190104

Termination date: 20200409