CN205293062U - Novel unmanned aerial vehicle horn folding mechanism - Google Patents

Novel unmanned aerial vehicle horn folding mechanism Download PDF

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Publication number
CN205293062U
CN205293062U CN201620018210.8U CN201620018210U CN205293062U CN 205293062 U CN205293062 U CN 205293062U CN 201620018210 U CN201620018210 U CN 201620018210U CN 205293062 U CN205293062 U CN 205293062U
Authority
CN
China
Prior art keywords
horn
hole
fixed
unmanned plane
novel unmanned
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
CN201620018210.8U
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Chinese (zh)
Inventor
黄键耿
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.)
Zhejiang Tianma Xingkong Innovation Technology Co Ltd
Original Assignee
Zhejiang Tianma Xingkong Innovation 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 Zhejiang Tianma Xingkong Innovation Technology Co Ltd filed Critical Zhejiang Tianma Xingkong Innovation Technology Co Ltd
Priority to CN201620018210.8U priority Critical patent/CN205293062U/en
Application granted granted Critical
Publication of CN205293062U publication Critical patent/CN205293062U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model discloses a novel unmanned aerial vehicle horn folding mechanism, including the carousel, the carousel evenly sets up the fixed boss of horn along the circumference, is equipped with the through -hole on the fixed boss of horn, and the rotation axis is installed at the carousel center, and the rotation axis facial make -up has a horn, and the horn end is equipped with the rotor mounting bracket, and the horn corresponds horn fixed station position and is equipped with the fixed orifices, and fixed orifices and through -hole pass through the fixed pin hub connection, the utility model discloses novel structure, it is simple, install on the rotation axis through the horn, realize that the horn can be rotatory around the rotation axis, realize six and accomodate that the convenience is stored and is carried, the rethread horn passes through the through -hole on fixed orifices and the carousel to and the fixed pin axle, make the horn deployable fixed, satisfied the operation requirement.

Description

A kind of novel unmanned plane horn fold mechanism
Technical field
This utility model relates to a kind of UAV Components, specifically a kind of novel unmanned plane horn fold mechanism.
Background technology
UAV is called for short " unmanned plane ", and english abbreviation is " UAV ", is the not manned aircraft of the presetting apparatus manipulation utilizing radio robot with providing for oneself. Can being divided into from technical standpoint definition: depopulated helicopter, unmanned fixed-wing aircraft, unmanned multi-rotor aerocraft, unmanned airship, unmanned parasol etc., unmanned plane presses application, can be divided into military and civilian. Military aspect, unmanned plane is divided into reconnaissance plane and target drone, unmanned plane+sector application, is real just the needing of unmanned plane. At present taking photo by plane, agricultural plant protection, the field such as mapping application, greatly expanded the purposes of unmanned plane itself. It addition, many model telecontrolled aircrafts are also referred to as unmanned plane.
Development and maturation along with unmanned air vehicle technique, unmanned plane has been widely used for taking photo by plane and search and rescue field, field, owing to field flight environment of vehicle is changeable, the stability of unmanned plane is critically important, so unmanned plane mostly is four axles or six axle unmanned planes now, but due to six axle unmanned planes, horn is many, and long, carry and receive very inconvenient.
Utility model content
The purpose of this utility model is in that to provide a kind of novel unmanned plane horn fold mechanism, with the problem solving to propose in above-mentioned background technology.
For achieving the above object, this utility model provides following technical scheme:
A kind of novel unmanned plane horn fold mechanism, including rotating disk, described rotating disk is circumferentially uniformly arranged horn fixing lug boss, described horn fixing lug boss is provided with through hole, described center of turntable is provided with rotating shaft, and equipped with horn on described rotating shaft, described horn end is provided with rotor installing rack, described horn correspondence horn fixed station position is provided with fixing hole, and described fixing hole is connected by fixed pin shaft with through hole.
As further program of the utility model: described horn installation base is along the circumferential direction uniformly provided with six, the through hole on described horn installation base is rectangular opening.
As further program of the utility model: described horn is provided with six, the described rotating installation of horn head end is on the rotary shaft.
As further program of the utility model: described rotor installing rack is provided with installation through hole.
As further program of the utility model: described rotating disk is provided with rack mounting apertures.
Compared with prior art, the beneficial effects of the utility model are: this utility model novel structure, simply, install on the rotary shaft by horn, it is achieved horn can rotate around rotating shaft, realize six axle storages, conveniently store and carry, again through horn by the through hole on fixing hole and rotating disk, and fixed pin shaft, make horn deployable fixing, meet instructions for use.
Accompanying drawing explanation
Fig. 1 is the structural representation of novel unmanned plane horn fold mechanism.
In figure: 1-horn fixing lug boss, 2-through hole, 3-rotating disk, 4-rack mounting apertures, 5-horn, 6-fixing hole, 7-install through hole, 8-rotor installing rack, 9-rotating shaft, 10-fixed pin shaft.
Detailed description of the invention
Below in conjunction with the accompanying drawing in this utility model embodiment, the technical scheme in this utility model embodiment is clearly and completely described, it is clear that described embodiment is only a part of embodiment of this utility model, rather than whole embodiments. Based on the embodiment in this utility model, the every other embodiment that those of ordinary skill in the art obtain under not making creative work premise, broadly fall into the scope of this utility model protection.
Refer to Fig. 1, in this utility model embodiment, a kind of novel unmanned plane horn fold mechanism, including rotating disk 2, rotating disk 2 is circumferentially uniformly arranged horn fixing lug boss 1, horn fixing lug boss 1 is provided with through hole 2, rotating disk 1 center is provided with rotating shaft 9, equipped with horn 5 on rotating shaft 9, horn 5 end is provided with rotor installing rack 8, corresponding horn fixed station 1 position of horn 5 is provided with fixing hole 6, fixing hole 6 is connected by fixed pin shaft 10 with through hole 2, horn installation base 1 is along the circumferential direction uniformly provided with six, through hole on horn installation base 1 is rectangular opening, horn 5 is provided with six, horn 5 head end is rotating to be arranged on rotating shaft 9, rotor installing rack 8 is provided with installation through hole 7, rotating disk 3 is provided with rack mounting apertures 4.
This utility model novel structure, simply, installed on the rotary shaft by six horn head ends, it is achieved horn can rotate around rotating shaft, realize six axle storages, conveniently store and carry, again through horn by the through hole on fixing hole and rotating disk, and fixed pin shaft, make horn deployable fixing, the rack mounting apertures that rotating disk is provided with, meets instructions for use, facilitates the operation of user of service.
In those skilled in the art, it is clear that this utility model is not limited to the details of above-mentioned one exemplary embodiment, and when without departing substantially from spirit of the present utility model or basic feature, it is possible to realize this utility model in other specific forms. Therefore, no matter from which point, embodiment all should be regarded as exemplary, and be nonrestrictive, scope of the present utility model is limited by claims rather than described above, it is intended that all changes in the implication of the equivalency dropping on claim and scope included in this utility model. Any accompanying drawing labelling in claim should be considered as the claim that restriction is involved.
In addition, it is to be understood that, although this specification is been described by according to embodiment, but not each embodiment only comprises an independent technical scheme, this narrating mode of description is only for clarity sake, description should be made as a whole by those skilled in the art, and the technical scheme in each embodiment through appropriately combined, can also form other embodiments that it will be appreciated by those skilled in the art that.

Claims (5)

1. a novel unmanned plane horn fold mechanism, including rotating disk, it is characterized in that, described rotating disk is circumferentially uniformly arranged horn fixing lug boss, and described horn fixing lug boss is provided with through hole, and described center of turntable is provided with rotating shaft, equipped with horn on described rotating shaft, described horn end is provided with rotor installing rack, and described horn correspondence horn fixed station position is provided with fixing hole, and described fixing hole is connected by fixed pin shaft with through hole.
2. novel unmanned plane horn fold mechanism according to claim 1, it is characterised in that described horn installation base is along the circumferential direction uniformly provided with six, and the through hole on described horn installation base is rectangular opening.
3. novel unmanned plane horn fold mechanism according to claim 1, it is characterised in that described horn is provided with six, and the described rotating installation of horn head end is on the rotary shaft.
4. novel unmanned plane horn fold mechanism according to claim 1, it is characterised in that described rotor installing rack is provided with installation through hole.
5. novel unmanned plane horn fold mechanism according to claim 1, it is characterised in that described rotating disk is provided with rack mounting apertures.
CN201620018210.8U 2016-01-08 2016-01-08 Novel unmanned aerial vehicle horn folding mechanism Expired - Fee Related CN205293062U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201620018210.8U CN205293062U (en) 2016-01-08 2016-01-08 Novel unmanned aerial vehicle horn folding mechanism

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201620018210.8U CN205293062U (en) 2016-01-08 2016-01-08 Novel unmanned aerial vehicle horn folding mechanism

Publications (1)

Publication Number Publication Date
CN205293062U true CN205293062U (en) 2016-06-08

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN201620018210.8U Expired - Fee Related CN205293062U (en) 2016-01-08 2016-01-08 Novel unmanned aerial vehicle horn folding mechanism

Country Status (1)

Country Link
CN (1) CN205293062U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2018214124A1 (en) * 2017-05-25 2018-11-29 SZ DJI Technology Co., Ltd. Rotational expansion of propulsion systems of a movable vehicle

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2018214124A1 (en) * 2017-05-25 2018-11-29 SZ DJI Technology Co., Ltd. Rotational expansion of propulsion systems of a movable vehicle

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Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20160608

Termination date: 20210108

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