CN206954500U - The blade protection device and UAS of unmanned vehicle - Google Patents
The blade protection device and UAS of unmanned vehicle Download PDFInfo
- Publication number
- CN206954500U CN206954500U CN201720566645.0U CN201720566645U CN206954500U CN 206954500 U CN206954500 U CN 206954500U CN 201720566645 U CN201720566645 U CN 201720566645U CN 206954500 U CN206954500 U CN 206954500U
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- blade protection
- shade assembly
- blade
- main body
- clamp
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- 230000004224 protection Effects 0.000 title claims abstract description 158
- 230000001681 protective effect Effects 0.000 claims description 72
- 230000035939 shock Effects 0.000 abstract description 9
- 238000000034 method Methods 0.000 description 4
- 238000010586 diagram Methods 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 230000002787 reinforcement Effects 0.000 description 2
- 238000005728 strengthening Methods 0.000 description 2
- 208000035473 Communicable disease Diseases 0.000 description 1
- 230000000712 assembly Effects 0.000 description 1
- 238000000429 assembly Methods 0.000 description 1
- 230000004888 barrier function Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 208000015181 infectious disease Diseases 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
- B64U10/13—Flying platforms
- B64U10/14—Flying platforms with four distinct rotor axes, e.g. quadcopters
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U30/00—Means for producing lift; Empennages; Arrangements thereof
- B64U30/20—Rotors; Rotor supports
- B64U30/29—Constructional aspects of rotors or rotor supports; Arrangements thereof
- B64U30/291—Detachable rotors or rotor supports
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/40—Engine management systems
Abstract
The utility model discloses the blade protection device and UAS of a kind of unmanned vehicle.Blade protection device includes the first blade protection shade assembly, the second blade protection shade assembly and latch components; wherein the first blade protects shade assembly and the second blade protection shade assembly to be arranged at the opposite sides of unmanned vehicle; and engage respectively with the horn of unmanned vehicle; latch components are used to lock the first blade protection shade assembly and the second blade protection shade assembly, to keep the first blade protection shade assembly and the fastening state of the second blade protection shade assembly and unmanned vehicle.Therefore, the utility model enhances the stability of blade protection shade assembly, so as to improve the shock resistance of blade protection shade assembly.
Description
Technical field
The utility model is related to unmanned air vehicle technique field, a kind of blade protection device more particularly, to unmanned vehicle and
UAS.
Background technology
Unmanned plane is the not manned aircraft manipulated using radio robot and the presetting apparatus provided for oneself, and it is navigating
It is widely used in terms of the fields such as bat, agricultural, disaster relief, monitoring infectious disease, mapping, news report, movies-making.With
Attention of the society to unmanned plane security, the actual demand to oar protective cover becomes increasingly stronger, existing oar protective cover
Shock resistance is not high, influences the safety of unmanned vehicle.
Utility model content
The utility model mainly solving the technical problems that provide a kind of unmanned vehicle blade protection device and nobody
Machine system, there is higher shock resistance.
In order to solve the above technical problems, the technical scheme that the utility model uses is：A kind of unmanned vehicle is provided
Blade protection device, blade protection device includes the first blade protection shade assembly, the second blade protection shade assembly and lock
Component, wherein the first blade protection shade assembly and the second blade protection shade assembly are arranged at the opposite sides of unmanned vehicle, and
Engage respectively with the horn of unmanned vehicle, latch components are used to lock the first blade protection shade assembly and the second blade protective cover
Component, to keep the first blade protection shade assembly and the fastening state of the second blade protection shade assembly and unmanned vehicle.
Wherein, latch components include the first lock main body and the second lock main body, the first lock main body and the second lock master
Body is used to protect shade assembly and the second blade protection shade assembly removably to lock connection the first blade.
Wherein, the first lock main body is fixedly installed on the first blade protection shade assembly, and the second lock main body is pivotally connected
In the second blade protection shade assembly on, and can relative to the second blade protect shade assembly pivot into and first lock main body
It is fixed.
Wherein, the second lock main body includes pivot and connecting plate, and pivot is fixedly installed on the second blade protection shade assembly.
Wherein, connecting plate and pivot are detachably connected.
Wherein, the first blade protection shade assembly and the second blade protection shade assembly are centrosymmetric structure.
Wherein, the first lock main body is the card column being be arranged in parallel with the pivot direction of the second lock main body, and the second lock is led
Neck corresponding with card column is provided with body.
Wherein, the first lock main body is the buckle being be arranged in parallel with the pivot direction of the second lock main body, and the second lock is led
Neck corresponding with buckle is provided with body.
Wherein, the first lock main body is the first buckle being be arranged in parallel with the pivot direction of the second lock main body, and second locks
The second buckle corresponding with the first buckle is provided with button main body.
Wherein, the first blade protection shade assembly includes two the first adjutages being intervally installed, the first lock main body
It is fixedly installed between two the first adjutages；
Second blade protection shade assembly includes two the second adjutages being intervally installed, and the second lock main body pivot connects
It is connected between two the second adjutages.
Wherein, the end set of the first adjutage and the second adjutage has contraposition plug structure, so that the first blade is protected
Shade assembly and the protection shade assembly contraposition of the second blade patch.
Wherein, the first connector is further provided between two the first adjutages, enters one between two the second adjutages
Step is provided with the second connector.
Wherein, the first blade protection shade assembly further comprises first time clamp, and first time clamp is fastened on unmanned flight
The lower surface of the side fuselage of device；
Second blade protection shade assembly further comprises second time clamp, and second time clamp is fastened on the another of unmanned vehicle
On the lower surface of side fuselage.
Wherein, the first blade protection shade assembly further comprises clamp and first time clamp on spaced first, the
On one clamp and first time clamp be arranged to the first blade protect shade assembly and the second blade protection shade assembly respectively with nobody
It is fastened in respectively in the upper and lower surface of two adjacent horns of unmanned vehicle during the both sides engaging of aircraft, the second oar
Leaf protection shade assembly further comprises clamp and second time clamp on spaced second, clamp and second time clamp on second
For distinguishing when the first blade protects shade assembly and the second blade protection shade assembly engages with the both sides of unmanned vehicle respectively
It is fastened in the upper and lower surface of two other adjacent horn of unmanned vehicle.
Wherein, the first blade protection shade assembly further comprises being connected to two of clamp and first time clamp on first the
Side clamp, two the first side clamps are fastened in the adjacent side of two adjacent horns respectively, the second blade protective cover group
Part further comprises being connected to two the second side clamps of clamp and second time clamp on second, and two the second side clamps are fastened in
In the adjacent side of two other adjacent horn.
Wherein, the first protection shade assembly includes at least two first protective covers, and at least two first protective covers are fixedly connected
Or the first adjutage is separately positioned in, the second protection shade assembly includes at least two second protective covers, at least two second protections
Cover is fixedly connected with or is separately positioned in the second adjutage.
Wherein, the first protective cover and the second protective cover are fan-shaped cover body.
In order to solve the above technical problems, another technical scheme that the utility model uses is：A kind of unmanned plane system is provided
System, the UAS include the blade protection device and unmanned vehicle of any one above, blade protection device lock
In on the fuselage of unmanned vehicle.
The beneficial effects of the utility model are：The situation of prior art is different from, the utility model offer is a kind of, and nobody flies
The blade protection device and UAS of row device, the blade protection device include the first blade protection shade assembly, the second blade
Shade assembly and latch components are protected, wherein the first blade protection shade assembly and the second blade protection shade assembly are arranged at nobody and flown
The opposite sides of row device, and engage respectively with the both sides of unmanned vehicle, latch components are used to lock the first blade protective cover group
Part and the second blade protection shade assembly, to keep the first blade protection shade assembly and the second blade protection shade assembly and unmanned flight
The fastening state of device.Therefore, the utility model by the first blade protect shade assembly and the second blade protect shade assembly respectively with
The opposite sides engaging of unmanned vehicle so that when running into collision thing, the both sides of unmanned vehicle can offset part shock
Power, the stability of protection shade assembly is thereby enhanced, so as to improve the shock resistance of blade protection shade assembly.
Brief description of the drawings
Fig. 1 is a kind of blast overlooking the structure diagram for UAS that the utility model embodiment provides；
Fig. 2 is a kind of assembling overlooking the structure diagram for UAS that the utility model embodiment provides；
Fig. 3 is a kind of side structure schematic view for UAS that the utility model embodiment provides；
Fig. 4 is a kind of structural representation of the latch components for unmanned vehicle that the utility model embodiment provides；
Fig. 5 is the structural representation of the latch components for another unmanned vehicle that the utility model embodiment provides.
Embodiment
Also referring to Fig. 1-Fig. 3.The UAS 10 of the present embodiment includes unmanned vehicle 100 and blade protection dress
Put 200.Wherein, unmanned vehicle 100 includes fuselage 180, horn 101-104, blade 106 and the motor for driving blade 106
190.Wherein, horn 101 and 102 is arranged on the both ends of the side of fuselage 180, the He of horn 103 along the long axis direction of fuselage 180
104 are arranged on the both ends of the opposite side of fuselage 180 along the long axis direction of fuselage 180.Motor 190 is four, is separately positioned on machine
One end of arm 101-104 remote fuselage 180.Two panels blade 106 is set on each motor 190.
Blade protection device 200 is located at the periphery of the blade 106 of protection unmanned vehicle 100, for protecting blade 106
From shock etc..
Wherein, blade protection device 200 include the first blade protection shade assembly 11, the second blade protection shade assembly 12 and
Latch components 13.First blade protection shade assembly 11 and second blade protection shade assembly 12 is arranged at the phase of unmanned vehicle 100
To both sides 150 and 160, and the both sides with unmanned vehicle 100 engage respectively, and latch components 13 are used to lock the protection of the first blade
The blade of shade assembly 11 and second protects shade assembly 12, to keep the first blade protection shade assembly 11 and second blade protection shade assembly
12 with the fastening state of unmanned vehicle 100.
In the present embodiment, the first blade protection shade assembly 11 and second blade protection shade assembly 12 is arranged at unmanned vehicle
100 position can be 150 Hes that is, shown in Fig. 1 along the opposite sides of the long axis direction of the fuselage 180 of unmanned vehicle 100
160。
In other embodiments, the first blade protection shade assembly 11 and second blade protection shade assembly 12 is arranged at nobody and flown
The position of row device 100 can also be the opposite sides along the short-axis direction of the fuselage 180 of unmanned vehicle 100.
In the present embodiment, the first blade protection shade assembly 11 and second blade protection shade assembly 12 is completely right in structure
Claim, therefore, only need once to mold on manufacturing process, it is possible to make two blade protection shade assemblies, simplify making work
Skill.The gravity motion of unmanned vehicle 100 can additionally influenceed by blade protection shade assembly as far as possible small.
Therefore, the present embodiment is by protecting the blade of shade assembly 11 and second to protect shade assembly 12 to set respectively the first blade
In the opposite sides of unmanned vehicle 100, and the both sides with unmanned vehicle 100 engage respectively, thus in the first oar protective cover
When the oar of component 11 and/or second protection shade assembly 12 receives shock, unmanned vehicle 100 can offset part impact, so as to increase
The strong stability of first blade protection shade assembly 11 and second blade protection shade assembly 12, improves the first blade protective cover group
The blade of part 11 and second protects the shock resistance of shade assembly 12.
Wherein, the lock mode of latch components 13 can be non-dismountable lock mode, i.e., the first blade is protected into shade assembly
11 and second blade protection shade assembly 12 connection is locked in a manner of non-dismountable.Non-dismountable mode, which locks connection, may include flanging
Connection, rivet interlacement, bonding connection and it is welded to connect.The utility model is not limited the concrete structure of latch components 13
System, as long as realizing the locking connection function of above-mentioned non-dismountable mode.Non-removable locking connected mode can be strengthened
The steadiness of blade protection device 100.
On the other hand, consider blade protection device 100 in actual use, easily collide and cause its easy
Damage is, it is necessary to often be dismounted, therefore the utility model can carry out fast assembling-disassembling in order that obtaining blade protection device 100, incite somebody to action
Latch components 13 are arranged to removably lock the first blade protection blade protective cover group 12 of shade assembly 11 and second
Connection.Specifically, latch components 13, which include the first lock main body 131 and second, latches main body 132.The first lock He of main body 131
Second lock main body 132 is used to protect the blade of shade assembly 11 and second protection shade assembly 12 removably to lock the first blade
Fixed connection.
Wherein, the first lock main body 131 is fixedly installed on the first blade protection shade assembly 11.Second lock main body 132
Be pivotally connected to the second blade protection shade assembly 12 on, and can relative to the second blade protect shade assembly 12 pivot into
First lock main body 131 is fixed.More specifically, the first lock main body 131 can be the pivot side with the second lock main body 132
To the card column 133 be arrangeding in parallel, the second lock main body 132 includes pivot 1321 and connecting plate 1322, and pivot 1321 is fixedly installed
In on the second blade protection shade assembly 12.Connecting plate 1322 and pivot 1321 are detachably connected.Set in second lock main body 132
There is neck 134 corresponding with card column 133.Neck 134 corresponding with card column 133 is specially provided with connecting plate 1322.Cause
This, dismountable connection can be achieved by neck 134 and card column 133 in the latch components 13 of the present embodiment, simple in construction, and
Weight is light and handy, is adapted to the unmanned vehicle of small volume.
In other embodiments, referring to the also settable first lock main bodys 131 of Fig. 4 is and the second lock main body 132
The buckle 136 that pivot direction be arranged in parallel, second lock main body 132 on be provided with neck 137 corresponding with buckle 136.Wherein,
Buckle 136 includes the buckling parts 138 of a hook.In snap-fitting process, neck 137, which pivots, makes buckle 136 buckle into neck 137
In, and neck 137 is engaged by the hook buckling parts 138 of buckle 136.
Referring to Fig. 5, also settable first lock main body 131 is sets parallel with the pivot direction of the second lock main body 132
The first buckle 141 put, second lock main body 132 on be provided with and 141 corresponding second buckle 142 of the first buckle.Wherein,
One buckle 141 includes the first buckling parts 143 of a hook, and the second buckle 142 includes the second buckling parts 144 of a hook.In card
During conjunction, the direction of the second buckle 142 to the first buckle 141 pivots, and is fastened by the first buckling parts 143 and second
Portion 144 mutually fastens.
Referring again to shown in Fig. 1-Fig. 3, reinforcement structure 135, reinforcement structure are further provided with the second lock main body 132
135 can be the projection of setting of intersecting, for strengthening the intensity of the second lock main body 132.
Further, the first blade protection shade assembly 11 includes two Hes of the first adjutage 111 being intervally installed
112, the first lock main body 131 is fixedly installed between two the first adjutages 111 and 112.Second blade protects shade assembly 12
Also include two the second adjutages 121 and 122 being intervally installed, the second lock main body 132 is pivotally connected to two second
Between adjutage 121 and 122.Specifically, the card column of the first lock main body 131 is fixedly installed on two Hes of the first adjutage 111
Between 112, the pivot 1321 of the second lock main body 132 is pivotally connected between two the second adjutages 121 and 122.
Wherein, the first adjutage 111 and 112 protects shade assembly 11 to the second blade protection shade assembly 12 from the first blade
Direction extends, and the second adjutage 121 and 122 protects shade assembly 12 to the direction of the first blade protection shade assembly 11 from the second blade
Extension.
Further, the first adjutage 111 and 112 can also be aligned with the second adjutage 121 and 122 and patched, specifically,
The end of first adjutage 111 and 112 and the end of the second adjutage 121 and 122 are respectively arranged with the contraposition He of plug structure 113
123, so that the first blade protection shade assembly 11 and second blade protection shade assembly 12 realizes that contraposition patches.Wherein, the first extension
The end of arm 111 and 112 is the end that shade assembly 11 is protected away from the first blade, similarly, the end of the second adjutage 121 and 122
Portion is the end away from the second blade protective cover 12.
Specifically, the end set of one in two the first adjutages 111 and 112 has inserting column 114, two first extensions
Another end set in arm 111 and 112 has jack 115.As shown in fig. 1, the end set of the first adjutage 111 has
Inserting column 114, the end set of the first adjutage 112 have jack 115.The end of one in two the second adjutages 121 and 122
Be provided with the jack that cooperation is patched with inserting column 114, another the end set in two the second adjutages 121 and 122 have with
Jack 115 patches the inserting column of cooperation, as shown in figure 1, the end set of the second adjutage 121 has patches cooperation with inserting column 114
Jack (not shown), the end set of the second adjutage 122 have the inserting column 124 that cooperation is patched with jack 115.
Wherein, 114 and 124 specification size and the big I of the specification of jack 115 and the jack on adjutage 121 is stuck in
To be identical so that can both have been formed by same set of template in the fabrication process, and reach cost-effective purpose.
In other embodiments, one inserting column can also be set in the end of two the first adjutages 111 and 112 respectively,
In the end of two the second adjutages 121 and 122, jack corresponding with inserting column is set respectively.Or in two the first adjutages
111 and 112 end sets a jack respectively, is set respectively and jack pair in the end of two the second adjutages 121 and 122
The inserting column answered.
Further, it is further provided with the first connector 1112 between two the first adjutages 111 and 112, two
The second connector 1212 is further provided between two adjutages 121 and 122.Wherein, the first connector 1112 is relative to card column
133 are set closer to inserting column 114 and jack 115.Second connector 1212 is relative to pivot 1321 closer to inserting column 124 and second
Jack is set.
First connector 1112 and the second connector 1212 are used to strengthen the first adjutage 111 and 112 and second respectively
The intensity of adjutage 121 and 122.
Further, the first blade protection shade assembly 11 also includes clamp 116 and first time card on spaced first
Plate 117.Clamp 116 and first time clamp 117 are arranged in the protection shade assembly 11 and second blade protection of the first blade on first
Two adjacent horns of unmanned vehicle 100 are fastened in when shade assembly 12 engages with the both sides of unmanned vehicle 100 respectively respectively
In 101 and 102 upper and lower surface.
In the present embodiment, on first two of clamp 116 and the unmanned vehicle 100 of first time clamping of clamp 117 it is adjacent
Horn can be two phases of the same side set along the long axis direction of the fuselage 180 of unmanned vehicle 100 and positioned at fuselage 180
Adjacent horn, i.e., the horn 101 and 102 shown in Fig. 1.
In other embodiments, two of clamp 116 and the unmanned vehicle 100 of first time clamping of clamp 117 on first
Adjacent horn can also be the same side set along the short-axis direction of the fuselage 180 of unmanned vehicle 100 and positioned at fuselage 180
Two adjacent horns.Horn 101 and 104 or horn 102 and 103 i.e. shown in Fig. 1.
Second blade protection shade assembly 12 further comprises clamp 125 and second time clamp 126 on spaced second,
Clamp 125 and second time clamp 126 are used in the first blade protection shade assembly 11 and second blade protection shade assembly 12 on second
Engage the time-division in both sides of the first blade protection shade assembly 11 and second blade protection shade assembly 12 respectively with unmanned vehicle 100
It is not fastened in the upper and lower surface of two other adjacent horn 103 and 104 of unmanned vehicle 100.
Similarly, in the present embodiment, two of clamp 125 and the unmanned vehicle 100 of second time clamping of clamp 126 on second
Adjacent horn can be the two of the same side set along the long axis direction of the fuselage 180 of unmanned vehicle 100 and positioned at fuselage 180
Individual adjacent horn, i.e., the horn 103 and 104 shown in Fig. 1.
In other embodiments, two of clamp 125 and the unmanned vehicle 100 of second time clamping of clamp 126 on second
Adjacent horn can also be the same side set along the short-axis direction of the fuselage 180 of unmanned vehicle 100 and positioned at fuselage 180
Two adjacent horns.Horn 101 and 104 or horn 102 and 103 i.e. shown in Fig. 1.
Further, the first blade protection shade assembly 11 also includes being connected to clamp 116 and first time clamp 117 on first
Two the first side clamps 118 and 119, two the first side clamps 118 and 119 are used to protect shade assembly 11 and the in the first blade
Two blades protection shade assembly 12 be fastened in respectively when engaging respectively with the both sides of unmanned vehicle 100 two adjacent horns 101 and
In 102 adjacent side.Second blade protection shade assembly 12 further comprises being connected to clamp 125 and second time card on second
Two the second side clamps 127 and 128 of plate 126, two the second side clamps 127 and 128 are used to protect shade assembly in the first blade
11 and second blade protection shade assembly 12 to be fastened in two other respectively when engaging respectively with the both sides of unmanned vehicle 100 adjacent
In the adjacent side of horn 103 and 104.
In the present embodiment, side clamp described above is to be obliquely installed, its inclined angle and the horn of its clamping
Angle of inclination is corresponding.Thus in side clamp and horn clamping, the face of its clamping can be with seamless fitting, so as to obtain more
Good clamping fixation.
Further, the first blade protection shade assembly 11 also includes at least two first protective covers, and at least two first protect
Shield is fixedly connected with or is separately positioned in the first adjutage 111 and 112.Second protection shade assembly 12, which includes at least two second, to be protected
Shield, at least two second protective covers are fixedly connected with or are separately positioned in the second adjutage 121 and 122.
In the present embodiment, it is contemplated that each to protect shade assembly only the problems such as the intensity of the convenience of technique and protective cover
Two protective covers, i.e. two the first protective covers 110 and 120 and two the second protective covers 130 and 140 are set.Wherein, each oar
Leaf is correspondingly arranged a protective cover.It is specific to set as described below.
In other embodiments, also each two or more protective covers can be correspondingly arranged by blade.
In the present embodiment, two the first protective covers 110 and 120 are arranged on first on clamp 116 and further covered at
The periphery of the blade 105 and 106 set on two adjacent horns 101 and 102.Two the first adjutages 111 and 112 are set respectively
In on two the first protective covers 110 and 120.
Further, the first blade protection shade assembly 11 also includes what is extended downwardly respectively from the first protective cover 110 and 120
First linking arm 1101 and 1201, the first linking arm 1101 clamp 116 on the first protective cover 110 and first of connection, first
Linking arm 1201 is used to connect clamp 116 on the first protective cover 120 and first.So that the first protective cover 110 and 120 is arranged at
On one on clamp 116.
Two the second protective covers 130 and 140 are arranged on second on clamp 125 and further to cover at two other adjacent
The periphery of the blade 107 and 108 set on horn 103 and 104, two the second adjutages 121 and 122 are respectively arranged at two
On two protective covers 130 and 140.
Similarly, the second blade protection shade assembly 12 also includes second extended downwardly respectively from the second protective cover 130 and 140
Linking arm 1301 and 1401, the second linking arm 1301 are used to connect clamp 125 on the second protective cover 130 and second, the second connection
Arm 1401 is used to connect clamp 125 on the second protective cover 140 and second.So that the second protective cover 130 and 140 is arranged on second
On clamp 125.
In other embodiments, first time clamp 117 and second time clamp 126, first time clamp 117 can also be only set
It is fastened on the lower surface of side fuselage, second time clamp 126 is fastened on the lower surface of opposite side fuselage.Specifically,
Once clamp 117 is connected with the first protective cover 110 and 120 respectively by the first linking arm 1101 and 1201, second time clamp 12
It is connected respectively with the second protective cover 130 and 140 by the second linking arm 1301 and 1401.
Wherein, first time clamp 117 and second time clamp 126 can be set along the long axis direction of fuselage, can also be along fuselage
Short-axis direction set.In addition, when the short-axis direction of first time clamp 117 and second time clamp 126 along fuselage is set, can set
Two first time clamps 117 and two second time clamps 126 of horizontalization row, it can be arranged at intervals and block along the long axis direction of fuselage
Close in both sides of the fuselage along long axis direction, thus can strengthen to snap action.
From the foregoing it will be appreciated that first protective cover 110 and 120 of the present embodiment is the fuselage 180 along unmanned vehicle 100
Long axis direction set and positioned at fuselage 180 the same side two adjacent protective covers.Similarly, the second protective cover 130 and 140
Also it is two adjacent guarantors of the same side set along the long axis direction of the fuselage 180 of unmanned vehicle 100 and positioned at fuselage 180
Shield.Wherein, the first protective cover 110 and 120 and the second protective cover 130 and 140 are separately positioned on unmanned vehicle 100
Two offsides.In the present embodiment, the first adjutage 111 and 112 is respectively from the first protective cover 110 and 120 to the He of the second protective cover 130
140 direction extension, the second adjutage 121 and 122 is respectively from the second protective cover 130 and 140 to the first protective cover 110 and 120
Direction extension.So that the first blade protection shade assembly 11 and second blade protection shade assembly 12 respectively with unmanned vehicle
During 100 both sides engaging, it is arranged at card column 133 between two the first adjutages 111 and 112 and is arranged at two second extensions
The neck 134 of the second lock main body 132 between arm 121 and 122 can be carried out at the middle part of fuselage 180 of unmanned vehicle 100
It is fixed, which thereby enhances fixing intensity.
In the present embodiment, two the first protective covers 110 are fixedly connected with 120 is arranged at the first adjutage 111 and 112, and two
Individual second protective cover 130 is fixedly connected with 140 is arranged at the second adjutage 121 and 122.Wherein, two Hes of the first protective cover 110
120 and two the second protective covers 130 and 140 can be made by being integrally formed.In other embodiments, can also be protected first
Detachable components are set between shield 110 and 120 and between the second protective cover 130 and 140, by the first protective cover 110 and 120
Removably connected with the second protective cover 130 and 140.Or between the first protective cover 110 and 120 and second
Protective cover 130 and 140 sets articulated structure so that the first protective cover 110 and 120 connects in articulated manner.
In other embodiments, can not be mutual between the first protective cover 110 and 120 and the second protective cover 130 and 140
Connection.That is the first protective cover 110 and 120 is separately positioned in the first adjutage 111 and 112, and the second protective cover 130 and 140 points are opened
It is arranged at the second adjutage 121 and 122.
In the present embodiment, the first protective cover 110 and 120 and the second protective cover 130 and 140 are fan-shaped cover body, and
The support arm 170 being internally provided with for strengthening fan-shaped cover body intensity of fan-shaped cover body.The quantity of support arm 170 can be according to need
Set.On the one hand intensity that support arm 170 can be carried out to protective cover is strengthened, on the other hand can also be in unmanned vehicle
100 protect when knocking barrier to unmanned vehicle 100.
In the present embodiment, fan-shaped cover body can be 270 degree of settings, be advantageous to the lightness of unmanned vehicle, be also prevented from
Protective cover blocks the camera or other vision sensors being arranged on unmanned vehicle.
In other embodiments, the angle of fan-shaped cover body may be arranged as other, as long as without prejudice to camera and other
The normal work of vision sensor.Further, it is contemplated that the protection to protective cover, the first protective cover can also be set
110 and 120 and second protective cover 130 and 140 be circular cover body structure.
In summary, the utility model can protect shade assembly to carry out fast quick-detach blade, be convenient for changing, during saving
Between.In addition, the stability of blade protection shade assembly is also enhanced, so as to improve the shock resistance of blade protection shade assembly.
Embodiment of the present utility model is the foregoing is only, not thereby limits the scope of the claims of the present utility model, it is every
The equivalent structure or equivalent flow conversion made using the utility model specification and accompanying drawing content, or be directly or indirectly used in
Other related technical areas, similarly it is included in scope of patent protection of the present utility model.
Claims (18)
1. the blade protection device of a kind of unmanned vehicle, it is characterised in that the blade protection device is protected including the first blade
Cover assembly, the second blade protection shade assembly and latch components, wherein first blade protects shade assembly and described second
Blade protection shade assembly is arranged at the opposite sides of the unmanned vehicle, and the both sides card with the unmanned vehicle respectively
Close, the latch components are used to lock the first blade protection shade assembly and second blade protection shade assembly, to keep
The fastening state of the first blade protection shade assembly and second blade protection shade assembly and the unmanned vehicle.
2. blade protection device according to claim 1, it is characterised in that the latch components include the first lock main body
With the second lock main body, the first lock main body and the second lock main body are used to first blade protecting shade assembly
Connection is removably locked with second blade protection shade assembly.
3. blade protection device according to claim 2, it is characterised in that the first lock main body is fixedly installed on institute
To state on the first blade protection shade assembly, the second lock main body is pivotally connected on the second blade protection shade assembly, and
Shade assembly can be protected to pivot into relative to second blade to be fixed with the described first lock main body.
4. blade protection device according to claim 3, it is characterised in that the second lock main body includes pivot and company
Fishplate bar, the pivot are fixedly installed on the second blade protection shade assembly.
5. blade protection device according to claim 4, it is characterised in that the connecting plate and the pivot detachably connect
Connect.
6. blade protection device according to claim 4, it is characterised in that first blade protection shade assembly and described
Second blade protection shade assembly is centrosymmetric structure.
7. blade protection device according to claim 3, it is characterised in that it is described first lock main body be and described second
The card column that the pivot direction of main body be arranged in parallel is latched, card corresponding with the card column is provided with the second lock main body
Groove.
8. blade protection device according to claim 3, it is characterised in that it is described first lock main body be and described second
The buckle that the pivot direction of main body be arranged in parallel is latched, card corresponding with the buckle is provided with the second lock main body
Groove.
9. blade protection device according to claim 3, it is characterised in that it is described first lock main body be and described second
The first buckle that the pivot direction of main body be arranged in parallel is latched, is provided with and first buckle pair in the second lock main body
The second buckle answered.
10. blade protection device according to claim 3, it is characterised in that the first blade protection shade assembly includes
Two the first adjutages being intervally installed, it is described first lock main body be fixedly installed on described two first adjutages it
Between；
The second blade protection shade assembly includes two the second adjutages being intervally installed, the second lock main body pivot
Axis connection is between described two second adjutages.
11. blade protection device according to claim 10, it is characterised in that first adjutage and described second prolongs
The end set of semi-girder has contraposition plug structure, so that first blade protection shade assembly and the second blade protective cover group
Part contraposition patches.
12. blade protection device according to claim 10, it is characterised in that enter one between two first adjutages
Step is provided with the first connector, and the second connector is further provided between two second adjutages.
13. blade protection device according to claim 1, it is characterised in that the first blade protection shade assembly enters one
Step includes first time clamp, and first time clamp is fastened on the lower surface of the side fuselage of the unmanned vehicle；
Second blade protection shade assembly further comprises second time clamp, and second time clamp is fastened on that described nobody is winged
On the lower surface of the opposite side fuselage of row device.
14. blade protection device according to claim 1, it is characterised in that the first blade protection shade assembly enters one
Walking includes clamp and first time clamp on spaced first, and clamp and first time clamp are arranged to described on described first
First blade protects the both sides of shade assembly and second blade protection shade assembly respectively with the unmanned vehicle to engage the time-division
It is not fastened in the upper and lower surface of two adjacent horns of the unmanned vehicle, second blade protects shade assembly
Further comprise clamp and second time clamp on spaced second, clamp and second time clamp are used in institute on described second
The first blade protection shade assembly and second blade protection shade assembly are stated when engaging respectively with the both sides of the unmanned vehicle
It is fastened in respectively in the upper and lower surface of two other adjacent horn of the unmanned vehicle.
15. blade protection device according to claim 14, it is characterised in that the first blade protection shade assembly enters one
Step includes being connected to two the first side clamps of clamp and first time clamp on described first, described two first sides clamp
It is fastened in respectively in the adjacent side of described two adjacent horns, the second blade protection shade assembly further comprises connecting
Two the second side clamps of clamp and second time clamp on described second, described two second sides clamp are fastened in described
In the adjacent side of two other adjacent horn.
16. blade protection device according to claim 10, it is characterised in that the first blade protection shade assembly includes
At least two first protective covers, at least two first protective cover are fixedly connected with or are separately positioned in first adjutage,
Second blade protection shade assembly includes at least two second protective covers, at least two second protective cover be fixedly connected or
It is separately positioned in second adjutage.
17. blade protection device according to claim 16, it is characterised in that first protective cover and described second is protected
Shield is fan-shaped cover body.
18. a kind of UAS, it is characterised in that the UAS is included as described in claim 1-17 any one
Blade protection device and unmanned vehicle, the blade protection device latch on the fuselage of the unmanned vehicle.
Priority Applications (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720566645.0U CN206954500U (en) | 2017-05-19 | 2017-05-19 | The blade protection device and UAS of unmanned vehicle |
| CN201780068011.5A CN109906185A (en) | 2017-05-19 | 2017-06-27 | The blade protective device and UAV system of unmanned vehicle |
| PCT/CN2017/090415 WO2018209765A1 (en) | 2017-05-19 | 2017-06-27 | Blade protection device for unmanned aerial vehicle, and unmanned aerial vehicle system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720566645.0U CN206954500U (en) | 2017-05-19 | 2017-05-19 | The blade protection device and UAS of unmanned vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206954500U true CN206954500U (en) | 2018-02-02 |
Family
ID=61375167
Family Applications (2)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720566645.0U Active CN206954500U (en) | 2017-05-19 | 2017-05-19 | The blade protection device and UAS of unmanned vehicle |
| CN201780068011.5A Pending CN109906185A (en) | 2017-05-19 | 2017-06-27 | The blade protective device and UAV system of unmanned vehicle |
Family Applications After (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201780068011.5A Pending CN109906185A (en) | 2017-05-19 | 2017-06-27 | The blade protective device and UAV system of unmanned vehicle |
Country Status (2)
| Country | Link |
|---|---|
| CN (2) | CN206954500U (en) |
| WO (1) | WO2018209765A1 (en) |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109906185A (en) * | 2017-05-19 | 2019-06-18 | 深圳市大疆创新科技有限公司 | The blade protective device and UAV system of unmanned vehicle |
| CN112119007A (en) * | 2019-10-21 | 2020-12-22 | 深圳市大疆创新科技有限公司 | Blade protection device and aircraft |
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| US4856732A (en) * | 1987-05-01 | 1989-08-15 | Karl Eickmann | Airborne vehicle with hydraulic drive and control |
| DE202005004698U1 (en) * | 2005-03-23 | 2005-06-16 | Dolch, Stefan, Dipl.-Ing. (FH) | Collision protection device for helicopter rotors is detachably fastened on at least three points on helicopter and split into several sub-assemblies, with at least one sub-assembly connected to another only through helicopter |
| WO2015200209A1 (en) * | 2014-06-23 | 2015-12-30 | Nixie Labs, Inc. | Wearable unmanned aerial vehicles, launch- controlled unmanned aerial vehicles, and associated systems and methods |
| WO2016112124A2 (en) * | 2015-01-08 | 2016-07-14 | Vantage Robotics, Llc | Unmanned aerial vehicle with propeller protection and high impact survivability |
| CN104608923B (en) * | 2015-01-31 | 2016-05-11 | 中南大学 | A kind of honeycomb fashion six rotor transporter aircrafts |
| KR101956535B1 (en) * | 2015-04-09 | 2019-03-11 | 주식회사 헬셀 | Unmanned air vehicle with a rotor portion emergency stop function |
| CN204776022U (en) * | 2015-07-03 | 2015-11-18 | 安徽泽众安全科技有限公司 | Protector can be dismantled to rotor craft |
| CN205418098U (en) * | 2015-11-30 | 2016-08-03 | 湖北易瓦特科技股份有限公司 | Keep away barrier rotor unmanned aerial vehicle |
| CN205524952U (en) * | 2016-01-29 | 2016-08-31 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle and horn mechanism thereof |
| CN205524937U (en) * | 2016-01-29 | 2016-08-31 | 深圳市大疆创新科技有限公司 | Screw safety cover and use horn structure, unmanned aerial vehicle of this screw safety cover |
| CN105775149B (en) * | 2016-02-29 | 2017-10-27 | 深圳市大疆创新科技有限公司 | Protective cover, barrier-avoiding method and the unmanned vehicle of unmanned vehicle |
| CN205707325U (en) * | 2016-04-26 | 2016-11-23 | 普宙飞行器科技（深圳）有限公司 | Telescopic blade driving means and unmanned plane |
| CN205707341U (en) * | 2016-07-01 | 2016-11-23 | 浙江智天科技有限公司 | A kind of dismountable propeller guard circle |
| CN205952286U (en) * | 2016-08-19 | 2017-02-15 | 韩振铎 | Folding mechanism and take folding mechanism's unmanned aerial vehicle |
| CN206954500U (en) * | 2017-05-19 | 2018-02-02 | 深圳市大疆创新科技有限公司 | The blade protection device and UAS of unmanned vehicle |
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2017
- 2017-05-19 CN CN201720566645.0U patent/CN206954500U/en active Active
- 2017-06-27 CN CN201780068011.5A patent/CN109906185A/en active Pending
- 2017-06-27 WO PCT/CN2017/090415 patent/WO2018209765A1/en active Application Filing
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109906185A (en) * | 2017-05-19 | 2019-06-18 | 深圳市大疆创新科技有限公司 | The blade protective device and UAV system of unmanned vehicle |
| CN112119007A (en) * | 2019-10-21 | 2020-12-22 | 深圳市大疆创新科技有限公司 | Blade protection device and aircraft |
Also Published As
| Publication number | Publication date |
|---|---|
| WO2018209765A1 (en) | 2018-11-22 |
| CN109906185A (en) | 2019-06-18 |
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| TR01 | Transfer of patent right |
Effective date of registration: 20190709 Address after: 518005 Baiwang Creative Factory, 1051 Songbai Road, Xili Street, Nanshan District, Shenzhen City, Guangdong Province, 7 101, 102-1 and 201/9 buildings Patentee after: Shenzhen City, Jiang Baiwang science and Technology Co Ltd Address before: 518057 Shenzhen Nanshan High-tech Zone, Shenzhen, Guangdong Province, 6/F, Shenzhen Industry, Education and Research Building, Hong Kong University of Science and Technology, No. 9 Yuexingdao, South District, Nanshan District, Shenzhen City, Guangdong Province Patentee before: Shenzhen Dji Technology Co., Ltd. |