CN106477052A - A kind of aircraft rail mounted mechanical arm deicing system - Google Patents
A kind of aircraft rail mounted mechanical arm deicing system Download PDFInfo
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- CN106477052A CN106477052A CN201611131604.5A CN201611131604A CN106477052A CN 106477052 A CN106477052 A CN 106477052A CN 201611131604 A CN201611131604 A CN 201611131604A CN 106477052 A CN106477052 A CN 106477052A
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- deicing
- mechanical arm
- traveling track
- aircraft
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- 238000010438 heat treatment Methods 0.000 claims abstract description 24
- 239000007788 liquid Substances 0.000 claims description 36
- 238000011084 recovery Methods 0.000 claims description 7
- 238000005507 spraying Methods 0.000 claims description 7
- 230000005540 biological transmission Effects 0.000 claims description 3
- 238000000034 method Methods 0.000 abstract description 5
- 230000000694 effects Effects 0.000 abstract description 3
- 230000007246 mechanism Effects 0.000 abstract description 3
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 6
- 239000000203 mixture Substances 0.000 description 5
- 239000000243 solution Substances 0.000 description 5
- 238000005516 engineering process Methods 0.000 description 4
- 238000002347 injection Methods 0.000 description 4
- 239000007924 injection Substances 0.000 description 4
- 230000008901 benefit Effects 0.000 description 3
- 238000010586 diagram Methods 0.000 description 3
- 239000012530 fluid Substances 0.000 description 3
- 238000001802 infusion Methods 0.000 description 3
- 230000008859 change Effects 0.000 description 2
- 238000010276 construction Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 238000012544 monitoring process Methods 0.000 description 2
- 239000000126 substance Substances 0.000 description 2
- 230000015556 catabolic process Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 230000003111 delayed effect Effects 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 230000009977 dual effect Effects 0.000 description 1
- 238000005485 electric heating Methods 0.000 description 1
- 238000001914 filtration Methods 0.000 description 1
- 235000015073 liquid stocks Nutrition 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 238000002156 mixing Methods 0.000 description 1
- 238000012806 monitoring device Methods 0.000 description 1
- 239000007921 spray Substances 0.000 description 1
- 239000011550 stock solution Substances 0.000 description 1
- 238000010257 thawing Methods 0.000 description 1
- 230000007306 turnover Effects 0.000 description 1
- 239000011800 void material Substances 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
- B64D15/00—De-icing or preventing icing on exterior surfaces of aircraft
- B64D15/02—De-icing or preventing icing on exterior surfaces of aircraft by ducted hot gas or liquid
-
- 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
- B64D15/00—De-icing or preventing icing on exterior surfaces of aircraft
- B64D15/02—De-icing or preventing icing on exterior surfaces of aircraft by ducted hot gas or liquid
- B64D15/06—Liquid application
- B64D15/10—Liquid application sprayed over surface
-
- 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
- B64D15/00—De-icing or preventing icing on exterior surfaces of aircraft
- B64D15/12—De-icing or preventing icing on exterior surfaces of aircraft by electric heating
-
- 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
- B64D15/00—De-icing or preventing icing on exterior surfaces of aircraft
- B64D15/16—De-icing or preventing icing on exterior surfaces of aircraft by mechanical means
-
- 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
- B64D15/00—De-icing or preventing icing on exterior surfaces of aircraft
- B64D15/20—Means for detecting icing or initiating de-icing
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Vehicle Cleaning, Maintenance, Repair, Refitting, And Outriggers (AREA)
Abstract
The invention discloses a kind of aircraft rail mounted mechanical arm deicing system, including：Deicing mechanical arm system, front traveling track, rear traveling track and independent storage heating system；Front traveling track and rear traveling track are two tracks, and are arranged at aircraft tip both sides；Deicing mechanical arm system includes：Multi-degree-of-freemechanical mechanical arm, deicing shower nozzle and deicing mechanical arm base；Deicing mechanical arm base is the walking mechanism that all can coordinate with front traveling track and rear traveling track；Multi-degree-of-freemechanical mechanical arm is fixed on deicing mechanical arm base；Deicing shower nozzle is fixed in multi-degree-of-freemechanical mechanical arm；Deicing shower nozzle is provided with video image acquisition unit；The present invention using technique scheme, the multi-degree-of-freemechanical mechanical arm on both sides is walked to correct position by deicing mechanical arm base in front and back, and extend to and need deicing position, carry out de-icing work, video image acquisition unit is monitored feedback operation simultaneously, automatic identification deicing effect, carries out deicing operation again to residual ice.
Description
Technical field
The present invention relates to aircraft deicing field, particularly to a kind of aircraft rail mounted mechanical arm deicing system.
Background technology
At present the big-and-middle-sized airport of China commonly used deicing work pattern have three kinds：A kind of is traditional seat in the plane deicing
Operation；Two kinds are also had to be Concentration De-ice operation and the slow train deicing operation starting in recent years to promote.No matter which kind of deicing operator
Method is required for using deicing vehicle to complete de-icing work.
The aircraft deicing of early stage does not have specialized deicing equipment, is to be stood on ladder or support with hot-water line degree aircraft by people
Collective's icing position is purged.But increasing with body, this deicing mode can not meet requirement, then just produce
Specialized deicing vehicle.At present, existing aircraft deicing vehicle can be divided into self-propelled deicing vehicle, vehicle-mounted by walking manner both at home and abroad
Front hanging type deicing vehicle and three kinds of pulling type deicing vehicle.Self-propelled deicing vehicle is applied the most universal, vehicle-mounted front-hanging type and pulling type
Deicing vehicle typically carries out deicing just for baby plane or to the short position of aircraft.Deicing liquid is loaded deicing vehicle storage by deicing vehicle
In flow container, deicing liquid course of injection is heated to uniform temperature, staff stands in deicing vehicle operation bucket, when being raised to
After certain altitude, around airplane spray deicing liquid.
Because deicing liquid can work the mischief to environment, occur in that a kind of new deicing mode infrared heating side recently again
Formula.Its infrared heater is divided into fixing and moveable two kinds.It is mainly used in the part of the states such as the U.S. and Norway at present
The Newark airport on airport, such as New Jersey, the Rhinelander-Oneida airport of the state of Wisconsin and Norway
Oslo airport employs this technology and carries out deicing to aircraft.Fixing infrared heater is mainly canopy formula heater, by deicing
Canopy, infrared deicing facility, infrared deicing control system composition.Movably infrared heater, is to be arranged on this device to remove
On the support arm of ice machine, so can adjust the distance that infrared heating plate shows to aircraft, so as to wing, empennage and fuselage are each
Part carries out deicing.
Aircraft deicing vehicle mainly includes running gear, aerial platform, heating system and liquid injection system.Walking dress
Put and need to meet chassis low speed walking, good stability carrys out requirement to ensure the high-altitude working safety of operator.Aerial platform master
Working arm to be included, revolving dial, working bucket, hydraulic system and manipulation device etc., for transporting staff and working equipment
Carry out operation to specified altitude assignment.The heater of aircraft deicing vehicle can be divided into two classes：One is circulating-heating mode, and another kind of is to be
Hot type.Commonly used is Instant heating type mode of heating in hgher efficiency both at home and abroad.The clear ice of aircraft deicing vehicle, defrosting are mainly by spraying
Penetrate system to complete.The topmost part of spraying system is control section.
Technique scheme defect is：
1. generally require 2～3 staff during aircraft deicing vehicle work, wherein aerial platform belongs to manned operation
Equipment, it is necessary to possess very high security reliability, improves the dynamicss to deicing vehicle working arm and requires.In vile weather
Under environment, increased artificial aloft work danger coefficient；
2. its vehicle-mounted Large Copacity flow container leads to deicing vehicle bulky and needs running gear and apparatus for work are carried
For dual dynamic source, not only increase layout difficulty, also lead to deicing vehicle construction costs expensive, airport is equipped with deicing vehicle number
Amount is also restrained；
3. spraying system belongs to manual control it is impossible to reflection deicing operation effectiveness is it is difficult to improve deicing efficiency in time；
4. large-scale transport tank car turnover airport by safety check and need to wait guiding vehicle, just can sail for deicing by guiding
Level ground, and the internal strict speed limit in airport, this have impact on deicing working performance to a certain extent；
5. the liquid filling station fluid infusion outside movement area in addition it is also necessary to deicing vehicle is had a meeting as generation tank car breakdown, extends deicing operation
Time, around here aircraft be possible to secondary icing, cause flight be delayed；
6. after deicing operation, deicing liquid is not easily cleaned, and the airplane parking area on airport is polluted.
Content of the invention
The present invention is directed to above-mentioned technical problem, proposes a kind of aircraft rail mounted mechanical arm deicing system.
For reaching object above, it is achieved through the following technical solutions：
Aircraft rail mounted mechanical arm deicing system, including：
Deicing mechanical arm system, front traveling track, rear traveling track, independent storage heating system, reclaim curb and from
Driving wheel keeps off；
Front traveling track is two tracks, is arranged at aircraft tip both sides, covers wing position；
Traveling track is two tracks afterwards, is arranged at aircraft rear end both sides, covers wing position；
Deicing mechanical arm system includes：Multi-degree-of-freemechanical mechanical arm, deicing shower nozzle and deicing mechanical arm base；
Deicing mechanical arm base is the walking mechanism that all can coordinate with front traveling track and rear traveling track；
Multi-degree-of-freemechanical mechanical arm is fixed on deicing mechanical arm base；
Deicing shower nozzle is fixed on multi-degree-of-freemechanical mechanical arm extreme ends；
Deicing shower nozzle is provided with the deicing nozzle for liquid for spraying deicing liquid and the video image for real-time Transmission image
Collecting unit；
Independent storage heating system is arranged at deicing mechanical arm system working region side or underground, and independent storage adds
Hot systems export pipeline is connected with multi-degree-of-freemechanical mechanical arm；
Wherein, front traveling track and rear traveling track close region are provided with the deicing liquid for collecting, converging and guide
Recovery curb；
Deicing mechanical arm system is 4 sets, is provided with a set of deicing after traveling track and two before two on traveling track
Mechanical arm system.
Using the present invention of technique scheme, treat that deicing aircraft is being got in touch with control tower and deicing Operation control room
Afterwards, under commander, flight or towing vehicle are pulled to deicing region, and by automatic wheel shelves, aircraft are fixed on the positioning.
4, both sides multi-degree-of-freemechanical mechanical arm is walked to correct position by deicing mechanical arm base in front and back, and extends to void
Deicing position, carries out de-icing work, and video image acquisition unit is monitored feedback operation simultaneously, automatic identification deicing effect,
Deicing operation again is carried out to residual ice；
The deicing liquid falling from sprinkling fuselage flows into deicing liquid with mixture of ice and water by the recovery curb in deicing region and returns
Receiving apparatus, the series of physical chemical treatment such as filtered, purified and fed, standard compliant deicing liquid is infused by underground
Pump is transmitted back to independent storage heating system, and independent storage heating system deicing liquid will be with giving a warning when finishing, and deicing controls
Personnel can carry out fluid infusion at any time, does not affect de-icing work.
To sum up, the invention has the advantages that：
1. the present invention is advanced in two-orbit using multi-degree-of-freemechanical mechanical arm simultaneously and aircraft is carried out with deicing liquid injection, deicing system
System small volume, no manned work high above the ground, reduce to mechanical arm design requirement, much smaller than deicing vehicle construction costs, can be on airport
Carry out multiposition arrangement.Increase substantially airport deicing efficiency.
2. the present invention need not manually work high above the ground, decrease cost of labor, and greatly reduce in bad weather conditions
Manual work danger coefficient.
3., equipped with video image acquisition real-time monitoring device on deicing nozzle for liquid, residual ice in deicing region can be identified
Positioning and monitoring feedback, can carry out deicing operation more in time.
4. the present invention can be kept away using arrangement underground independence storage system and heater (collection heating and storage conveying integrated)
Exempt from deicing vehicle and repeatedly hurried back and forth to carry out rushing liquid between seat in the plane and liquid filling station, while substantially reducing the deicing activity duration, carried
High work efficiency.
5. deicing region is provided with deicing and reclaims curb simultaneously, and the deicing liquid that aircraft body is fallen is entered with mixture of ice and water
Corresponding retracting device, filtration treatment is delivered to deicing liquid thesauruss and recycles.
6. the present invention is integrated with that mechanical arm duplicate rows enters track, deicing liquid supply, spraying operation, monitoring feedback, deicing liquid returns
It is achieved that " one-stop automatization " deicing operation, equipment and personnel etc. can play several big key elements such as receipts, prosthetic work high above the ground
Go out the advantage of maximum.
Described above is only the general introduction of technical solution of the present invention, in order to better understand the technological means of the present invention,
And can be practiced according to the content of description, and in order to allow the above and other objects, features and advantages of the present invention can
Become apparent, below especially exemplified by preferred embodiment, and coordinate accompanying drawing, describe in detail as follows.
Brief description
The present invention totally 4 width accompanying drawing, wherein：
Fig. 1 is the track laying schematic diagram of the present invention.
Fig. 2 is the total system main structure diagram of the present invention.
Fig. 3 is the structural representation of the deicing mechanical arm system of the present invention.
Fig. 4 is the deicing nozzle structure schematic diagram of the present invention.
In figure：1st, deicing mechanical arm system, 2, front traveling track, 3, rear traveling track, 4, independent storage heating system, 5,
Reclaim curb, 6, automatic catch, 7, multi-degree-of-freemechanical mechanical arm, 8, deicing shower nozzle, 9, deicing mechanical arm base, 10, video figure
As collecting unit, 11, deicing nozzle for liquid.
Specific embodiment
The rail mounted mechanical arm deicing system of aircraft as shown in Figure 1, Figure 2, Figure 3 and Figure 4, including：Deicing mechanical arm system
System 1, front traveling track 2, rear traveling track 3, independent storage heating system 4, recovery curb 5 and automatic catch 6；
Front traveling track 2 is two tracks, is arranged at aircraft tip both sides, covers wing position；
Traveling track 3 is two tracks afterwards, is arranged at aircraft rear end both sides, covers wing position；
Deicing mechanical arm system 1 includes：Multi-degree-of-freemechanical mechanical arm 7, deicing shower nozzle 8 and deicing mechanical arm base 9；
Deicing mechanical arm base 9 is the walking mechanism that all can coordinate with front traveling track 2 and rear traveling track 3；
Multi-degree-of-freemechanical mechanical arm 7 is fixed on deicing mechanical arm base 9；
Deicing shower nozzle 8 is fixed on multi-degree-of-freemechanical mechanical arm 7 extreme ends；
Deicing shower nozzle 8 is provided with the deicing nozzle for liquid 11 for spraying deicing liquid and the video figure for real-time Transmission image
As collecting unit 10；
Independent storage heating system 4 is arranged at deicing mechanical arm system 1 working region side or underground, and independent storage
Heating system 4 export pipeline is connected with multi-degree-of-freemechanical mechanical arm 7；Generally independent storage heating system 4 (is used for melting from collection heating
Change mixture of ice and water, deicing liquid stock solution and water carried out as desired with proportioning and using Electric heating heating), storage is (main
It is the mixing liquid reclaiming), the injection of new deicing liquid, conveying reaches the deicing liquid of concentration standard to each mechanical arm deicing nozzle
Beneath system or overground system that function is integrated；
Wherein, front traveling track 2 and rear traveling track 3 close region are provided with the deicing for collecting, converging and guide
The recovery curb 5 of liquid；
Deicing mechanical arm system 1 is 4 sets, is provided with a set of removing after traveling track 2 and two before two on traveling track 3
Ice mechanical arm system 1.
Using the present invention of technique scheme, treat that deicing aircraft is being got in touch with control tower and deicing Operation control room
Afterwards, under commander, flight or towing vehicle are pulled to deicing region, and by automatic wheel shelves 6, aircraft are fixed on the positioning.
4, both sides multi-degree-of-freemechanical mechanical arm 7 is walked to correct position by deicing mechanical arm base 9 in front and back, and extends to
Empty deicing position, carries out de-icing work, and video image acquisition unit 10 is monitored feedback operation simultaneously, and automatic identification deicing is imitated
Really, deicing operation again is carried out to residual ice；
The deicing liquid falling from sprinkling fuselage flows into deicing liquid with mixture of ice and water by the recovery curb 5 in deicing region and returns
Receiving apparatus, the series of physical chemical treatment such as filtered, purified and fed, standard compliant deicing liquid is infused by underground
Pump is transmitted back to independent storage heating system 4, and independent storage heating system 4 deicing liquid will be with giving a warning when finishing, deicing control
Personnel processed can carry out fluid infusion at any time, does not affect de-icing work.
The above, be only presently preferred embodiments of the present invention, not the present invention is made with any pro forma restriction, though
So the present invention is disclosed above with preferred embodiment, but is not limited to the present invention, any is familiar with this professional technology people
Member, in the range of without departing from technical solution of the present invention, a little change or is modified to when the technology contents of available the disclosure above are made
The Equivalent embodiments of equivalent variations, as long as being the content without departing from technical solution of the present invention, according to the technical spirit pair of the present invention
Any simple modification made for any of the above embodiments, equivalent variations and modification, all still fall within the range of technical solution of the present invention.
Claims (2)
1. aircraft with rail mounted mechanical arm deicing system it is characterised in that include：
Deicing mechanical arm system (1), front traveling track (2), rear traveling track (3), independent storage heating system (4), recovery are led
Stream ditch (5) and automatic catch (6)；
Front traveling track (2) is two tracks, is arranged at aircraft tip both sides；
Traveling track (3) is two tracks afterwards, is arranged at aircraft rear end both sides；
Described deicing mechanical arm system (1) includes：Multi-degree-of-freemechanical mechanical arm (7), deicing shower nozzle (8) and deicing mechanical arm base
(9)；
Described deicing mechanical arm base (9) is the vehicle with walking machine that all can coordinate with front traveling track (2) and rear traveling track (3)
Structure；
Described multi-degree-of-freemechanical mechanical arm (7) is fixed in deicing mechanical arm base (9)；
Described deicing shower nozzle (8) is fixed on multi-degree-of-freemechanical mechanical arm (7) extreme ends；
Described deicing shower nozzle (8) is provided with the deicing nozzle for liquid (11) for spraying deicing liquid and regarding for real-time Transmission image
Frequency image acquisition units (10)；
Described independent storage heating system (4) is arranged at deicing mechanical arm system (1) working region side or underground, and independent
Storage heating system (4) export pipeline is connected with multi-degree-of-freemechanical mechanical arm (7)；
Wherein, front traveling track (2) and rear traveling track (3) close region are provided with the deicing for collecting, converging and guide
The recovery curb (5) of liquid.
2. aircraft according to claim 1 with rail mounted mechanical arm deicing system it is characterised in that：Described deicing mechanical arm
System (1) is 4 sets, is provided with a set of deicing mechanical arm system after traveling track (2) and two before two on traveling track (3)
(1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611131604.5A CN106477052A (en) | 2016-12-09 | 2016-12-09 | A kind of aircraft rail mounted mechanical arm deicing system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611131604.5A CN106477052A (en) | 2016-12-09 | 2016-12-09 | A kind of aircraft rail mounted mechanical arm deicing system |
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| Publication Number | Publication Date |
|---|---|
| CN106477052A true CN106477052A (en) | 2017-03-08 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201611131604.5A Pending CN106477052A (en) | 2016-12-09 | 2016-12-09 | A kind of aircraft rail mounted mechanical arm deicing system |
Country Status (1)
| Country | Link |
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| CN (1) | CN106477052A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107804475A (en) * | 2017-11-03 | 2018-03-16 | 北京首都国际机场股份有限公司 | A kind of airport airborne vehicle slow train de-icing method |
| CN109018375A (en) * | 2018-08-16 | 2018-12-18 | 晨龙飞机（荆门）有限公司 | A kind of intelligent aircraft deicing device of modularization auxiliary heat transfer |
| CN112455718A (en) * | 2020-11-12 | 2021-03-09 | 成都民航六维航化有限责任公司 | Novel spraying operation method and device for airplane deicing fluid |
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Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107804475A (en) * | 2017-11-03 | 2018-03-16 | 北京首都国际机场股份有限公司 | A kind of airport airborne vehicle slow train de-icing method |
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| CN112455718A (en) * | 2020-11-12 | 2021-03-09 | 成都民航六维航化有限责任公司 | Novel spraying operation method and device for airplane deicing fluid |
| CN112455718B (en) * | 2020-11-12 | 2022-07-12 | 成都民航六维航化有限责任公司 | Novel spraying operation method and device for airplane deicing fluid |
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Application publication date: 20170308 |