CN206312404U - Multifunction aircraft boiler-plate - Google Patents
Multifunction aircraft boiler-plate Download PDFInfo
- Publication number
- CN206312404U CN206312404U CN201621119433.XU CN201621119433U CN206312404U CN 206312404 U CN206312404 U CN 206312404U CN 201621119433 U CN201621119433 U CN 201621119433U CN 206312404 U CN206312404 U CN 206312404U
- Authority
- CN
- China
- Prior art keywords
- underframe
- connecting shaft
- door
- boiler
- oil cylinder
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
Landscapes
- Ship Loading And Unloading (AREA)
Abstract
The utility model discloses a kind of multifunction aircraft boiler-plate,Including nacelle,Lifting mechanism and control device,It is characterized in that the lifting mechanism is by underframe,Lifting drive device and shear shank,The underframe front end center is provided with hydraulic pressure lifting device,Both sides are correspondingly provided with shear shank respectively,The shear shank is by left branching rod,Right pole,Connecting shaft,Upper connecting shaft,Lower connecting shaft composition,The heart channel of Hang-Shaoyin connecting shaft is hinged in left branching rod and right pole in the shear shank,Described left branching rod one end platform is hinged,The other end is rolled through the upper rail that bottom roller and underframe are provided with and is connected,Described right pole one end is hinged with underframe,The other end is rolled with the lower guideway of mesa base through upper roller and is connected,Two upper rollers are connected through upper connecting shaft,Two bottom rollers are connected through lower connecting shaft,The hydraulic pressure lifting device is through control device control,It is novel with structure,The advantages of simulation effect is true to nature.
Description
Technical field
The utility model aircraft simulation equipment technical field, it is specifically a kind of for being docked with airport special vehicle
Multifunction aircraft boiler-plate.
Background technology
For the fast development on China airport, flight is more and more, and the demand of airport special vehicle driver is increasing, but
It is relatively backward now for the training means and method of special vehicle driver, equipment is simpler and cruder, efficiency comparison is low, serious system
The about professional skill and operating efficiency of airport special vehicle driver.With the fast development on airport, for the demand of this product
Can be more and more.For such case, multifunction aircraft boiler-plate is researched and developed.
Through retrieval, it is special that CN101221698B discloses a kind of invention in the plane simulation cabin docked with airport special vehicle
Profit, the boiler-plate is provided with the passenger door and hatch door of unloading goods of passenger plane, another using the design size as prototype in nacelle side
Side is provided with cargo door and conveyer belt hatch door, and whole nacelle is supported by four height-adjustable hydraulic cylinder type cylinders,
The folding of hatch door and the lifting of nacelle have in electric control chamber hydraulic cylinder and magnetic valve to control, and meet special vehicle and aircraft pair
When connecing special training, the need for different type of machines personnel training.Can be carried out to hatch door highly according to the aircraft of different model during training
Adjustment, substantially increase flexibility and the adaptability of boiler-plate, reach training effect very true to nature.So, in training
The practical operation that can just realize nearly all model aircraft with a boiler-plate is trained, but in simulation process, also in the presence of such as
Lower deficiency：First, the hydraulic cylinder support of nacelle lower end four, due to machine error, four hydraulic cylinders can not reach synchronization
Lifting, it is difficult to ensure that balance and stability when causing nacelle to lift；Two is because the base plate in nacelle can not really simulate aircraft goods
The actual shipment process of thing.
Utility model content
The purpose of this utility model is to solve above-mentioned the deficiencies in the prior art, there is provided a kind of structure is novel, simulation effect is forced
Genuine multifunction aircraft boiler-plate.
The utility model solves the technical scheme that its technical problem used：
A kind of multifunction aircraft boiler-plate, including nacelle, lifting mechanism and control device, the nacelle bottom are provided with flat
Platform, the nacelle side is provided with the passenger door and hatch door of unloading goods of passenger plane, cargo door and bulk goods hatch door on opposite side is provided with, its spy
Levy is that the lifting mechanism is that, by underframe, lifting drive device and shear shank, the underframe front end center is provided with hydraulic lifting
Device, both sides are correspondingly provided with shear shank respectively, and the shear shank is by left branching rod, right pole, connecting shaft, upper connecting shaft, lower company
Spindle is constituted, and the heart channel of Hang-Shaoyin connecting shaft is hinged in the left branching rod and right pole in the shear shank, left branching rod one end platform phase
It is hinged, the other end is rolled through the upper rail that bottom roller and underframe are provided with and is connected, and described right pole one end is hinged with underframe, separately
One end rolls with the lower guideway of mesa base through upper roller and is connected, and two upper rollers are connected through upper connecting shaft, two bottom rollers
It is connected through lower connecting shaft, the hydraulic pressure lifting device is beneficial to and is manipulated by device through control device control, makes hydraulic pressure
Lifting device is acted, while supporting nacelle steadily to rise or fall by shear shank, reaches real simulation different model aircraft
The effect of practical operation training.
Lifting power drive device described in the utility model includes cylinder bracket, elevating ram, connects transverse axis, chain, leads
To bar and pulley, the platform front end is provided with hydraulic lifting groove, and the cylinder bracket lower end is fixedly connected with platform, in upper end
The heart is provided with guide post, is respectively provided on two sides with elevating ram, and the guiding bar side wall is provided with guide through hole, and the connection transverse axis is passed through
Guide through hole, one end is vertical with an elevating ram expansion link side wall to be fixedly connected, the flexible bar side of the other end and another elevating ram
Wall is vertically fixedly connected, and the connection transverse axis between the guide post and elevating ram is provided with pulley, and the chain bypasses pulley one
End is fixedly connected with cylinder bracket, and the other end is fixedly connected with the logical groove sidewall of the hydraulic lifting on platform, is beneficial to by lifting
Hydraulic oil cylinder driving, rises or falls the parallel stabilization of chain-driving nacelle.
The utility model can be provided with safety supports, and the underframe rear end is respectively provided on two sides with locating flange, the safety support
Support is made up of the handle of supporting plate and supporting plate side, and described supporting plate one end is provided with locating groove, and the other end is provided with arc
Inverted draw cut, after the nacelle rises to certain altitude, can mutually be blocked by the locating groove of one end of safety supports and locating flange
Connect, the arc inverted draw cut of the other end mutually block with lower connecting shaft and, reach further realize simulation aircraft actual location effect.
The utility model can be provided with cargo transfer base plate, described cargo transfer base plate one end and hatch door of unloading goods in the platform
Corresponding, the other end is vertical with safety screen to be fixedly connected, the cargo transfer base plate be by the parallel roller of an at least row,
And the roller two ends are fixedly connected through bearing with base plate, be beneficial to simulation aircraft platform carries out rolling transportation to goods.
The utility model can be respectively provided on two sides with altitude scale line in the underframe, be beneficial to by the left branch in shear shank
Bar moves horizontally the height that distance is converted into nacelle rising on underframe, reaches the convenient effect of observation.
Control device described in the utility model is made up of Hydraulic Station and electrical system and cable-control box, the underframe
Supporting leg side can be provided with control box bay, and the Hydraulic Station and electrical system control elevating ram, passenger door through control box respectively
On oil cylinder and the oil cylinder of hatch door of unloading goods, upper cargo door on oil cylinder and bulk goods hatch door on oil cylinder, be easy to operator to reach
Hand-held control box is operated in any direction of nacelle, works as end of operation, and control box can be inserted in control box bay, is reached
Easy to operate effect.
The utility model underframe is provided with emergent hand pump, the emergent hand pump control respectively oil cylinder on passenger door and
The oil cylinder on oil cylinder and bulk goods hatch door unloaded goods on the oil cylinder of hatch door, upper cargo door, reaches the effect of safety simulation.
The utility model has the advantages that structure is novel, it is true to nature to simulate effect due to using said structure.
Brief description of the drawings
Fig. 1 is structural representation of the present utility model.
Reference：1. underframe；2. Hydraulic Station and electrical system；3. shear shank；4. lifting mechanism；5. nacelle；6. bulk goods
Hatch door；7. cargo door is gone up；8. meet an urgent need hand pump；9. operating case；10. passenger door；11. unload goods hatch door；12. special purpose vehicle joints；13.
Power control box；14. rollers；15. baffle plates;16. safety supports；Cargo door platform on 17.；18. passenger door platforms；19. cabins
Door cylinder；20. height gauges；21. hand pump rocking bars；22. left branching rods；23. right poles；24. platforms；25 connecting shafts；26. oil cylinders
Support；27. elevating rams；28. connection transverse axis；29. chains；30. guide posts；31. pulleys；32. cargo transfer base plates.
Specific embodiment
The utility model is further illustrated below in conjunction with the accompanying drawings：
As shown in drawings, a kind of multifunction aircraft boiler-plate, including nacelle 5, lifting mechanism and control device, the nacelle
5 bottoms are provided with platform 24, and the front end of the nacelle 5 is provided with special purpose vehicle joint 12, are beneficial to the job process of simulation special purpose vehicle,
The side of the nacelle 5 is provided with the passenger door 10 of passenger plane and unloads goods hatch door 11, cargo door 7 and bulk goods hatch door 6 on opposite side is provided with,
The inwall of the nacelle 5 correspondence passenger door 10 is provided with that passenger door platform 18, the platform of hatch door 11 of unloading goods be corresponding, the correspondence of upper cargo door 7
Upper hatch door platform 17, the corresponding platform of bulk goods hatch door 6, the lifting mechanism 4 are by underframe 1, lift drive device and shear shank 3,
The front end center of the underframe 1 is provided with hydraulic pressure lifting device, and both sides are correspondingly provided with shear shank 3 respectively, and the shear shank 3 is by left branch
Bar 22, right pole 23, connecting shaft 25, upper connecting shaft, lower connecting shaft composition, left branching rod 22 and right pole in the shear shank 3
The heart channel of Hang-Shaoyin connecting shaft 25 is hinged in 23, and one end platform 24 of the left branching rod 22 is hinged, and the other end on bottom roller and underframe 1 through setting
Some upper rails roll connection, and described one end of right pole 23 is hinged with underframe 1, and the other end is through upper roller and the bottom of platform 24
Lower guideway rolls connection, and two upper rollers are connected through upper connecting shaft, and two bottom rollers are connected through lower connecting shaft, the hydraulic pressure
Lifting device is beneficial to and is manipulated by device through control device control, acts hydraulic pressure lifting device, while passing through scissors
Frame support nacelle steadily rises or falls, and reaches the effect of real simulation different model aircraft practical operation training.
Lifting power drive device described in the utility model includes cylinder bracket 26, elevating ram 27, connection transverse axis 28, chain
Bar, guide post 30 and pulley 31, the front end of the platform 24 are provided with hydraulic lifting groove, the lower end of the cylinder bracket 26 and platform 24
It is fixedly connected, upper end center is provided with guide post 30, is respectively provided on two sides with elevating ram 27, the side wall of the guide post 30 is provided with guiding
Through hole, the connection transverse axis 28 pass through guide through hole, one end is vertical with the expansion link of an elevating ram 27 to be fixedly connected, the other end and
The expansion link of another elevating ram 27 is vertically fixedly connected, and the connection transverse axis 28 between the guide post 30 and elevating ram 27 is provided with
Pulley 31, the chain bypasses the one end of pulley 31 and is fixedly connected with cylinder bracket 26, the hydraulic lifting on the other end and platform 24
Logical groove sidewall is fixedly connected, and is beneficial to and is driven by elevating ram, rises or falls the parallel stabilization of chain-driving nacelle 5.
The utility model can be provided with safety supports 16, and the rear end of the underframe 1 is respectively provided on two sides with locating flange and (does not show in figure
Go out), the safety supports 16 are made up of the handle of supporting plate and supporting plate side, and described supporting plate one end is provided with locator card
Groove, the other end is provided with arc inverted draw cut, after the nacelle rises to certain altitude, can be by the locator card of one end of safety supports
Groove and locating flange phase clamping, the arc inverted draw cut of the other end mutually block with lower connecting shaft and, reach further realize simulation aircraft reality
The effect of border positioning.
The utility model can be provided with cargo transfer base plate 32 in the platform 24, and described one end of cargo transfer base plate 32 is with
Cargo door 11 is corresponding, and the other end is vertical with safety screen 15 to be fixedly connected, and the cargo transfer base plate 32 is by an at least row
Parallel roller, and the roller two ends are fixedly connected through bearing with base plate, is beneficial to simulation aircraft container, pallet
Cargo handling process.
The utility model can be respectively provided on two sides with altitude scale line 20 in the underframe 1, and the altitude scale line 20 can be with
Using the concave less than underframe end face, can also be beneficial to and existed by the left branching rod in shear shank using the convex line for protruding from underframe
The distance that moves horizontally on underframe is converted into the corresponding height of different type of machines rising, reaches the convenient effect of observation.
Control device described in the utility model is made up of Hydraulic Station and electrical system and cable-control box, the electric system
The electrical principle of system is same as the prior art, and this is not repeated, and the Hydraulic Station and electrical system 2 are generally arranged at the bottom of underframe 1,
The supporting leg side of the underframe 1 can be provided with control box bay, and the Hydraulic Station and electrical system 2 control to lift respectively through control box 9
The oil cylinder on oil cylinder and bulk goods hatch door on the oil cylinder of oil cylinder and hatch door of unloading goods on oil-lifting jar 27, passenger door, upper cargo door, with
Reach and be easy to the hand-held control box of operator to be operated in any direction of nacelle, work as end of operation, control box can be inserted in control
In box bay processed, the effect of the switch conditions of the adjustable height and hatch door of being easy to observe nacelle is reached.
The utility model underframe is provided with emergent hand pump 8, and the emergent hand pump 8 controls the oil cylinder on passenger door respectively
With the oil cylinder on the oil cylinder and bulk goods hatch door on the oil cylinder of hatch door of unloading goods, upper cargo door, the effect of safety simulation is reached.
The utility model can also be provided with acoustic-optic alarm in nacelle（Not shown in figure）, the acoustic-optic alarm with
Control device is connected.
The utility model connects control device power supply in training, and the power knob on operation operating case opens electrically system
Nacelle is raised to system, the lifting button on operation operating case, height of observation scale the height of correspondence type, by correspondence type
Safety supports are put into shear shank safety supports position, then reduce the arc inverted draw cut that shear shank roller is leaned nacelle safety supports
On, the hatch door button on operating case is then operated, correspondence hatch door is opened, carry out the docking training and interface training of correspondence type.
The utility model can complete to simulate Boeing-737 to control car A380 institutes organic type due to using said structure
Operation, realizes the function of a cabin multi-model, has the advantages that easy to operate, simulation effect true to nature, enhancement training effect and efficiency.
Claims (7)
1. a kind of multifunction aircraft boiler-plate, including nacelle, lifting mechanism and control device, the nacelle bottom are provided with platform,
The nacelle side is provided with the passenger door and unload goods hatch door, cargo door and bulk goods hatch door, its feature on opposite side is provided with of passenger plane
It is that the lifting mechanism is that, by underframe, lifting drive device and shear shank, the underframe front end center is provided with hydraulic lifting dress
Put, both sides are correspondingly provided with shear shank respectively, the shear shank is by left branching rod, right pole, connecting shaft, upper connecting shaft, lower connection
Axle is constituted, and the heart channel of Hang-Shaoyin connecting shaft is hinged in the left branching rod and right pole in the shear shank, and described left branching rod one end platform mutually cuts with scissors
Connect, the other end is rolled through the upper rail that bottom roller and underframe are provided with and is connected, and described right pole one end is hinged with underframe, another
Hold to be rolled with the lower guideway of mesa base through upper roller and be connected, two upper rollers are connected through upper connecting shaft, two bottom roller warps
Lower connecting shaft is connected, and the hydraulic pressure lifting device is through control device control.
2. a kind of multifunction aircraft boiler-plate according to claim 1, it is characterised in that the lifting power drive device
Including cylinder bracket, elevating ram, connection transverse axis, chain, guide post and pulley, the platform front end is provided with hydraulic lifting and leads to
Groove, the cylinder bracket lower end is fixedly connected with platform, and upper end center is provided with guide post, is respectively provided on two sides with elevating ram, institute
State guiding bar side wall and be provided with guide through hole, the connection transverse axis passes through guide through hole, one end and an elevating ram expansion link side wall
Vertically it is fixedly connected, the flexible bar side wall of the other end and another elevating ram is vertical to be fixedly connected, the guide post and elevating ram
Between connection transverse axis be provided with pulley, the chain bypasses pulley one end and is fixedly connected with cylinder bracket, on the other end and platform
The logical groove sidewall of hydraulic lifting be fixedly connected.
3. a kind of multifunction aircraft boiler-plate according to claim 1 and 2, it is characterised in that be provided with safety supports, it is described
Underframe rear end is respectively provided on two sides with locating flange, and the safety supports are made up of the handle of supporting plate and supporting plate side, institute
State supporting plate one end and be provided with locating groove, the other end is provided with arc inverted draw cut, after the nacelle rises to certain altitude, by peace
The locating groove of one end of full support and locating flange phase clamping, the arc inverted draw cut of the other end mutually block with lower connecting shaft and.
4. a kind of multifunction aircraft boiler-plate according to claim 3, it is characterised in that the platform is provided with cargo transfer
Base plate, described cargo transfer base plate one end is corresponding with hatch door of unloading goods, and the other end is vertical with safety screen to be fixedly connected, the goods
Thing transmission base plate is that, by the parallel roller of an at least row, and the roller two ends are fixedly connected through bearing with base plate.
5. a kind of multifunction aircraft boiler-plate according to claim 1 or 4, it is characterised in that the underframe both sides set respectively
There is altitude scale line.
6. a kind of multifunction aircraft boiler-plate according to claim 1, it is characterised in that the control device is by hydraulic pressure
Stand and electrical system and cable-control box composition, the supporting leg side of the underframe can be provided with control box bay, the Hydraulic Station and
Electrical system is controlled on the oil cylinder of the oil cylinder and hatch door of unloading goods on elevating ram, passenger door, upper cargo door respectively through control box
Oil cylinder on oil cylinder and bulk goods hatch door.
7. a kind of multifunction aircraft boiler-plate according to claim 1, it is characterised in that underframe is provided with emergent hand pump,
The emergent hand pump controls the oil cylinder and bulk cargo hold on the oil cylinder of the oil cylinder and hatch door of unloading goods on passenger door, upper cargo door respectively
Oil cylinder on door.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621119433.XU CN206312404U (en) | 2016-10-13 | 2016-10-13 | Multifunction aircraft boiler-plate |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621119433.XU CN206312404U (en) | 2016-10-13 | 2016-10-13 | Multifunction aircraft boiler-plate |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206312404U true CN206312404U (en) | 2017-07-07 |
Family
ID=59242464
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621119433.XU Active CN206312404U (en) | 2016-10-13 | 2016-10-13 | Multifunction aircraft boiler-plate |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206312404U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107274748A (en) * | 2017-08-01 | 2017-10-20 | 中国民航大学 | A kind of aircraft light simulation teching training system |
| CN107862937A (en) * | 2017-12-26 | 2018-03-30 | 大连翼方科技有限公司 | A kind of simulation teching integrated cabin |
| CN110085088A (en) * | 2019-06-05 | 2019-08-02 | 福州高新区玲富科技有限公司 | A kind of airport baby plane seating simulation detection system |
| CN112482484A (en) * | 2020-11-25 | 2021-03-12 | 贵州詹阳动力重工有限公司 | Remote control simulation cabin and remote control system for excavator |
-
2016
- 2016-10-13 CN CN201621119433.XU patent/CN206312404U/en active Active
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107274748A (en) * | 2017-08-01 | 2017-10-20 | 中国民航大学 | A kind of aircraft light simulation teching training system |
| CN107862937A (en) * | 2017-12-26 | 2018-03-30 | 大连翼方科技有限公司 | A kind of simulation teching integrated cabin |
| CN110085088A (en) * | 2019-06-05 | 2019-08-02 | 福州高新区玲富科技有限公司 | A kind of airport baby plane seating simulation detection system |
| CN110085088B (en) * | 2019-06-05 | 2021-01-26 | 南京奔联软件科技有限公司 | Small airplane riding simulation detection system for airport |
| CN112482484A (en) * | 2020-11-25 | 2021-03-12 | 贵州詹阳动力重工有限公司 | Remote control simulation cabin and remote control system for excavator |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN206312404U (en) | Multifunction aircraft boiler-plate | |
| CN106629138B (en) | The application method of the synchronous automatic loading system of whole pile cabinet | |
| CN104355122B (en) | Conveyor of lifting roller machine | |
| CN105905630A (en) | Cargo handling conveying device | |
| CN107639139A (en) | A kind of convenient loading and unloading coiling machine bed | |
| CN205739553U (en) | Cargo handling transporter | |
| CN209161387U (en) | A kind of lifting device of logistics equipment | |
| CN205575133U (en) | From lifting handling device | |
| CN210528372U (en) | Logistics transportation device with electric lifting measures | |
| CN116399533A (en) | Vibration testing device | |
| CN204211152U (en) | A conveyer is rolled in a kind of lifting | |
| CN206375442U (en) | Whole pile casing automatic loading device | |
| CN218465012U (en) | Stacking device in compartment | |
| CN203976291U (en) | Suspension type Copper Foil volume transport trolley | |
| CN205973630U (en) | Multi -functional stacker | |
| CN214011121U (en) | Caterpillar track section magnetic particle inspection equipment | |
| CN205621760U (en) | Solar cell panel reprocesses production line | |
| CN112707157B (en) | Lifting, turning and sample loading device for multi-scale sample with continuously stepless adjustable width and operation method | |
| CN104085826A (en) | Adjustable lifting loading and unloading machine | |
| CN112573425A (en) | Device for rapidly conveying construction materials to high place | |
| CN106379022A (en) | Novel double-decorative panel production equipment | |
| CN220018886U (en) | Vibration testing device | |
| CN212892541U (en) | Double-speed chain lifting translation machine | |
| CN203976216U (en) | A kind of sheet metal hoisting machine | |
| CN217576996U (en) | Adjustable multifunctional drum type rechecking table |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CP03 | Change of name, title or address |
Address after: 264200 No. 301-1, Lianhai Road, Yangting Town, Huancui District, Weihai City, Shandong Province Patentee after: Shandong Guangda Aviation Service Co.,Ltd. Address before: 264200 sunjiatan Industrial Park, Yangting Town, Huancui District, Weihai City, Shandong Province Patentee before: SHANDONG GUANGDA AVIATION GROUND SERVICE CO.,LTD. |
|
| CP03 | Change of name, title or address |