CN108382597A - Universal unmanned plane article delivery device - Google Patents
Universal unmanned plane article delivery device Download PDFInfo
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- CN108382597A CN108382597A CN201810347248.3A CN201810347248A CN108382597A CN 108382597 A CN108382597 A CN 108382597A CN 201810347248 A CN201810347248 A CN 201810347248A CN 108382597 A CN108382597 A CN 108382597A
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- solenoid valve
- bar
- shell
- unmanned plane
- magnetic core
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- 238000004519 manufacturing process Methods 0.000 abstract description 5
- 238000013461 design Methods 0.000 abstract description 4
- 230000005611 electricity Effects 0.000 description 6
- 239000000758 substrate Substances 0.000 description 6
- 238000010586 diagram Methods 0.000 description 5
- 239000000463 material Substances 0.000 description 5
- 230000005484 gravity Effects 0.000 description 4
- 230000002146 bilateral effect Effects 0.000 description 3
- 230000000694 effects Effects 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 3
- 238000009434 installation Methods 0.000 description 3
- 229910000838 Al alloy Inorganic materials 0.000 description 2
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- 239000011347 resin Substances 0.000 description 2
- 229920005989 resin Polymers 0.000 description 2
- 208000035473 Communicable disease Diseases 0.000 description 1
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- 230000009286 beneficial effect Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 208000015181 infectious disease Diseases 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
- B64D1/02—Dropping, ejecting, or releasing articles
- B64D1/08—Dropping, ejecting, or releasing articles the articles being load-carrying devices
- B64D1/12—Releasing
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
- B64U2101/60—UAVs specially adapted for particular uses or applications for transporting passengers; for transporting goods other than weapons
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Magnetically Actuated Valves (AREA)
Abstract
The present invention provides a kind of universal unmanned plane article delivery device, wherein left and right sides solenoid valve or so relative spacing is arranged in the housing, left and right axis of sideslip is installed in the right left end of the magnetic core of left and right sides solenoid valve and at least partly protrudes from the shell of left and right sides solenoid valve respectively respectively, relative spacing is arranged, left side elastomeric element is located at the magnetic core that in the solenoid valve of left side and both ends bear against the solenoid housing and left side slide-bar or left side solenoid valve of left side solenoid valve, right side elastomeric element is located at the magnetic core that in the solenoid valve of right side and both ends bear against the solenoid housing and right side slide-bar or right side solenoid valve of right side solenoid valve, launch the reception of control device wireless signal connection signal and power control apparatus, signal receives and power control apparatus is arranged in the housing and difference circuit connects left and right sides solenoid valve.Structure of the invention is succinct, at low cost, and using simplicity, operational reliability is high, ingenious in design, and manufacture is easy, is suitable for large-scale promotion application.
Description
Technical field
The present invention relates to article delivery device technical field, more particularly to unmanned plane article delivery device technical field, tools
Body refers to a kind of universal unmanned plane article delivery device.
Background technology
Referred to as " unmanned plane ", english abbreviation is " UAV " to UAV, using radio robot and is provided for oneself
The not manned aircraft that presetting apparatus manipulates, or fully or intermittently automatically operated by car-mounted computer.
Compared with manned aircraft, unmanned plane is often more suitable for the task of those too " slow-witted, dirty or dangerous ".Nobody
Machine press application field, can be divided into it is military with it is civilian.Military aspect, unmanned plane are divided into reconnaissance plane and target drone.Civilian aspect, unmanned plane
+ sector application, which is unmanned plane, really just have been needed；At present take photo by plane, agricultural, plant protection, miniature self-timer, express transportation, disaster relief,
Observe wild animal, monitoring infectious disease, mapping, news report, electric inspection process, the disaster relief, movies-making, manufacture romance etc. field
Application, greatly expanded the purposes of unmanned plane itself, developed country is also in actively extension sector application and development unmanned plane
Technology.
Whole world unmanned plane market is burning hot at present, and various unmanned plane peripheries application apparatus is also dazzling, but is thrown for article
The special installation put may be selected seldom, and structure is unreasonable, and cost is higher, and operational reliability is relatively low.
It is at low cost accordingly, it is desirable to provide a kind of universal unmanned plane article delivery device, simple for structure, using simplicity,
Operational reliability is high.
Invention content
In order to overcome the disadvantages of the prior art mentioned above, it is an object of the present invention to provide a kind of universal unmanned planes
Article delivery device, simple for structure, at low cost, using simplicity, operational reliability is high, is suitable for large-scale promotion application.
It is ingenious in design another object of the present invention is to provide a kind of universal unmanned plane article delivery device, manufacture
Simplicity is suitable for large-scale promotion application.
To achieve the above objectives, the present invention provides a kind of universal unmanned plane article delivery device, including shell, the shell
Unmanned plane mounting structure is provided on body, its main feature is that, the universal unmanned plane article delivery device further include left side slide-bar,
Right side slide-bar, left side solenoid valve, right side solenoid valve, left side elastomeric element, right side elastomeric element, signal receive and power control dress
Control device is set and launches, the left side solenoid valve and the right side solenoid valve or so relative spacing are disposed in the housing,
The left side slide-bar is installed in the right end of the magnetic core of the left side solenoid valve and at least partly protrudes from the left side solenoid valve
Shell, the right side slide-bar are installed in the left end of the magnetic core of the right side solenoid valve and at least partly protrude from the right side electromagnetism
The shell of valve, the left side slide-bar are arranged with the right side slide-bar relative spacing, and the left side elastomeric element is located at the left side
In solenoid valve and both ends bear against the solenoid housing and the left side slide-bar or the left side electromagnetism of the left side solenoid valve
For being intended to that the left side slide-bar is made to move towards the right side slide-bar, the right side elastomeric element is located at described the magnetic core of valve
In the solenoid valve of right side and both ends bear against solenoid housing and the right side slide-bar or the right side of the right side solenoid valve
For the magnetic core of solenoid valve for being intended to that the right side slide-bar is made to move towards the left side slide-bar, the dispensing control device is wireless
Signal connects the signal reception and power control apparatus and is wirelessly sent to the signal reception and energization for that will launch signal
Control device, the signal receives and power control apparatus is disposed in the housing and circuit connects the left side electromagnetism respectively
Valve and the right side solenoid valve after receiving the dispensing signal for controlling the coil of the left side solenoid valve and the right side
The coil of side solenoid valve is powered to keep the magnetic core of the magnetic core of the left side solenoid valve and the right side solenoid valve mutually remote
From.
Preferably, the left side slide-bar is set in the right end of the magnetic core of the left side solenoid valve and wears the left side electricity
The shell of magnet valve.
Preferably, the right side slide-bar is set in the left end of the magnetic core of the right side solenoid valve and wears the right side electricity
The shell of magnet valve.
Preferably, the left end of the left side slide-bar has the first radial flange, the left side elastomeric element is against described the
One radial flange.
Preferably, the right end of the right side slide-bar has the second radial flange, the right side elastomeric element is against described the
Two radial flanges.
Preferably, the left side elastomeric element is the first spring, first spring is set in the left side solenoid valve
Magnetic core on.
Preferably, the right side elastomeric element is second spring, the second spring is set in the right side solenoid valve
Magnetic core on.
Preferably, the unmanned plane mounting structure is mounting hole.
More preferably, the mounting hole is sleeve configuration mounting hole.
Preferably, the shell includes top plate, left shell and right shell, the left shell and the right shell
Left and right is arranged at intervals on the lower surface of the top plate, and the unmanned plane mounting structure is arranged on the top plate, the left side electricity
Magnet valve is arranged in the left shell, and the right side solenoid valve is arranged in the right shell, and the signal receives and leads to
Controller for electric consumption is arranged in the left shell or the right shell.
Beneficial effects of the present invention essentially consist in：
1, left and right sides solenoid valve of universal unmanned plane article delivery device of the invention or so relative spacing is arranged in shell
In body, left and right axis of sideslip is installed in the right left end of the magnetic core of left and right sides solenoid valve and at least partly protrudes from left and right sides respectively respectively
The shell of solenoid valve, relative spacing setting, left side elastomeric element is located in the solenoid valve of left side and both ends bear against left side electromagnetism
The solenoid housing and the magnetic core of left side slide-bar or left side solenoid valve of valve make left side slide-bar be moved towards right side slide-bar for being intended to,
Right side elastomeric element is located at solenoid housing and right side slide-bar or the right side that in the solenoid valve of right side and both ends bear against right side solenoid valve
The magnetic core of side solenoid valve makes right side slide-bar be moved towards left side slide-bar for being intended to, and launches control device wireless signal connection letter
Number receive and power control apparatus for will launch signal be wirelessly sent to signal receive and power control apparatus, signal reception and
Circuit connection left and right sides solenoid valve is used to after receiving dispensing signal control in the housing and respectively for power control apparatus setting
The coil of left and right sides solenoid valve is powered to make the magnetic core of left and right sides solenoid valve be located remotely from each other, in use, in solenoid valve no power
In the case of, left and right axis of sideslip is mutually drawn close under the elastic force effect of respective left and right sides elastomeric element, is inserted into is located at a left side respectively
Locking is realized in load object between the slide-bar of right side, and when that need to unlock dispensing to load object, throwing is sent out by launching control device
Discharge signal is received to signal and power control apparatus, receives after launching signal, and signal receives and power control apparatus control is left
The coil of right side solenoid valve is powered, and electromagnetic valve coil generates magnetic force, and the magnetic core of left and right sides solenoid valve is inhaled into left and right sides electricity respectively
In magnet valve, left and right axis of sideslip is located remotely from each other therewith, is detached from load object, completes the unlock to load object, load object is with gravity
It falls and completes to launch, therefore, simple for structure, at low cost, using simplicity, operational reliability is high, is suitable for large-scale promotion application.
2, left and right sides solenoid valve of universal unmanned plane article delivery device of the invention or so relative spacing is arranged in shell
In body, left and right axis of sideslip is installed in the right left end of the magnetic core of left and right sides solenoid valve and at least partly protrudes from left and right sides respectively respectively
The shell of solenoid valve, relative spacing setting, left side elastomeric element is located in the solenoid valve of left side and both ends bear against left side electromagnetism
The solenoid housing and the magnetic core of left side slide-bar or left side solenoid valve of valve make left side slide-bar be moved towards right side slide-bar for being intended to,
Right side elastomeric element is located at solenoid housing and right side slide-bar or the right side that in the solenoid valve of right side and both ends bear against right side solenoid valve
The magnetic core of side solenoid valve makes right side slide-bar be moved towards left side slide-bar for being intended to, and launches control device wireless signal connection letter
Number receive and power control apparatus for will launch signal be wirelessly sent to signal receive and power control apparatus, signal reception and
Circuit connection left and right sides solenoid valve is used to after receiving dispensing signal control in the housing and respectively for power control apparatus setting
The coil of left and right sides solenoid valve is powered to make the magnetic core of left and right sides solenoid valve be located remotely from each other, in use, in solenoid valve no power
In the case of, left and right axis of sideslip is mutually drawn close under the elastic force effect of respective left and right sides elastomeric element, is inserted into is located at a left side respectively
Locking is realized in load object between the slide-bar of right side, and when that need to unlock dispensing to load object, throwing is sent out by launching control device
Discharge signal is received to signal and power control apparatus, receives after launching signal, and signal receives and power control apparatus control is left
The coil of right side solenoid valve is powered, and electromagnetic valve coil generates magnetic force, and the magnetic core of left and right sides solenoid valve is inhaled into left and right sides electricity respectively
In magnet valve, left and right axis of sideslip is located remotely from each other therewith, is detached from load object, completes the unlock to load object, load object is with gravity
It falls and completes to launch, therefore, ingenious in design, manufacture is easy, is suitable for large-scale promotion application.
These and other objects, feature and the advantage of the present invention, by following detailed descriptions, drawings and claims obtain
To fully demonstrate, and can be achieved by means, device and the combination thereof specially pointed out in appended claims.
Description of the drawings
Fig. 1, which is the specific embodiment locking of the universal unmanned plane article delivery device of the present invention, the solid of load object
Schematic diagram.
Fig. 2 is the main view partial schematic diagram of structure shown in Fig. 1.
Fig. 3 is that structure shown in Fig. 1 looks up partial schematic diagram.
Fig. 4 is the main view section view partial schematic diagram of structure shown in Fig. 1.
Fig. 5 is the close-up schematic view of structure shown in Fig. 4.
Fig. 6 is the main view section view partial schematic diagram of specific embodiment unlock load object shown in FIG. 1.
(symbol description)
1 shell；11 unmanned plane mounting structures；12 top plates；13 left shells, 14 right shells；15 substrates；16 cover boards；2 is left
Axis of sideslip；21 first radial flanges；3 right side slide-bars；31 second radial flanges；4 left side solenoid valves；The magnetic of 41 left side solenoid valves
Core；The solenoid housing of 42 left side solenoid valves；The coil of 43 left side solenoid valves；The shell of 44 left side solenoid valves；5 right side solenoid valves；
The magnetic core of 51 right side solenoid valves；The solenoid housing of 52 right side solenoid valves；The coil of 53 right side solenoid valves；Outside 54 right side solenoid valves
Shell；6 left side elastomeric elements；7 right side elastomeric elements；8 signals receive and power control apparatus；81 antennas；9 launch control device；
10 load objects；20 power lights；30 status indicator lamps；40 devices switch；50 charging interfaces.
Specific implementation mode
In order to be more clearly understood that the technology contents of the present invention, spy are lifted following embodiment and are described in detail.
It refers to shown in Fig. 1~Fig. 6, in the specific embodiment of the present invention, universal unmanned plane article of the invention
Delivery device include shell 1, left side slide-bar 2, right side slide-bar 3, left side solenoid valve 4, right side solenoid valve 5, left side elastomeric element 6,
Right side elastomeric element 7, signal receive and power control apparatus 8 and launch control device 9, are provided with unmanned plane on the shell 1
Mounting structure 11, the left side solenoid valve 4 and 5 or so relative spacing of the right side solenoid valve are arranged in the shell 1, described
Left side slide-bar 2 is installed in the right end of the magnetic core 41 of the left side solenoid valve 4 and is partially protrude through the shell of the left side solenoid valve 4
44, the right side slide-bar 3 is installed in the left end of the magnetic core 51 of the right side solenoid valve 5 and is partially protrude through the right side solenoid valve
5 shell 54, the left side slide-bar 2 are arranged with 3 relative spacing of right side slide-bar, and the left side elastomeric element 6 is located at described
In left side solenoid valve 4 and both ends bear against the solenoid housing 42 of the left side solenoid valve 4 and the left side slide-bar 2 is used to tend to
In making the left side slide-bar 2 be moved towards the right side slide-bar 3, the right side elastomeric element 7 is located in the right side solenoid valve 5
And both ends bear against the solenoid housing 52 of the right side solenoid valve 5 and the right side slide-bar 3 is used to be intended to make the right side
Slide-bar 3 is moved towards the left side slide-bar 2, and 9 wireless signal of dispensing control device connects the signal reception and the control that is powered
Device 8 processed is wirelessly sent to the signal reception and power control apparatus 8 for that will launch signal, and the signal receives and is powered
Control device 8 is arranged in the shell 1 and circuit connects the left side solenoid valve 4 respectively and the right side solenoid valve 5 is used for
The coil 53 of coil 43 and the right side solenoid valve 5 that the left side solenoid valve 4 is controlled after receiving the dispensing signal is logical
Electricity is to make the magnetic core 41 of the left side solenoid valve 4 and the magnetic core 51 of the right side solenoid valve 5 be located remotely from each other.
The both ends of the left side elastomeric element 6 can also bear against solenoid housing 42 and the institute of the left side solenoid valve 4
The both ends of the magnetic core 41 for the left side solenoid valve 4 stated, the right side elastomeric element 7 can also bear against the right side solenoid valve 5
Solenoid housing 52 and the right side solenoid valve 5 magnetic core 51；The left side slide-bar 2 can also all protrude from the left side
The shell 44 of solenoid valve 4, the right side slide-bar 3 can also all protrude from the shell 54 of the right side solenoid valve 5, equally can be with
It achieves the object of the present invention.
Any suitable knot may be used in the right end that the left side slide-bar 2 is installed in the magnetic core 41 of the left side solenoid valve 4
Structure refers to shown in Fig. 4 and Fig. 6, and in the specific embodiment of the present invention, the left side slide-bar 2 is set in the left side
The right end of the magnetic core 41 of solenoid valve 4 and the shell 44 for wearing the left side solenoid valve 4.
Any suitable knot may be used in the left end that the right side slide-bar 3 is installed in the magnetic core 51 of the right side solenoid valve 5
Structure refers to shown in Fig. 4~Fig. 6, and in the specific embodiment of the present invention, the right side slide-bar 3 is set in the right side
The left end of the magnetic core 51 of solenoid valve 5 and the shell 54 for wearing the right side solenoid valve 5.
Any suitable structure may be used against the left side slide-bar 2 in the left side elastomeric element 6, refer to Fig. 4 and
Shown in Fig. 6, in the specific embodiment of the present invention, the left end of the left side slide-bar 2 has the first radial flange 21, the left side
Side elastomeric element 6 is against first radial flange 21.
Any suitable structure may be used against the right side slide-bar 3 in the right side elastomeric element 7, refer to Fig. 4~
Shown in Fig. 6, in the specific embodiment of the present invention, the right end of the right side slide-bar 3 has the second radial flange 31, the right side
Side elastomeric element 7 is against second radial flange 31.
The left side elastomeric element 6 can be any suitable elastomeric element, refer to shown in Fig. 4 and Fig. 6, in the present invention
A specific embodiment in, the left side elastomeric element 6 is the first spring, and first spring is set in the left side electromagnetism
On the magnetic core 41 of valve 4.
The right side elastomeric element 7 can be any suitable elastomeric element, refer to shown in Fig. 4~Fig. 6, in the present invention
A specific embodiment in, the right side elastomeric element 7 is second spring, and the second spring is set in the right side electromagnetism
On the magnetic core 51 of valve 5.
The universal unmanned plane article delivery device of the present invention is mounted on unmanned plane by the unmanned plane mounting structure 11
On, which may be used any suitable structure, such as is detachably connected and such as bolt and nut is used to connect, can not also can
Dismantling connection is such as welded, preferably, using being detachably connected, the unmanned plane mounting structure 11 is mounting hole, passes through bolt
Corresponding mounting hole on mounting hole and unmanned plane is worn, then screws on nut and is fixed.It refers to shown in Fig. 1 and Fig. 3, in this hair
In a bright specific embodiment, the mounting hole is sleeve configuration mounting hole, that is, lengthens compatible type mounting hole, and bolt can be
Length direction in sleeve configuration mounting hole along sleeve configuration mounting hole moves, can be according to the position of the mounting hole of different unmanned planes
Highly compatible is realized in difference, position of the adjustment bolt in sleeve configuration mounting hole.
The shell 1 can have any suitable structure, refer to shown in Fig. 1~Fig. 6, and one in the present invention is specific real
It applies in example, the shell 1 includes top plate 12, left shell 13 and right shell 14, the left shell 13 and the right side shell
Body 14 or so is arranged at intervals on the lower surface of the top plate 12, and the unmanned plane mounting structure 11 is arranged on the top plate 12,
(such as being embedded) is arranged in the left shell 13 in the left side solenoid valve 4, and (such as being embedded) is arranged in the right side solenoid valve 5
In the right shell 14, the signal receives and power control apparatus 8 is arranged in the right shell 14.Obviously, institute
Stating signal reception and power control apparatus 8 can also be arranged in the left shell 13.
The top plate 12 can have any suitable structure, refer to shown in Fig. 1~Fig. 2 and Fig. 4~Fig. 6, in this hair
In a bright specific embodiment, the top plate 12 includes substrate 15 and cover board 16, and the cover board 16 is arranged in the substrate 15
On upper surface, the left shell 13 and the right shell 14 or so are arranged at intervals on the lower surface of the substrate 15.
The substrate 15 can be the substrate of any suitable material, such as aluminium alloy base plate.The cover board 16 can be appointed
The cover board of what suitable material, such as resin cover board.The left shell 13 and the right shell 14 can be any suitable materials
The shell of matter, such as Al-alloy casing.The shell 54 of the shell 44 of the left side solenoid valve 4 and the right side solenoid valve 5
Can be the shell of any suitable material, such as resin enclosure.The solenoid housing 42 of the left side solenoid valve 4 and the right side
The solenoid housing 52 of side solenoid valve 5 can be the solenoid housing of any suitable material, such as iron solenoid housing.The signal connects
It receives and power control apparatus 8 receives the dispensing signal and can be received by antenna 81.
The present invention is in use, universal unmanned plane article delivery device is mounted on unmanned plane by unmanned plane mounting structure 11
On, load object 10 is placed between left side solenoid valve 4 and right side solenoid valve 5, left side slide-bar cold in solenoid valve
2 and right side slide-bar 3 mutually drawn close under the effect of the elastic force of left side elastomeric element 6 and right side elastomeric element 7 respectively, to inserting respectively
Enter and realize locking (as shown in Figure 4) in load object 10, when dispensing need to be unlocked to load object 10, is sent out by launching control device 9
Go out to launch signal to signal reception and power control apparatus 8, signal receives and power control apparatus 8 is received after launching signal and controlled
The coil 43 of system left side solenoid valve 4 and the coil 53 of right side solenoid valve 5 are powered, and electromagnetic valve coil generates magnetic force, left side solenoid valve 4
Magnetic core 41 and right side solenoid valve 5 magnetic core 51 be inhaled into respectively left side solenoid valve 4 and right side solenoid valve 5 in and be located remotely from each other,
Left side slide-bar 2 and right side slide-bar 3 are located remotely from each other with the magnetic core 51 of the magnetic core 41 of left side solenoid valve 4 and right side solenoid valve 5 respectively, from
And it is detached from load object 10, the unlock to load object 10 is completed, load object 10 falls with gravity and completes to launch (such as Fig. 6 institutes
Show).
In order to switch the universal unmanned plane article delivery device of the present invention, refer to shown in Fig. 1~Fig. 3, in the present invention
A specific embodiment in, can on shell 1 (be specifically left shell 13) setting device switch 40.In order to have a clear understanding of this
The universal unmanned plane article delivery device state in which of invention, can be arranged various indicator lights, such as on the right side on shell 1
Power lights 20 and status indicator lamp 30 are set on side body 14, and power lights 20 are always on after the booting of device for opening switch 40 is powered, and are locked
When determining load object 10, status indicator lamp 30 is always on, and coil is powered after unlock load object 10, and status indicator lamp 30 extinguishes.The present invention
Universal unmanned plane article delivery device in accumulator can also be set, then shell 1 (be specifically right shell 14, certainly
Can be left shell 13) on be arranged charging interface 50.
Therefore, the present invention uses bilateral extension type slide-bar structural bearing load object, while slide-bar passes through contained spring pressure
The top bullet of power keeps the locking to load object.When that need to unlock dispensing to load object, user passes through remote controler and launches control
Device sends out control signal and launches signal, signal reception and power control apparatus receive in device control signal after, while it is right
Double-side electromagnetic valve is powered, and electromagnetic valve coil generates magnetic force, and both sides magnetic core is sucked simultaneously, and two axiss of sideslip is driven to take in dress simultaneously
In setting, the unlock to load object is completed, load object falls with gravity to be completed to launch.
The present invention can quickly and easily be mounted on various commonly use and take photo by plane on unmanned plane, and reliable fortune under circumstances
Make.Using independent remote control, the present apparatus can be made not need to carry out additionally control device because replacing unmanned aerial vehicle platform
Adaptation, bilateral extension type slide-bar carries that locking structure-is simple in structure, load-bearing is reliable, and bilateral magnet valve synchronizing unlocking-dispensing is fast
Speed, reliability are high, and lengthening compatible type mounting hole-applicability is extensive, installation is simple.
To which the present invention, which is one kind, to be quickly and easily mounted on various common unmanned planes, and applicability is good, installation letter
Just, movement structure is simple, the high multipurpose article delivery device of operational reliability.
To sum up, universal unmanned plane article delivery device of the invention is simple for structure, and at low cost, using simplicity, running can
Ingenious in design by property height, manufacture is easy, is suitable for large-scale promotion application.
It can be seen that the purpose of the present invention is achieved completely and effectively.The function and structural principle of the present invention
It is shown and is illustrated in embodiment, under without departing substantially from the principle, embodiment can make arbitrary modification.So this hair
Bright includes all variant embodiments based on claim spirit and right.
Claims (10)
1. a kind of universal unmanned plane article delivery device, including shell, it is provided with unmanned plane mounting structure on the shell,
It is characterized in that, the universal unmanned plane article delivery device further includes left side slide-bar, right side slide-bar, left side solenoid valve, right side
Solenoid valve, left side elastomeric element, right side elastomeric element, signal reception and power control apparatus and dispensing control device, the left side
Side solenoid valve and the right side solenoid valve or so relative spacing are disposed in the housing, and the left side slide-bar is installed in the left side
The right end of the magnetic core of side solenoid valve and the shell at least partly protruding from the left side solenoid valve, the right side slide-bar are installed in institute
It states the left end of the magnetic core of right side solenoid valve and at least partly protrudes from the shell of the right side solenoid valve, the left side slide-bar and institute
Right side slide-bar relative spacing setting is stated, described in the left side elastomeric element is located in the left side solenoid valve and both ends bear against
The solenoid housing of left side solenoid valve and the magnetic core of the left side slide-bar or the left side solenoid valve are for being intended to make the left side
Axis of sideslip is moved towards the right side slide-bar, and the right side elastomeric element is located in the right side solenoid valve and both ends are born against
The solenoid housing of the right side solenoid valve and the magnetic core of the right side slide-bar or the right side solenoid valve are for being intended to make institute
It states right side slide-bar to move towards the left side slide-bar, the dispensing control device wireless signal connects the signal and receives and be powered
Control device is wirelessly sent to the signal reception and power control apparatus for that will launch signal, and the signal receives and is powered
Control device is disposed in the housing and circuit connects the left side solenoid valve and the right side solenoid valve for connecing respectively
The coil for receiving the coil and the right side solenoid valve that control the left side solenoid valve after the dispensing signal is powered to make
The magnetic core of the magnetic core for the left side solenoid valve stated and the right side solenoid valve is located remotely from each other.
2. universal unmanned plane article delivery device as described in claim 1, which is characterized in that the left side slide-bar is set in
The right end of the magnetic core of the left side solenoid valve and the shell for wearing the left side solenoid valve.
3. universal unmanned plane article delivery device as described in claim 1, which is characterized in that the right side slide-bar is set in
The left end of the magnetic core of the right side solenoid valve and the shell for wearing the right side solenoid valve.
4. universal unmanned plane article delivery device as described in claim 1, which is characterized in that the left end of the left side slide-bar
With the first radial flange, the left side elastomeric element is against first radial flange.
5. universal unmanned plane article delivery device as described in claim 1, which is characterized in that the right end of the right side slide-bar
With the second radial flange, the right side elastomeric element is against second radial flange.
6. universal unmanned plane article delivery device as described in claim 1, which is characterized in that the left side elastomeric element is
First spring, first spring are set on the magnetic core of the left side solenoid valve.
7. universal unmanned plane article delivery device as described in claim 1, which is characterized in that the right side elastomeric element is
Second spring, the second spring are set on the magnetic core of the right side solenoid valve.
8. universal unmanned plane article delivery device as described in claim 1, which is characterized in that the unmanned plane mounting structure
For mounting hole.
9. universal unmanned plane article delivery device as claimed in claim 8, which is characterized in that the mounting hole is sleeve configuration
Mounting hole.
10. universal unmanned plane article delivery device as described in claim 1, which is characterized in that the shell include top plate,
Left shell and right shell, the left shell and the right shell or so are arranged at intervals on the lower surface of the top plate,
The unmanned plane mounting structure is arranged on the top plate, and the left side solenoid valve is arranged in the left shell, the right side
Side solenoid valve is arranged in the right shell, and the signal receives and power control apparatus is arranged in the left shell or institute
It states in right shell.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810347248.3A CN108382597A (en) | 2018-04-18 | 2018-04-18 | Universal unmanned plane article delivery device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810347248.3A CN108382597A (en) | 2018-04-18 | 2018-04-18 | Universal unmanned plane article delivery device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108382597A true CN108382597A (en) | 2018-08-10 |
Family
ID=63065008
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810347248.3A Pending CN108382597A (en) | 2018-04-18 | 2018-04-18 | Universal unmanned plane article delivery device |
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| CN (1) | CN108382597A (en) |
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| CN107806291A (en) * | 2017-11-27 | 2018-03-16 | 王福君 | A kind of electromagnetic lock |
| CN208198836U (en) * | 2018-04-18 | 2018-12-07 | 上海唯成电子科技有限公司 | Universal unmanned plane article delivery device |
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- 2018-04-18 CN CN201810347248.3A patent/CN108382597A/en active Pending
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| WO1982002527A1 (en) * | 1981-01-26 | 1982-08-05 | Rockwell International Corp | An ejector device for stores |
| CN2752103Y (en) * | 2004-11-19 | 2006-01-18 | 姚流文 | Distance and near lamp dimming means for vehicle lamp |
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