CN205872497U - Cloud platform quick detach formula unmanned aerial vehicle - Google Patents

Abstract

The utility model discloses a cloud platform quick detach formula unmanned aerial vehicle belongs to the unmanned air vehicle technique field, cloud platform quick detach formula unmanned aerial vehicle includes: the fuselage includes: a housing. The organism, the inside of organism is hollow structure, just be provided with at least one installing port on the organism, the 2nd detaching assembly, the 2nd detaching assembly will the detachable connection of casing is on the organism to close through machine cover the installing port, a detaching assembly, a detaching assembly is fixed in on the organism, the signal positioning subassembly, the signal positioning subassembly is fixed in on the casing, rapid detaching assembly, first rotor passes through rapid detaching assembly is fixed in with rotating on the rotor power component. This application through a detaching assembly with the cloud platform is detachable be fixed in the fuselage on to realize the installation of cloud platform or dismantle, solved or the partial technical defect that the dismantlement process is very complicated who has solved prior art medium cloud platform.

Description

The Cloud Terrace fast disassembly type unmanned plane

Technical field

This utility model belongs to unmanned air vehicle technique field, particularly to a kind of The Cloud Terrace fast disassembly type unmanned plane.

Background technology

UAV is called for short " unmanned plane ", is to utilize radio robot and the presetting apparatus provided for oneself to handle The most manned aircraft.Without driving cabin on machine, but the equipment such as automatic pilot, presetting apparatus, information collecting device are installed. On ground, naval vessels or machine tool remote control station personnel are by the equipment such as radar, be tracked it, position, remote control, remote measurement and numeral pass Defeated.Can take off as conventional airplane under wireless remotecontrol or launch with booster rocket, it is possible to be taken in the air by machine tool Throw in flight.

Unmanned plane of the prior art, including fuselage, rotor shaft and The Cloud Terrace, and rotor shaft is rotationally fixed on fuselage, Fuselage interior is additionally provided with flight control system simultaneously.

But, in the prior art, the connection between The Cloud Terrace and unmanned plane, it is provided with often by the bottom at fuselage One base plate, this base plate, as a part for fuselage, connects The Cloud Terrace for fixing, and when The Cloud Terrace is dismantled by needs, just By extraneous utensil such as spanner etc., base plate must be dismantled, then realize the dismounting of The Cloud Terrace.This allows for the unloading process of The Cloud Terrace Extremely complex.

Utility model content

This utility model provides a kind of The Cloud Terrace fast disassembly type unmanned plane, is consolidated by detachable for The Cloud Terrace by the first dismounting assembly On fuselage, to realize installation or the dismounting of The Cloud Terrace, solve or part solves the dismounting of The Cloud Terrace in prior art The technological deficiency that journey is extremely complex.

For solving above-mentioned technical problem, this utility model provides a kind of The Cloud Terrace fast disassembly type unmanned plane, wherein, unmanned plane bag Including the first rotor, rotor shaft, The Cloud Terrace and flight control system, described The Cloud Terrace fast disassembly type unmanned plane includes: fuselage, described fuselage bag Include: casing；Body, the inside of described body is hollow-core construction, and is provided with at least one installing port on described body；Second tears open Unloading assembly, detachable for described casing is connected on described body by described second dismounting assembly, and by described cabinet cover Close described installing port；Wherein, parts to be installed in described body are placed into relative to described body by described installing port Or it is removed；

First dismounting assembly, described first dismounting assembly is fixed on described body；

Signal framing assembly, described signal framing assembly is fixed in described casing, and sets in described signal framing assembly It is equipped with the localizer for unmanned plane being carried out signal framing；

Quick-dismantle component, described first rotor is rotationally fixed on described rotor power assembly by described Quick-dismantle component；

Wherein, by described first dismounting assembly, described The Cloud Terrace is connected on described body so that described The Cloud Terrace passes through Between described first dismounting assembly and described body detachable, and described localizer is arranged on institute by described signal framing assembly State in casing, be isolated with the external air flow by described localizer with described fuselage.

Optionally, described first dismounting assembly includes:

Fixed plate, described fixed plate is fixed on described body, and is slidably connected with described The Cloud Terrace, so that described The Cloud Terrace phase Described fixed plate is slided；

Positioning element, described positioning element is fixed in described fixed plate, with to described The Cloud Terrace relative to described fixed plate Position position, and then realize described The Cloud Terrace relative to described body install or dismounting.

Optionally, described fixed plate includes:

First side plate；

Second side plate, described first side plate and described second side plate are parallel；

Transverse slat, described first side plate and described second side plate are perpendicular with described transverse slat, and described transverse slat is respectively with described First side plate and described second side plate are slidably connected, and described The Cloud Terrace is fixing with described transverse slat to be connected, and then is made by described transverse slat Obtain described The Cloud Terrace to slide relative to described first side plate and described second side plate；

Described positioning element is individually fixed on described first side plate and described second side plate, with to described transverse slat relative to The position of described first side plate and described second side plate positions.

Optionally, described first side plate and described second side plate are respectively arranged with a chute, to be arranged by described transverse slat In described chute so that described transverse slat is slided relative to described first side plate and described second side plate by described chute Dynamic；One end of described positioning element corresponding through described first side plate, described second side plate, and in described chute internal projection or Person shrink so that one end of described positioning element relative to described chute when described chute internal projection, described positioning element One end stop described transverse slat slide in described chute, one end of described positioning element relative to described chute in described cunning During groove contract, one end of described positioning element is separated with described transverse slat, so that described transverse slat is slided in described chute Dynamic.

Optionally, described positioning element includes: the first location plunger, and described first location plunger includes the first positioning end； Second location plunger, described second location plunger includes the second positioning end；Wherein, described first positioning end corresponding through described First side plate, and the chute internal projection in described first side plate or contraction, so that described first positioning end is relative to institute When stating the chute internal projection in the first side plate, described first positioning end stops that described transverse slat slides in chute, described the One positioning end is when relative to chute contract in described first side plate, and described first positioning end is separated with described transverse slat, So that described transverse slat slides in chute；Wherein, described second positioning end corresponding through described second side plate, and in institute State the chute internal projection in the second side plate or contraction, so that described second positioning end is relative to the cunning in described second side plate During groove internal projection, described second positioning end stop described transverse slat slide in chute, described second positioning end relative to During chute contract in described second side plate, described second positioning end is separated with described transverse slat, so that described transverse slat is being slided Slide in groove.

Optionally, described first location plunger includes: the first bolt, described first bolt is provided with described the One positioning end；First positioning thread insert, described first positioning thread insert is set on described first bolt, and described first location One first compression stroke it is provided with between swivel nut and described first bolt；First location spring, described first location spring It is arranged in described first compression stroke；Wherein, described first positioning end sequentially pass through described first location spring, described first Compression stroke and described first side plate, with the chute internal projection in described first side plate or contraction；With, described second location Plunger includes: the second bolt, and described second bolt is provided with described second positioning end；Second positioning thread insert, described Second positioning thread insert is set on described second bolt, and between described second positioning thread insert and described second bolt It is provided with one second compression stroke；Second location spring, described second location spring is arranged in described second compression stroke； Wherein, described second positioning end sequentially passes through described second location spring, described second compression stroke and described second side plate, with Chute internal projection in described second side plate or contraction.

Optionally, on described first positioning end of described first bolt, it is provided with one first card convex, with by described One location spring is limited in described first compression stroke, and makes described first positioning end relative in described first side plate Chute contract time, by described first card convex compression described first location spring；And/or, described second bolt On described second positioning end, it is provided with one second card convex, so that described second location spring is limited to described second compression stroke In, and make described second positioning end when relative to chute contract in described second side plate, by described second card convex Compress described second location spring.

Optionally, described second dismounting assembly includes: socket, described socket is fixed on described body；3rd locating dowel Plug, described 3rd location plunger is fixed in described casing, and described 3rd location plunger includes the 3rd positioning end；Wherein, institute State in the described socket of insertion that the 3rd positioning end is corresponding, with by described casing and described body clamping.

Optionally, described 3rd location plunger includes: locating dowel and the 3rd caging bolt, described locating dowel is fixed on described In casing, and described 3rd caging bolt is fixed in described locating dowel；It is fixed that described 3rd caging bolt is provided with the described 3rd Position end.

Optionally, described signal framing assembly also includes: location bar, and described location bar includes fixing end and a support End, described location bar is fixed in described casing by described fixing end；Spiral shell dish, described spiral shell dish is fixed on by described support end On the bar of described location, and the inside of described spiral shell dish is hollow-core construction so that described localizer is fixed in described spiral shell dish.

The The Cloud Terrace fast disassembly type unmanned plane that this utility model provides, is fixed on removable for The Cloud Terrace by the first dismounting assembly On fuselage, to realize installation or the dismounting of The Cloud Terrace, solve the technology that in prior art, the unloading process of The Cloud Terrace is extremely complex Defect.This utility model has feature simple to operate, that efficiency is high and The Cloud Terrace security performance is high.

Accompanying drawing explanation

In order to be illustrated more clearly that this utility model embodiment or technical scheme of the prior art, below will be to embodiment The accompanying drawing used required in is briefly described, it should be apparent that, the accompanying drawing in describing below is the most of the present utility model Some embodiments, for those of ordinary skill in the art, on the premise of not paying creative work, it is also possible to according to this A little accompanying drawings obtain other accompanying drawing.

The unmanned plane overall structure schematic diagram that Fig. 1 provides for this utility model embodiment；

The side view of the unmanned plane that Fig. 2 provides for Fig. 1；

First dismounting assembly and the annexation overall structure schematic diagram of The Cloud Terrace in the unmanned plane that Fig. 3 provides for Fig. 1；

First dismounting assembly and the annexation overall structure side view of The Cloud Terrace in the unmanned plane that Fig. 4 provides for Fig. 1；

Fig. 5 is the first dismounting assembly overall structure schematic diagram in Fig. 4；

Fig. 6 is the first dismounting assembly overall structure front view in Fig. 5；

In the unmanned plane that Fig. 7 provides for this utility model embodiment, the first location plunger is in the section view under contraction state Figure；

The overall knot that in the unmanned plane that Fig. 8 provides for this utility model embodiment, the first location plunger is under contraction state Structure schematic diagram；

In the unmanned plane that Fig. 9 provides for this utility model embodiment, the first location plunger is in the section view under raised position Figure；

In the unmanned plane that Figure 10 provides for this utility model embodiment, the first location plunger is in the entirety under raised position Structural representation；

The overall structure schematic diagram of fuselage in the unmanned plane that Figure 11 provides for this utility model embodiment；

Figure 12 is the close-up schematic view of the second dismounting assembly in Figure 11；

The overall structure schematic diagram of signal framing assembly in the unmanned plane that Figure 13 provides for this utility model embodiment；

The sectional view of signal framing assembly in the unmanned plane that Figure 14 provides for this utility model embodiment；

The annexation signal of the first motor, refrigerating seat and rotor shaft three that Figure 15 provides for this utility model embodiment Figure；

The annexation section view of the first motor, refrigerating seat and rotor shaft three that Figure 16 provides for this utility model embodiment Figure；

The overall structure schematic diagram that Figure 17 adjusts for the first electricity that this utility model embodiment provides；

The side view that Figure 18 adjusts for the first electricity that this utility model embodiment provides；

The first motor that Figure 19 provides for this utility model embodiment, the second motor, refrigerating seat, the connection of rotor shaft Relation schematic diagram；

The structural front view of the Quick-dismantle component that Figure 20 provides for this utility model embodiment；

The overall structure schematic diagram of the Quick-dismantle component that Figure 21 provides for this utility model embodiment.

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 carried out Clearly and completely describe, it is clear that described embodiment is only a part of embodiment of this utility model rather than whole Embodiment.Based on the embodiment in this utility model, the every other embodiment that those of ordinary skill in the art are obtained, all belong to Scope in this utility model protection；Wherein involved in this enforcement "and/or" key word, represent and or two kinds of situations, change Sentence is talked about, A and/or B mentioned by this utility model embodiment illustrates A and B, two kinds of situations of A or B, describe A with B and deposited Three kinds of states, such as A and/or B, represent: only include A and do not include B；Only include B and do not include A；Including A and B.

Meanwhile, in this utility model embodiment, when assembly is referred to as " being fixed on " another assembly, it can be directly separately On one assembly or assembly placed in the middle can also be there is.When an assembly is considered as " connection " another assembly, and it can be It is directly connected to another assembly or may be simultaneously present assembly placed in the middle.When assembly be considered as " being arranged at " another Assembly, it can be to be set directly on another assembly or may be simultaneously present assembly placed in the middle.This utility model embodiment Used in term " vertical ", " level ", "left", "right" and similar statement be merely for purposes of illustration, not It is intended to limit this utility model.

The The Cloud Terrace fast disassembly type unmanned plane that this utility model provides, is fixed on removable for The Cloud Terrace by the first dismounting assembly On fuselage, to realize installation or the dismounting of The Cloud Terrace, solve the technology that in prior art, the unloading process of The Cloud Terrace is extremely complex Defect.This utility model has feature simple to operate, that efficiency is high and The Cloud Terrace security performance is high.In order to this utility model is provided The Cloud Terrace fast disassembly type unmanned plane elaborate, to support technical problem to be solved in the utility model, below, this practicality is new In the embodiment that type provides, first the overall structure of unmanned plane is elaborated, then during narration unmanned plane, enter One step draws the The Cloud Terrace fast disassembly type unmanned plane that this utility model provides targetedly, to reach mesh complete, clear, that understand 's.

Referring to Fig. 1-2,11,14, this utility model embodiment provides a kind of unmanned plane, including fuselage 1, rotor shaft 2, The Cloud Terrace 3, the first dismounting assembly 4, signal framing assembly 5 and rotor power assembly 6.

Wherein, described rotor shaft 2 is rotationally fixed on described fuselage 1 by its one end, with realize rotor shaft 2 relative to Fuselage is collapsible, then completes rotor shaft 2 and the expansion action of fuselage or contractive action.In this utility model embodiment, The quantity of rotor shaft 2 can be 4, and four corner portions being distributed in fuselage 1 of 4 described rotor shaft 2 symmetries.Described machine The inside of body 1 is additionally provided with the flight control system for controlling unmanned plane during flying.On the other end of rotor shaft 2, it is fixed with Described rotor power assembly 6, and be connected with the flight control system set by fuselage 1 inside, think that the rotation of rotor provides dynamic An electricity tune described above is at least included in power, and described rotor power assembly 6.

Meanwhile, described first dismounting assembly 4 is fixed on described fuselage 1, and by described first dismounting assembly 4 by described What The Cloud Terrace 3 was detachable is connected on described fuselage 1 so that described The Cloud Terrace 3 can be with described by described first dismounting assembly 4 Fuselage 1 quickly, dismantle flexibly, to constitute The Cloud Terrace fast disassembly type unmanned plane described in the utility model.Certainly, the first dismounting assembly 4 With the fixing connected mode between described fuselage 1 can be diversified, as can be bolt connect, can be screw even Connect, can be welding, it is also possible to being one-body molded, not limiting in this this utility model embodiment, as long as being capable of first Dismounting assembly 4 is fixed on described fuselage 1.

Further, described signal framing assembly 5 is fixed on described fuselage 1, and sets in described signal framing assembly 5 It is equipped with a localizer 53.Certainly, localizer 53 is mainly used between unmanned plane and earth station in this utility model embodiment Carry out the transmission of positional information, to be monitored position and the flight information of unmanned plane in real time by localizer 53, for fixed The type of position device 53, this utility model embodiment is not limited to, and can be navigational route type receiver, geodetic type receiver or time service Type receiver etc..It should be understood that, in this utility model embodiment, described localizer 53 is by described signal framing group Part 6 is arranged on described fuselage 1, thus makes the extraneous gas of localizer 53 with described fuselage 1 by signal framing assembly 6 Stream is isolated；Effectively avoid localizer 53 the most exposed when external fuselage, external air flow during unmanned plane during flying, outer Boundary's dampness or extraneous shelter because of with localizer 53 Long Term Contact or friction and the localizer 53 that causes makes moist or damages, Have the advantages that security performance is high.

Below, the building block of each several part of unmanned plane is elaborated.

For above-mentioned first dismounting assembly 4,

Referring to Fig. 3-11, wherein, described first dismounting assembly 4 at least includes: fixed plate 41 and positioning element 42.

Wherein, described fixed plate 41 is fixed on described fuselage 1, and is slidably connected with described The Cloud Terrace 3, so that described The Cloud Terrace 3 slide relative to described fixed plate 41, and owing to fixed plate 41 is fixed relative to fuselage 1, so realize The Cloud Terrace 3 relative to Fuselage 1 slides.Certainly, the fixing connected mode between fixed plate 41 and described fuselage 1 can be diversified, as can To be bolt connection, can be screw connection, can be welding, it is also possible to be one-body molded, in this this utility model embodiment Do not limit, as long as being capable of fixed plate 41 to be fixed on described fuselage 1.Described positioning element 42 is fixed on described fixing On plate 41, so that described The Cloud Terrace 3 is positioned relative to the position of described fixed plate 41, so realize described The Cloud Terrace 3 relative to Described fuselage is installed or dismounting.

Here, positioning element 42 is equivalent to screens parts, when The Cloud Terrace 3 is installed on fuselage 1 by needs, now A certain position is slid into relative to fixed plate 41, then by positioning element 42 to this position between The Cloud Terrace 3 and fixed plate 41 The Cloud Terrace 3 positions, to prevent The Cloud Terrace 3 from sliding relative to fixed plate 41.And when The Cloud Terrace 3 pulled down by needs, the most only need manually Stir positioning element 42, it is allowed to The Cloud Terrace 3 skids off relative to fixed plate 41, can realize The Cloud Terrace 3 quick, dismantle flexibly.This mistake Cheng Zhong, the installation and removal of The Cloud Terrace are without by any extraneous utensil such as spanner etc., easy to operate, have quickly, spy easily Point.

In this utility model embodiment, as preferably, please continue to refer to Fig. 5-6, described fixed plate 42 can be cross section U-shaped shape, the described fixed plate 42 under this shape at least may include that the first side plate 411；Second side plate 412 and transverse slat 413。

Wherein, described first side plate 411 and described second side plate 412 are parallel；And described first side plate 411 and described Two side plates 412 are perpendicular with described transverse slat 413, and described transverse slat 413 respectively with described first side plate 411 and described second side plate 412 are slidably connected, and described The Cloud Terrace 3 is fixing with described transverse slat 413 to be connected, and then makes described The Cloud Terrace 3 phase by described transverse slat 413 Described first side plate 411 and described second side plate 412 are slided.Meanwhile, described positioning element 41 is individually fixed in institute State on the first side plate 411 and described second side plate 412, with to described transverse slat 413 relative to described first side plate 411 and described The position of two side plates 412 positions.Certainly, described first side plate 411, between described second side plate 412 and described fuselage 1 Fixing connected mode can be diversified, as being bolt connection, can be screw connection, can be welding, it is possible to To be one-body molded, do not limit in this this utility model embodiment, if be capable of described first side plate 411, described Two side plates 412 are fixed on described fuselage 1.

Same principle, the fixing connected mode between described The Cloud Terrace 3 and described transverse slat 413 can also be varied , as being bolt connection, can be screw connection, can be welding, it is also possible to be one-body molded, at this this utility model Embodiment does not limits, and is relatively fixed with described transverse slat 413, all guarantor of the present utility model as long as being capable of described The Cloud Terrace 3 Within the scope of protecting.

Further, for ease of being fixed with the transverse slat 413 of The Cloud Terrace 3, it is possible to and the spirit of first side plate the 411, second side plate 412 Live, quickly slide, in order to The Cloud Terrace 3 flexibly, is quickly installed or dismounting.One as this utility model embodiment is real Execute and be respectively arranged with a chute, to be arranged by described transverse slat 413 on mode, described first side plate 411 and described second side plate 412 In described chute so that described transverse slat 413 passes through described chute relative to described first side plate 411 and described second side plate 412 slide.

Meanwhile, one end of described positioning element 42 corresponding through described first side plate 411, described second side plate 412, And in described chute internal projection or contraction so that one end of described positioning element 42 relative to described chute in described chute Time protruding, one end of described positioning element 42 stops that described transverse slat 413 slides in described chute, described positioning element 42 One end relative to described chute when described chute contract, one end of described positioning element 42 is divided with described transverse slat 413 phase From, so that described transverse slat 413 slides in described chute.

Needing exist for explanation, in this utility model embodiment, described " protruding " is it can be understood as be one Parts slip in some parts, and " contraction " can be understood as parts and skid off some parts.Such as, described above One end of described positioning element 42 when described chute internal projection, i.e. refers to one end of described positioning element 42 relative to described chute Slipping in described chute, one end of positioning element 42 described above, i.e. refers to when described chute contract relative to described chute One end of described positioning element 42 skids off described chute.The Cloud Terrace 3 tearing open relative to fuselage 1 is realized by positioning element 42 with this Unload or install.

For described positioning element 42, in this utility model embodiment, as a kind of realization side of the present embodiment Formula, described positioning element 42 can at least include: the first location plunger and described second location plunger.And described first locating dowel Plug includes the first positioning end；Described second location plunger includes the second positioning end.

Wherein, described first positioning end corresponding through described first side plate, and the chute in described first side plate 411 Internal projection or contraction, so that described first positioning end is when relative to chute internal projection in described first side plate 411, described First positioning end stops that described transverse slat 413 slides in chute, and described first positioning end is relative to described first side plate During chute contract in 411, described first positioning end is separated, so that described transverse slat 413 is in chute with described transverse slat 413 Slide.Wherein, described second positioning end corresponding through described second side plate 412, and in described second side plate 412 Chute internal projection or contraction, so that described second positioning end is when relative to chute internal projection in described second side plate 412, Described second positioning end stops that described transverse slat 413 slides in chute, and described second positioning end is relative to described second During chute contract in side plate 412, described second positioning end is separated with described transverse slat, so that described transverse slat 413 is at chute Inside slide.

Here, can be it can be understood as the first side plate 411 and the second side plate 412 symmetry as shown in Fig. 5 or Fig. 6 It is distributed in the both sides of described transverse slat 413, while thus making the both sides correspondence of described transverse slat 413, inserts described first side plate 411 and the chute offered of described second side plate 412 in, realize being fixed with the transverse slat 413 of The Cloud Terrace 3 relative to the first side with this Plate 411 and the second side plate 412 slide.Meanwhile, in order to preferably the transverse slat 413 in sliding process be positioned.This reality By new embodiment by the first location plunger and the second location plunger, the both sides at transverse slat 413 of symmetrical setting, Ye Ji One location plunger and the first side plate 411 are corresponding, and the second location plunger and the second side plate 412 are corresponding.It should be noted that In this utility model embodiment, the first side plate 411 and the structure of the second side plate 412 can identical can also be different, first Location plunger and the second location plunger can identical can also be different.And in this utility model embodiment, for description side Just, the first selected side plate 411 is identical with the second side plate 412 structure, and the first location plunger and second positions plunger Structure is identical.

Certainly, it will be understood by those skilled in the art that the first side plate 411 and the second side plate 412, first position plunger and the Two location plungers can also be mutually different various structures, if the first side plate 411 can be square structure, and the second side plate 412 can be rectangle structure, or the first side plate 411 can be trapezium structure, the second side plate 412 can be square or The polygonized structure such as rectangle or rhombus.In other words, as long as be capable of the first side plate 411 and the second side plate 412 with Fuselage 1 is relatively fixed, and transverse slat 413 can first side plate 411 that slide relative with the first side plate 411 and the second side plate 412 and Second side plate 412 structure, all within protection domain of the present utility model.Same, the first location plunger and the second locating dowel Plug can also be multiple different structure, if disclosure satisfy that the first location plunger can be corresponding through the first side plate 411, the Two location plungers can be corresponding through carrying out projection or flexible in the second side plate 412, and the chute of each its correspondence of leisure, with Carry out transverse slat 413 spacing to the greatest extent may be used.The planform being placed in the first location plunger and the second location plunger is the most identical, this Utility model embodiment does not do restriction further.

Please continue to refer to Fig. 7-10, as stated above, as a kind of embodiment of this utility model embodiment, it is assumed that The first location plunger selected in this utility model embodiment and the second location plunger are completely identical in structure, to scheme As a example by the first location plunger 421 shown in 7-10, the internal structure of location plunger is described in further detail.

Such as Fig. 7-10, described first location plunger 421 includes: first bolt the 4211, first positioning thread insert 4212, the One location spring 4213.

Wherein, described first bolt 4211 is provided with described first positioning end 4211a；Described first positioning thread insert 4212 are set on described first bolt 4211, and described first positioning thread insert 4212 and described first bolt 4211 Between be provided with one first compression stroke 4214.Can be understood as the first positioning thread insert described in this utility model embodiment The internal diameter of 4212, more than the external diameter of described first bolt 4211, thus makes the first positioning thread insert 4212 be set in described Time on first bolt 4211, there is therebetween neutral region, this neutral region is above-mentioned first compression stroke 4214.Described first location spring is arranged in described first compression stroke 4214；Wherein, described first positioning end 4211a depends on Secondary through described first location spring 4213, described first compression stroke 4214 and described first side plate 411, with described first Chute internal projection in side plate 411 or contraction.

It is noted that shown in Fig. 7-8 be first positioning end 4211a chute in described first side plate 411 in Schematic diagram during contraction state.Shown in Fig. 9-10 is first positioning end 4211a chute convex in described first side plate 411 The schematic diagram during state of rising.And in order to preferably by the first location spring 4213 the most now at the first compression stroke 4214 In, on the described first positioning end 4211a of the first bolt 4211 described in this utility model embodiment, it is provided with one first Card convex 4215, to be fully defined in described first compression stroke 4214 by described first location spring 4213, and makes described First positioning end 4211a, when relative to chute contract in described first side plate 411, is pressed by described first card convex 4215 Contract described first location spring 4213.

Specifically, this utility model embodiment is during actual job, and the first location spring 4213 is in the first compression In space 4214, whole process is in compression or its pre-compressed state, thus makes in its natural state, the first location spring 4213 Described first positioning end 4211a is promoted to be entered by the first side plate 411 by the elasticity tension of self in the first compression stroke 4214 Enter in the chute of described first side plate 411, and then the transverse slat 413 in being in chute is positioned.And when needing transverse slat 413 When skidding off from chute, namely when needing to dismantle The Cloud Terrace 3 from fuselage 1, now have only to manual toggle the first bolt 4211 so that the first positioning end 4211a compresses the first location spring 4213 by the first card convex 4215, then makes the first location End 4211a skids off in the chute of the first side plate 411, and then realizes skidding off relative to the first side plate 411 of transverse slat 413.And work as Without External Force Acting after the first bolt 4211, under the elasticity tension effect of the first location spring 4213, continue to press on the One positioning end 4211a carries out return, namely the duty of the first location plunger 421 shown in Fig. 9 or Figure 10.Effective real Show the installation and removal of The Cloud Terrace without by any extraneous utensil such as spanner etc., easy to operate, have quickly, spy easily Point.

In this utility model embodiment, described second location plunger includes: the second bolt, described second location spiral shell Bolt is provided with described second positioning end；Second positioning thread insert, described second positioning thread insert is set on described second bolt, And it is provided with one second compression stroke between described second positioning thread insert and described second bolt；Second location spring, institute State the second location spring to be arranged in described second compression stroke；Wherein, described second positioning end sequentially passes through described second calmly Position spring, described second compression stroke and described second side plate, with the chute internal projection in described second side plate or contraction. On described second positioning end of described second bolt, it is provided with one second card convex, to be limited by described second location spring In described second compression stroke, and make described second positioning end relative to the chute contract in described second side plate Time, by the described second location spring of described second card convex compression.

As it has been described above, the second location plunger in this utility model embodiment and the first location plunger shown in Fig. 7-10 The structure of 421 is identical, the most no longer repeats the internal structure of the second location plunger, for the second location plunger The non-detailed portion of internal structure, see the detailed portion of the first location plunger 421 in this utility model embodiment.

Secondly, for the fuselage 1 that this utility model embodiment provides,

See Fig. 1-2 and 11-12, the fuselage 1 that this utility model embodiment provides has removable feature.Thus Make again when the internally installed device of fuselage 1, convenient, fast.Specifically, described fuselage 1 at least may include that body 12, casing 11 and the second dismounting assembly 13.

Wherein, the inside of described body 12 is hollow-core construction；At least one installing port 121 it is provided with on described body 12； Detachable for described casing 11 is connected on described body 12 by described second dismounting assembly 13.Meanwhile, described first dismounting Assembly 4 is fixed on the bottom of described body, and described signal framing assembly 5 is fixed on described body 12；So that at described machine Parts to be installed in body 12 are placed into by described installing port relative to described body 12 or are removed.As preferably, this The quantity of the described second dismounting assembly 13 in utility model embodiment is at least 2, and 2 described two dismounting assemblies are symmetrically It is distributed in the both sides of described casing 11, in order to the connection between casing 11 and body 12 is more firm.

Further, see Figure 12, described second dismounting assembly 13 includes: socket 131 and the 3rd location plunger 132. Wherein, described socket 131 is fixed on described body 12；Described 3rd location plunger 132 is fixed in described casing 11, and institute State the 3rd location plunger 132 and include the 3rd positioning end.Thus make the described socket of insertion 131 that described 3rd positioning end is corresponding In, with by described casing 11 and described body 12 clamping.

Here it should be noted that described second dismounting assembly 13 in socket 131 be for insert parts carry out The effect of screens, is similar to keeper principle.In described second dismounting assembly 13, the 3rd location plunger 132 is for insertion into socket In 131, and then casing 11 and body 12 are played the effect that bridge connects.Certainly, the 3rd location in this utility model embodiment The structure of plunger 132 can be diversified.

Such as, can as shown in figure 12, described 3rd location plunger 132 may include that locating dowel 1321 and the 3rd spacing spiral shell Bolt 1322, described locating dowel 1321 is fixed in described casing 11, and described 3rd caging bolt 1322 is fixed on described location On post 1321；Described 3rd caging bolt 1322 is provided with described 3rd positioning end.And then insert socket by the 3rd positioning end In 131, casing 11 is removably connected with body 12.As the quantity of above-mentioned second dismounting assembly 13 is at least 2, and 2 Individual described two dismounting assemblies are symmetrically dispersed in the both sides of described casing 11.In specific implementation process, can first mate insertion one 3rd caging bolt 1322 of side and socket 131, then at the 3rd caging bolt 1322 and socket of corresponding coupling opposite side 131.Certainly, in this kind of embodiment, casing 11 can also be to be made up of flexible material so that casing 11 presents flexible special Levy, so pinch the both sides of casing 11 by hands and casing 11 can be made to prolong the center portion thereof position be curved, the casing 11 after bending Corresponding body 12 of placing is fixed with on the position of two sockets 131, loosens the casing 11 being pinched, and such casing 11 is at self Elasticity tension effect under automatically restore to original state, the casing 11 in recovery process is owing to being precisely placed on two 3rd caging bolt 1322 and the position of two socket 131 correspondences, thus make the most corresponding the leading to of the casing after recovering 11 Cross two the 3rd caging bolts 1322 each to insert in two sockets 131, complete to be connected with the quick of body 12.Have conveniently, Feature efficiently.

For another example, the 3rd location plunger 132 in this utility model embodiment can also is that as in above-mentioned first dismounting assembly 4 First location plunger structure.That is: the described 3rd positions plunger 132 may include that locating dowel 1321, described locating dowel 1321 It is fixed in described casing 11；3rd bolt, described 3rd bolt is fixed in described locating dowel, and the described 3rd is fixed Position bolt is provided with described 3rd positioning end；3rd positioning thread insert, described 3rd positioning thread insert is set in described 3rd location spiral shell On bolt, and it is provided with one the 3rd compression stroke between described 3rd positioning thread insert and described 3rd bolt；3rd location bullet Spring, described 3rd location spring is arranged in described 3rd compression stroke；Wherein, described 3rd positioning end sequentially passes through described Three location springs, described 3rd compression stroke insert in described socket.Further, the described 3rd of described 3rd bolt On positioning end, it is provided with one the 3rd card convex, so that described 3rd location spring is limited in described 3rd compression stroke, and makes When described 3rd positioning end and described socket are separated, by the described 3rd location spring of described 3rd card convex compression.

In this utility model embodiment, as the presently preferred embodiments, described 3rd caging bolt and/or described 3rd location Bolt is mutually perpendicular to described locating dowel.Fixing connection between described locating dowel and described casing is welding；And/or, described Locating dowel and described casing are one-body molded.Described locating dowel and described 3rd caging bolt and/or described 3rd bolt it Between fixing connection be welding；And/or, described locating dowel and described 3rd caging bolt are one-body molded.

Again, for described signal framing assembly 5,

Referring to Figure 13-14, described signal framing assembly 5 also includes: location bar 51 and spiral shell dish 52.

Wherein, described location bar 51 includes fixing end 511 and a support end 512, and described location bar 51 is by described solid Fixed end 511 is fixed in described casing 11.Described spiral shell dish 52 is fixed on described location bar 51 by described support end 512, and The inside of described spiral shell dish 52 is hollow-core construction so that described localizer 53 is fixed in described spiral shell dish 52.Described localizer 53 leads to Cross location bar 51 and spiral shell dish 52 is arranged on described fuselage 1, thus make localizer 53 and described fuselage by spiral shell dish 52 The external air flow of 1 is isolated；Effectively avoid localizer 53 the most exposed when external fuselage, during unmanned plane during flying outside Boundary's air-flow, extraneous dampness or extraneous shelter because of with localizer 53 Long Term Contact or friction and the localizer 53 that causes makes moist Or damage, have the advantages that security performance is high.

As preferably, described location bar 51 and described casing 11 are one-body molded；And/or, described location bar 5151 and described Spiral shell dish 52 is one-body molded.

Certainly, for spiral shell dish 52, it is the equal of a protective cover of localizer 53, for carrying out localizer 53 Protection, in this utility model embodiment, described spiral shell dish 52 can at least include: the first blind nut 521, described first blind nut 521 It is provided with female thread；Second blind nut 522, described second blind nut 522 is provided with external screw thread, described first blind nut 521 and described The threaded composition of two blind nuts 522 described spiral shell dish 52；Wherein, described first blind nut 521 and described second blind nut 522 can be in circles Shape, it is also possible to be square shape, or diamond shaped, this utility model embodiment does not limits.It is noted that described location The angle constituted between bar 51 and described casing 11 is an acute angle.That is, center vertical pivot and casing 11 place of bar 51 are positioned Plane be not mutually perpendicular to, and location bar 51 inclined plane with towards tail orientation, the most further reduce location bar 51 during unmanned plane during flying with the contact resistance of external air flow.

Again, for rotor power assembly 6, referring to Figure 15-16, described rotor power assembly 6 at least includes: the (it is electric that the first electricity tune 64 and the following second electricity tune all can be understood as heat radiating type for one motor 61, refrigerating seat 63 and the first electric tune 64 Adjust).Being fixed on described first motor 61 of first rotor rotational of power is provided owing to rotating to be unmanned plane during flying；Described cold But seat 63 is fixed in described rotor shaft 2, and described first motor 61 is fixed on described refrigerating seat 63.Real at this utility model Executing in example, the inside of refrigerating seat 63 is hollow-core construction, and described first electricity adjusts 64 inside being fixed on described refrigerating seat 63, and divides It is not connected with the described flight control system within described first motor 61 and fuselage 1, with by described flight control system control Make described first electricity and adjust 64, it is achieved drive described first motor 61 to drive described first rotor to rotate.

It should be strongly noted that described refrigerating seat 63 is provided with at least one vent 631, with by described refrigerating seat The inner space of 63 communicates with free surrounding space.Thus make when the first electricity is adjusted the inside that 64 are fixed on refrigerating seat 63, real Time form convection current with the cold air of refrigerating seat 63 periphery, to adjust 64 to cool down in real time the first electricity, effectively avoid because of the One electricity adjust 64 overheated mistakes scald and cause first electricity adjust 64 cannot be properly functioning technological deficiency.Meanwhile, by direct for the first electricity tune 64 It is fixed on the peripheral position of fuselage 1, and owing to the first rotor is arranged on refrigerating seat 63, therefore the first electricity tune 64 and the first rotor Between connection line the shortest, significantly reduce the first electricity and adjust between first rotor long and cause because there is circuit Power attenuation, possesses efficient, energy-conservation feature.

Certainly, in this utility model embodiment, referring to Figure 19, rotor power assembly 6 can also include the second motor 62 and second electricity adjust, and described second electricity adjust be connected with described second motor 62 and described flight control system respectively.Now, may be used Solid to be interpreted as that described refrigerating seat 63 includes that the first stationary plane and the second stationary plane, described first motor 61 are fixed on described first Determining on face, described second motor 62 is fixed on described second stationary plane, to move described second electricity by described second electricity transfer drive Machine 63 drives the second rotor to rotate.Same with the first electricity phase modulation, described second electricity is adjusted and also is secured to the interior of described refrigerating seat 63 Portion.So by shown in Figure 19 2 motors are set and 2 electricity are adjusted, and then realize the unmanned plane structure of coaxial double-oar.

In this utility model embodiment, it can be identical structure that first electricity mediation the second electricity is adjusted, with the first electricity As a example by adjusting 64, referring to Figure 17-18, it at least may include that the first electric capacity 641, first circuit board 642 and the first heat sink 643.Wherein, described first circuit board 642 controls with described first electric capacity 641, described first motor 61 and described flight respectively System connects, and described first heat sink 643 is attached on described first circuit board 642.As preferably, described first heat sink 643 can be aluminium sheet.So on the one hand, the first electricity is adjusted 64 to enter by convection by the vent 631 offered at refrigerating seat Row cooling, adjusts 64 to dispel the heat the first electricity simultaneously also by the first heat sink 643 further.To reach to ensure that the first electricity adjusts 64 The technique effect of safe operation.

For the second electricity is adjusted, identical with the first electricity tune 64, it is also possible to include: the second electric capacity；Second circuit board；And the Two heat sinks；Wherein, described second circuit board respectively with described second electric capacity, described second motor and described flight control system Connect, and described second heat sink is attached on described second circuit board.Owing to, in this utility model embodiment, second is electric The internal structure that the internal structure adjusted is adjusted with the first electricity is identical, and here is omitted, and the internal structure that the second electricity is adjusted is the most detailed State part, refer to the first electricity and adjust.

As preferably, described first circuit board is between described first electric capacity and described first heat sink；And/or, institute State second circuit board between described second electric capacity and described second heat sink.

Further, continuing with seeing Figure 20-21, for the annexation between the first motor 61 and the first rotor 8 For, this utility model embodiment additionally provides a kind of Quick-dismantle component, the Quick Release between the first motor 61 and the first rotor Connect.Realize when carrying out installation or the dismantlement work of the first rotor 8, it is only necessary to by rotating described first rotor 8, Ji Keshi The now fastening between the first rotor 8 and the first motor 61 or separation, namely without by external operation instrument (such as handle) i.e. Installation or the dismantlement work of the first rotor 8 can be completed, there is quick, portable and that working performance is high feature.

Specifically, referring to Figure 20-21, in the present embodiment, the first motor 61 includes first surface 611 and second surface 612.In an embodiment, first surface 611 can be understood as the upper surface of the first motor 61, and second surface 612 is appreciated that For being the lower surface of the first motor 61, and described first motor 61 is fixed on described refrigerating seat 63 by described first surface 611 On.Meanwhile, the described first rotor 8 detachable company of first surface 611 by described Quick-dismantle component 7 with described first motor 61 Connect.

During actual job, Quick-dismantle component 7 is by threaded to both the first rotor 8 and the first motor 61.Make in reality In the operation process of border when needing the first rotor of unmanned plane is installed or dismantled, the most only need to rotate described first rotation The wing 8, as turned clockwise the first rotor 8 or rotate counterclockwise the first rotor 8, can realize described first rotor 8 and described Installation or removal between first motor 61.Compared to traditional bolt that directly uses, the first rotor 8 is fixed on the first motor On 61, when the first rotor 8 is dismantled from the first motor 61 by needs, or when installing, it is both needed to by extraneous handle to turn spiral shell Bolt, can complete dismounting and the installment work of the first rotor 8.And due to for connecting consolidating of the first rotor 8 and the first motor 61 Determine the individual component that bolt is individualism, when by handle turn bolt unloaded time, often due to execute-in-place environment Complexity, easily cause the loss of fixing bolt, and once fix bolt and lose, the most just cannot complete the first rotor 8 and the The installment work of one motor 61, i.e. causes the serious consequence that flight equipment cannot fly.And the present embodiment, it is exactly based on employing Quick-dismantle component 7 is by threaded to both the first rotor 8 and the first motor 61 so that the two is when installing or dismantle, it is not necessary to borrow Help external operation instrument (such as handle), quick and convenient, have the advantages that working performance is high.

For Quick-dismantle component 7, continuing with seeing Figure 21, described Quick-dismantle component 7 at least includes: first screw the 71, second spiral shell Nail the 72, first screw buckle 73 and the first dismounting nut 74.Wherein, the inwall of described first screw buckle 73 is provided with the first female thread 76, and the bottom of described first screw buckle 73 offers the first screw 77 so that described first screw 432 is through described first spiral shell Described first screw buckle 73 is fixed on the first surface 611 of described first motor 61 by hole 77.Described first dismounting nut 74 Outer wall be provided with first external screw thread 78 suitable with described first female thread 76, and the top of described first dismounting nut 74 Offer the second screw 79 so that described second screw 72 sequentially passes through described first rotor 8, described second screw 79 by described First dismounting nut 74 is fixed on described first rotor 8.

Wherein, the first screw buckle 73 is fixed on the first surface 611 of the first motor 61 by the first screw 71, and first tears open Removing nut 74 is fixed on the first rotor 8 by the second screw 72.And first the inwall of screw buckle 73 offered first in spiral shell Stricture of vagina 76, and first external screw thread 78 offered of outer wall of the first dismounting nut 74 mates completely, namely the first female thread 76 and the Occlusion locking can be realized between one external screw thread 78.Thus make, when the first rotor 8 is arranged in rotor shaft 3 by needs, Owing to the first motor 61 is fixed on the end of rotor shaft 3, also will be arranged on the first motor 61 by the first rotor 8.Now, it is only necessary to Manual rotation the first rotor 8 so that the first external screw thread 78 is engaged mutually with the first female thread 76, continues to rotate, then realizes first Dismounting nut 74 and the locking of the first screw buckle 73, owing to the first dismounting nut 74 is fixed on the first rotor 8, the first screw buckle 73 are fixed on the first motor 61, namely the locking achieving the first rotor 8 and the first motor 61 (rotor shaft 3) is installed.And work as When needing dismounting, the most only need to reversely rotate the first rotor 8, it is achieved the separation of the first external screw thread 78 and the first female thread 76 is i.e. Can.There is feature swift to operate, convenient.

It should be noted that unmanned plane is during practical flight, the direction of rotation of the first rotor 8 is the side of rotation counterclockwise To, now, owing in flight course, the first rotor 8 itself is in rotating state, and the first rotor 8 and the first motor Itself also it is to use to rotate the connected mode realizing fastening in an embodiment between 61.Such as, when the first rotor 8 is relative to When one motor 61 is to be fastened therebetween by the realization that turns clockwise, due to the normal rotation of the first rotor 8 in flight course For counterclockwise, now rotate along with the most normal of the first rotor 8, namely the first rotor 8 is equivalent to the first motor 61 and has inverse The driving that hour hands rotate.And owing to the first rotor 8 is to realize the two it by turning clockwise relative to the first motor 61 Between fastening, then otherwise when occurring that the first rotor 8 is to rotate counterclockwise relative to the first motor 61, i.e. can cause the first rotation Loosening occurs in fastening relationships between the wing 8 and the first motor 61, and even results in the first rotor 8 and flies away from the first motor 61 and cause nothing The phenomenon of man-machine crash occurs.

Therefore, in flight course, the is caused due to normal the rotation counterclockwise of the first rotor 8 in order to avoid unmanned plane Loosening occurs in fastening relationships between one rotor 8 and the first motor 61, and this utility model embodiment is by the first rotor 8 and the first electricity The direction that the direction tightened is also configured to rotate counterclockwise is rotated between machine 61.That is, set by the outer wall of the first dismounting nut 74 The first external screw thread 78 put and the occlusion locking direction of first female thread 76 set by inwall of the first screw buckle 73 are also inverse Clockwise.It is the tightest by rotating realization counterclockwise for thus making to work as the first rotor 8 relative to the first motor 61 Gu time, due in flight course the first rotor 8 normally rotate to be counterclockwise, now the most normal along with the first rotor 8 Rotate, namely the first rotor 8 is equivalent to the first motor 61 and also has the trend of rotation counterclockwise.

And owing to the first rotor 8 could be realized therebetween by rotation counterclockwise exactly relative to the first motor 61 Fastening, so on the one hand, is effectively prevented when the first rotor 8 is to be stung by the realization that turns clockwise relative to the first motor 61 When closing locking, owing to normally rotating to be of the first rotor 8 causes the fastening between the first rotor 8 and the first motor 61 counterclockwise Loosening occurs in relation, and even results in the first rotor 8 and flies away from the first motor 61 and the technological deficiency that causes unmanned plane to crash.The opposing party Face, owing to the first rotor 8 itself is also by rotating counterclockwise the fastening that could realize therebetween relative to the first motor 4, When rotating along with the most normal of the first rotor 8, and make the first rotor 8 be equivalent to the first motor 61 and also have rotation counterclockwise Trend, the most also increase the first rotor 8 and the first motor 61 fastening relationships therebetween, it is ensured that flight equipment Normal safe flies, and has the advantages that security performance is high.

Further, continuing with seeing Figure 20-21, as described above, when sequentially passing through described by the second screw 72 When described first dismounting nut 74 is fixed on described first rotor 8 by one rotor 8, described second screw 79, due to unmanned plane In flight course, the external resistance many factors suffered by the first rotor 8, such as air-flow, wind direction etc..This allows for flight course In the first rotor 8 bigger relative to the vibrations of the first motor 61 and/or rotor shaft 3, but, long vibrations can make Annexation extremely unstable between two screw the 72, first rotors 8 and the first dismounting nut 74 three, even causes the second screw 72 loosen, and then cause security incident.Therefore, the present embodiment is by setting up the first vibration damping sheet 75, and at described first vibration damping sheet The first through hole is offered, so that described second screw 72 sequentially passes through described first through hole, described first rotor 8 and the second spiral shell on 75 Described first dismounting nut 437 is fixed on described first rotor 8 by hole 79.As preferably, the first vibration damping sheet 75 can be in disk Shape, to increase the first vibration damping sheet 75 and contact area of the first rotor 8 upper surface, by the second screw 72 by the first vibration damping sheet 75 With the first rotor 8 upper surface relative to fastening, to reduce the vibrations relative to the first motor 61 of first rotor 8, improve and flew Safety and stability performance in journey.

As preferably, the quantity of described first screw 71 is 2；The quantity of described second screw 72 is 2；Described first The quantity of screw 77 is 2；The quantity of described second screw 79 is 2.Wherein, each corresponding one of described first screw 71 Described first screw 77 so that each described first screw 71 passes corresponding described first screw 77 by described first Screw buckle 73 is fixed on described first motor 61；Each corresponding described second screw 79 of described second screw 72, makes Obtain each described second screw 72, through corresponding described second screw 79, described first screw buckle 73 is fixed on institute State on the first motor 61.

It is last it should be noted that although the present embodiment merely illustrates the first motor and the first rotor passes through Quick-dismantle component 7 are attached so that its first rotor has the feature of fast quick-detach.But for many rotor wing unmanned aerial vehicles, described above Between second rotor and the second motor, it is also possible to be attached by Quick-dismantle component 7 so that the second rotor has equally quickly to be torn open The feature unloaded.The connected mode by Quick-dismantle component for the second motor and the second rotor, with the first motor and the first rotor it Between exercise mode identical, here is omitted.

Although having been described for preferred embodiment of the present utility model, but those skilled in the art once knowing substantially Creative concept, then can make other change and amendment to these embodiments.So, claims are intended to be construed to The all changes including preferred embodiment and falling into this utility model scope and amendment.

Obviously, those skilled in the art can carry out various change and modification without deviating from this practicality to this utility model Novel spirit and scope.So, if of the present utility model these amendment and modification belong to this utility model claim and Within the scope of its equivalent technologies, then this utility model is also intended to comprise these change and modification.

Claims (10)

1. a The Cloud Terrace fast disassembly type unmanned plane, wherein, unmanned plane includes the first rotor, rotor shaft, The Cloud Terrace and flight control system, It is characterized in that, described The Cloud Terrace fast disassembly type unmanned plane includes:

Fuselage, described fuselage includes:

Casing；

Body, the inside of described body is hollow-core construction, and is provided with at least one installing port on described body；

Second dismounting assembly, detachable for described casing is connected on described body, and passes through by described second dismounting assembly Described casing covers described installing port；

Wherein, parts to be installed in described body are placed into relative to described body by described installing port or are taken Go out；

First dismounting assembly, described first dismounting assembly is fixed on described body；

Signal framing assembly, described signal framing assembly is fixed in described casing, and is provided with in described signal framing assembly For unmanned plane being carried out the localizer of signal framing；

Quick-dismantle component, described first rotor is rotationally fixed on described rotor power assembly by described Quick-dismantle component；

Wherein, by described first dismounting assembly, described The Cloud Terrace is connected on described body so that described The Cloud Terrace is by described Between first dismounting assembly and described body detachable, and described localizer is arranged on described machine by described signal framing assembly On shell, it is isolated with the external air flow by described localizer with described fuselage.

2. The Cloud Terrace fast disassembly type unmanned plane as claimed in claim 1, it is characterised in that described first dismounting assembly includes:

Fixed plate, described fixed plate is fixed on described body, and is slidably connected with described The Cloud Terrace so that described The Cloud Terrace relative to Described fixed plate is slided；

Positioning element, described positioning element is fixed in described fixed plate, with to described The Cloud Terrace relative to the position of described fixed plate Put and position, and then realize described The Cloud Terrace relative to the installation of described body or dismounting.

3. The Cloud Terrace fast disassembly type unmanned plane as claimed in claim 2, it is characterised in that described fixed plate includes:

First side plate；

Second side plate, described first side plate and described second side plate are parallel；

Transverse slat, described first side plate and described second side plate are perpendicular with described transverse slat, and described transverse slat is respectively with described first Side plate and described second side plate are slidably connected, and described The Cloud Terrace is fixing with described transverse slat to be connected, and then makes institute by described transverse slat State The Cloud Terrace to slide relative to described first side plate and described second side plate；

Described positioning element is individually fixed on described first side plate and described second side plate, with to described transverse slat relative to described The position of the first side plate and described second side plate positions.

4. The Cloud Terrace fast disassembly type unmanned plane as claimed in claim 3, it is characterised in that

It is respectively arranged with a chute, so that described transverse slat is arranged on described chute on described first side plate and described second side plate In so that described transverse slat is slided relative to described first side plate and described second side plate by described chute；

One end of described positioning element corresponding through described first side plate, described second side plate, and in described chute internal projection Or shrink so that one end of described positioning element relative to described chute when described chute internal projection, described positioning element One end stop described transverse slat slide in described chute, one end of described positioning element relative to described chute described During chute contract, one end of described positioning element is separated with described transverse slat, so that described transverse slat is carried out in described chute Slide.

5. The Cloud Terrace fast disassembly type unmanned plane as claimed in claim 4, it is characterised in that described positioning element includes:

First location plunger, described first location plunger includes the first positioning end；

Second location plunger, described second location plunger includes the second positioning end；

Wherein, described first positioning end corresponding through described first side plate, and the chute internal projection in described first side plate Or shrink, so that described first positioning end is when relative to chute internal projection in described first side plate, described first location End stops that described transverse slat slides in chute, and described first positioning end is received in relative to the chute in described first side plate During contracting, described first positioning end is separated with described transverse slat, so that described transverse slat slides in chute；

Wherein, described second positioning end corresponding through described second side plate, and the chute internal projection in described second side plate Or shrink, so that described second positioning end is when relative to chute internal projection in described second side plate, described second location End stops that described transverse slat slides in chute, and described second positioning end is received in relative to the chute in described second side plate During contracting, described second positioning end is separated with described transverse slat, so that described transverse slat slides in chute.

6. The Cloud Terrace fast disassembly type unmanned plane as claimed in claim 5, it is characterised in that

Described first location plunger includes:

First bolt, described first bolt is provided with described first positioning end；

First positioning thread insert, described first positioning thread insert is set on described first bolt, and described first positioning thread insert And it is provided with one first compression stroke between described first bolt；

First location spring, described first location spring is arranged in described first compression stroke；

Wherein, described first positioning end sequentially passes through described first location spring, described first compression stroke and described first side Plate, with the chute internal projection in described first side plate or contraction；

With,

Described second location plunger includes:

Second bolt, described second bolt is provided with described second positioning end；

Second positioning thread insert, described second positioning thread insert is set on described second bolt, and described second positioning thread insert And it is provided with one second compression stroke between described second bolt；

Second location spring, described second location spring is arranged in described second compression stroke；

Wherein, described second positioning end sequentially passes through described second location spring, described second compression stroke and described second side Plate, with the chute internal projection in described second side plate or contraction.

7. The Cloud Terrace fast disassembly type unmanned plane as claimed in claim 6, it is characterised in that

On described first positioning end of described first bolt, it is provided with one first card convex, with by described first location spring It is limited in described first compression stroke, and described first positioning end is received in relative to the chute in described first side plate During contracting, by the described first location spring of described first card convex compression；

And/or,

On described second positioning end of described second bolt, it is provided with one second card convex, with by described second location spring It is limited in described second compression stroke, and described second positioning end is received in relative to the chute in described second side plate During contracting, by the described second location spring of described second card convex compression.

8. The Cloud Terrace fast disassembly type unmanned plane as claimed in claim 1, it is characterised in that described second dismounting assembly includes:

Socket, described socket is fixed on described body；

3rd location plunger, described 3rd location plunger is fixed in described casing, and described 3rd location plunger includes the 3rd Positioning end；

Wherein, in the described socket of insertion that described 3rd positioning end is corresponding, with by described casing and described body clamping.

9. The Cloud Terrace fast disassembly type unmanned plane as claimed in claim 8, it is characterised in that

Described 3rd location plunger includes: locating dowel and the 3rd caging bolt, described locating dowel is fixed in described casing, and institute State the 3rd caging bolt to be fixed in described locating dowel；

Described 3rd caging bolt is provided with described 3rd positioning end.

10. The Cloud Terrace fast disassembly type unmanned plane as claimed in claim 1, it is characterised in that described signal framing assembly also includes:

Location bar, described location bar includes fixing end and a support end, and described location bar is fixed on institute by described fixing end State in casing；

Spiral shell dish, described spiral shell dish is fixed on the bar of described location by described support end, and the inside of described spiral shell dish is hollow-core construction, Described localizer is fixed in described spiral shell dish.