CN108216663B - Master control center device - Google Patents

Master control center device Download PDF

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Publication number
CN108216663B
CN108216663B CN201810057662.0A CN201810057662A CN108216663B CN 108216663 B CN108216663 B CN 108216663B CN 201810057662 A CN201810057662 A CN 201810057662A CN 108216663 B CN108216663 B CN 108216663B
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China
Prior art keywords
fixedly connected
shock absorption
wall
shock
hole
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CN201810057662.0A
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CN108216663A (en
Inventor
张利梅
丁清澍
樊凌风
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Shenzhen Davinci Innovation Technology Co ltd
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Shenzhen Davinci Innovation Technology Co ltd
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D47/00Equipment not otherwise provided for
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16FSPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F15/00Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
    • F16F15/02Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems
    • F16F15/04Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems using elastic means

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Acoustics & Sound (AREA)
  • Mechanical Engineering (AREA)
  • Vibration Prevention Devices (AREA)

Abstract

The utility model provides a master control center device, includes protective housing, protective housing's top threaded connection has the protective cover, protective housing's interior diapire fixedly connected with radiator fan, protective housing's interior diapire fixedly connected with shock tube, shock tube's interior diapire fixedly connected with damping spring, damping spring's top fixedly connected with shock absorber rod, the top of shock absorber rod is run through and is extended to the upper surface of shock tube, the top fixedly connected with shock attenuation board of shock absorber rod, the upper surface of shock attenuation board is provided with central processing unit. When vibrations appear in the protective housing, central processing unit cushions the shock attenuation through the damping spring of shock attenuation pole bottom on the shock attenuation board to the effectual easy problem of vibrations of unmanned aerial vehicle control center of having solved.

Description

Master control center device
Technical Field
The invention relates to the technical field of unmanned aerial vehicles, in particular to a master control center device.
Background
An unmanned aircraft, referred to as "drone", is an unmanned aircraft that is operated by a radio remote control device and a self-contained program control device, or is operated autonomously, either completely or intermittently, by an onboard computer.
Drones tend to be more suitable for tasks that are too "fool, dirty, or dangerous" than are manned aircraft. Unmanned aerial vehicles can be classified into military and civil applications according to the application field. For military use, unmanned aerial vehicles divide into reconnaissance aircraft and target drone. In the civil aspect, the industrial application of the unmanned aerial vehicle is really just needed by the unmanned aerial vehicle; at present, the unmanned aerial vehicle is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, power inspection, disaster relief, film and television shooting, romantic manufacturing and the like, the application of the unmanned aerial vehicle is greatly expanded, and developed countries actively expand industrial application and develop unmanned aerial vehicle technology.
The field that present unmanned aerial vehicle used is more and more extensive, and is also higher and more higher to the requirement of its control, all has control center in present the most unmanned aerial vehicle, and control center can shake along with unmanned aerial vehicle's vibrations, and the heat of its production also all is controlled alone by control center, and this increases control center's calculation load very easily, so needs a master control center device.
Disclosure of Invention
Technical problem to be solved
Aiming at the defects of the prior art, the invention provides a master control center device, which solves the problems that an unmanned aerial vehicle control center is easy to vibrate and increase load.
(II) technical scheme
In order to achieve the purpose, the invention is realized by the following technical scheme:
a main control center device comprises a protective shell, wherein the top of the protective shell is in threaded connection with a protective cover, the inner bottom wall of the protective shell is fixedly connected with a cooling fan, the inner bottom wall of the protective shell is fixedly connected with a shock absorption tube, the inner bottom wall of the shock absorption tube is fixedly connected with a shock absorption spring, the top of the shock absorption spring is fixedly connected with a shock absorption rod, the top of the shock absorption rod penetrates through and extends to the upper surface of the shock absorption tube, the top of the shock absorption rod is fixedly connected with a shock absorption plate, the upper surface of the shock absorption plate is provided with a central processing unit, the bottom end side surface of the central processing unit is fixedly connected with a connecting block, the middle part of the upper surface of the connecting block is provided with a jack, two ends of the upper surface of the shock absorption plate are fixedly connected with an insert column, the surface of the insert column is inserted into the inner wall of the jack, and the top of the insert column extends to the upper surface of the connecting block, the telescopic hole is formed in the top of the inserting column, a clamping plate is connected to the inner wall of the telescopic hole in a sliding mode, the surface of the clamping plate is connected with the inner wall of the telescopic hole in a sliding mode, a pressure spring is fixedly connected to the surface of one end of the clamping plate, one end of the clamping plate extends to the outside of the telescopic hole, and the lower surface of the clamping plate is connected with the upper surface of a connecting block of the inserting column in a sliding mode.
The utility model discloses a refrigeration pipe, protection casing's outer fixed surface is connected with the refrigeration pipe, the inlet port has been seted up to the interior diapire of refrigeration pipe, the inner wall fixedly connected with semiconductor refrigeration piece of refrigeration pipe, the heat dissipation end of semiconductor refrigeration piece runs through and extends to the surface of refrigeration pipe, the air guide hole has been seted up to protection casing's inner wall, the one end of air guide hole extends to the inside of refrigeration pipe, the other end of air guide hole extends to protection casing's interior diapire.
Preferably, the inner bottom wall of the protective shell is provided with an oil through hole, two ends of the oil through hole are communicated with the inner bottom wall of the damping tube, and hydraulic oil is arranged inside the damping tube and the oil through hole.
Preferably, the other end surface of the clamping plate is triangular, and the number of the clamping plates is two.
Preferably, the heat dissipation outlet is opened to the interior roof of protective cover, the inner wall of heat dissipation outlet is provided with the protection network.
Preferably, the inner wall of the air inlet is fixedly connected with a filter screen, the inner wall of the other end of the air guide hole is fixedly connected with a drying layer, and a drying agent is arranged inside the drying layer.
(III) advantageous effects
The invention provides a master control center device, which has the following beneficial effects:
(1) this master control center device, inner diapire fixedly connected with damping spring through setting up the shock tube, damping spring's top fixedly connected with shock-absorbing rod, the top of shock-absorbing rod is run through and is extended to the upper surface of shock tube, the top fixedly connected with shock attenuation board of shock-absorbing rod, the upper surface of shock attenuation board is provided with central processing unit, it carries out absorbing effect to central processing unit to have reached, when vibrations appear when protective housing, central processing unit cushions the shock attenuation through the damping spring of shock-absorbing rod bottom on the shock attenuation board, thereby the effectual problem of having solved the easy vibrations of unmanned aerial vehicle control center.
(2) This master control center device, through the surface that sets up the cardboard and the inner wall sliding connection in flexible hole, the one end fixed surface of cardboard is connected with pressure spring, the one end of cardboard extends to the outside in flexible hole, the lower surface of cardboard and the upper surface sliding connection who inserts the connecting block of post, convenient to detach's effect when can effectively strengthen central processing unit's the installation rate and maintenance, jack on the connecting block is pegged graft with inserting the post, the cardboard is to inserting the central department of post and returning, when the jack slides to the cardboard lower surface, the upper surface sliding connection of cardboard roll-off and connecting block, and then be convenient for installation and maintenance.
Drawings
FIG. 1 is a schematic structural view of the present invention;
FIG. 2 is an enlarged view taken at A of FIG. 1 in accordance with the present invention;
in the figure: the device comprises a protective shell 1, a protective cover 2, a heat radiation fan 3, a damping pipe 4, a damping spring 5, a damping rod 6, a damping plate 7, a central processing unit 8, a connecting block 9, a jack 10, an insertion column 11, a telescopic hole 12, a clamping plate 13, a pressure spring 14, a refrigerating pipe 15, an air inlet 16, a semiconductor refrigerating sheet 17, an air guide hole 18, a temperature sensor 19, a heat radiation outlet 26, a protective screen 27, a filter screen 28 and a drying layer 29.
Detailed Description
The technical solution in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention.
A master control center device comprises a protective shell 1, wherein the top of the protective shell 1 is in threaded connection with a protective cover 2, the inner top wall of the protective cover 2 is provided with a heat dissipation outlet 26, the inner wall of the heat dissipation outlet 26 is provided with a protective net 27, the inner bottom wall of the protective shell 1 is fixedly connected with a cooling fan 3, the inner bottom wall of the protective shell 1 is fixedly connected with a damping pipe 4, the inner bottom wall of the protective shell 1 is provided with an oil through hole 25, two ends of the oil through hole 25 are communicated with the inner bottom wall of the damping pipe 4, hydraulic oil is arranged inside the damping pipe 4 and the oil through hole 25 and can effectively damp and buffer the top of the damping pipe 4, the inner bottom wall of the damping pipe 4 is fixedly connected with a damping spring 5, the top of the damping spring 5 is fixedly connected with a damping rod 6, the top of the damping rod 6 penetrates through and extends to the upper surface of the damping pipe 4, and the top of the damping rod 6 is fixedly connected with a damping plate 7, the upper surface of the shock absorption plate 7 is provided with a central processing unit 8, a shock absorption spring 5 is fixedly connected through the inner bottom wall of the shock absorption tube 4, the top of the shock absorption spring 5 is fixedly connected with a shock absorption rod 6, the top of the shock absorption rod 6 penetrates through and extends to the upper surface of the shock absorption tube 4, the top of the shock absorption rod 6 is fixedly connected with the shock absorption plate 7, the upper surface of the shock absorption plate 7 is provided with the central processing unit 8, the shock absorption effect on the central processing unit 8 is achieved, when the protective shell 1 vibrates, the central processing unit 8 performs buffering shock absorption on the shock absorption plate 7 through the shock absorption spring 5 at the bottom end of the shock absorption rod 6, so that the problem that an unmanned aerial vehicle control center is easy to vibrate is effectively solved, the bottom end side surface of the central processing unit 8 is fixedly connected with a connecting block 9, the middle part of the upper surface of the connecting block 9 is provided with a jack 10, and two ends of the upper surface of the shock absorption plate 7 are both fixedly connected with plug posts 11, the surface of the insert column 11 is inserted into the inner wall of the jack 10, the top of the insert column 11 extends to the upper surface of the connecting block 9, a telescopic hole 12 is formed in the top of the insert column 11, the inner wall of the telescopic hole 12 is slidably connected with two clamping plates 13, the surface of each clamping plate 13 is slidably connected with the inner wall of the telescopic hole 12, one end of each clamping plate 13 is fixedly connected with a pressure spring 14, one end of each clamping plate 13 extends to the outside of the telescopic hole 12, the surface of the other end of each clamping plate 13 is triangular, the lower surfaces of the clamping plates 13 are slidably connected with the upper surface of the connecting block 9 of the insert column 11, the surface of each clamping plate 13 is slidably connected with the inner wall of the telescopic hole 12, one end of each clamping plate 13 is fixedly connected with a pressure spring 14, one end of each clamping plate 13 extends to the outside of the telescopic hole 12, the lower surfaces of the clamping plates 13 are slidably connected with the upper surface of the connecting block 9 of the insert column 11, the installation speed of the central processing unit 8 and the effect of convenient disassembly during maintenance can be effectively enhanced, the jack 10 on the connecting block 9 is inserted with the inserting column 11, the clamping plate 13 retracts towards the center of the inserting column 11, and when the jack 10 slides to the lower surface of the clamping plate 13, the clamping plate 13 slides out to be connected with the upper surface of the connecting block 9 in a sliding mode, so that the installation and the maintenance are facilitated.
Protection casing 1's outer fixed surface is connected with refrigeration pipe 15, inlet port 16 has been seted up to refrigeration pipe 15's interior diapire, refrigeration pipe 15's inner wall fixedly connected with semiconductor refrigeration piece 17, semiconductor refrigeration piece 17's heat dissipation end runs through and extends to refrigeration pipe 15's surface, air guide 18 has been seted up to protection casing 1's inner wall, air guide 18's one end extends to refrigeration pipe 15's inside, air guide 18's the other end extends to protection casing 1's interior diapire, the inner wall fixedly connected with filter screen 28 of inlet port 16, air guide 18's other end inner wall fixedly connected with drying layer 29, drying layer 29's inside is provided with the drier, can reach the effect that the moisture that produces carries out the drying and detach behind the air quench in refrigeration pipe 2.
In summary, in the main control center device, by arranging the surface of the clamping plate 13 to be slidably connected with the inner wall of the telescopic hole 12, the surface of one end of the clamping plate 13 is fixedly connected with the pressure spring 14, one end of the clamping plate 13 extends to the outside of the telescopic hole 12, and the lower surface of the clamping plate 13 is slidably connected with the upper surface of the connecting block 9 of the inserting column 11, so that the installation speed of the central processing unit 8 and the effect of convenient disassembly during maintenance can be effectively enhanced, the inserting hole 10 on the connecting block 9 is inserted into the inserting column 11, the clamping plate 13 retracts towards the center of the inserting column 11, when the inserting hole 10 slides to the lower surface of the clamping plate 13, the clamping plate 13 slides out to be slidably connected with the upper surface of the connecting block 9, so as to facilitate installation and maintenance, by arranging the damping spring 5 fixedly connected with the inner bottom wall of the damping tube 4, the top of the damping spring 5 is fixedly connected with the damping rod 6, and the top of the damping rod 6 penetrates and extends to the upper surface of the damping tube 4, the top fixedly connected with shock attenuation board 7 of shock attenuation pole 6, the upper surface of shock attenuation board 7 is provided with central processing unit 8, has reached and has carried out absorbing effect to central processing unit 8, when vibrations appear in protective housing 1, central processing unit 8 cushions the shock attenuation through damping spring 5 of 6 bottoms of shock attenuation pole on shock attenuation board 7 to the effectual easy problem of vibrations of unmanned aerial vehicle control center of having solved, protective housing 1's inner wall is provided with temperature sensor, and temperature sensor is connected to the singlechip, and the singlechip is connected with radiator fan 3 and semiconductor refrigeration piece 17 electricity simultaneously, and when temperature sensor detected the temperature and reached design temperature, the singlechip started radiator fan 3 and semiconductor refrigeration piece 17, thereby the effectual problem of unmanned aerial vehicle control center increase load of having solved.

Claims (3)

1. The utility model provides a master control center device, includes protecting housing (1), the top threaded connection of protecting housing (1) has protective cover (2), the interior diapire fixedly connected with radiator fan (3) of protecting housing (1), its characterized in that: the shock absorption tube (4) is fixedly connected to the inner bottom wall of the protective shell (1), the shock absorption spring (5) is fixedly connected to the inner bottom wall of the shock absorption tube (4), the shock absorption rod (6) is fixedly connected to the top of the shock absorption spring (5), the top of the shock absorption rod (6) penetrates through and extends to the upper surface of the shock absorption tube (4), the shock absorption plate (7) is fixedly connected to the top of the shock absorption rod (6), the central processing unit (8) is arranged on the upper surface of the shock absorption plate (7), the connecting block (9) is fixedly connected to the bottom end side face of the central processing unit (8), the jack (10) is formed in the middle of the upper surface of the connecting block (9), the inserting columns (11) are fixedly connected to two ends of the upper surface of the shock absorption plate (7), the surfaces of the inserting columns (11) are inserted into the inner walls of the jack (10), and the tops of the inserting columns (11) extend to the upper surface of the connecting block (9), a telescopic hole (12) is formed in the top of the inserting column (11), a clamping plate (13) is connected to the inner wall of the telescopic hole (12) in a sliding mode, the surface of the clamping plate (13) is connected with the inner wall of the telescopic hole (12) in a sliding mode, a pressure spring (14) is fixedly connected to the surface of one end of the clamping plate (13), one end of the clamping plate (13) extends to the outside of the telescopic hole (12), and the lower surface of the clamping plate (13) is connected with the upper surface of a connecting block (9) of the inserting column (11) in a sliding mode;
the outer surface of the protective shell (1) is fixedly connected with a refrigerating pipe (15), an air inlet hole (16) is formed in the inner bottom wall of the refrigerating pipe (15), a semiconductor refrigerating sheet (17) is fixedly connected to the inner wall of the refrigerating pipe (15), the heat dissipation end of the semiconductor refrigerating sheet (17) penetrates through and extends to the outer surface of the refrigerating pipe (15), an air guide hole (18) is formed in the inner wall of the protective shell (1), one end of the air guide hole (18) extends to the inner portion of the refrigerating pipe (15), and the other end of the air guide hole (18) extends to the inner bottom wall of the protective shell (1);
the inner wall of the protective shell (1) is provided with a temperature sensor (19), the temperature sensor (19) is connected to a single chip microcomputer, and the single chip microcomputer is simultaneously electrically connected with the cooling fan (3) and the semiconductor refrigerating sheet (17);
a heat dissipation outlet (26) is formed in the inner top wall of the protective cover (2), and a protective net (27) is arranged on the inner wall of the heat dissipation outlet (26); the inner wall of the air inlet hole (16) is fixedly connected with a filter screen (28), the inner wall of the other end of the air guide hole (18) is fixedly connected with a drying layer (29), and a drying agent is arranged inside the drying layer (29).
2. The key center device according to claim 1, wherein: oil through hole (25) have been seted up to the inner bottom wall of protective housing (1), the both ends of oil through hole (25) all communicate with the inner bottom wall of shock tube (4), the inside of shock tube (4) and oil through hole (25) all is provided with hydraulic oil.
3. The key center device according to claim 1, wherein: the surface of the other end of each clamping plate (13) is triangular, and the number of the clamping plates (13) is two.
CN201810057662.0A 2018-01-22 2018-01-22 Master control center device Active CN108216663B (en)

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CN108216663B true CN108216663B (en) 2021-12-03

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Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108937870B (en) * 2018-07-16 2021-02-12 青岛市妇女儿童医院(青岛市妇幼保健院、青岛市残疾儿童医疗康复中心、青岛市新生儿疾病筛查中心) Health monitoring intelligent clothing
CN109626313B (en) * 2019-01-14 2020-09-11 赵郁 Unmanned tanker aircraft with protect function
CN110694392A (en) * 2019-10-22 2020-01-17 安徽财经大学 Dustproof equipment for outdoor computer network exchanger
CN111010502A (en) * 2019-12-24 2020-04-14 吴文娟 Automatic radiating shock-proof type image processor
CN112855353B (en) * 2021-03-12 2024-05-03 四川鸿鹏航空航天装备智能制造有限公司 Automatic control and monitoring system for engine

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2010127191A (en) * 2008-11-28 2010-06-10 Hitachi Appliances Inc Hermetic type compressor
CN102128234A (en) * 2011-03-09 2011-07-20 哈尔滨工程大学 Hydraulic driving vibration isolator based on piezoelectric actuation
CN204726678U (en) * 2015-04-18 2015-10-28 中国计量学院 A kind of quartz conductor Intelligent temperature reduction device for aircraft
CN205686617U (en) * 2016-06-25 2016-11-16 漯河职业技术学院 A kind of novel unmanned plane heat abstractor
CN107524750A (en) * 2017-10-19 2017-12-29 成都创年科技有限公司 Unmanned plane landing damping device
CN107600420A (en) * 2017-10-13 2018-01-19 南京涵曦月自动化科技有限公司 A kind of multi-rotor unmanned aerial vehicle control module

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2010127191A (en) * 2008-11-28 2010-06-10 Hitachi Appliances Inc Hermetic type compressor
CN102128234A (en) * 2011-03-09 2011-07-20 哈尔滨工程大学 Hydraulic driving vibration isolator based on piezoelectric actuation
CN204726678U (en) * 2015-04-18 2015-10-28 中国计量学院 A kind of quartz conductor Intelligent temperature reduction device for aircraft
CN205686617U (en) * 2016-06-25 2016-11-16 漯河职业技术学院 A kind of novel unmanned plane heat abstractor
CN107600420A (en) * 2017-10-13 2018-01-19 南京涵曦月自动化科技有限公司 A kind of multi-rotor unmanned aerial vehicle control module
CN107524750A (en) * 2017-10-19 2017-12-29 成都创年科技有限公司 Unmanned plane landing damping device

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Inventor after: Zhang Limei

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