CN207062653U - Utilize the component installation unmanned plane and cradle of BIM combination planar bar code technologies - Google Patents
Utilize the component installation unmanned plane and cradle of BIM combination planar bar code technologies Download PDFInfo
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- CN207062653U CN207062653U CN201720860249.9U CN201720860249U CN207062653U CN 207062653 U CN207062653 U CN 207062653U CN 201720860249 U CN201720860249 U CN 201720860249U CN 207062653 U CN207062653 U CN 207062653U
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- 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
- Y02T90/00—Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02T90/10—Technologies relating to charging of electric vehicles
- Y02T90/16—Information or communication technologies improving the operation of electric vehicles
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Abstract
The utility model provides the unmanned plane of the component installation method using BIM combination planar bar code technologies, the unmanned plane includes protective cradle capture apparatus, and supporting cradle, cradle then has fixed structure, the utility model provides the component installation unmanned plane and cradle using BIM combination planar bar code technologies, BIM combination radio frequency chips are substituted using BIM combinations planar bar code technology, so cost is cheaper, can each component using easily facilitate management, it is identified for the supporting dedicated unmanned machine of large-scale component, unmanned plane can be used as patrol unmanned machine when not having to, equipment will not be caused to waste, and supporting special charging equipment, so as to greatly improve the building efficiency of assembled architecture.
Description
Technical field
Building corollary equipment field is the utility model is related to, more particularly to the component using BIM combination planar bar code technologies
Installation unmanned plane and cradle.
Background technology
Currently, the environmental problem come with China's economic development becomes increasingly conspicuous.Traditional architecture industry is because of its resource waste rate
Height, pollution is heavy and endures to the fullest extent and denounces, and at the same time, assembled architecture is because its construction pollution is few, speed of application is fast, resource utilization
The advantages that high, is increasingly paid close attention to by the whole society.Assembled architecture has systematization of design, component production plant, installation special
The features such as industry, these features make assembled architecture build in design, prefabricated components production and construct with traditional cast-type
There is marked difference in journey.
In recent years, China's building trade progressively promotes BIM correlation techniques and method, for assembled architecture,
Technology platform and instrument related BIM can effectively improve assembled architecture design, production and the efficiency of construction, promote assembling
Formula is built this new model building form indeed and faster and better promoted.
For this, someone expects, using related BIM technology platform and instrument, using BIM technology combination RFID technique, passing through
The embedded RFID chip containing the component information such as installation position and purposes information, storage are checked and accepted during prefabricated components produce
Personnel and logistics distribution personnel can directly read the relevant information of prefabricated components, realize the automatic control of electronic information, reduce
Examination volume deviation, component stowed location deviation, the outbound record occurred under traditional artificial examination and logistic pattern is inaccurate
The generation of really the problems such as, can significantly save time and cost.
But RFID chip cost is often higher, common method is to unify the product of a batch with one altogether at present
Individual radio frequency chip is managed to reduce corresponding cost, but prefabricated component often varies, cost remains unchanged very high, radio frequency core
Though piece can pick and place recycling due to Large Precast Members pick and place it is often relatively difficult, and with planar bar code technology
Popularization, and Quick Response Code paster price extremely friend, therefore corresponding information can be converted into Quick Response Code, it is covered in corresponding
Component, so almost each component can paste, and so as to be more convenient for that it is managed accordingly, consider that partial component is higher
Greatly, Quick Response Code can not be remotely identified, therefore large-scale component identification can be carried out using unmanned plane with supporting corresponding unmanned plane.
Utility model content
In order to solve above-mentioned problem, the utility model provides to be installed using the component of BIM combination planar bar code technologies
With unmanned plane and cradle, BIM combination radio frequency chips are substituted using BIM combinations planar bar code technology, such cost is cheaper,
Each component using management is easily facilitated, it can be identified for the supporting dedicated unmanned machine of large-scale component, unmanned plane is not
By the use of when equipment can will not be caused to waste as patrol unmanned machine, and supporting special charging equipment, so as to significantly carry
The building efficiency of high assembled architecture, pacified for up to this purpose, the utility model provides using the component of BIM combination planar bar code technologies
Dress method, is comprised the following steps that：
Step 1: establishing prefabricated member according to project situation splits combined method, it is to project using BIM technology
System analysis, project assembly method is carried out reasonably to plan and arrange before model is established；
Step 2: establish corresponding BIM models, enter prefabricated member lifting arrangement using above-mentioned BIM models, and by three-dimensional
Model, which imports, carries out construction simulation optimization in BIM5D, and contrasts the difference of construction cost plan and estimated cost plan；
Step 3: prefabricated components are generated into Quick Response Code paster in a model by component generation 2-D data information；
Step 4: the production and processing each prefabricated components of prefabricated components are covered with Quick Response Code paster；
Step 5: building element installation is carried out, using corresponding device or unmanned plane to building element in installation process
Quick Response Code paster is identified, and carries out the monitoring and installation of system.
The further improvement of the utility model installation method, route inspection is fixed in unmanned plane in architectural process, nobody
Charged after machine landing by cradle, in order to ensure that unmanned plane makes full use of processing to be identified, be also used as inspection
Route inspection is fixed in unmanned plane, and is charged when supporting cradle does not have to, to ensure long-term use.
The further improvement of the utility model installation method, there is positioning at three angles of Quick Response Code in the Quick Response Code paster
Point, the supporting anchor point of Quick Response Code can improve recognition efficiency.
Respectively there are a positioning vitta, institute in the further improvement of the utility model installation method, the Quick Response Code paster both sides
Positioning vitta is stated as red, supporting positioning vitta can quickly determine two-dimentional code position in order to unmanned plane, and vitta is typically using red
Color coordinates infrared inductor to use.
The utility model provides unmanned plane used in the component installation method using BIM combination planar bar code technologies, including nobody
Owner's body, signal transceiver, side connecting bracket, Arcuate flexible protection board, connecting plate, interior empty rotor support, rotor motor,
Fin, landing gear, triangle landing gear link, video camera, electric rotating machine, fixed mount and infrared locator, the unmanned owner
Body front end is provided with signal transceiver, and the interior empty rotor support has 4 to be symmetrical arranged two-by-two, the interior empty rotor support
, with being connected on the outside of unmanned plane main body, there are connecting line, the interior empty rotor branch in end by connector in the interior empty rotor support
Rotor motor is installed with frame outboard end, the outer wall of the rotating shaft of each rotor motor is angularly installed with 2-4
Fin, the unmanned plane main body both sides are provided with side connecting bracket, there is an Arcuate flexible protection on the outside of each rotor motor
Plate, the Arcuate flexible protection board end of both sides are connected by connecting plate, are connected on the outside of the side connecting bracket with connecting plate, described
Triangle landing gear link has a pair, and the triangle landing gear link upper end is sleeved in the connecting bracket of side to enter by fastener
Row is fixed, and described two fulcrums in triangle landing gear link lower end are connected with corresponding landing gear, and the video camera both sides respectively have one
Individual electric rotating machine, with being connected on the outside of video camera, the electric rotating machine is fixed on nothing by fixed mount for the rotating shaft of the electric rotating machine
The bottom of man-machine main body, the both sides of the camera lens of the video camera are respectively provided with an infrared locator.
The further improvement of the utility model unmanned plane, the connecting plate outside are provided with colliding sensor, set collision
Inductor can in time find to collide thing, encounter unmanned plane to prevent debris and cause damage.
The further improvement of the utility model unmanned plane, side connecting bracket middle part lower section is provided with location-plate, described
Respectively there is a unmanned plane positioning inductor lower section at four angles of location-plate, and there is charging column location-plate middle part lower section, set
Unmanned plane automatic lifting can be realized after location-plate.
The utility model provides the cradle of unmanned plane, including cradle main body, solar panel, band guide rail land
Bar, interior empty support bar, reinforcing plate, cradle positioning inductor, charging ring, supporting plate and pin type locating rack, the cradle master
There are sun energy cell panel, band guide rail landing bar and interior empty support bar on body, the sun energy cell panel is laid in cradle main body, institute
It is flexible-belt guide rail landing bar to state band guide rail landing bar, and the band guide rail landing bar, which has a pair, to be fixed in cradle main body, nothing
Landing gear is stuck in the guide rail with guide rail landing bar after man-machine landing, there is connecting line, the interior empty branch in the interior empty support bar
Strut lower end is fixed in cradle main body, and there is reinforcing plate the interior empty support bar side, and the interior empty post upper has branch
There is cradle positioning inductor fagging, four angles top of the supporting plate, and there is charging ring supporting plate middle part top, institute
State the side bottom of cradle main body two and a pair of pin type locating racks are respectively installed, pilot pin is arranged at the pin type locating rack bottom.
The further improvement of the utility model cradle, side is provided with a pair of handles before and after the cradle main body, considers
Large-scale unmanned plane cradle is larger, sets handle to be moved in order to cradle.
The further improvement of the utility model cradle, the pin type locating rack are activity orientation frame, the pin type positioning
Frame, with being connected on the outside of cradle main body, has magnetic sheet relative with pin type locating rack by connects hinge on the outside of the cradle main body
Should, after pin type locating rack lifts absorption consider that it is cement flooring sometimes to place ground, therefore pin type locating rack should can on the outside of magnetic sheet
With activity.
The utility model provides the component installation unmanned plane and cradle using BIM combination planar bar code technologies, component peace
BIM combination radio frequency chips are substituted using BIM combinations planar bar code technology in dress method, radio frequency chip is substituted using Quick Response Code paster
Significantly saved cost, and can all components pasted, so as to easily facilitate centralized management, wherein Quick Response Code both sides
It can be positioned provided with colour identification bar in order to which unmanned plane identifies, for the supporting dedicated unmanned machine of installation containing large-scale component, nobody
There is the colored identification bar that infrared identification device can identify Quick Response Code both sides machine camera both sides, consequently facilitating unmanned plane positioning is swept
Retouch, unmanned plane wing can be flown containing protection mechanism in building site, and unmanned plane need not identify that operation can be used as and patrol
Examine unmanned plane to use, periodically building site is shot, find the dangerous timely early warning of progress, and be designed with special cradle and supply
Unmanned plane lands, and can directly be charged after unmanned plane landing, and cradle top is used for the nothing for supporting landing containing supporting support
Man-machine, the guide rail containing landing is placed for unmanned plane alighting carriage, is also equipped with solar panel, unmanned plane work and inspection process
In can voluntarily be charged, there is handle to be put in order to lift on the outside of cradle, and supporting pin type locating rack can be adapted to it is various
Landform is steadily placed, and will not be loosened after placement, and pin type locating rack can be packed up by magnetic sheet when level land, not influence so
Place on level land.
Brief description of the drawings
Fig. 1 is the utility model unmanned plane and cradle overall schematic；
Fig. 2 is the utility model unmanned plane schematic diagram；
Fig. 3 is the utility model cradle schematic diagram；
Fig. 4 is utility model works view；
Fig. 5 is the utility model Quick Response Code schematic diagram；
Illustrate；
1st, unmanned plane；1-1, unmanned plane main body；1-2, signal transceiver；1-3, side connecting bracket；1-4, arc are soft
Property protection board；1-5, connecting plate；1-6, colliding sensor；1-7, interior empty rotor support；1-8, rotor motor；1-9, fin；1-
10th, landing gear；1-11, triangle landing gear link；1-12, location-plate；1-13, unmanned plane positioning inductor；1-14, charging
Post；1-15, video camera；1-16, electric rotating machine；1-17, fixed mount；1-18, infrared locator；2nd, cradle；2-1, cradle
Main body；2-2, solar panel；2-3, band guide rail landing bar；2-4, handle；2-5, interior empty support bar；2-6, reinforcing plate；2-
7th, cradle positioning inductor；2-8, charging ring；2-9, supporting plate；2-10, pin type locating rack；2-10-1, pilot pin；2-11、
Connects hinge；2-12, magnetic sheet；3rd, building element；4th, Quick Response Code paster；4-1, Quick Response Code；4-2, anchor point；4-3, positioning color
Bar.
Embodiment
The utility model is described in further detail with embodiment below in conjunction with the accompanying drawings：
The utility model provides the component installation unmanned plane and cradle using BIM combination planar bar code technologies, utilizes BIM
Substitute radio frequency chip with reference to planar bar code technology, such cost is cheaper, can each component using easily facilitate management,
It is identified for the supporting dedicated unmanned machine of large-scale component, patrol unmanned machine, Bu Huizao can be used as when unmanned plane does not have to
Forming apparatus wastes, and supporting special charging equipment, so as to greatly improve the building efficiency of assembled architecture.
As a kind of specific embodiment of the utility model method, the utility model provides combines two using BIM as shown in Figure 4
The component installation method of code technology is tieed up, is comprised the following steps that：
Step 1: establishing prefabricated member according to project situation splits combined method, it is to project using BIM technology
System analysis, project assembly method is carried out reasonably to plan and arrange before model is established；
Step 2: establish corresponding BIM models, enter prefabricated member lifting arrangement using above-mentioned BIM models, and by three-dimensional
Model, which imports, carries out construction simulation optimization in BIM5D, and contrasts the difference of construction cost plan and estimated cost plan；
Step 3: by prefabricated components in a model by component generation 2-D data information, generation Quick Response Code paster 4；
Step 4: the production and processing each prefabricated components of prefabricated components are covered with Quick Response Code paster 4；
Installed Step 5: carrying out building element 3, using corresponding device or unmanned plane 1 to building element 3 in installation process
Quick Response Code paster 4 be identified, and carry out the monitoring and installation of system.
Further, route inspection is fixed in unmanned plane 1 in architectural process as shown in Figure 1, by filling after the landing of unmanned plane 1
Electric seat 2 is charged, and in order to ensure that unmanned plane makes full use of processing to be identified, is also used as patrol unmanned machine and is fixed
Route inspection, and charged when supporting cradle does not have to, to ensure long-term use.
Further, there is anchor point 4-2 at Quick Response Code 4-1 three angles in the Quick Response Code paster 4 as shown in Figure 5, two dimension
The supporting anchor point of code can improve recognition efficiency, and respectively there are a positioning vitta 4-3, the positioning color in the both sides of Quick Response Code paster 4
Bar 4-3 is red, and supporting positioning vitta can quickly determine two-dimentional code position in order to unmanned plane, and vitta is typically coordinated using red
Infrared inductor uses.
As a kind of specific embodiment of the utility model unmanned plane, the utility model provides and utilizes BIM combination Quick Response Code skills
Unmanned plane used in the component installation method of art, including unmanned plane main body 1-1, signal transceiver 1-2, side connecting bracket 1-3,
Arcuate flexible protection board 1-4, connecting plate 1-5, interior empty rotor support 1-7, rotor motor 1-8, fin 1-9, landing gear 1-10, three
Angle landing gear link 1-11, video camera 1-15, electric rotating machine 1-16, fixed mount 1-17 and infrared locator 1-18, the nothing
Man-machine main body 1-1 front ends, which are provided with signal transceiver 1-2, the interior empty rotor support 1-7, has 4 to be symmetrical arranged two-by-two,
The interior empty rotor support 1-7 ends are connected by connector with unmanned plane main body 1-1 outsides, the interior empty rotor support 1-7
Inside there is connecting line, rotor motor 1-8, each rotor motor 1-8 are installed with the interior empty rotor support 1-7 outboard ends
The outer wall of rotating shaft be angularly installed with 2-4 fin 1-9, the unmanned plane main body 1-1 both sides are provided with side connection branch
There are an Arcuate flexible protection board 1-4, the Arcuate flexible protection board 1-4 ends of both sides on the outside of frame 1-3, each rotor motor 1-8
Portion is connected by connecting plate 1-5, is connected on the outside of the side connecting bracket 1-3 with connecting plate 1-5, the triangle landing gear link
1-11 has a pair, and the triangle landing gear link 1-11 upper ends are sleeved on the connecting bracket 1-3 of side to be consolidated by fastener
Fixed, described two fulcrums in triangle landing gear link 1-11 lower ends are connected with corresponding landing gear 1-10, the video camera 1-15 two
Respectively there are electric rotating machine a 1-16, the electric rotating machine 1-16 rotating shaft in side with being connected on the outside of video camera 1-15, the electric rotating
Machine 1-16 is fixed on unmanned plane main body 1-1 bottom by fixed mount 1-17, and the both sides of the camera lens of the video camera 1-15 are respectively pacified
Equipped with an infrared locator 1-18.
As a kind of optimal specific embodiment of the utility model unmanned plane, the utility model provides and utilizes BIM as shown in Figure 2
The unmanned plane with reference to used in the component installation method of planar bar code technology, including unmanned plane main body 1-1, signal transceiver 1-2, side
Connecting bracket 1-3, Arcuate flexible protection board 1-4, connecting plate 1-5, interior empty rotor support 1-7, rotor motor 1-8, fin 1-9,
Landing gear 1-10, triangle landing gear link 1-11, video camera 1-15, electric rotating machine 1-16, fixed mount 1-17 and infrared positioning
Device 1-18, the unmanned plane main body 1-1 front ends, which are provided with signal transceiver 1-2, the interior empty rotor support 1-7,4
It is symmetrical arranged two-by-two, the interior empty rotor support 1-7 ends are connected by connector with unmanned plane main body 1-1 outsides, described interior
There is connecting line in empty rotor support 1-7, be installed with rotor motor 1-8 in the interior empty rotor support 1-7 outboard ends, often
The outer wall of individual rotor motor 1-8 rotating shaft is angularly installed with 2-4 fin 1-9, the unmanned plane main body 1-1 both sides peace
Equipped with side connecting bracket 1-3, there are an Arcuate flexible protection board 1-4, the Arcuate flexible of both sides on the outside of each rotor motor 1-8
Protection board 1-4 ends are connected by connecting plate 1-5, and colliding sensor 1-6 is provided with the outside of the connecting plate 1-5, set collision
Inductor can in time find to collide thing, encounter unmanned plane to prevent debris and cause damage, with connecting on the outside of the side connecting bracket 1-3
Fishplate bar 1-5 is connected, and the triangle landing gear link 1-11 has a pair, and the triangle landing gear link 1-11 upper ends are sleeved on
It is fixed on the connecting bracket 1-3 of side by fastener, lower section is provided with location-plate 1-12 in the middle part of the side connecting bracket 1-3,
Under the lower section at four angles of the location-plate 1-12 respectively has in the middle part of unmanned plane positioning inductor a 1-13, the location-plate 1-12
There is a charging column 1-14 side, and unmanned plane automatic lifting can be realized after location-plate by setting, under the triangle landing gear link 1-11
Two fulcrums in end are connected with corresponding landing gear 1-10, and respectively there are an electric rotating machine 1-16, the rotation in the video camera 1-15 both sides
With being connected on the outside of video camera 1-15, the electric rotating machine 1-16 is fixed on nobody by fixed mount 1-17 for rotating motor 1-16 rotating shaft
Owner's body 1-1 bottom, the both sides of the camera lens of the video camera 1-15 are respectively provided with an infrared locator 1-18.
As a kind of specific embodiment of the utility model unmanned plane, the utility model provides the cradle of unmanned plane, including
Cradle main body 2-1, solar panel 2-2, band guide rail landing bar 2-3, interior empty support bar 2-5, reinforcing plate 2-6, cradle
There is positive energy electricity on positioning inductor 2-7, charging ring 2-8, supporting plate 2-9 and pin type locating rack 2-10, the cradle main body 2-1
Pond plate 2-2, band guide rail landing bar 2-3 and interior empty support bar 2-5, the sun energy cell panel 2-2 are laid on cradle main body 2-1
On, the band guide rail landing bar 2-3 is flexible-belt guide rail landing bar, and the band guide rail landing bar 2-3, which has a pair, is fixed on charging
On seat main body 2-1, landing gear 1-10 is stuck in the guide rail with guide rail landing bar 2-3 after unmanned plane 1 lands, the interior empty support bar
There is connecting line in 2-5, the interior empty support bar 2-5 lower ends are fixed on cradle main body 2-1, the interior empty support bar 2-5 mono-
There is reinforcing plate 2-6 side, and the interior empty support bar 2-5 upper ends have above supporting plate 2-9, the supporting plate 2-9 four angles and had
There are charging ring 2-8, the cradle main body 2-1 both sides bottom in top in the middle part of cradle positioning inductor 2-7, the supporting plate 2-9
Portion is respectively provided with a pair of pin type locating rack 2-10, and pilot pin 2-10-1 is arranged at the pin type locating rack 2-10 bottoms.
As a kind of optimal specific embodiment of the utility model unmanned plane, the utility model provides unmanned plane as shown in Figure 3
Cradle, including cradle main body 2-1, solar panel 2-2, band guide rail landing bar 2-3, interior empty support bar 2-5, strengthen
Plate 2-6, cradle positioning inductor 2-7, charging ring 2-8, supporting plate 2-9 and pin type locating rack 2-10, the cradle main body
There are sun energy cell panel 2-2, band guide rail landing bar 2-3 and interior empty support bar 2-5 on 2-1, the sun energy cell panel 2-2, which is laid on, to be filled
On electric seat main body 2-1, the band guide rail landing bar 2-3 is flexible-belt guide rail landing bar, and the band guide rail landing bar 2-3 has a pair
It is fixed on cradle main body 2-1, landing gear 1-10 is stuck in the guide rail with guide rail landing bar 2-3 after unmanned plane 1 lands, described
There is connecting line in interior empty support bar 2-5, the interior empty support bar 2-5 lower ends are fixed on cradle main body 2-1, the interior empty branch
There is reinforcing plate 2-6 strut 2-5 sides, and there are supporting plate 2-9, the supporting plate 2-9 four angles the interior empty support bar 2-5 upper ends
Top has top in the middle part of cradle positioning inductor 2-7, the supporting plate 2-9 to have charging ring 2-8, the cradle main body 2-
1 liang of side bottom is respectively provided with a pair of pin type locating rack 2-10, and pilot pin 2-10-1 is arranged at the pin type locating rack 2-10 bottoms, described
Pin type locating rack 2-10 is activity orientation frame, and the pin type locating rack 2-10 passes through connects hinge 2-11 and cradle main body 2-1
Outside is connected, and has that magnetic sheet 2-12 is corresponding with pin type locating rack 2-10 on the outside of the cradle main body 2-1, pin type locating rack 2-10
Absorption considers that it be cement flooring sometimes to place ground on the outside of magnetic sheet 2-12 after lifting, thus pin type locating rack should can be movable, institute
Side is provided with a pair of handle 2-4 before and after stating cradle main body 2-1, considers that large-scale unmanned plane cradle is larger, sets handle can be with
It is easy to cradle to move.
It is described above, only it is preferred embodiment of the present utility model, is not that any other is made to the utility model
The limitation of form, and any modification made according to the technical essence of the utility model or equivalent variations, it is new to still fall within this practicality
Type scope claimed.
Claims (6)
1. utilize the component installation unmanned plane of BIM combination planar bar code technologies, including unmanned plane main body（1-1）, signal transmitting connect
Receive device（1-2）, side connecting bracket（1-3）, Arcuate flexible protection board（1-4）, connecting plate（1-5）, interior empty rotor support（1-7）、
Rotor motor（1-8）, fin（1-9）, landing gear（1-10）, triangle landing gear link（1-11）, video camera（1-15）, rotation
Motor（1-16）, fixed mount（1-17）And infrared locator（1-18）, it is characterised in that：The unmanned plane main body（1-1）Front end
Signal transceiver is installed（1-2）, the interior empty rotor support（1-7）There are 4 to be symmetrical arranged two-by-two, the interior empty rotor
Support（1-7）End passes through connector and unmanned plane main body（1-1）Outside is connected, the interior empty rotor support（1-7）Inside there is company
Wiring, the interior empty rotor support（1-7）Rotor motor is installed with outboard end（1-8）, each rotor motor（1-8）
The outer wall of rotating shaft be angularly installed with 2- fin（1-9）, the unmanned plane main body（1-1）Both sides are provided with side connection
Support（1-3）, each rotor motor（1-8）There is an Arcuate flexible protection board in outside（1-4）, the Arcuate flexible protection of both sides
Plate（1-4）End passes through connecting plate（1-5）It is connected, the side connecting bracket（1-3）Outside and connecting plate（1-5）It is connected, it is described
Triangle landing gear link（1-11）Have a pair, the triangle landing gear link（1-11）Upper end is sleeved on side connecting bracket
（1-3）On be fixed by fastener, the triangle landing gear link（1-11）The fulcrum of lower end two and corresponding landing gear
（1-10）It is connected, the video camera（1-15）Respectively there is an electric rotating machine both sides（1-16）, the electric rotating machine（1-16）Turn
Axle and video camera（1-15）Outside is connected, the electric rotating machine（1-16）Pass through fixed mount（1-17）It is fixed on unmanned plane main body
（1-1）Bottom, the video camera（1-15）The both sides of camera lens one infrared locator is respectively installed（1-18）.
2. the component installation unmanned plane according to claim 1 using BIM combination planar bar code technologies, it is characterised in that：
The connecting plate（1-5）Outside is provided with colliding sensor（1-6）.
3. the component installation unmanned plane according to claim 1 using BIM combination planar bar code technologies, it is characterised in that：
The side connecting bracket（1-3）Location-plate is installed below middle part（1-12）, the location-plate（1-12）Four angles lower section
Respectively there is a unmanned plane positioning inductor（1-13）, the location-plate（1-12）There is charging column below middle part（1-14）.
4. the cradle used for the unmanned plane described in claim 1-3 any one, including cradle main body（2-1）, the sun
Can cell panel（2-2）, band guide rail landing bar（2-3）, interior empty support bar（2-5）, reinforcing plate（2-6）, cradle positioning inductor
（2-7）, charging ring（2-8）, supporting plate（2-9）With pin type locating rack（2-10）, it is characterised in that：The cradle main body（2-
1）On have it is positive can cell panel（2-2）, band guide rail landing bar（2-3）With interior empty support bar（2-5）, the sun can cell panel（2-2）
It is laid on cradle main body（2-1）On, the band guide rail landing bar（2-3）For flexible-belt guide rail landing bar, the band guide rail drop
Fall bar（2-3）Have a pair and be fixed on cradle main body（2-1）On, unmanned plane（1）Landing gear after landing（1-10）It is stuck in band guide rail
Land bar（2-3）Guide rail in, the interior empty support bar（2-5）Inside there are connecting line, the interior empty support bar（2-5）Lower end is fixed
In cradle main body（2-1）On, the interior empty support bar（2-5）There is reinforcing plate side（2-6）, the interior empty support bar（2-5）
There is supporting plate upper end（2-9）, the supporting plate（2-9）Four angles above have cradle positioning inductor（2-7）, the branch
Fagging（2-9）There is charging ring above middle part（2-8）, the cradle main body（2-1）Two side bottoms, which are respectively provided with a pair of pin types, to be determined
Position frame（2-10）, the pin type locating rack（2-10）Pilot pin is arranged at bottom（2-10-1）.
5. cradle according to claim 4, it is characterised in that：The cradle main body（2-1）Front and rear side is provided with one
To handle（2-4）.
6. cradle according to claim 4, it is characterised in that：The pin type locating rack（2-10）For activity orientation frame,
The pin type locating rack（2-10）Pass through connects hinge（2-11）With cradle main body（2-1）Outside is connected, the cradle master
Body（2-1）There is magnetic sheet in outside（2-12）With pin type locating rack（2-10）It is corresponding, pin type locating rack（2-10）Absorption exists after lifting
Magnetic sheet（2-12）Outside.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720860249.9U CN207062653U (en) | 2017-07-17 | 2017-07-17 | Utilize the component installation unmanned plane and cradle of BIM combination planar bar code technologies |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720860249.9U CN207062653U (en) | 2017-07-17 | 2017-07-17 | Utilize the component installation unmanned plane and cradle of BIM combination planar bar code technologies |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108427061A (en) * | 2018-03-05 | 2018-08-21 | 国网湖南省电力有限公司 | A kind of transmission line forest fire distribution monitoring device and method based on unmanned plane |
| CN110095108A (en) * | 2019-05-23 | 2019-08-06 | 马鞍山市雷铭网络科技有限公司 | One kind being based on BIM unmanned plane plotting board and mapping method |
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Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108427061A (en) * | 2018-03-05 | 2018-08-21 | 国网湖南省电力有限公司 | A kind of transmission line forest fire distribution monitoring device and method based on unmanned plane |
| CN108427061B (en) * | 2018-03-05 | 2021-03-09 | 国网湖南省电力有限公司 | Unmanned aerial vehicle-based power transmission line forest fire distribution monitoring device and method |
| CN110095108A (en) * | 2019-05-23 | 2019-08-06 | 马鞍山市雷铭网络科技有限公司 | One kind being based on BIM unmanned plane plotting board and mapping method |
| CN110095108B (en) * | 2019-05-23 | 2021-02-12 | 马鞍山市雷铭网络科技有限公司 | Surveying and mapping device and method based on BIM unmanned aerial vehicle |
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