CN104709460B - Fixed-wing unmanned aerial vehicle capable of being quickly disassembled and assembled - Google Patents
Fixed-wing unmanned aerial vehicle capable of being quickly disassembled and assembled Download PDFInfo
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- CN104709460B CN104709460B CN201510107698.1A CN201510107698A CN104709460B CN 104709460 B CN104709460 B CN 104709460B CN 201510107698 A CN201510107698 A CN 201510107698A CN 104709460 B CN104709460 B CN 104709460B
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/36—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like adapted to receive antennas or radomes
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
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- Aviation & Aerospace Engineering (AREA)
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Abstract
The invention discloses a fixed-wing unmanned aerial vehicle capable of being quickly disassembled and assembled. The fixed-wing unmanned aerial vehicle comprises an airframe main body, wings mounted on the airframe main body, and a tail part, wherein the tail part comprises empennages and a tail rod fixed between the airframe main body and the empennages; a tail rod passage is formed in the airframe main body; one end of the tail rod is mounted in the tail rod passage; the depth by which the tail rod is inserted in the tail rod passage can be adjusted. According to the fixed-wing unmanned aerial vehicle capable of being quickly disassembled and assembled disclosed by the invention, in the transportation process, the tail rod can be inserted frontwards to reduce the space usage.
Description
Technical field
The application belongs to technical field of taking photo by plane, and more particularly to a kind of quick release installs fixed-wing unmanned vehicle.
Background technology
Unmanned vehicle have small volume, low lightweight, expense, flexible operation and it is safe the characteristics of, extensively can answer
For taking photo by plane, monitoring, search and rescue, the field such as resource exploration.
Existing fixed-wing unmanned vehicle, as left and right wing and empennage are longer, takes up room big, not readily portable
And transport.In addition, the antenna of fixed-wing unmanned vehicle is usually mounted to the top of fuselage main body, due to antenna it is above,
On the one hand there is a problem of that signal is bad, on the other hand, as antenna convexedly stretches in top, easily send out in transport or moving process
Life is collided and causes to damage.
In view of this, it is necessary to which a kind of new fixed-wing unmanned vehicle is provided.
The content of the invention
It is an object of the invention to provide a kind of quick release installs fixed-wing unmanned vehicle, to overcome prior art
In deficiency.
For achieving the above object, the present invention provides following technical scheme：
The embodiment of the present application discloses a kind of quick release and installs fixed-wing unmanned vehicle, including fuselage main body, with
And the wing that is installed in fuselage main body and afterbody, the afterbody includes empennage and is fixed between fuselage main body and empennage
Foot piece, the fuselage main body are provided with a foot piece passage, and one end of the foot piece is installed in the foot piece passage, the foot piece
The depth adjustable being inserted in the foot piece passage.
Preferably, install in fixed-wing unmanned vehicle in above-mentioned quick release, the foot piece passage is through described
Fuselage main body.
Preferably, install in fixed-wing unmanned vehicle in above-mentioned quick release, the fuselage main body includes skeleton
And the housing being installed on the outside of skeleton, the skeleton includes a horizontally disposed gripper shoe, and the both sides of the gripper shoe are symmetrical
Reinforcing plate is installed, the reinforcing plate is vertically arranged with gripper shoe, fixed support, the tail are installed above the gripper shoe
Bar passage is formed between the fixed support and gripper shoe.
Preferably, install in fixed-wing unmanned vehicle in above-mentioned quick release, offer on the fixed support
Fixing hole, the gripper shoe are provided with screw, offer through hole on the foot piece, and described fixing hole, screw and through hole are upper and lower
Correspondence.
Preferably, install in fixed-wing unmanned vehicle in above-mentioned quick release, offer in the gripper shoe many
Individual lightening hole.
Preferably, install in fixed-wing unmanned vehicle in above-mentioned quick release, the front end of the gripper shoe is fixed
There is an on-hook plate, the on-hook plate vertical support plate arranges, offers to hang the suspension of aerial camera on the on-hook plate
Hole, is capped with head-shield, detachably installs between the head-shield and fuselage main body on the outside of the on-hook plate.
Preferably, install in fixed-wing unmanned vehicle in above-mentioned quick release, the top of the fuselage main body is recessed
If being formed with a umbrella storehouse space, umbrella Cang Gai above the space of the umbrella storehouse, is capped with, can between the umbrella Cang Gai and fuselage main body
Dismounting is fixed.
Preferably, install in fixed-wing unmanned vehicle in above-mentioned quick release, the lower direction of the fuselage main body
It is upper it is recessed be formed with an on-hook space, be capped with Lower Hold lid at the opening in the on-hook space, the Lower Hold lid and fuselage main body it
Between be detachably fixed.
Preferably, install in fixed-wing unmanned vehicle in above-mentioned quick release, the wing include stage casing wing,
Left section of wing and right section of wing, the stage casing wing are fixed in the fuselage main body, and the left section of wing and right section of wing divide
The left and right sides of stage casing wing is not removably mounted to.
Preferably, install in fixed-wing unmanned vehicle in above-mentioned quick release, the left section of wing and right section of machine
The end of the wing has each extended over guide rod, and the end of the stage casing wing is provided with the installing hole for accommodating the guide rod, the guide rod bag
The first guide rod and the second guide rod being set up in parallel is included, the diameter and development length of first guide rod are all higher than described second and lead
Bar, the diameter of second guide rod are gradually reduced along the direction for deviating from the left section of wing or right section of wing, the left section of wing
Between the wing of stage casing, and right section of wing and stage casing wing between be respectively fixed with the card of relative movement between restriction adjacent wing
Button, the buckle include from middle part bending two elastic arms for being formed, and two elastic arms are in the opposite recessed formation of relative position
There is holding section, the holding section has curved surfaces, and outwards bending is formed with adjutage respectively for the end of described two elastic arms,
It is in splayed opening between described two adjutages, on the end face of the stage casing wing both sides, is respectively fixed with the first installing plate,
Be fixed with the second installing plate on the end face of the left section of wing and right section of wing, on first installing plate and the second installing plate in
Hole clipping or draw-in groove is respectively equipped with correspondence position, is respectively equipped with for described on the stage casing wing, left section of wing and right section of wing
The insert port of buckle elastic arm insertion, the insert port presses close to first installing plate or the second installing plate is arranged.
Preferably, install in fixed-wing unmanned vehicle in above-mentioned quick release, the both sides of the wing are symmetrical
A rotor is separately installed with position, and respectively by a Motor drive, the rear of the motor is formed with one to described each rotor
Heat dissipation channel, the heat dissipation channel are located at the lower section of the wing, are wherein provided with antenna in heat dissipation channel described in；The day
Line both horizontally and vertically between it is rotatable.
Compared with prior art, it is an advantage of the current invention that：
(1), of the invention for larger-size whole wing carries out three-stage fractionation, wherein stage casing wing can be integrated winged
The electronic circuit apparatus such as empty, reception, which is between fuselage main body without the need for dismounting.In transportation, can by left section of wing and
Right section of wing is disassembled, and saves space, convenient to transport.
(2), after, three sections of wings complete assembly, the separation between wing can be limited by buckle.
(3), in transportation, foot piece can be taken up room by front slotting reduction；
(4), antenna is installed on the lower section of wing, shares heat dissipation channel with motor, is not take up upper and lower space, and is moved through
Contact-impact being not susceptible in journey, and antenna being located at lower section, signal of communication is good.
Description of the drawings
In order to be illustrated more clearly that the embodiment of the present application or technical scheme of the prior art, below will be to embodiment or existing
Accompanying drawing to be used needed for having technology description is briefly described, it should be apparent that, drawings in the following description are only this
Some embodiments described in application, for those of ordinary skill in the art, on the premise of not paying creative work,
Can be with according to these other accompanying drawings of accompanying drawings acquisition.
Fig. 1 show the schematic perspective view of fixed-wing unmanned vehicle in the specific embodiment of the invention；
Fig. 2 show the exploded perspective view of fixed-wing unmanned vehicle in the specific embodiment of the invention；
Fig. 3 show the structural representation of fixed-wing unmanned vehicle skeleton in the specific embodiment of the invention；
Fig. 4 show in the specific embodiment of the invention the fixed schematic diagram between buckle and installing plate；
Fig. 5 show the sectional view of A-A in Fig. 4；
Fig. 6 show the upward view of fixed-wing unmanned vehicle in the specific embodiment of the invention；
Fig. 7 show the schematic perspective view after inserting before foot piece in the specific embodiment of the invention.
Specific embodiment
Below in conjunction with the accompanying drawing in the embodiment of the present invention, detailed retouching is carried out to the technical scheme in the embodiment of the present invention
State, it is clear that described embodiment is only a part of embodiment of the invention, rather than the embodiment of whole.Based on the present invention
In embodiment, the every other enforcement obtained on the premise of creative work is not made by those of ordinary skill in the art
Example, belongs to the scope of protection of the invention.
Shown in ginseng Fig. 1 and Fig. 2, fixed-wing unmanned vehicle includes fuselage main body 10, and is installed in fuselage main body 10
Wing 20 and afterbody 30, the foot piece 32 that afterbody 30 includes empennage 31 and is fixed between fuselage main body 10 and empennage 31.
Wing 20 includes stage casing wing 21, left section of wing 22 and right section of wing 23, and wherein, stage casing wing 21 is fixed on fuselage
In main body 10, left section of wing 22 and right section of wing 23 are removably mounted to the left and right sides of stage casing wing 21 respectively.
In the technical scheme, for larger-size whole wing carries out three-stage fractionation, wherein stage casing wing can be whole
Close and fly the electronic circuit apparatus such as empty, reception, which is between fuselage main body without the need for dismounting.In transportation, can be by left section of machine
The wing and right section of wing are disassembled, and save space, convenient to transport.
The end of left section of wing 22 and right section of wing 23 has each extended over guide rod 221, and the end of stage casing wing 21 coordinates leads
Bar 221 is provided with installing hole 211, and left section of wing 22 and right section of wing 23 can be quick with stage casing wing 21 by the realization of guide rod 221
It is fixed.Guide rod 221 is preferably set side by side with 2.When guide rod 221 is provided only with 1, which is preferably flat.
In the technical scheme, left section of wing 22 or right section of wing 23 are plugged on stage casing wing by two guide rods respectively
In installing hole, it is possible to achieve quickly assembly and disassembly, using two guide rods, can avoid assembling rear left section wing or right section of machine
Relatively rotate between the wing and stage casing wing.
Shown in ginseng Fig. 4 and Fig. 5, between left section of wing 22 and stage casing wing 21, and right section of wing 23 and stage casing wing 21
Between be respectively fixed with buckle 40, after stage casing wing 21 completes assembling with left section of wing 22 and right section of wing 23 respectively, card
40 being relatively fixed to the place of achieving a butt joint of button, therefore left section of wing 22 and right section of wing 23 can be prevented after fixation from stage casing
Transfer on wing 21.
Buckle 40 includes from middle part bending two elastic arms 41 for being formed, and two elastic arms 41 are recessed in opposite directions in relative position
If being formed with holding section 42, holding section 42 has curved surfaces.Outwards bending is formed with and prolongs respectively for the end of two elastic arms 41
Semi-girder 43, is in splayed opening between two adjutages 43.
With reference to shown in Fig. 3 and Fig. 6, the first installing plate 212, left section of machine on the end face of 21 both sides of stage casing wing, is respectively fixed with
Be fixed with the second installing plate 222 on the end face of the wing 22 and right section of wing 23, on the first installing plate 212 and the second installing plate 222 in
Hole clipping 2221 is respectively equipped with correspondence position.
The insertion for the insertion of 40 elastic arm of buckle 41 is respectively equipped with stage casing wing 21, left section of wing 22 and right section of wing 23
Mouth 231, insert port 231 presses close to the first installing plate 212 or the second installing plate 222 is arranged.
After stage casing wing 21 completes assembling with left section of wing 22 and right section of wing 23 respectively, the first installing plate 212 with
Second installing plate 222 is fitted, while the hole clipping on two installing plates is relative.The end of the first installing plate 212 and the second installing plate 222
End is clamp-oned between two elastic arms 41 by the splayed opening between two adjutages 43,41 points of two elastic arms of buckle 40
In insert port 231 that Cha Ru be on stage casing wing 21 and left section of wing 22, further buckle 40 is promoted until two holding sections 42
In the hole clipping for being slipped on two installing plates respectively.It is thus, buckle 40 will not come off from insert port 231 after completing engaging, while logical
Cross that buckle 40 can limit left section of wing 22 and right section of wing 23 comes off from stage casing wing 21, when needing left section of 22 He of wing
When right section of wing 23 is dismantled, directly buckle 40 is extracted.
Will be readily apparent, hole clipping 2221 can also be arranged to groove, the first installing plate 212 and the second installing plate 222 it
Between multiple buckles can also be set.
Fuselage main body 10 is provided with a foot piece passage, and one end of foot piece 32 is installed in the foot piece passage, and foot piece 32 is received
The adjustable length contracted in foot piece passage.Further, foot piece passage can be by interspersed super through fuselage main body 10, i.e. foot piece 32
Go out the head of fuselage main body 10.Structure after foot piece 32 shrinks is as shown in Figure 7.
In the technical scheme, foot piece 32 can be interted forward to shorten the space shared by whole afterbody 30, dismounting
Conveniently, space is saved, is facilitated and is transported, is easy to carry.When deployed, foot piece 32 can be extracted to relevant position, then by tail
Bar 32 is relatively fixed with fuselage main body 10.
Shown in ginseng Fig. 3, fuselage main body 10 includes skeleton and the housing being installed on the outside of skeleton, and skeleton includes that a level sets
The gripper shoe 11 put, the both sides of gripper shoe 11 are symmetrically installed with reinforcing plate 12, and reinforcing plate 12 is vertically arranged with gripper shoe 11.Support
Multiple lightening holes 111 are offered on plate 11.
In the technical scheme, skeleton structure is simple, greatly reduces the weight of body, and gripper shoe 11 passes through reinforcing plate 12
Fix with housing, the contact surface between skeleton and housing can be increased so that more consolidate between skeleton and housing, and,
Fagging 11 is not easy to bending deformation.
The top of gripper shoe 11 is provided with fixed support 13, foot piece passage be formed at fixed support 13 and gripper shoe 11 it
Between.Fixing hole is offered on fixed support 13, to being provided with screw below fixing hole in gripper shoe 11, is offered on foot piece
Through hole, it is in assembling, first that through hole on foot piece is corresponding with the fixing hole on fixed support, screw is each passed through into fixation then
Hole and through hole are simultaneously fixed with the screw in gripper shoe, so as to realize being relatively fixed between foot piece and fuselage main body.When needs are torn open
When unloading transport, unclamp screw and screw is extracted, insert before foot piece.
Stage casing wing 21 includes two support bars 213 being set up in parallel, and two support bars 213 are fixed by screws in machine
In body main body 10.In disassembled for transport, stage casing wing 21 is without the need for dismounting, stage casing wing 21 and fuselage main body from fuselage main body 10
10 can be transported as an entirety.
Gripper shoe 11 is fixedly arranged at the front end with an on-hook plate 14, and 14 vertical support plate 11 of on-hook plate arranges, open on on-hook plate 14
It is provided with to hang the suppending hole of aerial camera.The outside of on-hook plate 14 is capped with head-shield 50, head-shield 50 and fuselage main body 10 it
Between detachably install.
When needing to take photo by plane operation, first head-shield 50 is pulled down, then aerial camera is suspended on on-hook plate 14, knot of taking photo by plane
Beam, removes aerial camera and covers head-shield 50.
Left section of wing 22 and right section of wing 23 are separately installed with a rotor 61 in symmetric position, and each rotor 61 leads to respectively
Cross a motor 62 to drive, wherein, the rear of the motor 62 on left section of wing 22 is formed with a heat dissipation channel 63, the heat dissipation channel 63
Antenna 70 is inside installed, antenna 70 can both horizontally and vertically between rotate.Antenna 70 is installed on left section of wing 22
Lower section.
Will be readily apparent, antenna 70 can also be arranged in the heat dissipation channel of right section of wing 23.
Antenna 70 is installed on the lower section of wing, and one side communication efficiency is good, is on the other hand not take up 10 top of fuselage main body
Space, for above fuselage main body arrange umbrella storehouse space possibility is provided.And, the ingenious radiating that make use of motor 62 of antenna 70 is empty
Between, it is convenient not only to radiate, and does not additionally take up room.In transport, antenna can turn to horizontal level, be not take up sky
Between.
The top of fuselage main body 10 is recessed to be formed with a umbrella storehouse space 15, and the top in umbrella storehouse space 15 is capped with umbrella Cang Gai
16, it is detachably fixed between umbrella storehouse lid 16 and fuselage main body 10.
In the technical scheme, by reserving umbrella storehouse space 15, facilitate user that parachute is installed as needed.
The lower section of fuselage main body 10 is recessed upwards to be formed with an on-hook space 17, is capped with bottom at the opening in on-hook space 17
Storehouse lid 18, is detachably fixed between Lower Hold lid 18 and fuselage main body 10.
In the technical scheme, aerial camera head can be hung in on-hook space 17 as needed, be easy to shooting to take
Scape.In this case fuselage main body 10 head and bottom be respectively provided with the position of an installation camera, therefore provide the user
Various different selections.
It should be noted that herein, such as first and second or the like relational terms are used merely to a reality
Body or operation are made a distinction with another entity or operation, and are not necessarily required or implied these entities or deposit between operating
In any this actual relation or order.And, term " including ", "comprising" or its any other variant are intended to
Nonexcludability is included, so that a series of process, method, article or equipment including key elements not only will including those
Element, but also including other key elements being not expressly set out, or also include for this process, method, article or equipment
Intrinsic key element.In the absence of more restrictions, the key element for being limited by sentence "including a ...", it is not excluded that
Also there is other identical element in process, method, article or equipment including the key element.
The above is only the specific embodiment of the application, it is noted that for the ordinary skill people of the art
For member, on the premise of without departing from the application principle, some improvements and modifications can also be made, these improvements and modifications also should
It is considered as the protection domain of the application.
Claims (9)
1. a kind of quick release installs fixed-wing unmanned vehicle, it is characterised in that including fuselage main body and be installed on machine
Wing and afterbody in body main body, the afterbody include empennage and the foot piece being fixed between fuselage main body and empennage, described
Fuselage main body is provided with a foot piece passage, and one end of the foot piece is installed in the foot piece passage, and the foot piece is inserted in institute
The depth adjustable in foot piece passage is stated, the foot piece interts to shorten the space shared by whole afterbody forward, and the wing includes
Stage casing wing, left section of wing and right section of wing, the stage casing wing are fixed in the fuselage main body, the left section of wing and the right side
Section wing is removably mounted to the end of the left and right sides of stage casing wing, the left section of wing and right section of wing respectively and each extends over
There is guide rod, the end of the stage casing wing is provided with the installing hole for accommodating the guide rod, and the guide rod includes first for being set up in parallel
Guide rod and the second guide rod, the diameter and development length of first guide rod are all higher than second guide rod, second guide rod
Diameter is gradually reduced along the direction for deviating from the left section of wing or right section of wing, between the left section of wing and stage casing wing, with
And be respectively fixed with the buckle of relative movement between restriction adjacent wing between right section of wing and stage casing wing, the buckle include from
Two elastic arms that middle part bending is formed, two elastic arms recessed are formed with holding section, the clamping in relative position is opposite
Portion has curved surfaces, and outwards bending is formed with adjutage respectively for the end of described two elastic arms, described two adjutages it
Between be in splayed opening, be respectively fixed with the first installing plate, the left section of wing and the right side on the end face of the stage casing wing both sides
The second installing plate is fixed with the end face of section wing, is set on correspondence position respectively on first installing plate and the second installing plate
There are hole clipping or draw-in groove, be respectively equipped with the stage casing wing, left section of wing and right section of wing for buckle elastic arm insertion
Insert port, the insert port presses close to first installing plate or the second installing plate is arranged.
2. quick release according to claim 1 installs fixed-wing unmanned vehicle, it is characterised in that：The foot piece leads to
Road runs through the fuselage main body.
3. quick release according to claim 1 installs fixed-wing unmanned vehicle, it is characterised in that：The fuselage master
Body includes skeleton and the housing being installed on the outside of skeleton, and the skeleton includes a horizontally disposed gripper shoe, the gripper shoe
Both sides be symmetrically installed with reinforcing plate, the reinforcing plate is vertically arranged with gripper shoe, is provided with fixation above the gripper shoe
Support, the foot piece passage are formed between the fixed support and gripper shoe.
4. quick release according to claim 3 installs fixed-wing unmanned vehicle, it is characterised in that：The fixation
Fixing hole is offered on frame, the gripper shoe is provided with screw, offer through hole on the foot piece, described fixing hole, screw
Corresponded to through hole up and down.
5. quick release according to claim 3 installs fixed-wing unmanned vehicle, it is characterised in that：The gripper shoe
On offer multiple lightening holes.
6. quick release according to claim 3 installs fixed-wing unmanned vehicle, it is characterised in that：The gripper shoe
Be fixedly arranged at the front end with an on-hook plate, the on-hook plate vertical support plate is arranged, and offers to hang and take photo by plane on the on-hook plate
The suppending hole of camera, is capped with head-shield, detachably installs between the head-shield and fuselage main body on the outside of the on-hook plate.
7. quick release according to claim 1 installs fixed-wing unmanned vehicle, it is characterised in that：The fuselage master
The top of body is recessed to be formed with a umbrella storehouse space, is capped with umbrella Cang Gai, the umbrella Cang Gai and fuselage above the space of the umbrella storehouse
It is detachably fixed between main body.
8. quick release according to claim 1 installs fixed-wing unmanned vehicle, it is characterised in that：The fuselage master
The lower section of body is recessed upwards to be formed with an on-hook space, is capped with Lower Hold lid at the opening in the on-hook space, the Lower Hold lid with
It is detachably fixed between fuselage main body.
9. quick release according to claim 1 installs fixed-wing unmanned vehicle, it is characterised in that：The wing
Both sides are separately installed with a rotor in symmetric position, and described each rotor passes through a Motor drive respectively, after the motor
Side is formed with a heat dissipation channel, and the heat dissipation channel is located at the lower section of the wing, is wherein provided with heat dissipation channel described in
Antenna；The antenna both horizontally and vertically between it is rotatable.
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510107698.1A CN104709460B (en) | 2015-03-12 | 2015-03-12 | Fixed-wing unmanned aerial vehicle capable of being quickly disassembled and assembled |
| PCT/CN2015/097380 WO2016141742A1 (en) | 2015-03-12 | 2015-12-15 | Fixed-wing unmanned aircraft capable of being quickly disassembled and installed |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510107698.1A CN104709460B (en) | 2015-03-12 | 2015-03-12 | Fixed-wing unmanned aerial vehicle capable of being quickly disassembled and assembled |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN104709460A CN104709460A (en) | 2015-06-17 |
| CN104709460B true CN104709460B (en) | 2017-03-22 |
Family
ID=53409295
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510107698.1A Active CN104709460B (en) | 2015-03-12 | 2015-03-12 | Fixed-wing unmanned aerial vehicle capable of being quickly disassembled and assembled |
Country Status (2)
| Country | Link |
|---|---|
| CN (1) | CN104709460B (en) |
| WO (1) | WO2016141742A1 (en) |
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| CN104709460B (en) * | 2015-03-12 | 2017-03-22 | 江苏艾锐泰克无人飞行器科技有限公司 | Fixed-wing unmanned aerial vehicle capable of being quickly disassembled and assembled |
| CN106697259A (en) * | 2016-12-30 | 2017-05-24 | 马晓辉 | Fixed wing unmanned plane |
| CN106986032A (en) * | 2016-12-30 | 2017-07-28 | 马晓辉 | A kind of fixed-wing unmanned plane provided with sprinkling system |
| CN106945819A (en) * | 2016-12-30 | 2017-07-14 | 马晓辉 | A kind of fixed-wing unmanned plane provided with sprinkling system and protection device |
| CN106986040A (en) * | 2016-12-30 | 2017-07-28 | 马晓辉 | A kind of fixed-wing unmanned plane provided with protection device |
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| CN106741842A (en) * | 2016-12-30 | 2017-05-31 | 马晓辉 | A kind of three-stage fixed-wing unmanned plane for being provided with protection device |
| CN107054624A (en) * | 2016-12-30 | 2017-08-18 | 马晓辉 | A kind of three-stage fixed-wing unmanned plane provided with sprinkling system |
| CN106628106A (en) * | 2017-03-07 | 2017-05-10 | 厦门南羽科技有限公司 | Fixed wing unmanned aerial vehicle framework and fixed wing unmanned aerial vehicle |
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- 2015-03-12 CN CN201510107698.1A patent/CN104709460B/en active Active
- 2015-12-15 WO PCT/CN2015/097380 patent/WO2016141742A1/en active Application Filing
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| WO2016141742A1 (en) | 2016-09-15 |
| CN104709460A (en) | 2015-06-17 |
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