CN209617537U - Can independent-lifting operational window aircraft deicing vehicle - Google Patents
Can independent-lifting operational window aircraft deicing vehicle Download PDFInfo
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- CN209617537U CN209617537U CN201920140814.3U CN201920140814U CN209617537U CN 209617537 U CN209617537 U CN 209617537U CN 201920140814 U CN201920140814 U CN 201920140814U CN 209617537 U CN209617537 U CN 209617537U
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Abstract
The utility model relates to airport ground facilities technical fields, specifically refer to it is a kind of can independent-lifting operational window aircraft deicing vehicle, including automobile chassis, auxiliary beam assembly, high-altitude arm mechanism, operational window, waterway control system, hydraulic control system and rotation spraying mechanism, control system is equipped in operational window, auxiliary beam assembly is equipped with revolution of arm mechanism and operational window mechanism, revolution of arm mechanism is equipped with high-altitude arm mechanism, revolution of arm mechanism lower end is connected with auxiliary beam assembly, upper end is hinged with high-altitude arm mechanism, high-altitude arm mechanism includes lower arm, upper arm and lifting fluid cylinder, upper arm is equipped with rotation spraying mechanism, operational window mechanism includes operational window and elevating mechanism, elevating mechanism upper surface is fixedly connected with operational window bottom surface, lower end is fixedly connected with the vehicle frame of automobile chassis, display screen is equipped in operational window, spraying operation handle and aerial boom manipulator Handle, operational window can individually go up and down, greatly reduce work jibs load while guarantee operator's safety and health in the utility model.
Description
Technical field
The utility model relates to airport ground facilities technical field, in particular to it is a kind of can independent-lifting operational window aircraft
Deicing vehicle.
Background technique
Indispensability equipment of the aircraft deicing vehicle as airport ground service, is mainly used for aircraft deicing, anti-icing operation, existing
Aircraft deicing vehicle is generally by automobile chassis, auxiliary beam assembly, housing assembly, generating set, heating boiler, water pump, high altitude operation system
System, big (small) spray gun, liquid case, waterway control system, hydraulic control system, electric control system composition；Auxiliary beam assembly is fixed on
On automobile chassis, for accommodating liquid case, oil pump, the deicing liquid case of waterway control system, deicing liquid heating of hydraulic control system
The components such as device, pipeline, deicing liquid pump, spray gun can be used for spraying deicing liquid or anti-freeze fluid, carry out effective deicing or anti-icing operation；
Chinese patent CN101966833B discloses entitled vehicle chassis using the patent of invention of the aircraft deicing vehicle of wire control technology, has
Line traffic control vehicle chassis, car body, heater with ice liquid removal, deicing liquid pump, air compressor, driver's cabin, vehicle driving operation platform, away from
From alarm, deicing Job Operations panel, distance measuring sensor, fold large arm, telescopic arm, ECU, line traffic control vehicle chassis electric-controlled
Power drive module, steering module and brake module in cell board processed and line traffic control vehicle chassis, it is characterised in that deicing liquid
Heater is mounted on the rear portion of line traffic control vehicle chassis；Deicing liquid pump is mounted on the middle part of line traffic control vehicle chassis；Air
Compressor is mounted on the front of line traffic control vehicle chassis；Pipeline is equipped between heater with ice liquid removal and deicing liquid pump to connect；ECU
It is connected to the electric control unit plate of line traffic control vehicle chassis by data cable, folds large arm and is welded by one with line traffic control vehicle chassis
The pedestal connection connect, folds and connect between large arm and pedestal with rotating shaft mode；Folding is hydraulic drive between large arm and telescopic arm,
It between telescopic arm and folding forearm and is rotating shaft mode connection between folding forearm and support shaft；Driver's cabin chassis is placed in
In support shaft, driver's cabin chassis can horizontally rotate around support shaft, and driver's cabin is fixed with driver's cabin chassis, and cab bottom is equipped with gas
Liquid pipe road combination box is respectively equipped with deicing liquid jet pipe and altitude air jet pipe in air-liquid pipeline combination box, and deicing liquid jet pipe passes through
Special hose is connect with deicing liquid pump；Pressure-air jet pipe is connect also through special hose with air compressor, the line traffic control vehicle
Gas pedal in the power drive module on chassis is connected to accelerator pedal sensor, and accelerator pedal sensor passes through the line traffic control
The electric control unit plate of vehicle chassis and the data line of ECU are connected to engine fuel controller；The line traffic control vehicle chassis
Steering wheel in steering module is connected to torque sensor, and torque sensor passes through the electric control unit plate of line traffic control vehicle chassis
Data line is connected to steering motor, and the brake pedal in the brake module of the line traffic control vehicle chassis is connected to brake pedal sensor,
Brake pedal sensor is connected to wheel braking mechanism, the hair by the data line of the electric control unit plate of line traffic control vehicle chassis
The driving of motivation fuel controller, steering motor and wheel braking mechanism by the line traffic control vehicle chassis electric control unit
Plate and the micro machine of ECU manipulation execute；The front that the driver's cabin is located at the line traffic control vehicle chassis is used as driving driver's cabin, when
When the folding large arm and telescopic arm rise driver's cabin, the driver's cabin is as deicing Job Operations room；Above-mentioned patent
Deficiency is: first is that driver's cabin is located in support shaft in above-mentioned patent, support shaft is being located at folding forearm front end, folds forearm front end
It is big to bear torque, operator is mobile in high-altitude, and operator's health and safety are on the hazard；Second is that in the dedicated deicing liquid of aircraft
Alcohols can voluntarily degrade, but the degradability of additive and inhibitor is poor, pollutes the environment, and some of them alcohols is to human body
Toxic, operator's short distance deicing in above-mentioned patent, deicing liquid is easy to be mapped to operator, jeopardizes operator's peace
Complete and health.
Summary of the invention
Purpose of the utility model is to solve prior art deficiency, a kind of structure novel is provided, operational window can be independent
Go up and down, greatly reduce work jibs load at the same guarantee operator safety with health can independent-lifting operational window aircraft deicing
Vehicle.
To achieve the above object, the technical scheme adopted by the utility model is
It is a kind of can independent-lifting operational window aircraft deicing vehicle, including automobile chassis, auxiliary beam assembly, high-altitude arm mechanism, behaviour
Make cabin, waterway control system, hydraulic control system and rotation spraying mechanism, is equipped with control system, the water in the operational window
Path control system, hydraulic control system are connected to the control system respectively, it is characterised in that: the auxiliary beam assembly is returned equipped with arm
Rotation mechanism and operational window mechanism, revolution of arm mechanism lower end are connected with auxiliary beam assembly, and upper end is hinged with high-altitude arm mechanism,
The high-altitude arm mechanism includes lower arm, upper arm and lifting fluid cylinder, and the upper arm upper end is equipped with rotation spraying mechanism, lower end and lower arm
It is hinged, the lifting fluid cylinder both ends are hinged with upper and lower arms respectively, and the lifting fluid cylinder is connected with hydraulic control system
It connecing, the operational window mechanism includes operational window and elevating mechanism, and the elevating mechanism upper surface is fixedly connected with operational window bottom surface,
Elevating mechanism lower end passes through auxiliary beam assembly and is fixedly connected with the vehicle frame of automobile chassis, and control panel, institute are equipped in the operational window
Control panel is stated equipped with display screen, spraying operation handle and aerial boom operation handle, the elevating mechanism, display screen, sprinkling
Operation handle and aerial boom operation handle are connected to the control system respectively, in favor of operational window to be arranged by elevating mechanism
It on the vehicle frame of automobile chassis, is not in contact with high-altitude arm mechanism, reduces the load of high-altitude arm mechanism, while operational window can pass through
Elevating mechanism is gone up and down by a small margin to obtain big sighting distance, and operator is located in operational window, the rotation with aerial boom device front end
Turn spraying mechanism distance farther out, when such operation, deicing liquid will not be sprayed on the body of operator, ensure that operator's
Personal safety.
Revolution of arm mechanism described in the utility model includes fixed arm support, pivoting support, rotary motor, jacking fluid cylinder and change
Width oil cylinder, fixed arm support lower end are connected through pivoting support with auxiliary beam assembly, and fixed arm support is equipped with aerial boom branch
Frame and jacking fluid cylinder, the pivoting support are driven by the rotary motor being fixed on fixed arm support, the rotary motor and control
System processed is connected, and the aerial boom pedestal lower end is fixedly connected with fixed arm support, high-altitude arm support side and high-altitude
The lower end of arm mechanism is hinged, and the other side is hinged through amplitude oil cylinder and lower arm, and the jacking fluid cylinder is located at high-altitude arm support
Centre, described jacking fluid cylinder one end are connected with fixed arm support, and the other end is hinged with lower arm, the jacking fluid cylinder and luffing
Oil cylinder is connected with hydraulic control system respectively, and the aerial boom device front end is successively arranged video monitoring mechanism, rotation sprinkling
Mechanism and Anti-collision mechanism, the rotation spraying mechanism include spray gun, pipeline, flange and rotation monitor body, the rotation monitor body one
End is fixedly connected with spray gun, and the other end is connected through flange with pipeline upper end, and the pipeline lower end is connected with waterway control system
It connects, the channel sides are connected with high-altitude arm mechanism, the video monitoring mechanism, rotation spraying mechanism and Anti-collision mechanism point
It is not connected to the control system, in favor of passing through the monitoring of video monitoring mechanism, operator checks display screen in operational window,
It adjusts aerial boom operation handle and sprinkling of the spray gun to aircraft surfaces different location can be adjusted in spraying operation handle, and then reach
Remove the effect of aircraft surfaces ice sheet.
Rotation monitor body described in the utility model includes barrel, rotates horizontally component and vertical rotary component, the barrel one
End is fixedly connected with flange, and the other end is connected with spray gun, and the horizontal rotation component and vertical rotary component respectively include back
Trochanter and its casing, rotary joint, casing are respectively arranged on barrel, and casing, which can relatively rotate, to be sheathed on the outside of rotary joint, the rotary joint
Sealing ring and movable ball are installed with casing connection face, rotary joint is machined with worm gear, and worm screw, which is connected to the motor, to connect and fix
In on casing, the motor is connected to the control system, in favor of passing through control motor, to control the horizontal and vertical rotation of barrel
Turn, and then realizes the horizontal and vertical rotation of spray gun.
Elevating mechanism described in the utility model uses Multi-stage hydraulic cylinder or scissors frame mechanism, and the scissors frame mechanism is equipped with liquid
Supporting mechanism is pressed, the Multi-stage hydraulic cylinder lower end or hydraulic support mechanism lower end are connected through sliding rail with the vehicle frame of automobile chassis, liquid
Pressing supporting mechanism can be multistage hydraulic cylinder, be used to support scissors frame mechanism, can select to be arranged according to actual needs.
Balanced valve, the balanced valve are respectively equipped in lifting fluid cylinder described in the utility model, jacking fluid cylinder and amplitude oil cylinder
It is connected to the control system, in favor of promoting cylinder action steady, while in pipe breakage, balanced valve can lock oil cylinder,
Prevent cantilever crane from falling.
Video monitoring mechanism described in the utility model includes at least one camera and camera bracket, the camera warp
It crosses camera bracket to be fixedly connected with upper arm upper end, the camera is connected to the control system, when in favor of passing through camera
When shooting spray gun operating position and aircraft ice sheet situation, camera acquisition information feed back to control system, control system
It is shown by display screen, so that operator checks.
Anti-collision mechanism described in the utility model includes at least one anticollision bracket and anti-bump sensor, the anticollision
Sensor is fixedly connected by anticollision bracket with rotation monitor body, and the anti-collision sensor is connected to the control system, with benefit
In preventing spray gun from encountering aircraft surfaces, aircraft and spray gun are damaged.
Upper arm front end described in the utility model is additionally provided with sprinkling headlamp, and sprinkling headlamp passes through bracket and upper arm front end phase
Connection, the sprinkling headlamp is connected to the control system, can be compared in favor of in the case where bad weather or bad light
The case where seeing aircraft surfaces ice sheet clearly, and then better deicing are understood.
Before operational window described in the utility model and two sides are separately installed with glass, are equipped on the glass of the operational window
Electric wiper is equipped with headlamp before the operational window, and the electric wiper and headlamp are connect with control system, with benefit
It snows or rainy weather in reply, while glass can be further reduced airplane deicing volatilization and drift amount into operational window, into
One step protects operator.
Upper arm described in the utility model is folding retractable arm, so that scene as needed needs to adjust.
The utility model is due to using the above structure, there is structure novel, operational window can individually go up and down, greatly reduce operation
Arm load guarantees the advantages that operator's safety is with health simultaneously.
Detailed description of the invention
Fig. 1 is a kind of structural schematic diagram of the utility model.
Fig. 2 is the main view of Fig. 1 retracted state in the utility model.
Fig. 3 is the top view of Fig. 1 retracted state in the utility model.
Fig. 4 is the structural schematic diagram of operational window in the utility model.
Fig. 5 is enlarged drawing at A in Fig. 1 in the utility model.
Fig. 6 is the enlarged structure schematic diagram that monitor body is rotated in the utility model.
Fig. 7 is the enlarged section main view that monitor body is rotated in the utility model.
Fig. 8 is the enlarged section top view that monitor body is rotated in the utility model.
Specific embodiment
With reference to the accompanying drawing, specific embodiment of the present utility model is described in further detail.
It is a kind of can independent-lifting operational window aircraft deicing vehicle, including automobile chassis 1, auxiliary beam assembly 2, high-altitude arm mechanism 3,
Operational window 4, waterway control system, hydraulic control system and rotation spraying mechanism 5, the operational window is interior to be equipped with control system, control
System processed can be ECU and electrical control unit plate, and the waterway control system, hydraulic control system are connected with control system respectively
It connects, it is characterised in that: the auxiliary beam assembly 2 is equipped with revolution of arm mechanism 9 and operational window mechanism, sets in the revolution of arm mechanism 9
There is high-altitude arm mechanism 3,2 lower end of revolution of arm mechanism is connected with auxiliary beam assembly 2, and upper end is hinged with high-altitude arm mechanism 3, institute
State high-altitude arm mechanism 3 include lower arm 6, upper arm 7 and lifting fluid cylinder 8,7 upper end of upper arm be equipped with rotation spraying mechanism 5, lower end with
Lower arm 6 is hinged, and 8 both ends of lifting fluid cylinder are hinged with upper arm 7 and lower arm 6 respectively, the lifting fluid cylinder 8 and hydraulic control
System processed is connected, and the operational window mechanism includes operational window 4 and elevating mechanism 35,35 upper surface of elevating mechanism and operation
4 bottom surface of cabin is fixedly connected, and elevating mechanism lower end passes through auxiliary beam assembly 2 and is fixedly connected with the vehicle frame of automobile chassis 1, the operational window
Control panel is equipped in 4, control panel is equipped with display screen, spraying operation handle 15 and aerial boom operation handle 16, the liter
Descending mechanism 35, display screen, spraying operation handle 15 and aerial boom operation handle 16 are connected to the control system respectively, in favor of inciting somebody to action
Operational window is arranged on the vehicle frame of automobile chassis by elevating mechanism, is not in contact with high-altitude arm mechanism, reduces aerial boom machine
The load of structure, while operational window can be gone up and down by a small margin by elevating mechanism to obtain big sighting distance, and operator is located at operation
In cabin, farther out with the rotation spraying mechanism distance of aerial boom device front end, when such operation, deicing liquid will not be sprayed onto operator
On the body of member, the personal safety of operator ensure that.
Revolution of arm mechanism 9 described in the utility model includes fixed arm support 10, pivoting support 11, rotary motor, jacking liquid
Cylinder 12 and amplitude oil cylinder 13,10 lower end of fixed arm support are connected through pivoting support 11 with auxiliary beam assembly 2, fixed arm support
10 are equipped with high-altitude arm support 14 and jacking fluid cylinder 12, and the pivoting support 11 is by the revolution horse that is fixed on fixed arm support 10
Up to driving, the rotary motor is connected to the control system, 14 lower end of high-altitude arm support and the fixed company of fixed arm support 10
It connects, 14 side of high-altitude arm support and the lower end of high-altitude arm mechanism 3 are hinged, and the other side is through amplitude oil cylinder 13 and 6 phase of lower arm
Hingedly, the jacking fluid cylinder 12 is located at the centre of high-altitude arm support 14, described 12 one end of jacking fluid cylinder and 10 phase of fixed arm support
Connection, the other end are hinged with lower arm 6, and the jacking fluid cylinder 12 and amplitude oil cylinder 13 are connected with hydraulic control system respectively,
3 front end of high-altitude arm mechanism is successively arranged video monitoring mechanism 17, rotation spraying mechanism 5 and Anti-collision mechanism 18, the rotation
Turning spraying mechanism 5 includes spray gun 19, pipeline, flange and rotation monitor body 20, and described 20 one end of rotation monitor body and spray gun 19 are fixed and connected
It connects, the other end is connected through flange with pipeline upper end, and the pipeline lower end is connected with waterway control system, the channel sides
Be connected with high-altitude arm mechanism 3, the video monitoring mechanism 17, rotation spraying mechanism 5 and Anti-collision mechanism 18 respectively with control
System is connected, and in favor of passing through the monitoring of video monitoring mechanism, operator checks display screen in operational window, adjusts high-altitude
Sprinkling of the spray gun to aircraft surfaces different location can be adjusted in arm operation handle and spraying operation handle, and then reaches removing aircraft
The effect of surface ice sheet.
Rotation monitor body 20 described in the utility model includes barrel 21, rotates horizontally component 22 and vertical rotary component 23, institute
It states 20 one end of barrel to be fixedly connected with flange, the other end is connected with spray gun 19, the horizontal rotation component 22 and vertical rotary
Component 23 respectively includes rotary joint 24 and its casing 25, and rotary joint 24, casing 25 are respectively arranged on barrel 21, and casing 25 opposite can turn
Dynamic to be sheathed on 24 outside of rotary joint, the rotary joint 24 and 25 joint face of casing are equipped with sealing ring 26 and movable ball 27, return
Trochanter 24 is machined with worm gear 28, and worm screw 29 is connected with motor 30 and is fixed on casing 25, the motor 30 and control system
It is connected, in favor of to control the horizontal and vertical rotation of barrel, and then realizing the horizontal and vertical of spray gun by control motor
Rotation.
Elevating mechanism 3 described in the utility model uses Multi-stage hydraulic cylinder or scissors frame mechanism, and the scissors frame mechanism is equipped with
Hydraulic support mechanism, the Multi-stage hydraulic cylinder lower end or hydraulic support mechanism lower end are connected through sliding rail with the vehicle frame of automobile chassis,
Hydraulic support mechanism can be multistage hydraulic cylinder, be used to support scissors frame mechanism, can select to be arranged according to actual needs.
Balanced valve is respectively equipped in lifting fluid cylinder 8 described in the utility model, jacking fluid cylinder 12 and amplitude oil cylinder 13, it is described flat
Weighing apparatus valve is connected to the control system, and in favor of promoting cylinder action steady, while in pipe breakage, balanced valve can lock oil
Cylinder prevents cantilever crane from falling.
Video monitoring mechanism 17 described in the utility model includes at least one camera and camera bracket, the camera
It is fixedly connected by camera bracket with 7 upper end of upper arm, the camera is connected to the control system, in favor of passing through camera
The operating position of spray gun and the ice sheet situation of aircraft are constantly shot, the information of camera acquisition feeds back to control system, control system
System is shown by display screen, so that operator checks.
Anti-collision mechanism 18 described in the utility model includes at least one anticollision bracket and anti-bump sensor, the anti-collision
It hits sensor and is fixedly connected by anticollision bracket with rotation monitor body 20, the anti-collision sensor is connected to the control system,
In favor of preventing spray gun from encountering aircraft surfaces, aircraft and spray gun are damaged.
7 front end of upper arm described in the utility model is additionally provided with sprinkling headlamp 31, and sprinkling headlamp 31 passes through bracket and upper arm
Front end is connected, and the sprinkling headlamp 31 is connected to the control system, in favor of the situation bad in bad weather or light
Under, it can relatively understand the case where seeing aircraft surfaces ice sheet clearly, and then better deicing.
4 front of operational window described in the utility model and two sides are separately installed with glass 32, on the glass 32 of the operational window
Electric wiper 33 is installed, headlamp 34 is installed before the operational window 4, the electric wiper 33 and headlamp 34 with control
System processed connection, so that reply is snowed or rainy weather, while glass can be further reduced airplane deicing volatilization and drift
The amount for entering operational window, further protects operator.
Upper arm 7 described in the utility model is folding retractable arm, so that scene as needed needs to adjust.
Such as attached drawing, when the utility model is used, the utility model is reached deicing scene, stopped vehicle, operator into
Enter operational window, rotary motor, jacking fluid cylinder, amplitude oil cylinder, lifting fluid cylinder are driven by control system, adjust operational window and promotion
The position of arm mechanism, control system can also be controlled using the ECU and electric control unit plate in background technique using PLC
System processed opens display screen, camera, anti-bump sensor by control system after position suitable, rotates monitor body by control
Control spray gun, spray gun is connected by rotating monitor body with the pipeline of waterway control system, waterway control system include deicing liquid case,
The existing building blocks such as heater with ice liquid removal, deicing liquid pump, pipeline, pipeline, which depends on, to be mounted on lower arm and upper arm, water route control
System provides deicing liquid for spray gun, and operator side adjusts spraying operation handle, while check display screen, meanwhile, operational window can also
To be increased as desired by elevating mechanism, the case where more easily watching aircraft surfaces ice sheet in favor of operator, to flying
Machine surface ice sheet carries out deicing liquid sprinkling, at any time according to circumstances adjusts position and the operational window of high-altitude arm mechanism and spray gun
Highly, it is ensured that all ice sheets of aircraft surfaces are sprayed onto, sprayed, high-altitude arm mechanism are recycled, with the prior art
It compares, first is that the rear end of high-altitude arm mechanism is arranged in operational window by the utility model, is provided separately with high-altitude arm mechanism, subtracts significantly
The small load of high-altitude arm mechanism, while having ensured the safety of operator's operation；Second is that sprinkling of the operational window far from front end
Mechanism, operator control spray gun by control system, operation handle, do not need hand-held sprinkling, reduce operator's
Working strength, meanwhile, deicing liquid will not be with splash to operator, and operational window inner periphery is equipped with glass, the alcohol in deicing liquid
Class is diluted by distance between high-altitude arm mechanism and operational window, taste very little, in addition glass barrier, will not hurt operation
Personnel；Third is that operational window can be gone up and down by a small margin by elevating mechanism, biggish sighting distance can be obtained, is more advantageous to observation aircraft table
The ice sheet situation in face.
The utility model is since structure novel, operational window can individually go up and down, greatly reduce work jibs load while guaranteeing to grasp
The advantages that making personnel safety and health.
Claims (10)
1. one kind can independent-lifting operational window aircraft deicing vehicle, including automobile chassis, auxiliary beam assembly, high-altitude arm mechanism, operation
Cabin, waterway control system, hydraulic control system and rotation spraying mechanism, the operational window is interior to be equipped with control system, the water route
Control system, hydraulic control system are connected to the control system respectively, it is characterised in that: the auxiliary beam assembly is equipped with revolution of arm
Mechanism and operational window mechanism, revolution of arm mechanism lower end are connected with auxiliary beam assembly, and upper end is hinged with high-altitude arm mechanism, institute
Stating high-altitude arm mechanism includes lower arm, upper arm and lifting fluid cylinder, and the upper arm upper end is equipped with rotation spraying mechanism, lower end and lower arm phase
Hingedly, the lifting fluid cylinder both ends are hinged with upper and lower arms respectively, and the lifting fluid cylinder is connected with hydraulic control system,
The operational window mechanism includes operational window and elevating mechanism, and the elevating mechanism upper surface is fixedly connected with operational window bottom surface, is risen
Descending mechanism lower end passes through auxiliary beam assembly and is fixedly connected with the vehicle frame of automobile chassis, and control panel is equipped in the operational window, described
Control panel is equipped with display screen, spraying operation handle and aerial boom operation handle, the elevating mechanism, display screen, sprinkling behaviour
Make handle and aerial boom operation handle is connected to the control system respectively.
2. one kind according to claim 1 can independent-lifting operational window aircraft deicing vehicle, it is characterised in that: the arm return
Rotation mechanism includes fixed arm support, pivoting support, rotary motor, jacking fluid cylinder and amplitude oil cylinder, fixed arm support lower end
It is connected through pivoting support with auxiliary beam assembly, fixed arm support is equipped with high-altitude arm support and jacking fluid cylinder, the pivoting support
By the rotary motor driving being fixed on fixed arm support, the rotary motor is connected to the control system, the aerial boom branch
Frame lower end is fixedly connected with fixed arm support, and high-altitude arm support side and the lower end of high-altitude arm mechanism are hinged, the other side
Be hinged through amplitude oil cylinder and lower arm, the jacking fluid cylinder is located at the centre of high-altitude arm support, described jacking fluid cylinder one end with consolidate
Fixed arm support is connected, and the other end is hinged with lower arm, the jacking fluid cylinder and amplitude oil cylinder respectively with hydraulic control system phase
Connection, the aerial boom device front end are successively arranged video monitoring mechanism, rotation spraying mechanism and Anti-collision mechanism, the rotation
Spraying mechanism includes that spray gun, pipeline, flange and rotation monitor body, described rotation monitor body one end are fixedly connected with spray gun, other end warp
Flange is connected with pipeline upper end, and the pipeline lower end is connected with waterway control system, the channel sides and aerial boom machine
Structure is connected, and the video monitoring mechanism, rotation spraying mechanism and Anti-collision mechanism are connected to the control system respectively.
3. one kind according to claim 2 can independent-lifting operational window aircraft deicing vehicle, it is characterised in that: the rotation
Monitor body includes that barrel, horizontal rotation component and vertical rotary component, described barrel one end are fixedly connected with flange, the other end and spray
Rifle is connected, and the horizontal rotation component and vertical rotary component respectively include rotary joint and its casing, rotary joint, casing difference
Set on barrel, casing, which can relatively rotate, to be sheathed on the outside of rotary joint, the rotary joint and casing connection face be equipped with sealing ring and
Movable ball, rotary joint are machined with worm gear, and worm screw, which is connected to the motor, to connect and be fixed on casing, the motor and control system phase
Connection.
4. one kind according to claim 1 or 2 or 3 can independent-lifting operational window aircraft deicing vehicle, it is characterised in that: institute
Stating elevating mechanism is Multi-stage hydraulic cylinder or scissors frame mechanism, and the scissors frame mechanism is equipped with hydraulic support mechanism, the multistage liquid
Cylinder lower end or hydraulic support mechanism lower end are connected through sliding rail with the vehicle frame of automobile chassis, and hydraulic support mechanism is multistage hydraulic
Cylinder.
5. one kind according to claim 2 or 3 can independent-lifting operational window aircraft deicing vehicle, it is characterised in that: it is described
It is respectively equipped with balanced valve in lifting fluid cylinder, jacking fluid cylinder and amplitude oil cylinder, the balanced valve is connected to the control system.
6. one kind according to claim 2 or 3 can independent-lifting operational window aircraft deicing vehicle, it is characterised in that: it is described
Video monitoring mechanism includes at least one camera and camera bracket, and the camera is by camera bracket and upper arm upper end
It is fixedly connected, the camera is connected to the control system.
7. one kind according to claim 6 can independent-lifting operational window aircraft deicing vehicle, it is characterised in that: the anti-collision
The structure that collides includes at least one anticollision bracket and anti-bump sensor, and the anti-collision sensor passes through anticollision bracket and rotation
Monitor body is fixedly connected, and the anti-collision sensor is connected to the control system.
8. one kind according to claim 7 can independent-lifting operational window aircraft deicing vehicle, it is characterised in that: the upper arm
Front end is additionally provided with sprinkling headlamp, and the sprinkling headlamp is connected to the control system.
9. one kind according to claim 8 can independent-lifting operational window aircraft deicing vehicle, it is characterised in that: the operation
Before cabin and two sides are separately installed with glass, and electric wiper is equipped on the glass of the operational window, is pacified before the operational window
Equipped with headlamp, the electric wiper and headlamp are connect with control system.
10. one kind according to claim 9 can independent-lifting operational window aircraft deicing vehicle, it is characterised in that: on described
Arm is folding retractable arm.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920140814.3U CN209617537U (en) | 2019-01-28 | 2019-01-28 | Can independent-lifting operational window aircraft deicing vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920140814.3U CN209617537U (en) | 2019-01-28 | 2019-01-28 | Can independent-lifting operational window aircraft deicing vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209617537U true CN209617537U (en) | 2019-11-12 |
Family
ID=68451995
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201920140814.3U Active CN209617537U (en) | 2019-01-28 | 2019-01-28 | Can independent-lifting operational window aircraft deicing vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209617537U (en) |
-
2019
- 2019-01-28 CN CN201920140814.3U patent/CN209617537U/en active Active
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