CN114644117A - High-flexibility multi-type disinfection aircraft - Google Patents
High-flexibility multi-type disinfection aircraft Download PDFInfo
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- CN114644117A CN114644117A CN202210312781.2A CN202210312781A CN114644117A CN 114644117 A CN114644117 A CN 114644117A CN 202210312781 A CN202210312781 A CN 202210312781A CN 114644117 A CN114644117 A CN 114644117A
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- 238000004659 sterilization and disinfection Methods 0.000 title claims abstract description 134
- 239000007921 spray Substances 0.000 claims abstract description 9
- 230000001360 synchronised effect Effects 0.000 claims description 50
- 238000004891 communication Methods 0.000 claims description 29
- 239000007788 liquid Substances 0.000 claims description 15
- 230000000007 visual effect Effects 0.000 claims description 14
- 239000012530 fluid Substances 0.000 claims description 13
- 238000005507 spraying Methods 0.000 claims description 7
- CBENFWSGALASAD-UHFFFAOYSA-N Ozone Chemical compound [O-][O+]=O CBENFWSGALASAD-UHFFFAOYSA-N 0.000 claims description 6
- 230000000149 penetrating effect Effects 0.000 claims description 3
- 230000000694 effects Effects 0.000 abstract description 7
- 108010066114 cabin-2 Proteins 0.000 description 9
- MHAJPDPJQMAIIY-UHFFFAOYSA-N Hydrogen peroxide Chemical compound OO MHAJPDPJQMAIIY-UHFFFAOYSA-N 0.000 description 8
- 241000700605 Viruses Species 0.000 description 2
- 238000013480 data collection Methods 0.000 description 2
- 230000000249 desinfective effect Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 241000894006 Bacteria Species 0.000 description 1
- 206010011409 Cross infection Diseases 0.000 description 1
- 241000195493 Cryptophyta Species 0.000 description 1
- 206010029803 Nosocomial infection Diseases 0.000 description 1
- 238000013473 artificial intelligence Methods 0.000 description 1
- 230000001174 ascending effect Effects 0.000 description 1
- 230000000712 assembly Effects 0.000 description 1
- 238000000429 assembly Methods 0.000 description 1
- 230000002146 bilateral effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000009977 dual effect Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000003203 everyday effect Effects 0.000 description 1
- 244000005700 microbiome Species 0.000 description 1
- 244000045947 parasite Species 0.000 description 1
- 244000052769 pathogen Species 0.000 description 1
- 230000001172 regenerating effect Effects 0.000 description 1
- 230000000630 rising effect Effects 0.000 description 1
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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
- B64D1/16—Dropping or releasing powdered, liquid, or gaseous matter, e.g. for fire-fighting
- B64D1/18—Dropping or releasing powdered, liquid, or gaseous matter, e.g. for fire-fighting by spraying, e.g. insecticides
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- A—HUMAN NECESSITIES
- A61—MEDICAL OR VETERINARY SCIENCE; HYGIENE
- A61L—METHODS OR APPARATUS FOR STERILISING MATERIALS OR OBJECTS IN GENERAL; DISINFECTION, STERILISATION OR DEODORISATION OF AIR; CHEMICAL ASPECTS OF BANDAGES, DRESSINGS, ABSORBENT PADS OR SURGICAL ARTICLES; MATERIALS FOR BANDAGES, DRESSINGS, ABSORBENT PADS OR SURGICAL ARTICLES
- A61L2/00—Methods or apparatus for disinfecting or sterilising materials or objects other than foodstuffs or contact lenses; Accessories therefor
- A61L2/02—Methods or apparatus for disinfecting or sterilising materials or objects other than foodstuffs or contact lenses; Accessories therefor using physical phenomena
- A61L2/08—Radiation
- A61L2/10—Ultraviolet radiation
-
- A—HUMAN NECESSITIES
- A61—MEDICAL OR VETERINARY SCIENCE; HYGIENE
- A61L—METHODS OR APPARATUS FOR STERILISING MATERIALS OR OBJECTS IN GENERAL; DISINFECTION, STERILISATION OR DEODORISATION OF AIR; CHEMICAL ASPECTS OF BANDAGES, DRESSINGS, ABSORBENT PADS OR SURGICAL ARTICLES; MATERIALS FOR BANDAGES, DRESSINGS, ABSORBENT PADS OR SURGICAL ARTICLES
- A61L2/00—Methods or apparatus for disinfecting or sterilising materials or objects other than foodstuffs or contact lenses; Accessories therefor
- A61L2/16—Methods or apparatus for disinfecting or sterilising materials or objects other than foodstuffs or contact lenses; Accessories therefor using chemical substances
- A61L2/18—Liquid substances or solutions comprising solids or dissolved gases
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/52—Tilting of rotor bodily relative to fuselage
-
- 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
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
-
- 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
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Health & Medical Sciences (AREA)
- Mechanical Engineering (AREA)
- Life Sciences & Earth Sciences (AREA)
- Public Health (AREA)
- Epidemiology (AREA)
- Animal Behavior & Ethology (AREA)
- General Health & Medical Sciences (AREA)
- Veterinary Medicine (AREA)
- General Chemical & Material Sciences (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Chemical & Material Sciences (AREA)
- Remote Sensing (AREA)
- Pest Control & Pesticides (AREA)
- Apparatus For Disinfection Or Sterilisation (AREA)
Abstract
The invention discloses a high-flexibility multi-type disinfection aircraft, which belongs to the technical field of disinfectors and comprises a rack, a cabin, a disinfection component, a rotor component, a tilting control component and a vision component, wherein the top of the rack is provided with the cabin, the outer side of the cabin is provided with the vision component, the vision component collects field images, the rotor component is arranged at the corners of the rack and drives the whole device to ascend by virtue of the rotor component, the tilting control component is arranged on the rack and enables the rack to tilt so that the device can pass through a narrow disinfection area, the disinfection component is arranged at the bottom of the rack, and the disinfection component sprays and disinfects while performing ultraviolet disinfection. The invention can control the flight angle of the aircraft to enable the aircraft to incline and disinfect narrow areas, and has various disinfection measures and better disinfection effect.
Description
Technical Field
The invention belongs to the technical field of disinfectors, and particularly relates to a high-flexibility multi-type disinfection aircraft.
Background
For a long time, the disinfection of the crowded areas is mostly completed manually, but for the areas which are easy to be infected by the personnel such as hospitals, the risk of contacting viruses is greatly increased when the workers disinfect. The disinfection is carried out every day, the disinfection efficiency and quality are not high by adopting a manual disinfection mode, and in addition, the risk of cross infection is greatly increased.
Along with the development of artificial intelligence technology, the disinfection robot has higher and higher use rate. However, most of the disinfection robots on the market at present are ground disinfection robots, and high areas cannot be disinfected. In addition, when the ground disinfection robot is used for disinfecting multilayer corridors, the ground disinfection robot cannot carry out step crossing and needs to be conveyed to other layers through an elevator, so that the disinfection efficiency is not high; if the elevator-free building needs to be equipped with one robot on each floor, the disinfection cost is greatly increased. Finally, the ground type disinfection robot has a small disinfection range, and is too time-consuming to complete large-area disinfection work.
Disclosure of Invention
The invention aims to provide a multi-type disinfection aircraft with high flexibility, and aims to solve the problems that most disinfection robots on the market at present are ground-based disinfection robots, a high-altitude area cannot be disinfected, the disinfection range is small, and too much time is consumed if large-area disinfection work is to be completed.
The utility model provides a polymorphic type disinfection aircraft of high flexibility ratio, includes frame, cabin, disinfection subassembly, rotor subassembly, verts control assembly and vision subassembly, the top of frame is equipped with the cabin just the outside in cabin is equipped with the vision subassembly, the scene image is gathered to the vision subassembly, the edge of frame all is equipped with the rotor subassembly just with the help the rotor subassembly drives whole device and rises, be equipped with in the frame and vert control assembly just it makes the frame take place to heel so that the device can pass narrow disinfection region to vert control assembly, the bottom of frame is equipped with the disinfection subassembly, the disinfection subassembly sprays ultraviolet disinfection when sterile.
Preferably, the frame includes mount, last dead lever and lower dead lever, the mount is annular structure just the preceding, back both ends of mount are U type structure, the top and the bottom of mount be fixedly connected with respectively go up dead lever and lower dead lever, fixedly connected with on the last dead lever the cabin, fixedly connected with on the dead lever down the disinfection subassembly, the U type end of mount passes connecting rod one and connecting rod two respectively perpendicularly, connecting rod one and connecting rod two all with the mount rotates to be connected, the bottom in cabin with all be equipped with between connecting rod one and the connecting rod two the control assembly that verts, the both ends of connecting rod one and connecting rod two are equipped with the rotor subassembly respectively.
Preferably, the tilting control assembly comprises an inertial sensor, a driving wheel, a synchronous belt wheel I, a synchronous belt wheel II, a synchronous belt I, a synchronous belt wheel II, a connecting shaft and a steering engine I, one side of the middle part of the fixed frame is fixedly connected with a first mounting plate, one side of the mounting plate is fixedly connected with a first steering engine, the first steering engine and the output shaft of the first steering engine are connected with a rotating shaft by means of a coupler, one end of the rotating shaft penetrates through the other side of the middle part of the fixing frame and is rotationally connected with the fixing frame, the penetrating end of the rotating shaft is fixedly connected with the inertial sensor, the rotating shaft is sleeved with the driving wheel, the first synchronous belt wheel and the second synchronous belt wheel are respectively and fixedly sleeved on the first connecting rod and the second connecting rod, the synchronous belt I and the synchronous belt II are connected with the driving wheel respectively.
Preferably, the rotor subassembly includes wing connecting portion, rotor motor and rotor blade, the equal fixedly connected with of tip of connecting rod one and connecting rod two wing connecting portion just the top fixedly connected with of wing connecting portion rotor motor, rotor motor's the output shaft fixedly connected with that makes progress rotor blade.
Preferably, disinfection subassembly is including spraying disinfection mechanism and ultraviolet lamp disinfection mechanism, it includes circular draw-in groove, fluid reservoir, liquid pipe, disinfection pipeline and atomizer to spray disinfection mechanism, parallel fixedly connected with mounting bracket one and mounting bracket two between connecting rod one and the connecting rod two, mounting bracket one and mounting bracket two are established respectively the both sides of mount, the bottom of mounting bracket one and mounting bracket two all is equipped with the link just the both sides of link are with the help of circular draw-in groove buckle has the fluid reservoir, the fluid reservoir with the liquid pipe intercommunication just the liquid pipe with disinfection pipeline intercommunication, disinfection pipeline's bottom has a plurality ofly along its even interval intercommunication of length direction atomizer.
Preferably, ultraviolet lamp disinfection mechanism includes mounting panel two, lamp stand and no ozone ultraviolet lamp, the bottom fixedly connected with of dead lever down mounting panel two, the bottom fixedly connected with of mounting panel two is a plurality of the lamp stand, every the lamp stand on fixedly connected with no ozone ultraviolet lamp.
Preferably, the vision assembly comprises a camera, a second steering engine fixing platform, a camera platform and a vision control main body, the outer side of the cabin is fixedly connected with the second steering engine fixing platform, the bottom of the second steering engine fixing platform is fixedly connected with the second steering engine, an output shaft of the second steering engine penetrates out of the second steering engine fixing platform and the end portion of the second steering engine fixing platform is fixedly connected with the camera platform, the top of the camera platform is fixedly connected with the camera, and the vision control main body electrically connected with the camera is arranged in the cabin.
Preferably, the inside of cabin is separated for power supply chamber, control chamber and communication chamber with the aid of the baffle, the power supply intracavity is equipped with power module, the control intracavity is equipped with the controller assembly, the communication intracavity is equipped with visual control main part and communication module assembly, the communication control assembly with controller assembly and external control terminal wireless connection, controller assembly control vert control assembly, rotor subassembly, disinfection subassembly and the visual subassembly.
The invention has the following advantages:
the controller assembly controls the starting and stopping of the tilting control assembly, the rotor wing assembly, the disinfection assembly and the vision assembly; the communication module assembly receives an external instruction and positions the disinfection aircraft; the visual component collects a real-time image and transmits the real-time image to the communication module assembly; the communication module assembly transmits real-time images of the aircraft, the motion state of the aircraft and the like to the terminal. The start-up of rotor subassembly, can drive the aircraft body and remove appointed disinfection position, the disinfection region is bigger, the start-up of control assembly verts, the motion of verting of aircraft is accomplished to steering wheel drive synchronous pulley one and synchronous pulley two, be equipped with inertial sensor simultaneously and reduce control algorithm complexity, promote aircraft motion accuracy, realize the disinfection work of disinfection aircraft in narrow region, the start-up of disinfection subassembly, can realize spraying disinfection and ultraviolet ray disinfection, dual disinfection, the disinfection effect is better. The invention has wider disinfection area and better disinfection effect.
Drawings
FIG. 1 is a schematic structural diagram of the present invention.
Fig. 2 is a bottom view of the structure shown in fig. 1.
FIG. 3 is a schematic structural view of a frame of the structure shown in FIG. 1;
FIG. 4 is a schematic illustration of the tilt control assembly of the configuration of FIG. 1;
FIG. 5 is a schematic view of a visual element of the structure shown in FIG. 1;
fig. 6 is a schematic view of the internal structure of the nacelle, which is the structure shown in fig. 1.
The symbols in the drawings are:
1. a frame; 10. a fixed mount; 11. an upper fixing rod; 12. a lower fixing rod; 13. a first connecting rod; 14. a second connecting rod;
2. a nacelle; 20. a power supply cavity; 21. a control chamber; 22. a communication cavity; 23. a power supply module; 24. a controller assembly; 25. a communication module assembly;
3. a tilt control assembly; 30. a first mounting plate; 31. a first steering engine; 32. a rotating shaft; 33. a driving wheel; 34. A synchronous belt wheel I; 35. a second synchronous belt wheel; 36. a first synchronous belt; 37. a second synchronous belt; 38. an inertial sensor;
4. a rotor assembly; 40. a rod wing connecting part; 41. a rotor motor; 42. a rotor blade;
5. a spray disinfection mechanism; 50. a first mounting frame; 51. a second mounting frame; 52. a connecting frame; 53. a circular slot; 54. a liquid tank; 55. a liquid pipe; 56. disinfecting the pipeline; 57. an atomizing spray head;
6. an ultraviolet lamp disinfection mechanism; 60. a second mounting plate; 61. a lamp socket; 62. an ozone-free ultraviolet lamp;
7. a visual component; 70. a vision control body; 71. a steering engine fixing platform; 72. a second steering engine; 73. a camera platform; 74. a camera is provided.
Detailed Description
The following detailed description of the embodiments of the present invention will be given in order to provide those skilled in the art with a more complete, accurate and thorough understanding of the inventive concept and technical solutions of the present invention.
As shown in fig. 1 to 6, the present invention provides a high-flexibility multi-type disinfection aircraft, which includes a rack 1, a cabin 2, a disinfection component, a rotor component 4, a tilt control component 3, and a vision component 7, wherein the cabin 2 is disposed on the top of the rack 1, the vision component 7 is disposed on the outer side of the cabin 2, the vision component 7 collects field images, the rotor component 4 is disposed at each corner of the rack 1, the whole device is driven to ascend by the aid of the rotor component 4, the tilt control component 3 is disposed on the rack 1, the rack 1 is tilted by the tilt control component 3 so that the device can pass through a narrow disinfection area, the disinfection component is disposed at the bottom of the rack 1, and the disinfection component performs ultraviolet disinfection while performing spray disinfection.
Frame 1 includes mount 10, last dead lever 11 and dead lever 12 down, mount 10 is annular structure just preceding, the back both ends of mount 10 are U type structure, mount 10's top and bottom respectively fixedly connected with go up dead lever 11 and dead lever 12 down, go up fixedly connected with on the dead lever 11 cabin 2, fixedly connected with on the dead lever 12 down the disinfection subassembly, the U type end of mount 10 passes connecting rod 13 and connecting rod two 14 respectively perpendicularly, connecting rod 13 and connecting rod two 14 all with mount 10 rotates and is connected, cabin 2's bottom with all be equipped with between connecting rod 13 and the connecting rod two 14 control assembly 3 verts, the both ends of connecting rod 13 and connecting rod two 14 are equipped with rotor subassembly 4 respectively.
The mount 10 is the infrastructure of whole aircraft, and disinfection subassembly, cabin 2, rotor subassembly 4 and the control assembly 3 that verts all fix on mount 10, realize the motion operation of whole aircraft. Rotor subassembly 4 establishes at the tip of connecting rod one 13 and connecting rod two 14, makes the aircraft can the four rotor crafts of appearance as the main part, and the flight is more stable.
The tilting control component 3 comprises an inertial sensor 38, a driving wheel 33, a first synchronous pulley 34, a second synchronous pulley 35, a first synchronous belt 36, a second synchronous belt 37, a rotating shaft 32 and a first steering engine 31, one side of the middle part of the fixing frame 10 is fixedly connected with a first mounting plate 30, one side of the first mounting plate 30 is fixedly connected with a first steering engine 31, an output shaft of the first steering engine 31 is connected with a rotating shaft 32 through a coupler, one end of the rotating shaft 32 penetrates through the other side of the middle part of the fixed frame 10 and is rotatably connected with the fixed frame 10, the inertia sensor 38 is fixedly connected to the penetrating end of the rotating shaft 32, the driving wheel 33 is sleeved on the rotating shaft 32, the first synchronous belt wheel 34 and the second synchronous belt wheel 35 are respectively fixedly sleeved on the first connecting rod 13 and the second connecting rod 14, the synchronous belt I36 and the synchronous belt II 37 are respectively connected between the synchronous pulley I34 and the synchronous pulley II 35 and the driving wheel 33.
The steering engine 31 rotates, the rotating shaft 32 is driven to rotate by the aid of the coupler, the rotating shaft 32 is further used for driving the driving wheel 33 to rotate, the driving wheel 33, the connecting rod one 13 and the connecting rod two 14 are driven to rotate by the aid of the synchronous belt wheel one 34, the synchronous belt wheel two 35, the synchronous belt one 36 and the synchronous belt two 37, the driving wheel 33 rotates by the aid of the synchronous belt wheel one 34, the synchronous belt wheel two 35, the synchronous belt one 36 and the synchronous belt two 37, the connecting rod one 13 and the connecting rod two 14 rotate and further rotate relative to the rack 1, the rotor wing assemblies 4 at the end portions of the connecting rod one 13 and the connecting rod two 14 are inclined, the direction of lift force is changed, the whole aircraft can be inclined, the aircraft can pass through a narrow disinfection area, the disinfection effect is better, the inertial sensor 38 at the end portion of the rotating shaft 32 is used for measuring the inclined rotating angle of the aircraft, and the inertial sensor 38 is used for acquiring speed and angular speed information to reduce the complexity of a control algorithm, the motion precision of the aircraft is improved.
Rotor subassembly 4 includes wing connecting portion 40, rotor motor 41 and rotor blade 42, the equal fixedly connected with of tip of two 14 of connecting rod 13 wing connecting portion 40 just the top fixedly connected with of wing connecting portion 40 rotor motor 41, rotor motor 41's the ascending fixedly connected with of output shaft rotor blade 42.
Rotor motor 41 drives rotor blade 42 and rotates, and then the air downward flow makes whole device produce lift, drives whole aircraft whole rising, moves to appointed disinfection place to can disinfect to the region of eminence, the disinfection scope is wider.
The disinfection subassembly is including spraying disinfection mechanism 5 and ultraviolet lamp disinfection mechanism 6, it includes circular draw-in groove 53, fluid reservoir 54, liquid pipe 55, disinfection pipeline 56 and atomizer 57 to spray disinfection mechanism 5, parallel fixedly connected with mounting bracket 50 and mounting bracket two 51 between connecting rod 13 and the connecting rod two 14, mounting bracket 50 and mounting bracket two 51 are established respectively the both sides of mount 10, the bottom of mounting bracket 50 and mounting bracket two 51 all is equipped with link 52 just the both sides of link 52 have with the help of circular draw-in groove 53 buckle the fluid reservoir 54, the fluid reservoir 54 with the fluid pipe 55 intercommunication just the fluid pipe 55 with disinfection pipeline 56 communicates, the bottom of disinfection pipeline 56 has a plurality ofly along its even interval intercommunication of length direction atomizer 57.
Can save hydrogen peroxide liquid in the fluid reservoir 54, through in liquid pipe 55 pumps the hydrogen peroxide liquid to disinfection pipeline 56, make it convert dry fog to spray to in the air through atomizer 57, realize spraying the disinfection, the both sides of frame 1 all are equipped with disinfection pipeline 56 with the help of mounting bracket one 50 and mounting bracket two 51 and link 52, realize two side disinfection, and disinfection efficiency is higher.
Ultraviolet lamp disinfection mechanism 6 includes two mounting panels 60, lamp stand 61 and no ozone ultraviolet lamp 62, the bottom fixedly connected with of dead lever 12 down two mounting panels 60, the bottom fixedly connected with of two mounting panels 60 is a plurality of lamp stand 61, every lamp stand 61 on fixedly connected with no ozone ultraviolet lamp 62.
The ozone-free ultraviolet lamp 62 is harmless to human bodies, can be used for disinfection in a human environment, and can destroy the molecular structure of DNA or RNA in cells of a microorganism organism by using ultraviolet rays with proper wavelength to cause death of growing cells or death of regenerative cells, so that the effects of sterilization and disinfection are achieved. Various bacteria, viruses, parasites, algae and other pathogens in the air are directly killed.
The vision assembly 7 comprises a camera 74, a second steering engine 72, a fixed steering engine platform 71, a second camera platform 73 and a vision control main body 70, the outer side of the cabin 2 is fixedly connected with the fixed steering engine platform 71, the bottom of the fixed steering engine platform 71 is fixedly connected with the second steering engine 72, an output shaft of the second steering engine 72 penetrates out of the fixed steering engine platform 71 and the end part of the fixed steering engine platform 71 is fixedly connected with the camera platform 73, the top of the camera platform 73 is fixedly connected with the camera 74, and the vision control main body 70 is electrically connected with the camera 74 and arranged in the cabin 2.
The output shaft of the second steering engine 72 upwards penetrates out of the steering engine fixing platform 71 and the end part of the second steering engine 72 is fixedly connected with the camera platform 73, the camera platform 73 and the second steering engine 72 rotate together to complete 74360-degree rotation of a camera, omnibearing data collection is achieved, a disinfection area can be observed manually, if an unsterilized area exists, the aircraft is driven to move to the area, the aircraft is disinfected, and the disinfection is more comprehensive.
The inside of cabin 2 is separated for power supply chamber 20, control chamber 21 and communication chamber 22 with the help of the baffle, be equipped with power module 23 in the power supply chamber 20, be equipped with controller assembly 24 in the control chamber 21, be equipped with in the communication chamber 22 visual control main part 70 and communication module assembly 25, communication module assembly 25 with controller assembly 24 and external control terminal wireless connection, controller assembly 24 control tilting control component 3, rotor subassembly 4, disinfection subassembly and visual subassembly 7.
The whole cabin is divided into three areas, a power module 23 is arranged in a power cavity 20, a controller assembly 24 is arranged in a control cavity 21, the vision control main body 70 and a communication module assembly 25 are arranged in a communication cavity 22, and the power module 23 provides power for the whole aircraft; the controller assembly 24 controls the rotor motor 41, the first steering engine 31, the second steering engine 72 and the disinfection component to start and stop; the communication module assembly 25 receives an external instruction and positions the disinfection aircraft; the visual component 7 collects real-time images and transmits the real-time images to the communication module assembly 25; the communication module assembly 25 transmits the real-time images of the aircraft, the motion state of the aircraft and the like to the terminal.
The working principle is as follows: the power module 23 provides power for the entire aircraft; the controller assembly 24 controls the rotor motor 41, the first steering engine 31, the second steering engine 72 and the disinfection assembly to start and stop; the communication module assembly 25 receives an external instruction and positions the disinfection aircraft; the visual component 7 collects real-time images and transmits the real-time images to the communication module assembly 25; the communication module assembly 25 transmits the real-time image of the aircraft, the motion state of the aircraft and the like to a terminal, the rotor motor 41 drives the rotor blades 42 to rotate, and further the air flows downwards, so that the whole device generates lift force to drive the whole aircraft to ascend integrally and move to a specified disinfection place, and the high area can be disinfected, the disinfection range is wider, the steering engine I31 rotates, the rotating shaft 32 is driven to rotate by the aid of the coupler, and further the driving wheel 33 is driven to rotate by the rotating shaft 32, the driving wheel 33, the connecting rod I13 and the connecting rod II 14, the synchronous belt wheels I34 and the synchronous belt II 35, the synchronous belts I36 and the synchronous belt II 37 are used between the driving wheel 33 and the connecting rod I13 and the connecting rod II 14, so that the connecting rod I13 and the connecting rod II 14 can rotate by the aid of the synchronous belt wheels I34 and the synchronous belt II 35, and the synchronous belts I36 and the synchronous belt II 37, and further rotate relative to the rack 1, the rotor wing assembly 4 at the end parts of the first connecting rod 13 and the second connecting rod 14 is inclined, the lifting direction is changed, the whole aircraft can tilt, the aircraft can pass through a narrow disinfection area, the disinfection effect is better, the inertial sensor 38 at the end part of the rotating shaft 32 measures the tilting angle of the aircraft, the inertial sensor 38 is used for acquiring speed and angular speed information to reduce the complexity of a control algorithm and improve the motion precision of the aircraft, hydrogen peroxide liquid can be stored in the liquid tank 54, the hydrogen peroxide liquid is pumped into the disinfection pipeline 56 through the liquid pipe 55 and is converted into dry fog through the atomizing nozzle 57 to be sprayed into the air, the spraying disinfection is realized, the disinfection pipelines 56 are arranged on the two sides of the rack 1 by virtue of the first mounting rack 50, the second mounting rack 51 and the connecting rack 52, the bilateral disinfection is realized, the disinfection efficiency is higher, the ozone-free ultraviolet lamp 62 is harmless to the human body, and the disinfection can be carried out under the manned environment, double disinfection, the disinfection effect is better, and the output shaft of two steering wheel 72 upwards wears out steering wheel fixed platform 71 and its tip fixedly connected with camera platform 73, camera platform 73 and two 72 co-rotations of steering wheel accomplish the rotation of camera 74360, realize omnidirectional data collection, can the artificial observation disinfection region, if there is not sterile region, the drive aircraft removes this region in, disinfects it, and the disinfection is more comprehensive.
The invention is described above with reference to the accompanying drawings, it is obvious that the specific implementation of the invention is not limited by the above-mentioned manner, and it is within the scope of the invention to adopt various insubstantial modifications of the inventive concept and solution of the invention, or to apply the inventive concept and solution directly to other applications without modification.
Claims (8)
1. A high-flexibility multi-type disinfection aircraft is characterized in that: including frame (1), cabin (2), disinfection subassembly, rotor subassembly (4), control assembly (3) and vision subassembly (7) vert, the top of frame (1) is equipped with cabin (2) just the outside in cabin (2) is equipped with vision subassembly (7), the scene image is gathered in vision subassembly (7), the edge of frame (1) all is equipped with rotor subassembly (4) and with the help rotor subassembly (4) drive whole device and rise, be equipped with on frame (1) and vert control assembly (3) just it makes frame (1) take place to heel so that the device can pass narrow disinfection region to vert control assembly (3), the bottom of frame (1) is equipped with the disinfection subassembly, the disinfection subassembly carries out ultraviolet ray disinfection when spraying the disinfection.
2. The high-flexibility, multi-type disinfection aircraft of claim 1, wherein: the machine frame (1) comprises a fixing frame (10), an upper fixing rod (11) and a lower fixing rod (12), the fixing frame (10) is of an annular structure, the front end and the rear end of the fixing frame (10) are of a U-shaped structure, the top and the bottom of the fixing frame (10) are respectively fixedly connected with the upper fixing rod (11) and the lower fixing rod (12), the upper fixing rod (11) is fixedly connected with the engine room (2), the lower fixing rod (12) is fixedly connected with the disinfection component, the U-shaped end of the fixing frame (10) respectively vertically penetrates through a first connecting rod (13) and a second connecting rod (14), the first connecting rod (13) and the second connecting rod (14) are both rotatably connected with the fixing frame (10), and the tilting control component (3) is arranged between the bottom of the engine room (2) and the first connecting rod (13) and the second connecting rod (14), and two ends of the first connecting rod (13) and the second connecting rod (14) are respectively provided with a rotor wing assembly.
3. The high-flexibility multi-type disinfection aircraft of claim 2, wherein: the tilting control assembly (3) comprises an inertial sensor (38), a driving wheel (33), a synchronous pulley I (34), a synchronous pulley II (35), a synchronous belt I (36), a synchronous belt II (37), a rotating shaft (32) and a steering engine I (31), one side of the middle part of the fixing frame (10) is fixedly connected with a mounting plate I (30), one side of the mounting plate I (30) is fixedly connected with the steering engine I (31), an output shaft of the steering engine I (31) is connected with the rotating shaft (32) through a coupler, one end of the rotating shaft (32) penetrates through the other side of the middle part of the fixing frame (10) and is rotatably connected with the fixing frame (10), the penetrating end of the rotating shaft (32) is fixedly connected with the inertial sensor (38), the driving wheel (33) is sleeved on the rotating shaft (32), the synchronous pulley I (34) and the synchronous pulley II (35) are fixedly sleeved on the connecting rod I (13) and the connecting rod II (14) respectively, the synchronous belt I (36) and the synchronous belt II (37) are respectively connected between the synchronous belt I (34) and the synchronous belt II (35) and the driving wheel (33).
4. A high-flexibility multi-type disinfection aircraft according to claim 3, wherein: rotor subassembly (4) are including pole wing connecting portion (40), rotor motor (41) and rotor blade (42), the equal fixedly connected with of tip of connecting rod (13) and connecting rod two (14) pole wing connecting portion (40) just the top fixedly connected with of pole wing connecting portion (40) rotor motor (41), the output shaft of rotor motor (41) fixedly connected with that makes progress rotor blade (42).
5. The high-flexibility multi-type disinfection aircraft of claim 4, wherein: disinfection subassembly is including spraying disinfection mechanism (5) and ultraviolet lamp disinfection mechanism (6), it includes circular draw-in groove (53), fluid reservoir (54), liquid pipe (55), disinfection pipeline (56) and atomizer (57) to spray disinfection mechanism (5), parallel fixedly connected with mounting bracket (50) and mounting bracket two (51) between connecting rod (13) and connecting rod two (14), mounting bracket one (50) and mounting bracket two (51) are established respectively in the both sides of mount (10), the bottom of mounting bracket one (50) and mounting bracket two (51) all is equipped with link (52) just the both sides of link (52) are with the aid of circular draw-in groove (53) buckle has fluid reservoir (54), fluid reservoir (54) with liquid pipe (55) intercommunication just fluid reservoir (55) with disinfection pipeline (56) intercommunication, the bottom of disinfection pipeline (56) is followed its length direction even interval intercommunication and is had a plurality ofly atomizer(s) (5), (54) and atomizer (56) 57).
6. The high-flexibility, multi-type disinfection aircraft of claim 5, wherein: ultraviolet lamp disinfection mechanism (6) are including two (60) of mounting panel, lamp stand (61) and no ozone ultraviolet lamp (62), the bottom fixedly connected with of dead lever (12) down two (60) of mounting panel, the bottom fixedly connected with of two (60) of mounting panel is a plurality of lamp stand (61), every lamp stand (61) on fixedly connected with no ozone ultraviolet lamp (62).
7. A high-flexibility multi-type disinfection aircraft according to claim 2, wherein: the vision assembly (7) comprises a camera (74), a second steering engine (72), a fixed steering engine platform (71), a camera platform (73) and a vision control main body (70), the outer side of the cabin (2) is fixedly connected with the fixed steering engine platform (71), the bottom of the fixed steering engine platform (71) is fixedly connected with the second steering engine (72), an output shaft of the second steering engine (72) penetrates out of the fixed steering engine platform (71) and the end of the fixed steering engine platform (73), the top of the camera platform (73) is fixedly connected with the camera (74), and the vision control main body (70) is arranged in the cabin (2) and electrically connected with the camera (74).
8. The high-flexibility, multi-type disinfection aircraft of claim 7, wherein: the utility model discloses a visual control cabin, including cabin (2), cabin, communication chamber (22), power module (23), controller assembly (24), communication module assembly (24), controller assembly (24), visual control main part (70) and communication module assembly (25), communication module assembly (25) with controller assembly (24) and external control terminal wireless connection, controller assembly (24) control vert control assembly (3), rotor subassembly (4), disinfection subassembly and visual subassembly (7), the inside of cabin (2) is separated for power supply chamber (20), control chamber (21) and communication chamber (22) with the help of the baffle, be equipped with in power supply chamber (20), be equipped with controller assembly (24) in control chamber (21), be equipped with in communication chamber (22) visual control main part (70) and communication module assembly (25), communication module assembly (25) with controller assembly (24) and external control terminal wireless connection, controller assembly (24) control vert control assembly (3), rotor subassembly and visual subassembly (7).
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| CN202210312781.2A CN114644117A (en) | 2022-03-28 | 2022-03-28 | High-flexibility multi-type disinfection aircraft |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| CN118106259A (en) * | 2024-04-26 | 2024-05-31 | 智真海洋科技(威海)有限公司 | Underwater intelligent cleaning robot and system |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN118106259A (en) * | 2024-04-26 | 2024-05-31 | 智真海洋科技(威海)有限公司 | Underwater intelligent cleaning robot and system |
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