CN110371306A - A kind of multifunctional universal aircraft control switch - Google Patents
A kind of multifunctional universal aircraft control switch Download PDFInfo
- Publication number
- CN110371306A CN110371306A CN201910505091.7A CN201910505091A CN110371306A CN 110371306 A CN110371306 A CN 110371306A CN 201910505091 A CN201910505091 A CN 201910505091A CN 110371306 A CN110371306 A CN 110371306A
- Authority
- CN
- China
- Prior art keywords
- console
- button
- fixedly connected
- control button
- centimetres
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- 239000007787 solid Substances 0.000 claims description 2
- 238000009434 installation Methods 0.000 abstract description 6
- 230000006835 compression Effects 0.000 abstract description 4
- 238000007906 compression Methods 0.000 abstract description 4
- 238000000034 method Methods 0.000 description 6
- 230000006399 behavior Effects 0.000 description 3
- 238000010586 diagram Methods 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 3
- 230000006870 function Effects 0.000 description 3
- 230000010365 information processing Effects 0.000 description 3
- 238000012545 processing Methods 0.000 description 3
- 238000004378 air conditioning Methods 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 238000004886 process control Methods 0.000 description 2
- 238000003466 welding Methods 0.000 description 2
- 206010020852 Hypertonia Diseases 0.000 description 1
- 210000003484 anatomy Anatomy 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000009172 bursting Effects 0.000 description 1
- 238000012512 characterization method Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 230000013011 mating Effects 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
Classifications
-
- 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
- B64D43/00—Arrangements or adaptations of instruments
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
- G05B19/00—Programme-control systems
- G05B19/02—Programme-control systems electric
- G05B19/04—Programme control other than numerical control, i.e. in sequence controllers or logic controllers
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Aviation & Aerospace Engineering (AREA)
- Switch Cases, Indication, And Locking (AREA)
- Feedback Control In General (AREA)
Abstract
The invention discloses a kind of multifunctional universal aircraft control switches, including lower console and signal connecting line, the lower console front end middle position is provided with lower control button, because being equipped with spring card pole device, so six spring card pole devices are first inserted into inside the fixation hole of external fixing end by staff, after the fixation hole inner wall of two rounded-rectangular card columns and external fixing end contacts, two rounded-rectangular card columns will be made mobile towards middle position, but also adjustable spring carries out compression work, after two rounded-rectangular card columns are aligned with the fixing groove at two side positions above and below the fixation hole of external fixing end, adjustable spring just will do it extension work, so that two rounded-rectangular card columns are fixedly connected with the fixing groove at the fixation hole of external fixing end up and down two side positions, installation efficiency is not only increased in this way , and also reduce the spoilage of equipment.
Description
Technical field
The invention belongs to multifunctional universal aircraft control switch correlative technology fields, and in particular to a kind of multifunctional universal
Aircraft control switch.
Background technique
A kind of special key when control switch is the process control for electrical control and Thermal Meter.Specifically there is positioning
The functions such as operation, runback operation, positioning-runback operation, lock operation, positioning-lock operation, runback-positioning-lock operation.
A kind of control switch: special key when for electrical control and the process control of Thermal Meter.Pressure switch series of products are used
In air conditioning for automobiles, guarantee that automobile air conditioner compressor runs well；Vent valve is then the control unit of automobile engine supercharging system.
Both for energy-saving and environmental protection product, the former is the pressure switch being applied to aviation pressure-sensing device manufacturing technology on automobile,
The latter has used spring manufacture and processing technique.SYKG-1 pressure switch therein and Dragon Lord Citroen zx motorcar air conditioner are mating, right
The control of air-conditioning system pressure.III grade is high voltage control, and when control system hypertonia shuts down compressor to prevent pipelines from bursting；Ⅱ
Shelves be in voltage-controlled system, the on-off of the add ons (fan of such as condenser pipe) of control system；I grade is low voltage control, control system
It is too low to generate leak pressure, shuts down compressor, shields
Existing multifunctional universal aircraft is had the following problems with control switch technology: existing multifunctional universal aircraft is used
Control switch is to be fixed multifunctional universal aircraft with control switch and external fixing end by fixture nut when installation
Connection, so that staff will be empty because of external fixing end when installing multifunctional universal aircraft control switch
Between it is narrow, during installation so as to cause staff, working efficiency will reduce, at the same also can be easy increase equipment damage
Rate not only reduces installation efficiency in this way, and also adds the spoilage of equipment.
Summary of the invention
The purpose of the present invention is to provide a kind of multifunctional universal aircraft control switches, to solve in above-mentioned background technique
Reducing for proposing and increases the spoilage problem of equipment at installation efficiency.
To achieve the above object, the invention provides the following technical scheme: a kind of multifunctional universal aircraft control switch, packet
Lower console and signal connecting line are included, the lower console front end middle position is provided with lower control button, the lower control
It is provided with the aperture apparatus that amplifies at top position on the left of platform front end, the aperture apparatus that amplifies is located at lower control button upper left side position
Place, the lower console front end left side middle position are provided with isosceles triangle control button, and the isosceles triangle control button is located at
At lower control button leftward position, ball adjusting rod, the ball are socketed at interior location on the left of the lower console front end
Adjusting rod is located at isosceles triangle control button leftward position, is provided with Spring Card at position at left and right sides of the lower console rear end
Column device is socketed with Switching Power Supply line, the lower console upper end position inside middle position below the lower console rear end
The place of setting is provided with middle console, is provided with No.1 display screen, the middle console in the middle console front end at top position
Lower position is provided with middle control button in front end, and the middle control button is located at No.1 display screen lower position, described
Lateral adjustments button is provided at the middle upper left position in console front end, it is left that the lateral adjustments button is located at No.1 display screen
At side position, moccasin button is provided at the middle console front end upper right side position, the moccasin button is located at No.1 and shows
Shield at the position of upper right side, trapezoidal control button is provided at the middle console front end lower right position, the trapezoidal control is pressed
Button is located at middle control button right positions, and the trapezoidal control button is located at moccasin button lower right position, the middle control
Hexagonal jack devices are socketed at the upper right side position of platform front end processed, the hexagonal jack devices are located at trapezoidal control button upper position
Place is set, the hexagonal jack devices are located at moccasin button right positions, cover at interior location on the right side of the middle console front end
It is connected to vertical adjustment button, the vertical adjustment button is located at hexagonal jack devices and trapezoidal control button right positions, institute
It states and is provided with spring card pole device at left and right sides of middle console rear end at position, above the lower console rear end in the left and right sides
Signal connecting line is socketed with below at portion position and middle console rear end at the interior location of the left and right sides, on the middle console
Console is provided at end position, the upper console front end middle position is provided with No. two display screens, the upper control
Lateral adjustments button is provided at platform front end upper left side and front end lower-left side position respectively, two lateral adjustments buttons are located at
At No. two display screen leftward positions, be provided with respectively at the upper console front end upper right side and front end bottom right side position moccasin by
Button, two moccasin buttons are located at No. two display screen right positions, the upper console front end upper right side and front end bottom right
Double-direction control button is respectively arranged at side position, two double-direction control buttons are located at moccasin button right positions, institute
It states and is provided with spring card pole device at left and right sides of console rear end at position, below the upper console rear end in the left and right sides
Signal connecting line is socketed at the interior location of the left and right sides above at portion position and middle console rear end.
Preferably, the spring card pole device includes fixed connecting base, rounded-rectangular card column, is fixedly connected with slot, flexible bullet
Spring and anti-off board, the fixed connecting base are provided at the inside middle position of two sides are fixedly connected with slot up and down, two fixations
Link slot is provided with adjustable spring towards outer end middle position, and two adjustable springs, which are located at, is fixedly connected with slot interior location
Place, towards anti-off board is provided at outer end position, two anti-off boards are located to be fixedly connected inside slot two adjustable springs
At position, two anti-off boards are provided with rounded-rectangular card column, two rounded-rectangular card columns towards outer end middle position
Positioned at being fixedly connected at slot interior location, the spring card pole device by fixed connecting base respectively with upper console, middle control
Platform is fixedly connected with lower console.
Preferably, No. two display screens are set as four, and the model of four No. two display screens is set as IS-
F15ACP04, four No. two display screens are fixedly connected by fixture nut with upper console, four No. two display screens
By display screen and signal line group at.
Preferably, the lateral adjustments button is set as three, and three lateral adjustments buttons pass through fixture nut point
It is not fixedly connected with upper console and middle console, three lateral adjustments button annulus fixing sleeves adjust turn-button and signal
Line composition.
Preferably, the lower control button is by 11 level-one switch buttons, two secondary switch buttons and signal line group
At the lower control button is fixedly connected by fixture nut with lower console.
Preferably, processor, and the model of processor are provided at the upper console inside middle position
UCC38500, the upper console length, width and height decibel are set as 40 centimetres, ten centimetres and 20 centimetres, described
Upper console is shaped to I shape.
Preferably, processor, and the model of processor are provided at the middle console inside middle position
UCC38500, the middle console length, width and height decibel are set as 40 centimetres, ten centimetres and 30 centimetres, described
Middle console is shaped to I shape.
Preferably, processor, and the model of processor are provided at the lower console inside middle position
UCC38500, the lower console length, width and height decibel are set as 40 centimetres, ten centimetres and 20 lis, under described
Console is shaped to I shape.
Preferably, the aperture apparatus that amplifies is by amplifying hole shield and loudspeaker form, and the model SVF115WR of loudspeaker,
The aperture apparatus that amplifies is fixedly connected by welding with lower console.
Preferably, the ball adjusting rod is by ball handle, adjusting hand lever, rotary shaft and signal line group at the ball
Adjusting rod is fixedly connected by rotary shaft with the rotation of lower console.
Compared with prior art, the present invention provides a kind of multifunctional universal aircraft control switches, have following beneficial
Effect: the present invention is equipped with spring card pole device, and staff is first by the fixation of six spring card pole devices and external fixing end
After the alignment of hole, six spring card pole devices are inserted into inside the fixation hole of external fixing end, two above and below spring card pole device
After rounded-rectangular card column at side position is contacted with the fixation hole inner wall of external fixing end, two rounded-rectangular cards will be made
Column is mobile towards middle position, so that adjustable spring carries out compression work, when two rounded-rectangular card columns are fixed with outside
At position above and below the fixation hole at end inside two sides after fixing groove alignment, adjustable spring just will do it extension work, so that two
A rounded-rectangular card column is fixedly connected with fixing groove at the position inside the fixation hole of external fixing end up and down two sides, so that
Upper console, middle console and lower console are fixedly connected with external fixing end, not only increase installation efficiency in this way, and
And also reduce the spoilage of equipment.
Detailed description of the invention
Attached drawing is used to provide further understanding of the present invention, and constitutes part of specification, with reality of the invention
It applies example to be used to explain the present invention together, not be construed as limiting the invention, in the accompanying drawings:
Fig. 1 is a kind of multifunctional universal aircraft control switch structural schematic diagram proposed by the present invention；
Fig. 2 is rearview structural representation proposed by the present invention；
Fig. 3 is spring card pole apparatus structure schematic diagram proposed by the present invention；
Fig. 4 is spring card pole device internal anatomy schematic diagram proposed by the present invention；
In figure: 1, upper console；2, lateral adjustments button；3, No.1 display screen；4, middle console；5, middle control button；
6, amplify aperture apparatus；7, lower console；8, lower control button；9, isosceles triangle control button；10, ball adjusting rod；11, trapezoidal control
Button processed；12, vertical adjustment button；13, hexagonal jack devices；14, double-direction control button；15, moccasin button；16, No. two show
Display screen；17, Switching Power Supply line；18, spring card pole device；181, fixed connecting base；182, rounded-rectangular card column；183, fixed to connect
Access slot；184, adjustable spring；185, anti-off board；19, signal connecting line.
Specific embodiment
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete
Site preparation description, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.It is based on
Embodiment in the present invention, it is obtained by those of ordinary skill in the art without making creative efforts every other
Embodiment shall fall within the protection scope of the present invention.
Fig. 1-4 is please referred to, the present invention provides a kind of technical solution: a kind of multifunctional universal aircraft control switch, including
Lower console 7 and signal connecting line 19 are provided with processor, and the model of processor at lower 7 inside middle position of console
UCC38500, lower 7 length of console, width and height decibel are set as 40 centimetres, ten centimetres and 20 centimetres, lower console
7 are shaped to I shape, in order to preferably be fixed and support work, and also to preferably carry out information
The work of processing, lower 7 front end middle position of console are provided with lower control button 8, and lower control button 8 is opened by 11 level-ones
Button, two secondary switch buttons and signal line group are closed at lower control button 8 connects by the way that fixture nut and lower console 7 are fixed
It connects, in order to preferably carry out control switch operation, is provided with the aperture apparatus 6 that amplifies at top position on the left of lower 7 front end of console, expands
Sound hole device 6 is by amplifying hole shield and loudspeaker form, and the model SVF115WR of loudspeaker, the aperture apparatus 6 that amplifies pass through welding
It is fixedly connected with lower console 7, in order to allow staff that can not clearly hear the sound of operation, to allow staff
Control operation can be preferably carried out, the aperture apparatus 6 that amplifies is located at lower 8 upper left side position of control button, and lower 7 front end of console is left
Side middle position is provided with isosceles triangle control button 9, and isosceles triangle control button 9 is located at lower 8 leftward position of control button, under
Be socketed with ball adjusting rod 10 on the left of 7 front end of console at interior location, ball adjusting rod 10 by ball handle, adjust hand lever,
Rotary shaft and signal line group are at ball adjusting rod 10 is fixedly connected by rotary shaft with the rotation of lower console 7, and ball handle is passed through
It drives and adjusts rotary shaft progress rotary work on hand lever, so that rotation control work is more preferably carried out, so that multifunctional universal
Aircraft preferably carries out rotation control work with control switch, and ball adjusting rod 10 is located at 9 leftward position of isosceles triangle control button
Place, lower 7 rear end of the console left and right sides are provided with spring card pole device 18, inside middle below lower 7 rear end of console at position
It is socketed with Switching Power Supply line 17 at position, middle console 4, middle 4 inside middle of console are provided at lower 7 upper end position of console
Processor, and the model UCC38500 of processor, middle 4 length of console, width and the setting of height decibel are provided at position
It is 40 centimetres, ten centimetres and 30 centimetres, middle console 4 is shaped to I shape, in order to preferably be consolidated
Fixed and support work is arranged at top position in middle 4 front end of console and also to preferably carry out the work of information processing
There is No.1 display screen 3, lower position is provided with middle control button 5 in middle 4 front end of console, and middle control button 5 is located at No.1
3 lower position of display screen, middle 4 front end of console are provided with lateral adjustments button 2, lateral adjustments button at upper left position
2 are set as three, and three lateral adjustments buttons 2 are fixedly connected with upper console 1 and middle console 4 respectively by fixture nut,
Three 2 annulus fixing sleeves of lateral adjustments button, adjust turn-button and signal line group at, in order to preferably carry out following the work of modulation section,
So that middle console 4 and upper console 1 preferably carry out working, lateral adjustments button 2 is located at 3 left side of No.1 display screen
At position, moccasin button 15 is provided at middle 4 front end upper right side position of console, it is right that moccasin button 15 is located at No.1 display screen 3
At top position, it is provided with trapezoidal control button 11 at middle 4 front end lower right position of console, during trapezoidal control button 11 is located at
At 5 right positions of control button, trapezoidal control button 11 is located at 15 lower right position of moccasin button, and middle 4 front end of console is right
Hexagonal jack devices 13 are socketed at top position, hexagonal jack devices 13 are located at trapezoidal 11 top position of control button, and six
Angle jack devices 13 are located at 15 right positions of moccasin button, are socketed with vertical tune at interior location on the right side of middle 4 front end of console
Button 12 is saved, vertical adjustment button 12 is located at 11 right positions of hexagonal jack devices 13 and trapezoidal control button, middle console 4
Spring card pole device 18 is provided at left and right sides of rear end at position, spring card pole device 18 is straight including fixed connecting base 181, circular arc
Angle card column 182 is fixedly connected with slot 183, adjustable spring 184 and anti-off board 185, about 181 two sides inside middle of fixed connecting base
It is provided at position and is fixedly connected with slot 183, two are fixedly connected with slot 183 and outer end middle position are provided with adjustable spring 184,
Two adjustable springs 184, which are located at, to be fixedly connected at 183 interior location of slot, and two adjustable springs 184 are towards being provided at outer end position
Anti-off board 185, two anti-off boards 185, which are located at, to be fixedly connected at 183 interior location of slot, and two anti-off boards 185 are towards outer end interposition
The place of setting is provided with rounded-rectangular card column 182, and two rounded-rectangular card columns 182, which are located at, to be fixedly connected at 183 interior location of slot, spring
Card column device 18 is fixedly connected with upper console 1, middle console 4 and lower console 7 respectively by fixed connecting base 181, by six
A spring card pole device 18 is inserted into inside the fixation hole of external fixing end, when position in six about 181 two sides of fixed connecting base
When the fixation hole inner wall of the rounded-rectangular card column 182 of the place's of setting socket and external fixing end contacts, six fixations will be made
The rounded-rectangular card column 182 being socketed at about 181 two sides interior location of attachment base is moved towards 181 middle position of fixed connecting base
It is dynamic, so that the rounded-rectangular card column 182 of socket is to being fixedly connected at six about 181 two sides interior locations of fixed connecting base
Adjustable spring 184 at about 181 two sides inside middle positions of seat carries out compression work, when two rounded-rectangular card columns 182 and
At position above and below the fixation hole of external fixing end inside two sides when fixing groove alignment, about 181 two sides of fixed connecting base
Adjustable spring 184 inside middle position just will do it extension work, so that two rounded-rectangular card columns 182 and outside
Fixing groove is fixedly connected at position above and below the fixation hole of fixing end inside two sides, allows for entire multifunctional universal aircraft in this way
It is fixedly connected with control switch with external fixing end, so that upper console 1, middle console 4 and lower console 7 can be more
It is fixedly connected with the fixing groove at two side positions above and below the fixation hole of external fixing end well, which improves installment work effects
Rate, while the spoilage of equipment is also reduced, above lower 7 rear end of console at the interior location of the left and right sides and after middle console 4
It is socketed with signal connecting line 19 at the interior location of the end lower section left and right sides, is provided with control at middle 4 upper end position of console
Platform 1 is provided with processor at upper 1 inside middle position of console, and the model UCC38500 of processor, upper console 1 are long
Degree, width and height decibel are set as 40 centimetres, ten centimetres and 20 centimetres, and upper console 1 is shaped to I-shaped
Shape, in order to preferably be fixed and support work, and also to preferably carry out the work of information processing, upper console
1 front end middle position is provided with No. two display screens 16, and No. two display screens 16 are set as four, the type of four No. two display screens 16
It number is set as IS-F15ACP04, four No. two display screens 16 are fixedly connected by fixture nut with upper console 1, and four No. two
Display screen 16 is by display screen and signal line group in order to preferably show operating result, so that staff is preferably controlled
Operation element processed, is provided with lateral adjustments button 2 at upper 1 front end upper left side of console and front end lower-left side position respectively, and two
Lateral adjustments button 2 is located at No. two 16 leftward positions of display screen, at upper 1 front end upper right side of console and front end bottom right side position
It is respectively arranged with moccasin button 15, two moccasin buttons 15 are located at No. two 16 right positions of display screen, and upper 1 front end of console is right
Double-direction control button 14 is provided at upside and front end bottom right side position respectively, two double-direction control buttons 14 are located at moccasin button
At 15 right positions, it is provided with spring card pole device 18 at left and right sides of upper 1 rear end of console at position, under upper 1 rear end of console
Signal connecting line is socketed at the interior location of the side left and right sides and above 4 rear end of middle console at the interior location of the left and right sides
19, telecommunications connection is more preferably carried out with upper console 1, middle console 4 and lower console 7 respectively by four signal connecting lines 19,
Connected so that upper console 1, middle console 4 more preferably carry out telecommunications with lower console 7, can thus make console 1,
Middle console 4 and lower console 7 preferably work.
Processor working principle of the invention and process for using: CPU takes out from memory or cache memory to be referred to
It enables, is put into command register, and to Instruction decoding.Command Resolution at a series of microoperation, is then issued various controls by it
Order executes microoperation series, to complete the execution of an instruction；Instruction is that computer provides to execute type and the behaviour of operation
The basic command counted.Instruction is made of a byte or multiple bytes, including opcode field, one or more
The status word and condition code of field and some characterization machine states in relation to operand address；It is also directly wrapped in some instructions
Containing operand itself, the controller of CPU instructs from memory reading one and is put into command register；The format of instruction is usually this
A appearance drop: operation code is exactly the mov in assembler language, the symbolic codes such as add, jmp, is to have strictly between each instruction in program
Sequence, it is necessary to which the stringent sequence by procedure stipulation executes, and just can guarantee the correctness of computer working；Operand address
Illustrate the place where the operand that the instruction needs, is in memory or in the internal register of CPU；Command register
In instruction by decoding, determine the instruction should carry out which kind of operation (be exactly instruction in operation code), operand where (behaviour
The address counted)；It executes instruction and (writes back), simply write back the result in the stage that executes with certain format；The function of one instruction
A series of operation often can be executed by the component in computer to realize.CPU will be generated corresponding according to the function of instruction
Operating control signal, issue corresponding component, acted to control these components by the requirement of instruction；Operation result warp
The buffer being often written into inside CPU, for then instructing quick access；Location counter is modified, determines next instruction
Address carries out arithmetical operation and logical operation to data, or carry out other information processings.
The working principle of the invention and process for using: after the present invention installs, staff is first by Switching Power Supply line 17
Telecommunications connection is carried out with external power supply, is then again aligned six spring card pole devices 18 with the fixation hole of external fixing end, it
Six spring card pole devices 18 are inserted into inside the fixation hole of external fixing end again afterwards, when six fixed connecting bases about 181 two
When the fixation hole inner wall of the rounded-rectangular card column 182 and external fixing end that are socketed at the interior location of side contacts, it will make
The rounded-rectangular card column 182 being socketed at six about 181 two sides interior locations of fixed connecting base is towards 181 interposition of fixed connecting base
Place's movement is set, so that the rounded-rectangular card column 182 being socketed at six about 181 two sides interior locations of fixed connecting base is to solid
Determine the adjustable spring 184 at about 181 two sides inside middle position of attachment base and carry out compression work, when two rounded-rectangular card columns
182 with fixing groove at the position inside the fixation hole of external fixing end up and down two sides when be aligned, about 181 fixed connecting base
Adjustable spring 184 at the inside middle position of two sides just will do it extension work so that two rounded-rectangular card columns 182 with
Fixing groove is fixedly connected at position above and below the fixation hole of external fixing end inside two sides, allows for entire multifunctional universal in this way
Aircraft is fixedly connected with control switch with external fixing end, is later again opened the control of multifunctional universal aircraft by signal wire
It closes and carries out telecommunications connection with external power supply apparatus, at this time staff passes through operation lateral adjustments button 2, middle control respectively again
Button 5 processed, lower control button 8, isosceles triangle control button 9, ball adjusting rod 10, trapezoidal control button 11, vertical adjustment button
12, double-direction control button 14 and moccasin button 15 carry out control operation, at this moment will be input to by signal wire upper console 1,
In the processor of 7 inside model UCC38500 of middle console 4 and lower console, processor, will after receiving signal
Signal processing work is carried out, and the No.1 display screen 3 and four of treated signal is separately input to by signal wire model ODK
Inside No. two display screens 16 of a model IS-F15ACP04, No.1 display screen 3 and four No. two display screens 16 are receiving letter
It just will do it display work after number, treated signal can be also input to the power supply of outside by simultaneous processor by signal wire
Device inside so that external power supply apparatus can preferably work, and also can be by the aperture apparatus 6 that amplifies inside
Model SVF115WR loudspeaker will issue control operation sound, allow staff not hear behaviour clearly
The sound of work allows staff preferably to carry out operation element, and here it is the controls of entire multifunctional universal aircraft to open
The working principle of pass.
It although an embodiment of the present invention has been shown and described, for the ordinary skill in the art, can be with
A variety of variations, modification, replacement can be carried out to these embodiments without departing from the principles and spirit of the present invention by understanding
And modification, the scope of the present invention is defined by the appended.
Claims (10)
1. a kind of multifunctional universal aircraft control switch, including lower console (7) and signal connecting line (19), feature exists
In: lower console (7) the front end middle position is provided with lower control button (8), on lower console (7) the front end left side
The orientation place of setting is provided with the aperture apparatus that amplifies (6), and the aperture apparatus that amplifies (6) is located at lower control button (8) upper left side position, institute
It states middle position on the left of lower console (7) front end to be provided with isosceles triangle control button (9), the isosceles triangle control button (9)
At lower control button (8) leftward position, ball adjusting rod is socketed at interior location on the left of lower console (7) front end
(10), the ball adjusting rod (10) is located at isosceles triangle control button (9) leftward position, and lower console (7) rear end is left
It is provided with spring card pole device (18) at right two side positions, is socketed inside middle position below lower console (7) rear end
Have Switching Power Supply line (17), is provided with middle console (4) at lower console (7) upper end position, before the middle console (4)
It is provided at top position in end No.1 display screen (3), lower position is provided with middle control in middle console (4) front end
Button (5), the middle control button (5) are located at No.1 display screen (3) lower position, middle console (4) the front end upper left
It is provided with lateral adjustments button (2) at the position of side, the lateral adjustments button (2) is located at No.1 display screen (3) leftward position
Locate, is provided with moccasin button (15) at middle console (4) the front end upper right side position, the moccasin button (15) is located at No.1
At display screen (3) upper right side position, trapezoidal control button (11) are provided at middle console (4) the front end lower right position,
The trapezoidal control button (11) is located at middle control button (5) right positions, and the trapezoidal control button (11) is located at moccasin
At button (15) lower right position, hexagonal jack devices (13), institute are socketed at middle console (4) the front end upper right side position
It states hexagonal jack devices (13) to be located at trapezoidal control button (11) top position, the hexagonal jack devices (13) are located at moccasin
At button (15) right positions, vertical adjustment button (12), institute are socketed at interior location on the right side of middle console (4) front end
It states vertical adjustment button (12) to be located at hexagonal jack devices (13) and trapezoidal control button (11) right positions, the middle control
It is provided with spring card pole device (18) at position at left and right sides of platform (4) rear end, the left and right sides above lower console (7) rear end
It is socketed with signal connecting line (19) at the interior location of the left and right sides below at interior location and middle console (4) rear end, it is described
It is provided with console (1) at middle console (4) upper end position, upper console (1) the front end middle position is provided with two
Number display screen (16), be provided at upper console (1) the front end upper left side and front end lower-left side position respectively lateral adjustments by
Button (2), two lateral adjustments buttons (2) are located at No. two display screen (16) leftward positions, upper console (1) front end
It is provided with respectively moccasin button (15) at upper right side and front end bottom right side position, two moccasin buttons (15) are located at No. two and show
At display screen (16) right positions, it is provided with respectively at upper console (1) the front end upper right side and front end bottom right side position two-way
Control button (14), two double-direction control buttons (14) are located at moccasin button (15) right positions, the upper console
(1) it is provided with spring card pole device (18) at position at left and right sides of rear end, below upper console (1) rear end in the left and right sides
Signal connecting line (19) are socketed at the interior location of the left and right sides above at portion position and middle console (4) rear end.
2. a kind of multifunctional universal aircraft control switch according to claim 1, it is characterised in that: the spring card pole
Device (18) include fixed connecting base (181), rounded-rectangular card column (182), be fixedly connected slot (183), adjustable spring (184) and
Anti-off board (185), the fixed connecting base (181) are provided at two sides inside middle position are fixedly connected slot (183) up and down, and two
It is fixedly connected with slot (183) described in a to be provided with adjustable spring (184) towards outer end middle position, two adjustable springs
(184) it is located at and is fixedly connected at slot (183) interior location, two adjustable springs (184) is anti-towards being provided at outer end position
De- plate (185), two anti-off boards (185), which are located at, to be fixedly connected at slot (183) interior location, two anti-off boards
(185) it is provided with rounded-rectangular card column (182) towards outer end middle position, two rounded-rectangular card columns (182) are located at solid
Determine at link slot (183) interior location, the spring card pole device (18) by fixed connecting base (181) respectively with upper console
(1), middle console (4) is fixedly connected with lower console (7).
3. a kind of multifunctional universal aircraft control switch according to claim 1, it is characterised in that: No. two displays
Screen (16) is set as four, and the model of four No. two display screens (16) is set as IS-F15ACP04, and four described No. two aobvious
Display screen (16) is fixedly connected by fixture nut with upper console (1), and four No. two display screens (16) are by display screen and letter
Number line composition.
4. a kind of multifunctional universal aircraft control switch according to claim 1, it is characterised in that: the lateral adjustments
Button (2) is set as three, three lateral adjustments buttons (2) by fixture nut respectively with upper console (1) and middle control
Platform (4) processed is fixedly connected, three lateral adjustments button (2) annulus fixing sleeves, adjust turn-button and signal line group at.
5. a kind of multifunctional universal aircraft control switch according to claim 1, it is characterised in that: the lower control is pressed
Button (8) is by 11 level-one switch buttons, two secondary switch buttons and signal line group at the lower control button (8) passes through
Fixture nut is fixedly connected with lower console (7).
6. a kind of multifunctional universal aircraft control switch according to claim 1, it is characterised in that: the upper console
(1) processor, and the model UCC38500 of processor, upper console (1) length, width are provided with inside middle position
Degree and height decibel are set as 40 centimetres, ten centimetres and 20 centimetres, and the upper console (1) is shaped to I-shaped
Shape.
7. a kind of multifunctional universal aircraft control switch according to claim 1, it is characterised in that: the middle console
(4) processor, and the model UCC38500 of processor, middle console (4) length, width are provided with inside middle position
Degree and height decibel are set as 40 centimetres, ten centimetres and 30 centimetres, and the middle console (4) is shaped to I-shaped
Shape.
8. a kind of multifunctional universal aircraft control switch according to claim 1, it is characterised in that: the lower console
(7) processor, and the model UCC38500 of processor, lower console (7) length, width are provided with inside middle position
Degree and height decibel are set as 40 centimetres, ten centimetres and 20 centimetres, and the lower console (7) is shaped to I-shaped
Shape.
9. a kind of multifunctional universal aircraft control switch according to claim 1, it is characterised in that: the hole dress that amplifies
(6) are set by amplifying hole shield and loudspeaker form, and the model SVF115WR of loudspeaker, the aperture apparatus that amplifies (6) pass through weldering
It connects and is fixedly connected with lower console (7).
10. a kind of multifunctional universal aircraft control switch according to claim 1, it is characterised in that: the ball tune
Pole (10) by ball handle, adjust hand lever, rotary shaft and signal line group at, the ball adjusting rod (10) by rotary shaft with
Lower console (7) rotation is fixedly connected.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910505091.7A CN110371306B (en) | 2019-06-12 | 2019-06-12 | Multifunctional general control switch for airplane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910505091.7A CN110371306B (en) | 2019-06-12 | 2019-06-12 | Multifunctional general control switch for airplane |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN110371306A true CN110371306A (en) | 2019-10-25 |
| CN110371306B CN110371306B (en) | 2023-02-17 |
Family
ID=68250132
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910505091.7A Active CN110371306B (en) | 2019-06-12 | 2019-06-12 | Multifunctional general control switch for airplane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN110371306B (en) |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105292504A (en) * | 2015-11-30 | 2016-02-03 | 中国商用飞机有限责任公司北京民用飞机技术研究中心 | Large-sized passenger plane cockpit multi-screen display control system |
| CN206884942U (en) * | 2017-07-17 | 2018-01-16 | 厦门华联电子股份有限公司 | A kind of mounting structure of vehicle-mounted console device |
| KR101906476B1 (en) * | 2017-07-14 | 2018-10-10 | (주)에이.티.아이 | A control unit for Panic bar of platform screen door |
| CN109361418A (en) * | 2018-08-06 | 2019-02-19 | 江苏理工学院 | A kind of unmanned aerial vehicle communication device |
| CN208621936U (en) * | 2018-07-31 | 2019-03-19 | 上海海梵控制系统有限公司 | A kind of off line controller of DMX512 |
-
2019
- 2019-06-12 CN CN201910505091.7A patent/CN110371306B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105292504A (en) * | 2015-11-30 | 2016-02-03 | 中国商用飞机有限责任公司北京民用飞机技术研究中心 | Large-sized passenger plane cockpit multi-screen display control system |
| KR101906476B1 (en) * | 2017-07-14 | 2018-10-10 | (주)에이.티.아이 | A control unit for Panic bar of platform screen door |
| CN206884942U (en) * | 2017-07-17 | 2018-01-16 | 厦门华联电子股份有限公司 | A kind of mounting structure of vehicle-mounted console device |
| CN208621936U (en) * | 2018-07-31 | 2019-03-19 | 上海海梵控制系统有限公司 | A kind of off line controller of DMX512 |
| CN109361418A (en) * | 2018-08-06 | 2019-02-19 | 江苏理工学院 | A kind of unmanned aerial vehicle communication device |
Also Published As
| Publication number | Publication date |
|---|---|
| CN110371306B (en) | 2023-02-17 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN106500239B (en) | A kind of method that convertible frequency air-conditioner updates EEPROM data | |
| CN102855151B (en) | The optical module firmware not interrupting business is in application upgrade method | |
| US20170307246A1 (en) | Maintenance system and maintenance method of air conditioner | |
| US8171352B2 (en) | HVAC system, a method for determining a source of a reset and a HVAC controller configured for the same | |
| CN100568317C (en) | Control apparatus for airplane synthetic guarantee simulated training system | |
| AU2001290044A1 (en) | Multiple-platform virtual microprocessor architecture and its corresponding operation system, in particular for onboard and mobile computer field | |
| CN103246535B (en) | A kind of upgrade method of mosaic screen upgrade-system | |
| CN111241020B (en) | Serial port switching device and method based on FPGA and storage medium | |
| CN110371306A (en) | A kind of multifunctional universal aircraft control switch | |
| CN105402847A (en) | Backup method for system data and central air conditioning unit adopting backup method | |
| US20050216792A1 (en) | Debug system | |
| EP2985676A1 (en) | Television-and-computer all-in-one machine, method, and computer storage medium for performing remote control on external computer | |
| CN106773789B (en) | Operation and display system of engineering simulator | |
| EP2016352B1 (en) | Remote software loading for refrigerant system | |
| CN208662339U (en) | A kind of horizontal type tube expanding machine | |
| CN214889907U (en) | Wireless channel simulation upper computer display device | |
| CN210201233U (en) | Portable headstock | |
| CN205665467U (en) | Mist elimination control circuit of wireless video reception glasses | |
| CN212851494U (en) | Outdoor multimedia display screen frame | |
| CN110749043A (en) | Air conditioner debugging equipment and method | |
| CN109710350B (en) | Cross-screen status bar implementation method based on Android system | |
| CN218568360U (en) | Low-temperature starting display screen | |
| JP3763669B2 (en) | Turbine controller | |
| CN114330178B (en) | Drive system for debugging and verifying embedded hardware circuit | |
| CN102833935A (en) | Control device for high voltage generator and control system with same |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| TA01 | Transfer of patent application right |
Effective date of registration: 20230202 Address after: 506, Chuangye Building, High-tech Venture Park, No. 18, High-tech Second Road, High-tech Industrial Development Zone, Nanchang, Jiangxi Province, 330000 Applicant after: JIANGXI GUANYI AVIATION Co.,Ltd. Applicant after: Shanghai Guanyi general aircraft Co.,Ltd. Address before: Room 506, venture building, No.18, Gaoxin 2nd Road, Nanchang hi tech Industrial Development Zone, Jiangxi 330000 Applicant before: JIANGXI GUANYI AVIATION Co.,Ltd. |
|
| TA01 | Transfer of patent application right | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant |