CN108520643A - A kind of smart utility aviation automation control system - Google Patents

A kind of smart utility aviation automation control system Download PDF

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Publication number
CN108520643A
CN108520643A CN201810416273.2A CN201810416273A CN108520643A CN 108520643 A CN108520643 A CN 108520643A CN 201810416273 A CN201810416273 A CN 201810416273A CN 108520643 A CN108520643 A CN 108520643A
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CN
China
Prior art keywords
containing cavities
cavity
guide
face
motor
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Granted
Application number
CN201810416273.2A
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Chinese (zh)
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CN108520643B (en
Inventor
戎佰腾
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Beijing Huajia Safety Protection Technology Co ltd
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Individual
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Priority to CN201810416273.2A priority Critical patent/CN108520643B/en
Publication of CN108520643A publication Critical patent/CN108520643A/en
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    • GPHYSICS
    • G08SIGNALLING
    • G08GTRAFFIC CONTROL SYSTEMS
    • G08G5/00Traffic control systems for aircraft, e.g. air-traffic control [ATC]
    • G08G5/0017Arrangements for implementing traffic-related aircraft activities, e.g. arrangements for generating, displaying, acquiring or managing traffic information
    • G08G5/0026Arrangements for implementing traffic-related aircraft activities, e.g. arrangements for generating, displaying, acquiring or managing traffic information located on the ground
    • HELECTRICITY
    • H05ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05KPRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
    • H05K5/00Casings, cabinets or drawers for electric apparatus
    • H05K5/0017Casings, cabinets or drawers for electric apparatus with operator interface units
    • HELECTRICITY
    • H05ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05KPRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
    • H05K5/00Casings, cabinets or drawers for electric apparatus
    • H05K5/02Details
    • H05K5/0217Mechanical details of casings

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  • Engineering & Computer Science (AREA)
  • Microelectronics & Electronic Packaging (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Power-Operated Mechanisms For Wings (AREA)

Abstract

The invention discloses a kind of smart utility aviations to automate control system, including fuselage and the cylinder containing cavities upward in the fuselage inner opening are set, it is communicated equipped with annular groove in the cylinder storage cavity wall, perforation is equipped with guide groove symmetrical and at the top of the annular groove in the cylinder containing cavities or so inner wall, cylinder containing cavities bottom is equipped with the first cavity, annulus block is slidably connected in the annular groove, cylindrical cavity is equipped in the annulus block up and down, the annulus block screw-internal thread fit is connected with elevating screw thread bar that is symmetrical and extending up and down, elevating screw thread bar bottom extending end puts in first cavity and is equipped with first pulley in end face;The configuration of the present invention is simple, easy to operate, service life is long, and price is excellent, and practical performance is higher.

Description

A kind of smart utility aviation automation control system
Technical field
The present invention relates to aviation informationization technology field, specifically a kind of smart utility aviation automates control system.
Background technology
With the development of science and technology, social progress, country promotes always high-tech development, is led in aviation informationization technology In domain, a relatively difficult technical problem is always existed, general civil aviation control system is caused due to the limitation of fund technology Air traffic blocks, and generates greatly danger, and the radar display screen in general control system is integrally fixed at workbench On, mobile and storage is inconvenient, while operator's observation visual angle is not easy to adjust, and not only influences operator, but also it is serious when may Cause information to observe loophole, causes irremediable as a result, this device efficiently solves the problems, such as this.
Invention content
Technical problem to be solved by the invention is to provide a kind of smart utility aviations to automate control system, can solve The problems in certainly above-mentioned present technology.
The present invention is achieved through the following technical solutions:A kind of smart utility aviation automation control system of the present invention System, including fuselage and the cylinder containing cavities upward in the fuselage inner opening are set, it is communicated in the cylinder storage cavity wall It is penetrated through equipped with annular groove, in described cylinder containing cavities or so inner wall and is equipped with symmetrical and is located at the top of the annular groove Guide groove, cylinder containing cavities bottom is equipped with the first cavity, annulus block is slidably connected in the annular groove, described Cylindrical cavity is equipped in annulus block up and down, the annulus block screw-internal thread fit is connected with lifting that is symmetrical and extending up and down Threaded rod, elevating screw thread bar bottom extending end puts in first cavity and is equipped with first pulley in end face, described Extending end puts in the guide groove and is equipped with the first tooth runner in end at the top of elevating screw thread bar, is rotated in the cylindrical cavity It is connected with disk, the containing cavities of opening upwards are equipped in disk inner top end face, the containing cavities bottom, which communicates, to be set There are the first guide runner, the first guide runner right end to be equipped with the second cavity of opening to the right, set in the containing cavities bottom interior wall There are supporting rack, the containing cavities to be equipped with the pedestal positioned at support frame as described above right end, radar is hingedly connected on support frame as described above Elecscreen support plate, the radar elecscreen support plate top end surface are equipped with radar elecscreen, are set in the radar elecscreen support plate bottom end face There is the second guide runner that Open Side Down, the first slider guide, first slide guide are slidably connected in second guide runner It is hingedly connected with head rod between block and the pedestal, the second slide guide is slidably connected in first guide runner Block, the second slider guide screw-internal thread fit are connected with the adjusting threaded rod that left and right extends, and the adjusting threaded rod left end extends End is rotatably assorted with the first guide runner left end inner wall and connect, and the adjusting threaded rod right end extending end puts in described It is equipped with first bevel gear in two cavitys and in end, is hingedly connected with the second connecting rod at the top of second slider guide, described the The two connecting rod other ends are articulated and connected in the middle part of the head rod, and being rotatably assorted in second cavity, it is downward to be connected with The first rotation axis stretched, first rotation axis be equipped with to the first bevel gear and the ratcheting company of cylinder cavity wall The tooth cone dual-purpose wheel connect, cylinder containing cavities bottom is equipped with the activity-driven device to be connect with the disk power, institute It states fuselage right end end face and is equipped with electrical dust collector device.
Preferably technical solution, the activity-driven device include being arranged in the cylinder containing cavities positioned at described The movable block of disk bottom, is equipped with the first motor in the movable block top end surface, the first motor top end with Disk bottom end face be connected by power, the movable block bottom four corners are equipped with the slide guide bar extended up and down, and the slide guide bar is stretched It is slidably connected in into the cylinder containing cavities bottom interior wall body and therewith.
Preferably technical solution is embedded with the second motor, second electricity in the first cavity bottom inner wall Motivation top end be connected by power has the second belt wheel, and be connected by power has belt between the first pulley and second belt wheel.
Preferably technical solution is slidably connected with the protection door-plate that left and right extends in the guide groove, described It is equipped with that Open Side Down in protection door board bottom end surface and to the dynamic trough with the ratcheting connection of the first tooth runner.
Preferably technical solution, the electrical dust collector device include the electric precipitation being arranged on fuselage right end end face Body, the electric precipitation body is interior to be equipped with the slippage slot of opening to the right, is slidably connected with slipping block in the slippage slot, institute It states slipping block right end end face and is equipped with electric precipitator, the sliding is equipped with the adjusting threaded rod that left and right extends, the adjusting soon Threaded rod left end end be connected by power has third motor, third motor outer surface to be embedded in the slippage slot left end In wall and connection fixed thereto.
The beneficial effects of the invention are as follows:In the initial state due to equipment of the invention, the annulus block is located at the ring Shape sliding slot bottommost, at this point, the movable block bottom end face is abutted with the cylinder containing cavities bottom interior wall, two protections The opposite end face of door-plate abuts, and the protection door-plate completely encloses the cylinder containing cavities, and the radar elecscreen support plate is complete In the containing cavities and it is in horizontality, first slider guide is located at the second guide runner right end, and described the Two slider guides are located at the first guide runner right end, consequently facilitating device care and maintenance.
When carrying out air traffic control monitoring using the equipment of the present invention, first step starter is carried out first, described in startup Second motor drives the second belt wheel rotation, second belt wheel to pass through described in the belt and first pulley drive Elevating screw thread bar rotates, and the elevating screw thread bar drives the annulus block and the disk integrally to move up, and simultaneously described in drive First tooth runner rotates, and protection door-plate described in the first tooth driven by rotating wheel is away from each other movement, and the movable block is by the circle The pulling force of disk moves up, but since the effect of the slide guide bar makes first motor that can keep the power with the disk Connection, when the annulus block is moved to the annular groove top, two protection door-plate maximum distances are separate, described Cylinder containing cavities are opened completely, at this point, the radar elecscreen is fully exposed to extraneous member's observation easy to operation, at this point, control Second motor shuts down, to improve device convenience.
When carrying out second step observation position adjusting, starts first motor and drive the disk rotational, meanwhile, by In the ratcheting of the tooth cone dual-purpose wheel and the cylindrical cavity, make the tooth cone dual-purpose wheel rotation and drive the first bevel gear turn It is dynamic, make the rotation for adjusting threaded rod and second slider guide is driven to move to left, second slider guide passes through described second Connecting rod and the head rod make the radar elecscreen support plate rotate counterclockwise, until being adjusted to suitable operator's observation Position, to improve device working effect.
When completing need of work storage, controls first motor and the disk is driven to rotate backward, simultaneously as The tooth cone dual-purpose wheel is ratcheting with the cylindrical cavity, and the tooth cone dual-purpose wheel is made to rotate backward and drive the first bevel gear It rotates backward, makes rotating backward and second slider guide being driven to move to right recovery initial position for the adjusting threaded rod, it is described Second slider guide makes the radar elecscreen support plate rotate clockwise recovery by second connecting rod and the head rod Then initial position controls first motor and shuts down, start second motor later and drive second band Wheel rotates backward, and second belt wheel drives the elevating screw thread bar to rotate backward by the belt and the first pulley, The elevating screw thread bar drives the annulus block and the disk integrally to move down, and the first tooth runner is driven reversely to turn simultaneously It is dynamic, protect door-plate to move towards described in the first tooth driven by rotating wheel, the movable block is by the pressure of the disk to moving down Dynamic, when the annulus block is moved to the annular groove bottommost, two protection door-plates abut, the cylinder containing cavities It is fully blocked, controls second motor and shut down, to improve the practical performance of device.
The configuration of the present invention is simple, easy to operate, by using accommodating mechanism and protection mechanism in one, equipment is light and handy, behaviour To make simply, all parts cooperation is close but is independent of each other, while being internally provided with movable driving mechanism in accommodating mechanism again, Operating position is automatically adjusted by movable driving mechanism, service life is long, and price is excellent, and practical performance is higher.
Description of the drawings
The present invention is described in detail by following specific embodiment and attached drawing for ease of explanation,.
Fig. 1 is that overall structure when a kind of smart utility aviation of the present invention automates control system original state is illustrated Figure;
Fig. 2 is that a kind of smart utility aviation of the present invention automates overall structure diagram when control system works.
Specific implementation mode
As depicted in figs. 1 and 2, a kind of smart utility aviation of the invention automates control system, including fuselage 100 and The cylinder containing cavities 118 upward in 100 inner opening of the fuselage are set, are communicated equipped with ring in 118 inner wall of cylinder containing cavities Shape sliding slot 101, the interior perforation of 118 or so inner wall of the cylinder containing cavities are equipped with symmetrical and are pushed up positioned at the annular groove 101 The guide groove 121 in portion, 118 bottom of cylinder containing cavities are equipped with the first cavity 109, are slidably matched in the annular groove 101 It is connected with annulus block 104, cylindrical cavity 105,104 screw-internal thread fit of annulus block are equipped with up and down in the annulus block 104 It is connected with elevating screw thread bar 102 that is symmetrical and extending up and down, 102 bottom extending end of the elevating screw thread bar puts in described It is equipped with first pulley 108 in first cavity 109 and in end face, 102 top extending end of the elevating screw thread bar puts in described lead It is equipped with the first tooth runner 120 into slot 121 and in end, is rotatably assorted in the cylindrical cavity 105 and is connected with disk 134, it is described The containing cavities 123 of opening upwards are equipped in 134 inner top end face of disk, 123 bottom of the containing cavities is communicated equipped with the first slide guide Slot 130,130 right end of the first guide runner are equipped with opening the second cavity 116 to the right, in 123 bottom interior wall of the containing cavities Equipped with supporting rack 135, the containing cavities 123 are equipped with the pedestal 125 positioned at 135 right end of support frame as described above, support frame as described above 135 On be hingedly connected with radar elecscreen support plate 126,126 top end surface of radar elecscreen support plate is equipped with radar elecscreen 124, described It is equipped with the second guide runner 127 that Open Side Down in 126 bottom end face of radar elecscreen support plate, is slided in second guide runner 127 It is connected with the first slider guide 133, the first connection is hingedly connected between first slider guide 133 and the pedestal 125 Bar 128 is slidably connected with the second slider guide 132,132 internal thread of the second slider guide in first guide runner 130 It is connected with the adjusting threaded rod 131 that left and right extends, the 131 left end extending end of adjusting threaded rod and first slide guide 130 left end inner wall of slot is rotatably assorted connection, and the 131 right end extending end of adjusting threaded rod is put in second cavity 116 And it is equipped with first bevel gear 114 in end, and the top of second slider guide 132 is hingedly connected with the second connecting rod 129, and described the Two connecting rods, 129 other end is articulated and connected with 128 middle part of the head rod, the company of being rotatably assorted in second cavity 116 Be connected to the first rotation axis 115 extended up and down, first rotation axis 115 be equipped with to the first bevel gear 114 and The tooth of the ratcheting connection of 105 inner wall of the cylindrical cavity bores dual-purpose wheel 117,118 bottom of cylinder containing cavities be equipped with to it is described The activity-driven device of 134 be connected by power of disk, 100 right end end face of the fuselage are equipped with electrical dust collector device.
Valuably, the activity-driven device includes that setting is located at 134 bottom of the disk in the cylinder containing cavities 118 The movable block 106 in portion, 106 top end surface of the movable block is interior to be equipped with the first motor 113, first motor, 113 top End and 134 bottom end face be connected by power of the disk, 106 bottom four corners of the movable block are equipped with the slide guide bar extended up and down 107, the slide guide bar 107 puts in 118 bottom interior wall body of the cylinder containing cavities and is slidably connected therewith.
Valuably, the second motor 111, second motor 111 are embedded in 109 bottom interior wall of the first cavity Top end be connected by power has the second belt wheel 112, there is be connected by power between the first pulley 108 and second belt wheel 112 Belt 110.
Valuably, the protection door-plate 122 that left and right extends, the protection door are slidably connected in the guide groove 121 It is equipped with that Open Side Down in 122 bottom end face of plate and to the dynamic trough 119 with the 120 ratcheting connection of the first tooth runner.
Valuably, the electrical dust collector device includes the electric precipitation body 200 being arranged on 100 right end end face of the fuselage, It is equipped with the slippage slot 201 of opening to the right in the electric precipitation body 200, sliding is slidably connected in the slippage slot 201 Block 203,203 right end end face of the slipping block are equipped with electric precipitator 202, and the sliding fast 203 is equipped with the tune that left and right extends Threaded rod 204 is saved, 204 left end end be connected by power of the adjusting threaded rod has third motor 205, the third motor 205 outer surfaces are embedded in 201 left end inner wall of the slippage slot and connection fixed thereto.
In the initial state, the annulus block 104 is located at 101 bottommost of the annular groove to the equipment of the present invention, at this point, 106 bottom end face of the movable block is abutted with 118 bottom interior wall of cylinder containing cavities, and two protection door-plates 122 are opposite End face abut, the protection door-plate 122 completely encloses the cylinder containing cavities 118, and the radar elecscreen support plate 126 is completely In the containing cavities 123 and it is in horizontality, it is most right that first slider guide 133 is located at second guide runner 127 End, second slider guide 132 are located at 130 right end of the first guide runner.
When carrying out air traffic control monitoring using the equipment of the present invention, first step starter is carried out first, described in startup Second motor 111 drives second belt wheel 112 to rotate, and second belt wheel 112 passes through the belt 110 and described first Belt wheel 108 drives the elevating screw thread bar 102 to rotate, and the elevating screw thread bar 102 drives the annulus block 104 and the disk 134 entirety move up, and the first tooth runner 120 is driven to rotate simultaneously, and the first tooth runner 120 drives the protection door-plate 122 are away from each other movement, and the movable block 106 is moved up by the pulling force of the disk 134, but due to the slide guide bar 107 Effect make first motor 113 that can keep the be connected by power with the disk 134, when the annulus block 104 is moved to When 101 top of annular groove, two 122 maximum distances of the protection door-plate are separate, and the cylinder containing cavities 118 are complete It is opened, at this point, the radar elecscreen 124 is fully exposed to extraneous member's observation easy to operation, at this point, control described second is electronic Machine 111 shuts down.
When carrying out second step observation position adjusting, starts first motor 113 and the disk 134 is driven to rotate, Simultaneously as tooth cone dual-purpose wheel 117 and the cylindrical cavity 105 is ratcheting, make tooth cone dual-purpose wheel 117 rotation and drive The first bevel gear 114 rotates, and makes the rotation for adjusting threaded rod 131 and second slider guide 132 is driven to move to left, institute State the second slider guide 132 makes the radar elecscreen support plate 126 by second connecting rod 129 and the head rod 128 It rotates counterclockwise, until being adjusted to the position of suitable operator's observation.
When completing need of work storage, controls first motor 113 and the disk 134 is driven to rotate backward, together When, it is ratcheting due to the tooth cone dual-purpose wheel 117 and the cylindrical cavity 105, so that the tooth is bored dual-purpose wheel 117 and rotates backward and band It moves the first bevel gear 114 to rotate backward, makes rotating backward and driving second slider guide for the adjusting threaded rod 131 132 move to right recovery initial position, and second slider guide 132 passes through second connecting rod 129 and the head rod 128 So that the radar elecscreen support plate 126 is rotated clockwise recovery initial position, then controls first motor 113 and stop fortune Turn, starts second motor 111 later and second belt wheel 112 is driven to rotate backward, second belt wheel 112 passes through institute It states belt 110 and the first pulley 108 drives the elevating screw thread bar 102 to rotate backward, the elevating screw thread bar 102 drives The annulus block 104 and disk 134 is whole moves down, and the first tooth runner 120 is driven to rotate backward simultaneously, described the One tooth runner 120 drives the protection door-plate 122 to move towards, and the movable block 106 is downward by the pressure of the disk 134 Mobile, when the annulus block 104 is moved to 101 bottommost of annular groove, two protection door-plates 122 abut, institute It states cylinder containing cavities 118 to be fully blocked, controls second motor 111 and shut down.
The beneficial effects of the invention are as follows:In the initial state due to equipment of the invention, the annulus block is located at the ring Shape sliding slot bottommost, at this point, the movable block bottom end face is abutted with the cylinder containing cavities bottom interior wall, two protections The opposite end face of door-plate abuts, and the protection door-plate completely encloses the cylinder containing cavities, and the radar elecscreen support plate is complete In the containing cavities and it is in horizontality, first slider guide is located at the second guide runner right end, and described the Two slider guides are located at the first guide runner right end, consequently facilitating device care and maintenance.
When carrying out air traffic control monitoring using the equipment of the present invention, first step starter is carried out first, described in startup Second motor drives the second belt wheel rotation, second belt wheel to pass through described in the belt and first pulley drive Elevating screw thread bar rotates, and the elevating screw thread bar drives the annulus block and the disk integrally to move up, and simultaneously described in drive First tooth runner rotates, and protection door-plate described in the first tooth driven by rotating wheel is away from each other movement, and the movable block is by the circle The pulling force of disk moves up, but since the effect of the slide guide bar makes first motor that can keep the power with the disk Connection, when the annulus block is moved to the annular groove top, two protection door-plate maximum distances are separate, described Cylinder containing cavities are opened completely, at this point, the radar elecscreen is fully exposed to extraneous member's observation easy to operation, at this point, control Second motor shuts down, to improve device convenience.
When carrying out second step observation position adjusting, starts first motor and drive the disk rotational, meanwhile, by In the ratcheting of the tooth cone dual-purpose wheel and the cylindrical cavity, make the tooth cone dual-purpose wheel rotation and drive the first bevel gear turn It is dynamic, make the rotation for adjusting threaded rod and second slider guide is driven to move to left, second slider guide passes through described second Connecting rod and the head rod make the radar elecscreen support plate rotate counterclockwise, until being adjusted to suitable operator's observation Position, to improve device working effect.
When completing need of work storage, controls first motor and the disk is driven to rotate backward, simultaneously as The tooth cone dual-purpose wheel is ratcheting with the cylindrical cavity, and the tooth cone dual-purpose wheel is made to rotate backward and drive the first bevel gear It rotates backward, makes rotating backward and second slider guide being driven to move to right recovery initial position for the adjusting threaded rod, it is described Second slider guide makes the radar elecscreen support plate rotate clockwise recovery by second connecting rod and the head rod Then initial position controls first motor and shuts down, start second motor later and drive second band Wheel rotates backward, and second belt wheel drives the elevating screw thread bar to rotate backward by the belt and the first pulley, The elevating screw thread bar drives the annulus block and the disk integrally to move down, and the first tooth runner is driven reversely to turn simultaneously It is dynamic, protect door-plate to move towards described in the first tooth driven by rotating wheel, the movable block is by the pressure of the disk to moving down Dynamic, when the annulus block is moved to the annular groove bottommost, two protection door-plates abut, the cylinder containing cavities It is fully blocked, controls second motor and shut down, to improve the practical performance of device.
The configuration of the present invention is simple, easy to operate, by using accommodating mechanism and protection mechanism in one, equipment is light and handy, behaviour To make simply, all parts cooperation is close but is independent of each other, while being internally provided with movable driving mechanism in accommodating mechanism again, Operating position is automatically adjusted by movable driving mechanism, service life is long, and price is excellent, and practical performance is higher.
The above description is merely a specific embodiment, but scope of protection of the present invention is not limited thereto, any The change or replacement expected without creative work, should be covered by the protection scope of the present invention.Therefore, of the invention Protection domain should be determined by the scope of protection defined in the claims.

Claims (5)

1. a kind of smart utility aviation automates control system, including fuselage and the circle upward in the fuselage inner opening is set Column containing cavities, it is characterised in that:It is communicated equipped with annular groove in the cylinder storage cavity wall, in described cylinder containing cavities or so Perforation is equipped with guide groove symmetrical and at the top of the annular groove in wall body, and cylinder containing cavities bottom is equipped with first Cavity is slidably connected with annulus block in the annular groove, cylindrical cavity, the circle is equipped with up and down in the annulus block Ring block screw-internal thread fit is connected with elevating screw thread bar that is symmetrical and extending up and down, elevating screw thread bar bottom extending end It puts in first cavity and is equipped with first pulley in end face, extending end puts in the guiding at the top of the elevating screw thread bar It is equipped with the first tooth runner in slot and in end, is rotatably assorted in the cylindrical cavity and is connected with disk, disk inner top end face The interior containing cavities equipped with opening upwards, the containing cavities bottom are communicated equipped with the first guide runner, and the first guide runner right end is set There are the second cavity of opening to the right, the containing cavities bottom interior wall to be equipped with supporting rack, the containing cavities are equipped with positioned at described The pedestal of supporting rack right end is hingedly connected with radar elecscreen support plate, the radar elecscreen support plate top end surface on support frame as described above It is equipped with radar elecscreen, is equipped with the second guide runner that Open Side Down in the radar elecscreen support plate bottom end face, described second leads It is slidably connected with the first slider guide in sliding slot, the first connection is hingedly connected between first slider guide and the pedestal Bar is slidably connected with the second slider guide in first guide runner, and the second slider guide screw-internal thread fit is connected with a left side The adjusting threaded rod of right extension, the adjusting threaded rod left end extending end are rotatably assorted with the first guide runner left end inner wall Connection, the adjusting threaded rod right end extending end puts in second cavity and is equipped with first bevel gear in end, described The second connecting rod is hingedly connected at the top of second slider guide, the second connecting rod other end is cut with scissors in the middle part of the head rod It connects in succession, be rotatably assorted the first rotation axis for being connected with and extending up and down in second cavity, and first rotation axis is equipped with To bore dual-purpose wheel with the first bevel gear and the tooth of the ratcheting connection of cylinder cavity wall, cylinder containing cavities bottom is set There are the activity-driven device to be connect with the disk power, fuselage right end end face to be equipped with electrical dust collector device.
2. a kind of smart utility aviation according to claim 1 automates control system, it is characterised in that:The activity is driven Dynamic device includes that the movable block for being located at the disk bottom is arranged in the cylinder containing cavities, in the movable block top end surface Equipped with the first motor, the first motor top end and disk bottom end face be connected by power, the movable block bottom Portion quadrangle is equipped with the slide guide bar extended up and down, and the slide guide bar puts in the cylinder containing cavities bottom interior wall body and slides therewith It is connected.
3. a kind of smart utility aviation according to claim 1 automates control system, it is characterised in that:Described first is empty It is embedded with the second motor in chamber bottom interior wall, the second motor top end be connected by power has the second belt wheel, and described Be connected by power has belt between one belt wheel and second belt wheel.
4. a kind of smart utility aviation according to claim 1 automates control system, it is characterised in that:The guide groove Inside be slidably connected with the protection door-plate that left and right extends, be equipped with that Open Side Down in the protection door board bottom end surface and to The dynamic trough of the ratcheting connection of first tooth runner.
5. a kind of smart utility aviation according to claim 1 automates control system, it is characterised in that:The electric precipitation Device includes the electric precipitation body being arranged on fuselage right end end face, and the cunning of opening to the right is equipped in the electric precipitation body Slot is moved, slipping block is slidably connected in the slippage slot, slipping block right end end face is equipped with electric precipitator, the cunning It moves and is equipped with the adjusting threaded rod that left and right extends soon, adjusting threaded rod left end end be connected by power has third motor, institute Third motor outer surface is stated to be embedded in the slippage slot left end inner wall and connection fixed thereto.
CN201810416273.2A 2018-05-03 2018-05-03 A kind of smart utility aviation automation control system Active CN108520643B (en)

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Application Number Priority Date Filing Date Title
CN201810416273.2A CN108520643B (en) 2018-05-03 2018-05-03 A kind of smart utility aviation automation control system

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Application Number Priority Date Filing Date Title
CN201810416273.2A CN108520643B (en) 2018-05-03 2018-05-03 A kind of smart utility aviation automation control system

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CN108520643B CN108520643B (en) 2019-08-20

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Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN201008430Y (en) * 2006-12-29 2008-01-23 刘文其 Automatic meshwork multimedia platform
CN102485105A (en) * 2010-12-02 2012-06-06 樊立冬 Desk with adjustable horizontal-screen computer
CN102697288A (en) * 2012-06-07 2012-10-03 集美大学 Multifunctional desk
CN102697289A (en) * 2012-06-07 2012-10-03 集美大学 Computer concealed desk
CN204427139U (en) * 2015-03-04 2015-07-01 邵心玮 A kind of computer for students table
CN106820580A (en) * 2017-02-28 2017-06-13 广州市富可士数码科技有限公司 Fully-automatic intelligent multimedia lectern
CN107613809A (en) * 2015-06-16 2018-01-19 安玛思有限责任公司 Telescopic display
CN107830374A (en) * 2017-09-28 2018-03-23 洛阳师范学院 A kind of computer desk

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN201008430Y (en) * 2006-12-29 2008-01-23 刘文其 Automatic meshwork multimedia platform
CN102485105A (en) * 2010-12-02 2012-06-06 樊立冬 Desk with adjustable horizontal-screen computer
CN102697288A (en) * 2012-06-07 2012-10-03 集美大学 Multifunctional desk
CN102697289A (en) * 2012-06-07 2012-10-03 集美大学 Computer concealed desk
CN204427139U (en) * 2015-03-04 2015-07-01 邵心玮 A kind of computer for students table
CN107613809A (en) * 2015-06-16 2018-01-19 安玛思有限责任公司 Telescopic display
CN106820580A (en) * 2017-02-28 2017-06-13 广州市富可士数码科技有限公司 Fully-automatic intelligent multimedia lectern
CN107830374A (en) * 2017-09-28 2018-03-23 洛阳师范学院 A kind of computer desk

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