CN205971800U

CN205971800U - Unmanned aerial vehicle

Info

Publication number: CN205971800U
Application number: CN201620757938.2U
Authority: CN
Inventors: 王军
Original assignee: Shenzhen Wingsland Technology Co Ltd
Current assignee: Shenzhen Wingsland Technology Co Ltd
Priority date: 2016-07-15
Filing date: 2016-07-15
Publication date: 2017-02-22
Anticipated expiration: 2026-07-15

Abstract

The utility model relates to an aircraft technical field provides an unmanned aerial vehicle, rotate a plurality of horns that open / close including unmanned aerial vehicle casing and relative unmanned aerial vehicle casing, a plurality of horns respectively the pin joint on the unmanned aerial vehicle casing, still including the limit structure who opens the position who is used for spacing horn, limit structure including locate on the horn and at random arm pivoted locating part and locate the unmanned aerial vehicle casing on and be used for the stop part of backstop locating part when the horn when opening the position. The stop part on locating the unmanned aerial vehicle casing is replaced to the locating part of locating on the horn to spacing horn open the position, firm horn prevents that the horn excessively opens and skew open normal angle under the exogenic action, effectively improves the horn and is in the stability of correctly opening the position, protection horn.

Description

A kind of unmanned plane

Technical field

The utility model is related to vehicle technology field, more particularly, to a kind of unmanned plane.

Background technology

Unmanned plane refers to the not manned vehicle being controlled using wireless remote control device and the control device of itself.Nearly ten In the past few years, unmanned plane has been widely used in flight entertainment, photography of taking photo by plane, electric power inspection, environmental monitoring, forest fire protection, the condition of a disaster Patrol, be all the fields such as investigation, battle assessment, can effectively overcome the shortcomings of that manned aircraft carries out aerial work, reduce Buy and maintenance cost, improve the security of delivery vehicle.

The horn of SUAV is typically provided to folding with respect to unmanned plane housing, is easy to carry, and reduces and deposits Space, is prevented effectively from horn by scratching simultaneously, in prior art, is provided with limit assembly between horn and unmanned plane housing, when When opening horn, horn is pinned on the correct position opened by limit assembly, but because horn is relatively long, i.e. the arm of force Longer, when larger external force is applied on horn, so that limit assembly was lost efficacy, horn excessively opens it may occur that damaging horn Situation.

Utility model content

The purpose of this utility model is to provide a kind of unmanned plane it is intended to solve to bear because horn is longer in prior art Moment is larger, easily causes horn and rotates, and damages the problem of horn.

For solving above-mentioned technical problem, the technical solution of the utility model is：There is provided a kind of unmanned plane, including unmanned casing Body and some horns of relatively described unmanned plane housing into rotation open/close, some described horns are articulated in described unmanned plane respectively On housing, also include the position limiting structure of the deployed position for spacing described horn, described position limiting structure is included located at described machine On arm and with described horn rotate locating part and on described unmanned plane housing and when described horn is in deployed position When for locating part described in backstop stop part.

Further, described stop part and described unmanned plane housing are integrally formed.

Further, described stop part is formed by described unmanned plane housing outward.

Further, described locating part and described horn are integrally formed.

Further, described locating part is extended to outside it from described horn and forms.

Further, located at described horn root one lateral edges, described locating part is along described horn root for described locating part Direction progressive additive to described stop block.

Alternatively, the contact surface that described locating part is contacted with described stop part arranges a magnetic part, described locating part and institute State stop part and pass through magnetic part magnetic together.

Alternatively, the contact surface that described stop part is contacted with described locating part arranges a magnetic part, described locating part and institute State stop part and pass through magnetic part magnetic together.

Alternatively, described locating part is the limited block being fixedly arranged on described horn root, and described stop part is and described limit The position corresponding grab being fixedly arranged on described unmanned plane housing of block, described limited block is locked in described grab.

Alternatively, described locating part is the positive stop hook being fixedly arranged on described horn root, and described stop part is spacing with described The corresponding stop block being fixedly arranged on described unmanned plane housing of hook, described stop block is locked in described positive stop hook.

The beneficial effects of the utility model：It is resisted against the backstop on unmanned plane housing located at the locating part on horn Part, with the deployed position of spacing horn, firm horn, prevents horn under external force from excessively opening and deviateing and just opens Often angle, effectively improves the stability that horn is in correct deployed position, protects horn.

Brief description

Fig. 1 is the top view of the unmanned plane that the utility model embodiment provides；

Fig. 2 is the enlarged drawing of A in Fig. 1.

Label involved by above-mentioned accompanying drawing is detailed as follows：

Unmanned plane housing	10	Horn	20
				Second position limiting structure	30	Locating part	31
Stop part	32	Holding tank	11

Specific embodiment

In order that the purpose of this utility model, technical scheme and advantage become more apparent, below in conjunction with accompanying drawing and enforcement Example, is further elaborated to the utility model.It should be appreciated that specific embodiment described herein is only in order to explain The utility model, is not used to limit the utility model.

It should be noted that when element is referred to as on " being fixed on " or " being arranged at " another element, it can directly exist On another element or it may be indirectly secured to by third member or be arranged on another element.When an element quilt Referred to as " being connected to " another element, it can be directly to another element or it may be indirect by third member It is connected on another element.

Also, it should be noted the orientation term such as left and right, upper and lower in the present embodiment, be only each other relative concept or With the normal operating condition of product as reference, and should not be regarded as restrictive.

Refer to Fig. 1, the utility model provides a kind of unmanned plane, including unmanned plane housing 10 and relative unmanned plane housing Some horns 20 of 10 rotation open/close, some horns 20 are articulated in respectively on unmanned plane housing 10, also include for spacing horn Deployed position position limiting structure 30, position limiting structure 30 include on horn 20 and rotate with horn 20 spacing 31 and It is used for the stop part 32 of backstop locating part 31 on unmanned plane housing 10 and when horn 20 is in deployed position.

In the present embodiment, it is resisted against the stop part 32 on unmanned plane housing 10 located at the locating part 31 on horn 20 On, with the deployed position of spacing horn 20, prevent horn 20 under external force from excessively opening and deviateing the normal angle opening Degree, effectively improves the stability that horn 20 is in correct deployed position, protects horn 20, firm horn 20.

Specifically, unmanned plane also include for pin horn 20 be in respect to unmanned plane housing 10 open correct position and Be in closure draw in correct position stopping means (not shown), position limiting structure 30 can coordinate with stopping means together with work Make, to prevent horn 20 from departing from stopping means, make stopping means be in steady-working state, protect stopping means.This be due to Horn 20 is relatively long, and that is, the arm of force of horn 20 is longer, when on the horn 20 when larger external force is applied to open configuration, horn 20 are vulnerable to larger moment, when moment exceedes stopping means and pins the restraint that horn 20 is in correct deployed position, limit Position failure of apparatus or destroyed, horn 20 will rotate, and deviate the normal angled opened, lead to horn 20 to damage when serious, Unmanned plane falls, accordingly, it would be desirable to setting position limiting structure 30 is carrying out secondary position limitation protection, meanwhile, this position limiting structure 30 not only Limit is arranged on unmanned plane, and arbitrary aircraft all can flexibly select to arrange.

Specifically, horn 20 is four, and be uniformly placed in unmanned plane housing 10 both sides, when horn 20 draws in, each side Two horns 20 are oppositely buckled with unmanned plane housing 10；When horn 20 opens, two horns 20 of each side deviate from and open in unmanned Casing body 10 both sides.

More specifically, unmanned plane housing 10 is respectively provided on two sides with draws the horn 20 on unmanned plane housing 10 in for accommodating Holding tank 11, so that multiple horns 20 is drawn in the holding tank 11 on unmanned plane housing 10, make unmanned plane overall lighter, Compact.

Further, stop part 32 is to be formed by unmanned plane housing 10 outward, is integrally formed with unmanned plane housing 10, I.e. stop part 32 is generated by itself outward of unmanned plane housing 10.And, locating part 31 is also become with horn 20 one Type, is to be extended to outside it from horn 20 to form, that is, locating part 31 itself is extended laterally and generated by horn 20.Permissible It is interpreted as, stop part 32 and unmanned plane housing 10 are an overall structure, locating part 31 is also an overall structure with horn 20, this Sample, stop part 32 and locating part 31 are firmer, and can strengthen the resistivity to external force for the unmanned plane greatly, protect horn.

Further, horn 20 root is in arc-shaped, and locating part 31 is located at horn 20 root one lateral edges, locating part 31 edge The circular arc of horn 20 root, to backstop Block direction progressive additive, effectively increases the intensity of locating part 31.

Alternatively, locating part 31 and stop part 32 can be packet, can also be cylinder, flexibly all in block Selected shape.

Further, locating part 31 is contacted with stop part 32 contact surface setting magnetic part, locating part 31 and stop part 32 By magnetic part magnetic together.

Alternatively, the contact surface setting magnetic part that stop part 32 is contacted with locating part 31, locating part 31 is led to stop part 32 Cross magnetic part magnetic together.

Alternatively, locating part 31 is the limited block being fixedly arranged on horn 20 root, and stop part 32 is corresponding with limited block It is fixedly arranged on the grab on unmanned plane housing 10, limited block is locked in grab.

Alternatively, locating part 31 is the positive stop hook being fixedly arranged on horn 20 root, and stop part 32 is corresponding with positive stop hook solid A stop block on unmanned plane housing 10, stop block is locked in positive stop hook.

These are only preferred embodiment of the present utility model, not in order to limit the utility model, all in this practicality Any modification, equivalent and improvement made within new spirit and principle etc., should be included in guarantor of the present utility model Within the scope of shield.

Claims

1. a kind of unmanned plane, including some horns of unmanned plane housing and relatively described unmanned plane housing into rotation open/close, some Described horn is articulated on described unmanned plane housing respectively it is characterised in that also including opening position for spacing described horn The position limiting structure put, the locating part that described position limiting structure includes on described horn and rotates with described horn and located at institute State the stop part being used for locating part described in backstop on unmanned plane housing and when described horn is in deployed position.

2. unmanned plane as claimed in claim 1 is it is characterised in that described stop part is integrally formed with described unmanned plane housing.

3. unmanned plane as claimed in claim 1 is it is characterised in that described stop part is by described unmanned plane housing outward Become.

4. unmanned plane as claimed in claim 1 is it is characterised in that described locating part is integrally formed with described horn.

5. unmanned plane as claimed in claim 1 it is characterised in that described locating part extended to outside it from described horn and Become.

6. unmanned plane as claimed in claim 5 is it is characterised in that described locating part is located at described horn root one lateral edges, Described locating part is along described horn root to the direction progressive additive of described stop block.

7. the unmanned plane as any one of claim 1 to 6 is it is characterised in that described locating part is connect with described stop part Tactile contact surface setting magnetic part, described locating part is passed through together with magnetic part magnetic with described stop part.

8. the unmanned plane as any one of claim 1 to 6 is it is characterised in that described stop part is connect with described locating part Tactile contact surface setting magnetic part, described locating part is passed through together with magnetic part magnetic with described stop part.

9. unmanned plane as claimed in claim 1 is it is characterised in that described locating part is the limit being fixedly arranged on described horn root Position block, described stop part is the grab that is fixedly arranged on described unmanned plane housing on corresponding with described limited block, described limited block It is locked in described grab.

10. unmanned plane as claimed in claim 1 is it is characterised in that described locating part is the limit being fixedly arranged on described horn root Position hook, described stop part is the stop block that is fixedly arranged on described unmanned plane housing on corresponding with described positive stop hook, described backstop Block is locked in described positive stop hook.