CN106429647A - Automatic winding and unwinding device of aircraft ground air conditioning air supply hose and control method thereof - Google Patents
Automatic winding and unwinding device of aircraft ground air conditioning air supply hose and control method thereof Download PDFInfo
- Publication number
- CN106429647A CN106429647A CN201610295383.9A CN201610295383A CN106429647A CN 106429647 A CN106429647 A CN 106429647A CN 201610295383 A CN201610295383 A CN 201610295383A CN 106429647 A CN106429647 A CN 106429647A
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- China
- Prior art keywords
- air
- aircraft
- earth surface
- conditioning
- retraction device
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
- B65H—HANDLING THIN OR FILAMENTARY MATERIAL, e.g. SHEETS, WEBS, CABLES
- B65H75/00—Storing webs, tapes, or filamentary material, e.g. on reels
- B65H75/02—Cores, formers, supports, or holders for coiled, wound, or folded material, e.g. reels, spindles, bobbins, cop tubes, cans, mandrels or chucks
- B65H75/34—Cores, formers, supports, or holders for coiled, wound, or folded material, e.g. reels, spindles, bobbins, cop tubes, cans, mandrels or chucks specially adapted or mounted for storing and repeatedly paying-out and re-storing lengths of material provided for particular purposes, e.g. anchored hoses, power cables
- B65H75/38—Cores, formers, supports, or holders for coiled, wound, or folded material, e.g. reels, spindles, bobbins, cop tubes, cans, mandrels or chucks specially adapted or mounted for storing and repeatedly paying-out and re-storing lengths of material provided for particular purposes, e.g. anchored hoses, power cables involving the use of a core or former internal to, and supporting, a stored package of material
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
- B65H—HANDLING THIN OR FILAMENTARY MATERIAL, e.g. SHEETS, WEBS, CABLES
- B65H75/00—Storing webs, tapes, or filamentary material, e.g. on reels
- B65H75/02—Cores, formers, supports, or holders for coiled, wound, or folded material, e.g. reels, spindles, bobbins, cop tubes, cans, mandrels or chucks
- B65H75/34—Cores, formers, supports, or holders for coiled, wound, or folded material, e.g. reels, spindles, bobbins, cop tubes, cans, mandrels or chucks specially adapted or mounted for storing and repeatedly paying-out and re-storing lengths of material provided for particular purposes, e.g. anchored hoses, power cables
- B65H75/38—Cores, formers, supports, or holders for coiled, wound, or folded material, e.g. reels, spindles, bobbins, cop tubes, cans, mandrels or chucks specially adapted or mounted for storing and repeatedly paying-out and re-storing lengths of material provided for particular purposes, e.g. anchored hoses, power cables involving the use of a core or former internal to, and supporting, a stored package of material
- B65H75/44—Constructional details
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
- B65H—HANDLING THIN OR FILAMENTARY MATERIAL, e.g. SHEETS, WEBS, CABLES
- B65H75/00—Storing webs, tapes, or filamentary material, e.g. on reels
- B65H75/02—Cores, formers, supports, or holders for coiled, wound, or folded material, e.g. reels, spindles, bobbins, cop tubes, cans, mandrels or chucks
- B65H75/34—Cores, formers, supports, or holders for coiled, wound, or folded material, e.g. reels, spindles, bobbins, cop tubes, cans, mandrels or chucks specially adapted or mounted for storing and repeatedly paying-out and re-storing lengths of material provided for particular purposes, e.g. anchored hoses, power cables
- B65H75/38—Cores, formers, supports, or holders for coiled, wound, or folded material, e.g. reels, spindles, bobbins, cop tubes, cans, mandrels or chucks specially adapted or mounted for storing and repeatedly paying-out and re-storing lengths of material provided for particular purposes, e.g. anchored hoses, power cables involving the use of a core or former internal to, and supporting, a stored package of material
- B65H75/44—Constructional details
- B65H75/48—Automatic re-storing devices
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
- B65H—HANDLING THIN OR FILAMENTARY MATERIAL, e.g. SHEETS, WEBS, CABLES
- B65H2701/00—Handled material; Storage means
- B65H2701/30—Handled filamentary material
- B65H2701/33—Hollow or hose-like material
Landscapes
- Storing, Repeated Paying-Out, And Re-Storing Of Elongated Articles (AREA)
Abstract
The invention relates to an automatic winding and unwinding device of an aircraft ground air conditioning air supply hose and a control method thereof. The automatic winding and unwinding device comprises an automatic winding and unwinding system, a gallery bridge matching installation system and an automatic winding and unwinding device control system, wherein the automatic winding and unwinding system is connected with the gallery bridge matching installation system, and the automatic winding and unwinding device control system is interlocked with the gallery bridge matching installation system and is used for controlling the automatic winding and unwinding device to wind or unwind the air supply hose. According to the automatic winding and unwinding device, the automatic winding and unwinding control over the air supply hose is intelligently, automatically, accurately, safely and reliably performed by the automatic winding and unwinding device of the air supply hose, and by adopting an intelligent control method, the air supply hose automatically extends when a flight arrives, so that the workload of airport ground crew is reduced; after the flight leaves, the air supply hose is automatically retracted, so that the workload of the airport ground crew is reduced, the working strength is reduced, the working efficiency is improved, and the modern requirements of high intelligent and automatic degree and high working efficiency are satisfied.
Description
Technical field
The present invention relates to aircraft earth surface air-conditioning air supplying hose technical field, particularly a kind of aircraft earth surface air-conditioning air supplying hose
Automatic retraction device and control method thereof.
Background technology
At present existing general aircraft earth surface air-conditioning air supplying hose, its effect is that having of sending aircraft earth surface air-conditioning is certain
Flow, temperature, the fresh air of pressure, be delivered to airframe air-conditioning interface from this air-conditioner air outlet.But such general aircraft
Ground air conditioner air supplying hose, its length is typically from 10 ~ 40 meters, and length is longer, and airduct divides multilayer to sew, heavier-weight, often
Flight reaches and is required to be launched by airport ground workers, needs to be furled by airport ground workers, cause ground when flight leaves
The workload of diligent personnel is big, and working strength is high, inefficiency, does not meets that modern automation degree is more and more higher and operating efficiency
The requirement promoting.
If Fig. 5 is conventional manual airduct folding and unfolding figure, tradition airduct folding and unfolding uses old-fashioned air pipe vehicle to place aircraft floor
Air-conditioning flexible pipe, needs airport ground workers manually to close at airduct in old-fashioned air pipe vehicle, expend great effort and when
Between.
Applicant have submitted utility model patent on May 11st, 2015《A kind of automatic contractive aircraft earth surface air-conditioning send
Wind flexible pipe》, Application No. 201520298746.5.The automatic contractive aircraft earth surface air-conditioning air supplying hose which disclosing,
Including air supplying hose main body, being equipped with retraction cord in described air supplying hose main body, the fixing connection air-supply of described retraction cord one end is soft
Tube body end, the retraction cord other end connects compressive shrinkage machines, and described compressive shrinkage machines action is pullled retraction cord and made air supplying hose main body
Automatically shrink.Owing to retraction cord is easily broken off, and air supplying hose main body contractive effect can be caused not good at contraction process, efficiency
Not high.
Content of the invention
The present invention is directed to the deficiencies in the prior art, provide a kind of operating efficiency convenient aircraft earth surface air-conditioning high, intelligent to send
Wind flexible pipe automatic retraction device and control method thereof.
The purpose of the present invention is achieved by the following technical programs:
A kind of aircraft earth surface air-conditioning air supplying hose automatic retraction device, including the supporting installation system of automatic winding-unwinding system, shelter bridge and
Automatic retraction device control system, described automatic winding-unwinding system installation system supporting with shelter bridge is connected, described automatic retraction device
The control system interlocking supporting installation system of shelter bridge, and control automatic winding-unwinding system folding and unfolding air supplying hose.The present invention ensures to blow soft
Intelligent, automatic, accurate, the safe and reliable execution air supplying hose automatic deploying and retracting control of pipe automatic retraction device requires, uses intelligence
Control method, when flight reaches, it is achieved the automatic extension of air supplying hose, reduces the workload of airport ground workers;At flight
When leaving, it is achieved the automatic contraction of air supplying hose, reduce the workload of airport ground workers, reduce working strength, improve work
Efficiency, meets modern intelligence and the requirement that automaticity is more and more higher and operating efficiency promotes.
Further, described automatic winding-unwinding system includes aircraft floor air supplying hose, places aircraft floor air supplying hose
Airduct cartridge and airduct jack, shell one end of described airduct jack is connected with airduct cartridge, and the other end is pacified
Equipped with airduct arc-shaped transition part, described airduct jack includes multiple draw off gear, described draw off gear include driven gear,
Driven gear rolling bearing, driven gear shaft, folding and unfolding airduct Timing Belt, motor, driving gear, driving gear rolling bearing
With draw off gear side plate;
Described two pieces draw off gear side sheet room spacing is fixed, and driven gear shaft is installed in one end, and driven gear shaft is installed driven tooth
Wheel shaft holds and driven gear, and the other end is connected installation with motor, on motor reel install driving gear rolling bearing and
Driving gear;Described driven gear and driving gear outer surface are provided with folding and unfolding airduct Timing Belt, folding and unfolding airduct Timing Belt
Realize rotating clockwise or counterclockwise under motor-driven;
The inner surface of described folding and unfolding airduct Timing Belt is provided with tongue and groove and engages with driven gear and driving gear, and outer surface is provided with
The convex wear rib that tongue and groove is provided with aircraft earth surface air-conditioning air supplying hose outer surface engages;
Drive driving gear and driven gear to rotate by motor-driven, thus drive folding and unfolding airduct Timing Belt to turn round
Dynamic, by the folding and unfolding airduct convex wear rib of the tongue and groove engagement aircraft air condition air supplying hose outer surface of Timing Belt outer surface,
Drive aircraft earth surface air-conditioning air supplying hose to shrink and extend.
During aircraft earth surface air-conditioning air supplying hose folding and unfolding, airduct arc-shaped transition part is passed through on airduct surface, prevents aircraft floor empty
Adjust air supplying hose and surface abrasion and the situation such as block, it is ensured that automatic retraction device smooth and easy folding and unfolding airduct.
Described automatic winding-unwinding system also includes blast pipe anchor tip and airduct cartridge end plate, and described blast pipe is fixing to be connect
Head and airduct cartridge end plate connection, one end of blast pipe anchor tip is in airduct cartridge inside and send with aircraft earth surface air-conditioning
Wind flexible pipe connects, and the other end is outside airduct cartridge.
Further, the supporting installation system of described shelter bridge includes that connecting bridge, aircraft floor air conditioner group, connecting bridge move vertical
Post and aircraft earth surface air-conditioning air outlet to blast pipe anchor tip delivery hose, described connecting bridge and aircraft floor air conditioner group,
Connecting bridge mobile column connects respectively, and described aircraft floor air conditioner group is fixed to blast pipe by aircraft earth surface air-conditioning air outlet
Joint delivery hose is connected with blast pipe anchor tip.
Described automatic retraction device control system includes electric control box, display operating system, central control system, information
Call prisoners in after letting them out for exercise pipe activate switch, automatic retraction device of input system, aircraft earth surface air-conditioning signal input terminal, automatic retraction device leaks informaton
Pipe activate switch, automatic retraction device pause switch, automatic retraction device emergency stop switch, shelter bridge signal input terminal, motor
Group, shelter bridge signal output terminal and aircraft earth surface air-conditioning signal output terminal,
Described information input system receives the instruction of display operating system and shelter bridge supporting installation system interlocked control, is controlled by central authorities
System processed automatically calculates and exports control instruction, and the motor for controlling automatic winding-unwinding system performs clockwise, turn counterclockwise
Move or stop operating, drive aircraft earth surface air-conditioning air supplying hose to shrink or extend operation, and exporting shelter bridge supporting installation system connection
Lock control instructs.
Further, the control method of described aircraft earth surface air-conditioning air supplying hose automatic retraction device, when display operation
Automatic retraction device in system call prisoners in after letting them out for exercise pipe start switch when, central control system control motor rotate clockwise work
Make, drive aircraft earth surface air-conditioning air supplying hose to shrink operation, meanwhile, to shelter bridge signal output terminal, aircraft earth surface air-conditioning signal
Lead-out terminal output disconnects interlocking signal, forbids shelter bridge and aircraft floor air conditioner group when automatic winding-unwinding system calls prisoners in after letting them out for exercise pipe operation
Start;It is automatically stopped work and tripping automatic retraction device is called prisoners in after letting them out for exercise pipe activate switch after pipe operation of calling prisoners in after letting them out for exercise completes, and to shelter bridge
Signal is connected in signal output terminal output, it is allowed to shelter bridge moves, and disconnects interlocking to the output of aircraft earth surface air-conditioning signal output terminal
Signal, forbids that aircraft floor air conditioner group starts.
Specifically, when the automatic retraction device Snorting tube start switch showing in operating system, control system of central authorities
System control motor rotated counterclockwise work, drives aircraft earth surface air-conditioning air supplying hose to extend operation, meanwhile, defeated to shelter bridge signal
Go out terminal, the output of aircraft earth surface air-conditioning signal output terminal disconnects interlocking signal, forbids that shelter bridge and aircraft floor air conditioner group exist
Automatic winding-unwinding system call prisoners in after letting them out for exercise pipe operation when start;It is automatically stopped work tripping automatic retraction device after Snorting tube operation completes
Snorting tube activate switch, and export cut-off signal to shelter bridge signal output terminal, forbid that shelter bridge moves, to aircraft earth surface air-conditioning letter
Interlocking signal is connected in the output of number lead-out terminal, it is allowed to aircraft floor air conditioner group starts.
When the automatic retraction device pause switch showing in operating system is connected, central control system control motor stops
Only work, meanwhile, exports disconnect interlocking signal to shelter bridge signal output terminal, aircraft earth surface air-conditioning signal output terminal, forbid
Shelter bridge and aircraft floor air conditioner group start when automatic winding-unwinding system Suspend Job;Automatic deploying and retracting in display operating system
When device pause switch disconnects, state operation before suspending pressed by central control system control motor, and to shelter bridge signal output part
Son, aircraft earth surface air-conditioning signal output terminal export interlocking signal before suspending.
When the automatic retraction device emergency stop switch showing in operating system disconnects, central control system control motor stops
Only work, meanwhile, exports disconnect interlocking signal to shelter bridge signal output terminal, aircraft earth surface air-conditioning signal output terminal, forbid
Shelter bridge and aircraft floor air conditioner group start when automatic winding-unwinding system jerk;Automatic retraction device in display operating system
When emergency stop switch is connected, central control system control motor by state operation before jerk, and to shelter bridge signal output terminal, fly
Machine ground air conditioner signal output terminal is by output interlocking signal before jerk.
Described aircraft earth surface air-conditioning signal input terminal accesses aircraft floor air conditioner group interlocking signal line, works as aircraft floor
When signal is connected in the input of AIR COND SIG Air Conditioner Singnal input terminal, all buttons and the automatic retraction device control system of automatic winding-unwinding system are stopped
Only work, when aircraft earth surface air-conditioning signal input terminal input cut-off signal, all buttons of automatic winding-unwinding system and automatically
Draw off gear control system is resumed work.
Further, automatic winding-unwinding system is according to the mounting means of supporting aircraft floor air conditioner group, can use
Bridge hanging type is installed, it would however also be possible to employ ground type is installed.
When aircraft floor air conditioner group uses ground type to install, shelter bridge signal input terminal is not necessarily to wiring, is also not involved in
Control.When aircraft floor air conditioner group uses bridge hanging type to install, shelter bridge signal input terminal accesses shelter bridge interlocking signal line, ginseng
With control.Now, when signal is connected in the input of shelter bridge signal input terminal, all buttons of automatic winding-unwinding system and automatic deploying and retracting
Apparatus control system quits work, when aircraft earth surface air-conditioning signal input terminal input cut-off signal, automatic winding-unwinding system
All buttons and automatic retraction device control system are resumed work.
Compared with prior art, technical solution of the present invention has the advantages that:
The present invention effectively solves general aircraft earth surface air-conditioning air supplying hose flight each time of the prior art and is required to hand
Dynamic expansion and retracting, launch and retracting work causes the workload of airport ground workers big, working strength height, inefficiency etc.
Technical deficiency, automaticity is low, the not enough problem of Based Intelligent Control, uses the control program of the intelligence of innovation, is inputted by information
System receives the instruction of display operating system and shelter bridge and aircraft earth surface air-conditioning interlocked control, automatic by intelligent central control system
Calculating and exporting control instruction, the jack motor for controlling air supplying hose automatic retraction device performs clockwise, inverse
Hour hands rotate or stop operating, and drive aircraft earth surface air-conditioning air supplying hose to shrink or extend operation, and export shelter bridge and aircraft ground
Face air-conditioning interlocked control instruction, it is ensured that what air supplying hose automatic retraction device was intelligent, automatic, accurate, safe and reliable performs air-supply
The control of flexible pipe automatic deploying and retracting requires, the workload of airport ground workers is greatly reduced, and reduces working strength, improves work effect
Rate, meets the requirement that modern automation degree is more and more higher and operating efficiency promotes, has important economy and social effect, value
Must widely popularize.
Brief description
Fig. 1 is the folding and unfolding figure of automatic winding-unwinding system of the present invention;
Fig. 2 is the front view of automatic winding-unwinding system of the present invention;
Fig. 3 is the top view of automatic winding-unwinding system of the present invention;
Fig. 4 is the left view of automatic winding-unwinding system of the present invention;
Fig. 5 is conventional manual airduct folding and unfolding figure;
Fig. 6 is bridge hanging type installation diagram of the present invention;
Fig. 7 is ground type installation diagram of the present invention.
Wherein, the 11st, blast pipe anchor tip the 12nd, airduct cartridge the 13rd, aircraft earth surface air-conditioning air supplying hose the 14th, airduct
Jack shell the 15th, driven gear the 16th, folding and unfolding airduct Timing Belt the 17th, driving gear the 18th, airduct arc-shaped transition part
19th, the 113rd, motor the 110th, driving gear rolling bearing the 111st, airduct cartridge end plate the 112nd, driven gear rolling bearing is received
Put device side plate the 114th, driven gear shaft the 21st, connecting bridge the 22nd, aircraft floor air conditioner group the 23rd, connecting bridge mobile column the 24th,
Old-fashioned air pipe vehicle the 25th, aircraft earth surface air-conditioning air outlet quickly connects to blast pipe anchor tip delivery hose the 26th, air supplying hose
The 27th, airduct jack the 31st, electric control box.
Detailed description of the invention
Being described below in conjunction with principle and feature to the present invention for the accompanying drawing, examples cited are served only for explaining the present invention, this
The protection domain of invention is not limited only to this.
Embodiment 1
A kind of aircraft earth surface air-conditioning air supplying hose automatic retraction device, including the supporting installation system of automatic winding-unwinding system, shelter bridge and
Automatic retraction device control system, described automatic winding-unwinding system installation system supporting with shelter bridge is connected, described automatic retraction device
The control system interlocking supporting installation system of shelter bridge, and control automatic retraction device folding and unfolding air supplying hose.
Such as Fig. 1 ~ 4, described automatic winding-unwinding system includes that the 13rd, aircraft floor air supplying hose places aircraft floor air supplying hose 13
Airduct cartridge 12 and airduct jack 27, described airduct jack shell 14 one end is connected with airduct cartridge 12,
The other end is provided with airduct arc-shaped transition part 18, and described airduct jack 27 includes multiple draw off gear, described draw off gear
Including driven gear the 15th, driven gear rolling bearing the 112nd, driven gear shaft the 114th, folding and unfolding airduct Timing Belt the 16th, motor is the 19th,
Driving gear the 17th, driving gear rolling bearing 110 and draw off gear side plate 113;
Described 113 spacings of two pieces draw off gear side plate are fixed, and driven gear shaft 114 is installed in one end, and driven gear shaft 114 is pacified
Dress driven gear rolling bearing 112 and driven gear 15, the other end is connected installation with motor 19, motor 19 axle is installed main
Moving gear rolling bearing 110 and driving gear 17;Described driven gear 15 and driving gear 17 outer surface are provided with folding and unfolding airduct
With Timing Belt 16, folding and unfolding airduct Timing Belt 16 realizes rotating clockwise or counterclockwise under motor 19 driving;
The inner surface of described folding and unfolding airduct Timing Belt 16 is provided with tongue and groove and engages with driven gear 15 and driving gear 17, appearance
Face is provided with tongue and groove and engages with the convex wear rib that aircraft earth surface air-conditioning air supplying hose 13 outer surface is provided with;
Being driven by motor 19 drives driving gear 17 and driven gear 15 to rotate, thus drives folding and unfolding airduct Timing Belt 16
Carry out back rotation, engage the convex of aircraft air condition air supplying hose 13 outer surface by the tongue and groove of folding and unfolding airduct Timing Belt 16 outer surface
Type wear rib, drives aircraft earth surface air-conditioning air supplying hose 13 shrink and extend.
During aircraft earth surface air-conditioning air supplying hose 13 folding and unfolding, airduct arc-shaped transition part 18 is passed through on airduct surface, prevents aircraft ground
Face air-conditioning flexible pipe 13 and surface abrasion and the situation such as block, it is ensured that airduct jack 27 smooth and easy folding and unfolding airduct.
Described automatic winding-unwinding system also includes blast pipe anchor tip 11 and airduct cartridge end plate 111, described blast pipe
Anchor tip 11 is connected with airduct cartridge end plate 111, and it is internal that one end of blast pipe anchor tip 11 is in airduct cartridge 12
Being connected with aircraft earth surface air-conditioning air supplying hose 13, the other end is outside airduct cartridge 12.Such as Fig. 6, aircraft earth surface air-conditioning is blown
The other end of flexible pipe 13 is provided with air supplying hose snap joint 26.
Such as Fig. 6, the supporting installation system of described shelter bridge includes that connecting bridge the 21st, aircraft floor air conditioner group the 22nd, connecting bridge moves
Column 23 and aircraft earth surface air-conditioning air outlet are to blast pipe anchor tip delivery hose 25, and described connecting bridge 21 is empty with aircraft floor
Adjusting unit the 22nd, connecting bridge mobile column 23 to connect respectively, described aircraft floor air conditioner group 22 passes through aircraft earth surface air-conditioning air-out
Mouth to blast pipe anchor tip delivery hose 25 is connected with blast pipe anchor tip 11.
Described automatic retraction device control system includes that the 31st, electric control box shows operating system, central control system, letter
Breath input system, aircraft earth surface air-conditioning signal input terminal, automatic retraction device are called prisoners in after letting them out for exercise pipe activate switch, automatic retraction device
Snorting tube activate switch, automatic retraction device pause switch, automatic retraction device emergency stop switch, shelter bridge signal input terminal, electricity
Motivation group the 19th, shelter bridge signal output terminal and aircraft earth surface air-conditioning signal output terminal,
Described information input system receives the instruction of display operating system and shelter bridge supporting installation system interlocked control, is controlled by central authorities
System processed automatically calculates and exports control instruction, and the motor 19 for controlling automatic winding-unwinding system performs clockwise, counterclockwise
Rotate or stop operating, driving aircraft earth surface air-conditioning air supplying hose 13 to shrink or extends operation, and exporting supporting installation of shelter bridge and be
System interlocked control instruction.
Further, the control method of described aircraft earth surface air-conditioning air supplying hose automatic retraction device, when display operation
Automatic retraction device in system call prisoners in after letting them out for exercise pipe start switch when, central control system 33 controls motor 19 and rotates clockwise
Work, drives aircraft earth surface air-conditioning air supplying hose 13 to shrink operation, meanwhile, to shelter bridge signal output terminal, aircraft earth surface air-conditioning
Signal output terminal output disconnect interlocking signal, forbid shelter bridge and aircraft floor air conditioner group automatic winding-unwinding system call prisoners in after letting them out for exercise pipe make
Start during industry;It is automatically stopped work and tripping automatic retraction device is called prisoners in after letting them out for exercise pipe activate switch after pipe operation of calling prisoners in after letting them out for exercise completes, and to
Signal is connected in the output of shelter bridge signal output terminal, it is allowed to shelter bridge moves, and disconnects to the output of aircraft earth surface air-conditioning signal output terminal
Interlocking signal, forbids that aircraft floor air conditioner group 22 starts.
Specifically, when the automatic retraction device Snorting tube start switch showing in operating system, control system of central authorities
System control motor 19 rotates counterclockwise work, drives aircraft earth surface air-conditioning air supplying hose 13 to extend operation, meanwhile, to shelter bridge letter
Number lead-out terminal, the output of aircraft earth surface air-conditioning signal output terminal disconnect interlocking signal, forbid shelter bridge and aircraft floor air conditioner
Group starts when automatic winding-unwinding system calls prisoners in after letting them out for exercise pipe operation;It is automatically stopped work tripping automatic deploying and retracting after Snorting tube operation completes
Device Snorting tube activate switch, and export cut-off signal to shelter bridge signal output terminal, forbid that shelter bridge moves, empty to aircraft floor
Signal output terminal output is adjusted to connect interlocking signal, it is allowed to aircraft floor air conditioner group 22 starts.
When the automatic retraction device pause switch showing in operating system is connected, central control system 33 controls motor
Quit work, meanwhile, export disconnect interlocking signal to shelter bridge signal output terminal, aircraft earth surface air-conditioning signal output terminal, prohibit
Only shelter bridge and aircraft floor air conditioner group start when automatic winding-unwinding system Suspend Job;When the automatic receipts in display operating system
When putting the disconnection of device pause switch, central control system control motor 19 is by state operation before time-out and defeated to shelter bridge signal
Go out terminal, aircraft earth surface air-conditioning signal output terminal exports interlocking signal before suspending.
When the automatic retraction device emergency stop switch showing in operating system disconnects, central control system controls motor 19
Quit work, meanwhile, export disconnect interlocking signal to shelter bridge signal output terminal, aircraft earth surface air-conditioning signal output terminal, prohibit
Only shelter bridge and aircraft floor air conditioner group start when automatic winding-unwinding system jerk;When the automatic deploying and retracting dress in display operating system
When putting emergency stop switch connection, state operation before jerk pressed by central control system control motor 19, and to shelter bridge signal output part
Son, aircraft earth surface air-conditioning signal output terminal are by output interlocking signal before jerk.
Described aircraft earth surface air-conditioning signal input terminal accesses aircraft floor air conditioner group interlocking signal line, works as aircraft floor
When signal is connected in the input of AIR COND SIG Air Conditioner Singnal input terminal, all buttons and the automatic retraction device control system of automatic winding-unwinding system are stopped
Only work, when aircraft earth surface air-conditioning signal input terminal input cut-off signal, all buttons of automatic winding-unwinding system and automatically
Draw off gear control system is resumed work.
Further, automatic winding-unwinding system is according to the mounting means of supporting aircraft floor air conditioner group, can use
Bridge hanging type is installed, such as Fig. 6;Also ground type can be used to install, such as Fig. 7.
When aircraft floor air conditioner group 22 uses ground type to install, shelter bridge signal input terminal is not necessarily to wiring, does not also join
With control.When aircraft floor air conditioner group 22 uses bridge hanging type to install, shelter bridge signal input terminal accesses shelter bridge interlocking signal
Line, participates in control.Now, when signal is connected in the input of shelter bridge signal input terminal, all buttons of automatic winding-unwinding system and from
Dynamic draw off gear control system quits work, when aircraft earth surface air-conditioning signal input terminal input cut-off signal, and automatic deploying and retracting
All buttons of system and automatic retraction device control system are resumed work.
Claims (10)
1. an aircraft earth surface air-conditioning air supplying hose automatic retraction device, it is characterised in that include that automatic winding-unwinding system, shelter bridge are joined
Set installation system and automatic retraction device control system, described automatic winding-unwinding system installation system supporting with shelter bridge is connected, described
The automatic retraction device control system interlocking supporting installation system of shelter bridge, and control automatic winding-unwinding system folding and unfolding air supplying hose.
2. aircraft earth surface air-conditioning air supplying hose automatic retraction device according to claim 1, it is characterised in that described automatic receipts
Place system includes aircraft floor air supplying hose, the airduct cartridge placing aircraft floor air supplying hose and airduct jack, institute
The shell one end stating airduct jack is connected with airduct cartridge, and the other end is provided with airduct arc-shaped transition part, described airduct
Jack includes multiple draw off gear, and described draw off gear includes driven gear, driven gear rolling bearing, driven gear
Axle, folding and unfolding airduct Timing Belt, motor, driving gear, driving gear rolling bearing and draw off gear side plate;
Described two pieces draw off gear side sheet room spacing is fixed, and driven gear shaft is installed in one end, and driven gear shaft is installed driven tooth
Wheel shaft holds and driven gear, and the other end is connected installation with motor, on motor reel install driving gear rolling bearing and
Driving gear;Described driven gear and driving gear outer surface are provided with folding and unfolding airduct Timing Belt, folding and unfolding airduct Timing Belt
Realize rotating clockwise or counterclockwise under motor-driven;
The inner surface of described folding and unfolding airduct Timing Belt is provided with tongue and groove and engages with driven gear and driving gear, and outer surface is provided with
The convex wear rib that tongue and groove is provided with aircraft earth surface air-conditioning air supplying hose outer surface engages;
Drive driving gear and driven gear to rotate by motor-driven, thus drive folding and unfolding airduct Timing Belt to turn round
Dynamic, by the folding and unfolding airduct convex wear rib of the tongue and groove engagement aircraft air condition air supplying hose outer surface of Timing Belt outer surface,
Drive aircraft earth surface air-conditioning air supplying hose to shrink and extend.
3. aircraft earth surface air-conditioning air supplying hose automatic retraction device according to claim 1, it is characterised in that described automatic receipts
Place system also includes blast pipe anchor tip and airduct cartridge end plate, described blast pipe anchor tip and airduct cartridge end plate
Connecting, one end of blast pipe anchor tip is in airduct cartridge inside and is connected with aircraft earth surface air-conditioning air supplying hose, the other end
Outside airduct cartridge.
4. aircraft earth surface air-conditioning air supplying hose automatic retraction device according to claim 1 or 3, it is characterised in that described corridor
The supporting installation system of bridge includes connecting bridge, aircraft floor air conditioner group, connecting bridge mobile column and aircraft earth surface air-conditioning air outlet
To blast pipe anchor tip delivery hose, described connecting bridge is connected respectively with aircraft floor air conditioner group, connecting bridge mobile column,
Described aircraft floor air conditioner group is solid with blast pipe by aircraft earth surface air-conditioning air outlet to blast pipe anchor tip delivery hose
Determine joint to connect.
5. aircraft earth surface air-conditioning air supplying hose automatic retraction device according to claim 1, it is characterised in that described automatic receipts
Put apparatus control system and include electric control box, display operating system, central control system, information input system, aircraft floor
AIR COND SIG Air Conditioner Singnal input terminal, automatic retraction device call prisoners in after letting them out for exercise pipe activate switch, automatic retraction device Snorting tube activate switch, automatically receive
Put device pause switch, automatic retraction device emergency stop switch, shelter bridge signal input terminal, motor unit, shelter bridge signal output part
Son and aircraft earth surface air-conditioning signal output terminal,
Described information input system receives the instruction of display operating system and shelter bridge supporting installation system interlocked control, is controlled by central authorities
System processed automatically calculates and exports control instruction, and the motor for controlling automatic winding-unwinding system performs clockwise, turn counterclockwise
Move or stop operating, drive aircraft earth surface air-conditioning air supplying hose to shrink or extend operation, and exporting shelter bridge supporting installation system connection
Lock control instructs.
6. the control method of an aircraft earth surface air-conditioning air supplying hose automatic retraction device, it is characterised in that when display operation is
Automatic retraction device on system call prisoners in after letting them out for exercise pipe start switch when, central control system control motor rotate clockwise work,
Drive aircraft earth surface air-conditioning air supplying hose to shrink operation, export to shelter bridge signal output terminal, aircraft earth surface air-conditioning signal meanwhile
Terminal output disconnects interlocking signal, forbids that shelter bridge and aircraft floor air conditioner group open when automatic winding-unwinding system calls prisoners in after letting them out for exercise pipe operation
Dynamic;It is automatically stopped work and tripping automatic retraction device is called prisoners in after letting them out for exercise pipe activate switch after pipe operation of calling prisoners in after letting them out for exercise completes, and to shelter bridge letter
Signal is connected in the output of number lead-out terminal, it is allowed to shelter bridge moves, and disconnects interlocking letter to the output of aircraft earth surface air-conditioning signal output terminal
Number, forbid that aircraft floor air conditioner group starts.
7. the control method of aircraft earth surface air-conditioning air supplying hose automatic retraction device according to claim 6, it is characterised in that
When the automatic retraction device Snorting tube start switch showing in operating system, central control system controls the motor inverse time
Pin rotation work, drives aircraft earth surface air-conditioning air supplying hose to extend operation, meanwhile, to shelter bridge signal output terminal, aircraft floor
The output of AIR COND SIG Air Conditioner Singnal lead-out terminal disconnects interlocking signal, forbids that shelter bridge and aircraft floor air conditioner group are called prisoners in after letting them out for exercise at automatic winding-unwinding system
Start during pipe operation;It is automatically stopped work tripping automatic retraction device Snorting tube activate switch after Snorting tube operation completes,
And export cut-off signal to shelter bridge signal output terminal, forbid that shelter bridge moves, to the output of aircraft earth surface air-conditioning signal output terminal
Connect interlocking signal, it is allowed to aircraft floor air conditioner group starts.
8. the control method of aircraft earth surface air-conditioning air supplying hose automatic retraction device according to claim 6, it is characterised in that
When the automatic retraction device pause switch showing in operating system is connected, central control system controls motor stall,
Meanwhile, export disconnect interlocking signal to shelter bridge signal output terminal, aircraft earth surface air-conditioning signal output terminal, forbid shelter bridge and fly
Machine ground air conditioner unit starts when automatic winding-unwinding system Suspend Job;When the automatic retraction device in display operating system suspends
When switching off, state operation before suspending pressed by central control system control motor, and to shelter bridge signal output terminal, aircraft ground
Face AIR COND SIG Air Conditioner Singnal lead-out terminal exports interlocking signal before suspending.
9. the control method of aircraft earth surface air-conditioning air supplying hose automatic retraction device according to claim 6, it is characterised in that
When the automatic retraction device emergency stop switch showing in operating system disconnects, central control system controls motor stall,
Meanwhile, export disconnect interlocking signal to shelter bridge signal output terminal, aircraft earth surface air-conditioning signal output terminal, forbid shelter bridge and fly
Machine ground air conditioner unit starts when automatic winding-unwinding system jerk;Automatic retraction device emergency stop switch in display operating system
During connection, central control system control motor is by state operation before jerk and empty to shelter bridge signal output terminal, aircraft floor
Adjust signal output terminal by output interlocking signal before jerk.
10. the control method of aircraft earth surface air-conditioning air supplying hose automatic retraction device according to claim 6, its feature exists
In described aircraft earth surface air-conditioning signal input terminal accesses aircraft floor air conditioner group interlocking signal line, works as aircraft earth surface air-conditioning
When signal is connected in signal input terminal input, all buttons of automatic winding-unwinding system and automatic retraction device control system stop work
Make, when aircraft earth surface air-conditioning signal input terminal input cut-off signal, all buttons of automatic winding-unwinding system and automatic deploying and retracting
Apparatus control system is resumed work.
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Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
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CN112722314A (en) * | 2020-12-18 | 2021-04-30 | 中国民航大学 | Method for constructing microenvironment of airport airplane berth area |
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