CN106114897A - A kind of slide-type helicopter Intelligent lifting conveying arrangement - Google Patents
A kind of slide-type helicopter Intelligent lifting conveying arrangement Download PDFInfo
- Publication number
- CN106114897A CN106114897A CN201610643686.5A CN201610643686A CN106114897A CN 106114897 A CN106114897 A CN 106114897A CN 201610643686 A CN201610643686 A CN 201610643686A CN 106114897 A CN106114897 A CN 106114897A
- Authority
- CN
- China
- Prior art keywords
- platform
- lifting
- halfpace
- slideway
- 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.)
- Granted
Links
- 230000003028 elevating effect Effects 0.000 claims description 15
- 229910000831 Steel Inorganic materials 0.000 claims description 5
- 238000009826 distribution Methods 0.000 claims description 5
- 239000010959 steel Substances 0.000 claims description 5
- 230000001360 synchronised effect Effects 0.000 claims description 5
- 239000002131 composite material Substances 0.000 claims description 3
- 238000009434 installation Methods 0.000 claims description 3
- 230000001105 regulatory effect Effects 0.000 claims description 3
- 230000000630 rising effect Effects 0.000 claims description 3
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 2
- 239000000956 alloy Substances 0.000 claims description 2
- 229910045601 alloy Inorganic materials 0.000 claims description 2
- 229910052799 carbon Inorganic materials 0.000 claims description 2
- 230000008878 coupling Effects 0.000 claims description 2
- 238000010168 coupling process Methods 0.000 claims description 2
- 238000005859 coupling reaction Methods 0.000 claims description 2
- 230000000694 effects Effects 0.000 claims description 2
- 239000000835 fiber Substances 0.000 claims description 2
- 239000012467 final product Substances 0.000 claims description 2
- 238000003466 welding Methods 0.000 claims 1
- 230000032258 transport Effects 0.000 description 5
- 229920000049 Carbon (fiber) Polymers 0.000 description 1
- 241000209140 Triticum Species 0.000 description 1
- 235000021307 Triticum Nutrition 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 239000004917 carbon fiber Substances 0.000 description 1
- 230000001276 controlling effect Effects 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000000686 essence Substances 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 1
- 238000000034 method Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/22—Ground or aircraft-carrier-deck installations for handling aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/22—Ground or aircraft-carrier-deck installations for handling aircraft
- B64F1/222—Ground or aircraft-carrier-deck installations for handling aircraft for storing aircraft, e.g. in hangars
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Escalators And Moving Walkways (AREA)
Abstract
The present invention relates to a kind of slide-type helicopter Intelligent lifting conveying arrangement, including: stage apparatus, lifting device, halfpace device, driving means, spacing regulator, air cushion；Described stage apparatus includes: platform I, platform II, mobile platform, described platform I and described platform II is symmetrical structure, linked together by described spacing regulator, described lifting device has four sets, is separately mounted on described mobile platform, and described halfpace device lays respectively at described platform I and the middle part of described platform II；Described driving means includes Direct wheel drives and Mecanum wheel, it is achieved the comprehensive automatic walking of described stage apparatus, the impact that the smooth reliable reduction of described air cushion causes；The present invention controls whole device by control system and will be transported to hangar on helicopter automatic lifting to stage apparatus, and leaves hangar after automatically being unloaded by helicopter, has that automatization level is high, simple to operation, save manpower, widely used remarkable advantage.
Description
Technical field
The present invention relates to a kind of slide-type helicopter fuselage to be promoted, transported by stage apparatus and unload
Device, is specifically related to a kind of slide-type helicopter Intelligent lifting conveying arrangement.
Background technology
Helicopter is a class large-sized object, moves complex in unpowered lower artificial transport, and especially slide-type is gone straight up to
Machine, the fuselage bottom employing skid structure of helicopter, rather than roller structure；When after helicopter land, by manpower by helicopter
Transport is complex to hangar.Generally ground crew uses the form pulled, and is drawn in hangar by force by helicopter, but the most both
Body skid is caused damage, also consumes substantial amounts of manpower and materials simultaneously.
Constantly expansion and helicopter along with helicopter market moves the raising of storehouse demand automatically, promotes scientific research personnel continuous
Exploratory development, develop a kind of the full-automatic of slide-type this tailored version helicopter that be applicable to and move storehouse device.The present invention provides one
Kind of slide-type helicopter Intelligent lifting conveying arrangement, has automatic lifting, transports, unloads, moves the function in storehouse, and this apparatus function is complete
Kind, simple to operation, automatization level is high, can be substantially reduced the labor intensity of ground crew.
Summary of the invention
In order to realize foregoing invention purpose, the open a kind of slide-type helicopter Intelligent lifting conveying arrangement of the present invention, have
Automatic lifting, transporting, unload, move the function in storehouse, perfect in shape and function, simple to operation, automatization level is high, greatly reduces ground
The labor intensity of diligent personnel, is widely used.
The technical solution adopted in the present invention is as follows:
A kind of slide-type helicopter Intelligent lifting conveying arrangement, including: stage apparatus, lifting device, halfpace device,
Driving means, spacing regulator；Described stage apparatus includes: platform I, platform II, mobile platform, described platform I and described
Platform II is symmetrical structure, is linked together by described spacing regulator, and described platform I and described platform II uses high-strength
Degree I-steel is welded；Described mobile platform has four sets, and described mobile platform is respectively symmetrically by line slideway and is arranged on institute
State platform I and the two ends of described platform II, often overlap and on described mobile platform, have a cylinder block slideway and two liftings
Frame slideway, with locking device on described line slideway；Described lifting device has four sets, is separately mounted to described mobile platform
On, described lifting device includes: lifting bracket, cylinder block, oil cylinder cylinder rod, and described lifting bracket has three, in 120 ° of distributions
Supporting described cylinder block, the floor installation of described lifting bracket is in described lifting bracket slideway, and described cylinder block is installed
In described cylinder block slideway, described oil cylinder cylinder rod is connected with described cylinder block, and described oil cylinder cylinder rod uses high intensity to close
Jin Gang, the top of described oil cylinder cylinder rod is frustum structure, it is simple to the lifting hole of location fuselage, it is achieved the lifting of fuselage；Regulation institute
State the cylinder block position at described cylinder block slideway, regulate the base of described lifting bracket at described lifting bracket slideway
Position, it is achieved the lateral attitude regulation of described lifting device, regulates described mobile platform described flat by described line slideway
Platform I and the position of described platform II, it is achieved the lengthwise position regulation of described lifting device, regulate the height of described oil cylinder cylinder rod,
Finally realize the lifting of different model slide-type helicopter fuselage；Described halfpace device has two sets, lays respectively at described flat
Platform I and the middle part of described platform II；Described driving means includes Direct wheel drives and Mecanum wheel, described Mecanum wheel totally eight
Set, every two sets are one group and are connected with described Direct wheel drives, and the four described wheats of set are respectively installed in the bottom of described platform I and described platform II
Ke Namu takes turns, it is achieved the comprehensive automatic walking of described stage apparatus.
Further, described halfpace device includes: middle upper mounting plate, shears fork elevating device, lift oil tank, in
Between lower platform；Described middle lower platform is fixed on described stage apparatus, and described middle lower platform leads to described middle upper mounting plate
Crossing described shears fork elevating device to connect, one end of described shears fork elevating device is fixing with described middle upper mounting plate even
Connecing, the other end of described shears fork elevating device is arranged in the slideway of described middle lower platform, and described lift oil tank is fixed
On described middle lower platform, the piston rod of described lift oil tank is fixing with described middle upper mounting plate to be connected, and is hoisted by described
Stretching of cylinder piston rod, coordinates described shears fork elevating device to realize the lifting of described middle upper mounting plate；Described centre
Upper mounting plate is with sensor, when detecting the skid of helicopter, stops rising；The described halfpace device of described platform I
Described halfpace lock is fixed in the side of the described halfpace device that described halfpace lock I, described platform II are fixed in side
II, described halfpace lock I are sealed with described halfpace lock II, and auxiliary realizes being synchronized with the movement of described platform I and platform II；
Have equidistant air cushion groove on described middle upper mounting plate, described air cushion is installed in described air cushion groove；Described air cushion uses carbon fiber
Composite, the inside of described air cushion is distributed equidistant cellosilk and connects the levels of described air cushion, it is achieved described gas during inflation
That pads is smooth, increases its reliability simultaneously, and the end of described air cushion is equipped with rotary knob, opens rotary knob and can automatically fill
Gas, simple to operation；When slide-type helicopter contacts with described middle upper mounting plate, open air cushion described in rotary knob and automatically fill
Gas, after inflation the smooth reliable reduction slide-type helicopter of described air cushion in transportation because jolting to rushing that whole device causes
Hit.
Further, described spacing regulator includes: the fixed leading screw in one end, scalable connecting rod, guide post, electricity
Machine, constant speed gear-box, feed screw nut；Described motor is fixed on the bottom of described platform I one end, and the fixed leading screw in described one end has
Two sets, described feed screw nut has two sets, and two overlap described feed screw nut is fixed on the bottom of described platform II one end, respectively with described
The fixed leading screw in one end coordinates；The output shaft of described motor is connected with the power shaft of constant speed gear-box, two of constant speed gear-box
Output shaft overlaps the fixed leading screw in described one end with two respectively by shaft coupling and is connected, and axle is passed through in fixed leading screw one end, described one end
Bearing is fixed on the bottom of described platform I one end, and one end is connected with the bottom of described platform II one end by described feed screw nut,
Described guide post is connected between described platform I and described platform II；Described electric machine rotation, drives the fixed leading screw in described one end
Rotating, the fixed leading screw in described one end drives described feed screw nut to move, it is achieved the movement of described platform II, thus realizes described
The adjustment of the spacing of platform I and described platform II；Described scalable connecting rod one end is fixed on the end of one end of described platform I
Portion, the other end is flexibly connected with described platform II, and described scalable connecting rod uses Collapsible structure, when described platform I and institute
When stating the spacing adjustment of platform II, described scalable connecting rod realizes guide effect, realizes described platform I and platform II simultaneously
Be synchronized with the movement.
Further, a kind of slide-type helicopter Intelligent lifting conveying arrangement also includes a control system, described control system
System controls coordinated operation between whole device all parts；According to the feature of different model slide-type helicopter fuselage, described control
System processed controls the distance regulation between described platform I and described platform II, makes described platform I and described platform II the most certain
Distance after, scalable connecting rod is retracted to the bottom of described platform I；Described control system controls described driving means and realizes institute
Stating the comprehensive automatic walking of stage apparatus, described control system controls the described stage apparatus machine through slide-type helicopter
Body；Regulate the described cylinder block position at described cylinder block slideway, regulate the base of described lifting bracket at lifting bracket
The position of slideway, makes the top of described oil cylinder cylinder rod withstand in the lifting hole of fuselage, regulates the height of described oil cylinder cylinder rod, it is achieved
The lifting of helicopter fuselage, makes the skid of fuselage depart from ground；Described control system control described platform I and described platform II it
Between distance regulation, make described platform I and described platform II gradually draw close, described cylinder block along described cylinder block slideway to
Two side shiftings；Control described halfpace device to hoist, according to the sensor feedback information of described middle upper mounting plate, work as institute
When stating the skid of middle upper mounting plate contact helicopter, stop hoisting；Reduce the height of the described oil cylinder cylinder rod of described lifting device,
Controlling described halfpace device and carry out back fall, it is sealed that the stable rear described halfpace lock I of time fall and described halfpace lock II,
Described scalable connecting rod is elongated in described platform II；Described control system controls the described Mecanum of described driving means
Wheel all-directional is walked automatically；After being transported to hangar, described halfpace lock I is opened with described halfpace lock II, controls institute
State halfpace device to hoist, regulate the described cylinder block position at described cylinder block slideway, regulate described lifting
The base of support, in the position of lifting bracket slideway, makes the top of described oil cylinder cylinder rod withstand in the lifting hole of fuselage, controls institute
State halfpace device and carry out back fall, control to be gradually disengaged between described platform I and described platform II simultaneously, until helicopter is sliding
Sled completely disengages from described middle upper mounting plate, regulates the height of described oil cylinder cylinder rod, makes the skid of fuselage contact with ground；Finally control
Make whole device and leave hangar.
Implementing one slide-type helicopter Intelligent lifting conveying arrangement of the present invention, it has the beneficial effects that:
(1) one slide-type helicopter Intelligent lifting conveying arrangement of the present invention, has automatic lifting, transports, unloads, moves storehouse
Function, perfect in shape and function, simple to operation, automatization level is high, greatly reduces the labor intensity of ground crew.
(2) according to the feature of the slide-type helicopter fuselage of different model, position and the hoisting depth of lifting device is adjusted,
The regulation spacing of stage apparatus and the lifting altitude of halfpace device, it is achieved full-automatic to different model slide-type helicopter
Intelligent transport, is widely used.
Accompanying drawing explanation
Fig. 1: one slide-type helicopter Intelligent lifting conveying arrangement front view of the present invention；
Fig. 2: one slide-type helicopter Intelligent lifting conveying arrangement right view of the present invention；
Fig. 3: one slide-type helicopter Intelligent lifting conveying arrangement post exercise right view of the present invention.
In figure: 1-stage apparatus, 2-lifting device, 3-halfpace device, 4-Mecanum wheel, 5-spacing adjusts dress
Put, 6-air cushion, 11-platform I, 12-platform II, 13-mobile platform, 14-cylinder block slideway, 15-lifting bracket slideway, 16-
Line slideway, 21-lifting bracket, 22-cylinder block, 23-oil cylinder cylinder rod, upper mounting plate in the middle of 31-, 32-shears fork lowering or hoisting gear,
The fixed leading screw in 33-halfpace lock I, 34-halfpace lock II, 51-one end, the scalable connecting rod of 52-, 53-guide post.
Detailed description of the invention
Below in conjunction with the accompanying drawings the present invention is further described through.
1, as shown in Figure 1, 2, 3, a kind of slide-type helicopter Intelligent lifting conveying arrangement, including: stage apparatus 1, promote
Device 2, halfpace device 3, driving means, spacing regulator 5, air cushion 6；Described stage apparatus includes: platform I11, flat
Platform II12, mobile platform 13, described platform I11 and described platform II12 are symmetrical structure, by described spacing regulator 5 even
Being connected together, described platform I11 and described platform II12 uses high intensity I-steel to be welded；Described mobile platform 13 has four
Set, described mobile platform 13 is respectively symmetrically by line slideway 16 and is arranged on described platform I11 and the two ends of described platform II12,
Often overlap and on described mobile platform 13, have a cylinder block slideway 14 and two lifting bracket slideways 15, described line slideway 16
On with locking device；Described lifting device 2 has four sets, is separately mounted on described mobile platform 13, and described lifting device 2 wraps
Including: lifting bracket 21, cylinder block 22, oil cylinder cylinder rod 23, described lifting bracket 21 has three, supports described oil in 120 ° of distributions
Cylinder cylinder body 22, the floor installation of described lifting bracket 21 is in described lifting bracket slideway 15, and described cylinder block 22 is arranged on
In described cylinder block slideway 14, described oil cylinder cylinder rod 23 is connected with described cylinder block 22, and described oil cylinder cylinder rod 23 uses height
Strength alloys steel, the top of described oil cylinder cylinder rod 23 is frustum structure, it is simple to the lifting hole of location fuselage, it is achieved carrying of fuselage
Rise；Regulate the described cylinder block 22 position at described cylinder block slideway 14, regulate the base of described lifting bracket 21 in institute
State the position of lifting bracket slideway 15, it is achieved the lateral attitude regulation of described lifting device, regulated by described line slideway 16
Described mobile platform 13 is in described platform I11 and the position of described platform II12, it is achieved the lengthwise position of described lifting device is adjusted
Joint, regulates the height of described oil cylinder cylinder rod 23, finally realizes the lifting of different model slide-type helicopter fuselage；Described centre is put down
Table apparatus 3 has two sets, lays respectively at described platform I11 and the middle part of described platform II12；Described driving means includes that taking turns limit drives
Moving and Mecanum wheel 4, described Mecanum wheel 4 totally eight set, every two sets are one group and are connected with described Direct wheel drives, described platform
The four described Mecanum wheels of set 4 are respectively installed in the bottom of I11 and described platform II12, it is achieved described stage apparatus 1 comprehensive from
Dynamic walking；Described halfpace device 3 includes: middle upper mounting plate 31, shears fork elevating device 32, lift oil tank, under centre
Platform；Described middle lower platform is fixed on described stage apparatus 1, and described middle lower platform passes through with described middle upper mounting plate 31
Described shears fork elevating device 32 connects, and one end of described shears fork elevating device 32 is fixed with described middle upper mounting plate 31
Connecting, the other end of described shears fork elevating device 32 is arranged in the slideway of described middle lower platform, described lift oil tank
Being fixed on described middle lower platform, the piston rod of described lift oil tank is fixing with described middle upper mounting plate 31 to be connected, by institute
State the flexible of lift oil tank piston rod, coordinate described shears fork elevating device 32 to realize the liter of described middle upper mounting plate 31
Fall；Described middle upper mounting plate 31 is with sensor, when detecting the skid of helicopter, stops rising；Described platform I11's is described
The side of the described halfpace device 3 of described halfpace lock I, described platform II12 is fixed in the side of halfpace device 3
Fixing described halfpace lock II, described halfpace lock I are sealed with described halfpace lock II, and auxiliary realizes described platform
I11 and platform II12 is synchronized with the movement；Have equidistant air cushion groove on described middle upper mounting plate 31, institute is installed in described air cushion groove
State air cushion 6；Described air cushion 6 uses carbon fibre composite, and the cellosilk that the inside distribution of described air cushion 6 is equidistant connects described gas
The levels of pad 6, it is achieved during inflation, described air cushion 6 is smooth, increases its reliability simultaneously, and the end of described air cushion 6 is equipped with rotation
Turn button, open rotary knob and get final product automatic inflating, simple to operation；Slide-type helicopter connects with described middle upper mounting plate 31
When touching, opening air cushion 6 automatic inflating described in rotary knob, after inflation, the smooth reliable reduction slide-type helicopter of described air cushion 6 exists
Because of the impact that whole device is caused of jolting in transportation.
As shown in Figure 1, 2, 3, the method for work of a kind of slide-type of present invention helicopter Intelligent lifting conveying arrangement specifically walks
Rapid as follows:
According to the feature of different model slide-type helicopter fuselage, described control system controls described platform I11 and described
Distance regulation between platform II12, controls described electric machine rotation, drives the fixed leading screw in described one end 51 to rotate, described one end
Fixed leading screw 51 drives described feed screw nut to move, it is achieved described platform II12 moves, and makes described platform I11 and described platform
After II12 is separated by a distance, scalable connecting rod 52 is retracted to the bottom of described platform I11；Described control system controls institute
Stating driving means and realize the comprehensive automatic walking of described stage apparatus 1, described control system controls described stage apparatus 1 and passes
The fuselage of slide-type helicopter；Regulate the described cylinder block 22 position at described cylinder block slideway 14, regulate described lifting
The base of support 21, in the position of lifting bracket slideway 15, makes the top of described oil cylinder cylinder rod 23 withstand in the lifting hole of fuselage,
Regulate the height of described oil cylinder cylinder rod 23, it is achieved the lifting of helicopter fuselage, make the skid of fuselage depart from ground；Described control is
System controls the distance regulation between described platform I11 and described platform II12, makes described platform I11 and described platform II12 gradually
Draw close, described cylinder block 22 along described cylinder block slideway 14 to two side shiftings；Control described halfpace device 3 to have carried out
Rise, according to the sensor feedback information of described middle upper mounting plate 31, when described middle upper mounting plate 31 contacts the skid of helicopter,
Stopping hoists；Reduce the height of the described oil cylinder cylinder rod 23 of described lifting device 2, control described halfpace device 3 and carry out back
Fall, it is sealed that the stable rear described halfpace lock I of time fall and described halfpace lock II, and described scalable connecting rod 52 is elongated to institute
State in platform II12；Opening air cushion automatic inflating described in rotary knob, smooth reliable reduction of described air cushion after inflation is slided simultaneously
Sled formula helicopter in transportation because of the impact that whole device is caused of jolting；Described control system controls described driving means
The comprehensive automatic walking of described Mecanum wheel 4；After being transported to hangar, by described halfpace lock I and described halfpace
Lock II opens, and controls described halfpace device 3 and hoists, regulates described cylinder block 22 at described cylinder block slideway 14
Position, regulate the base of described lifting bracket 21 in the position of lifting bracket slideway 15, make the top of described oil cylinder cylinder rod 23
Withstand in the lifting hole of fuselage, control described halfpace device 3 and carry out back fall, control described platform I11 and described flat simultaneously
It is gradually disengaged between platform II12, until helicopter skid completely disengages from described middle upper mounting plate 31, regulates described oil cylinder cylinder rod 23
Height, make the skid of fuselage contact with ground；Finally control whole device and leave hangar.
The foregoing is only presently preferred embodiments of the present invention, not in order to limit the present invention, all essences in the present invention
Any amendment, equivalent and the improvement etc. made within god and principle, should be included within the scope of the present invention.
Claims (3)
1. a slide-type helicopter Intelligent lifting conveying arrangement, it is characterised in that including: stage apparatus (1), lifting device
(2), halfpace device (3), driving means, spacing regulator (5), air cushion (6)；Described stage apparatus includes: platform I
(11), platform II (12), mobile platform (13), described platform I (11) and described platform II (12) are symmetrical structure, by described
Spacing regulator (5) links together, described platform I (11) and described platform II (12) use the welding of high intensity I-steel and
Become；Described mobile platform (13) has four sets, described mobile platform (13) be respectively symmetrically by line slideway (16) be arranged on described
Platform I (11) and the two ends of described platform II (12), often overlap and have a cylinder block slideway on described mobile platform (13)
(14) and two lifting bracket slideway (15), with locking device on described line slideway (16)；Described lifting device (2) has four
Set, is separately mounted on described mobile platform (13), and described lifting device (2) including: lifting bracket (21), cylinder block
(22), oil cylinder cylinder rod (23), described lifting bracket (21) has three, supports described cylinder block (22) in 120 ° of distributions, described
The floor installation of lifting bracket (21) is in described lifting bracket slideway (15), and described cylinder block (22) is arranged on described oil cylinder
In cylinder body slideway (14), described oil cylinder cylinder rod (23) is connected with described cylinder block (22), and described oil cylinder cylinder rod (23) uses height
Strength alloys steel, the top of described oil cylinder cylinder rod (23) is frustum structure, it is simple to the lifting hole of location fuselage, it is achieved carrying of fuselage
Rise；Regulate the described cylinder block (22) position described cylinder block slideway (14), regulate the end of described lifting bracket (21)
Seat is in the position of described lifting bracket slideway (15), it is achieved the lateral attitude regulation of described lifting device, is led by described straight line
Rail (16) regulates described mobile platform (13) in described platform I (11) and the position of described platform II (12), it is achieved described lifting
The lengthwise position regulation of device, regulates the height of described oil cylinder cylinder rod (23), finally realizes different model slide-type helicopter machine
The lifting of body；Described halfpace device (3) has two sets, lays respectively in described platform I (11) and described platform II (12)
Portion；Described driving means includes Direct wheel drives and Mecanum wheel (4), described Mecanum wheel (4) totally eight set, and every two sets are one
Group is connected with described Direct wheel drives, and the bottom of described platform I (11) and described platform II (12) is respectively installed the four described Mikes of set and received
Nurse wheel (4), it is achieved the comprehensive automatic walking of described stage apparatus (1)；Described halfpace device (3) including: flat on centre
Platform (31), shears fork elevating device (32), lift oil tank, middle lower platform；Described middle lower platform is fixed on described platform
On device (1), described middle lower platform is connected by described shears fork elevating device (32) with described middle upper mounting plate (31),
One end of described shears fork elevating device (32) is fixing with described middle upper mounting plate (31) to be connected, and described shears fork elevating fills
The other end putting (32) is arranged in the slideway of described middle lower platform, and described lift oil tank is fixed on described middle lower platform
On, the piston rod of described lift oil tank is fixing with described middle upper mounting plate (31) to be connected, by described lift oil tank piston rod
Flexible, coordinate described shears fork elevating device (32) to realize the lifting of described middle upper mounting plate (31)；Put down on described centre
Platform (31) is with sensor, when detecting the skid of helicopter, stops rising；The described halfpace dress of described platform I (11)
Described halfpace lock I is fixed in the side putting (3), and the side of the described halfpace device (3) of described platform II (12) is fixed
Described halfpace lock II, described halfpace lock I are sealed with described halfpace lock II, and auxiliary realizes described platform I (11)
With being synchronized with the movement of platform II (12)；Have equidistant air cushion groove on described middle upper mounting plate (31), install in described air cushion groove
Described air cushion (6)；Described air cushion (6) uses carbon fibre composite, and the cellosilk that the inside distribution of described air cushion (6) is equidistant connects
Connect the levels of described air cushion (6), it is achieved during inflation, described air cushion (6) is smooth, increases its reliability, described air cushion simultaneously
(6) end is equipped with rotary knob, opens rotary knob and gets final product automatic inflating, simple to operation；Slide-type helicopter and institute
When stating middle upper mounting plate (31) contact, opening air cushion described in rotary knob (6) automatic inflating, after inflation, described air cushion (6) is smooth
Reliably reduce slide-type helicopter in transportation because of the impact that whole device is caused of jolting.
2. a kind of slide-type helicopter Intelligent lifting conveying arrangement as claimed in claim 1, it is characterised in that described spacing is adjusted
Engagement positions (5) including: the fixed leading screw in one end (51), scalable connecting rod (52), guide post (53), motor, constant speed gear-box,
Feed screw nut；Described motor is fixed on the bottom of described platform I (11) one end, and there are two sets the fixed leading screw in described one end (51),
Described feed screw nut has two sets, and two overlap described feed screw nut is fixed on the bottom of described platform II (12) one end, respectively with described
The fixed leading screw in one end (51) coordinates；The output shaft of described motor is connected with the power shaft of constant speed gear-box, constant speed gear-box
Two output shafts are connected with the two sets fixed leading screw in described one end (51) respectively by shaft coupling, the fixed leading screw in described one end
(51) one end is fixed on the bottom of described platform I (11) one end by bearing block, and one end is flat with described by described feed screw nut
The bottom of platform II (12) one end is connected, and described guide post (53) is connected between described platform I (11) and described platform II (12)；
Described electric machine rotation, drives the fixed leading screw in described one end (51) to rotate, and the fixed leading screw in described one end (51) drives described silk
Thick stick nut moves, it is achieved the movement of described platform II (12), thus realizes between described platform I (11) and described platform II (12)
The adjustment of distance；Described scalable connecting rod (52) one end is fixed on the bottom of one end of described platform I (11), the other end and institute
Stating platform II (12) to be flexibly connected, described scalable connecting rod (52) uses Collapsible structure, when described platform I (11) and described
When the spacing of platform II (12) adjusts, described scalable connecting rod (52) realizes guide effect, realizes described platform I simultaneously
And being synchronized with the movement of platform II (12) (11).
3. a kind of slide-type helicopter Intelligent lifting conveying arrangement as claimed in claim 2, it is characterised in that also include a control
System processed, described control system controls coordinated operation between whole device all parts；According to different model slide-type helicopter
The feature of fuselage, described control system controls the distance regulation between described platform I (11) and described platform II (12), makes described
After platform I (11) and described platform II (12) is separated by a distance, scalable connecting rod (52) is retracted to described platform I (11)
Bottom；Described control system controls described driving means and realizes the comprehensive automatic walking of described stage apparatus (1), described control
System processed controls the described stage apparatus (1) fuselage through slide-type helicopter；Regulate described cylinder block (22) at described oil
The position of cylinder cylinder body slideway (14), regulates the base of described lifting bracket (21) in the position of lifting bracket slideway (15), makes institute
State in the lifting hole that the top of oil cylinder cylinder rod (23) withstands on fuselage, regulate the height of described oil cylinder cylinder rod (23), it is achieved helicopter
The lifting of fuselage, makes the skid of fuselage depart from ground；Described control system controls described platform I (11) and described platform II (12)
Between distance regulation, make described platform I (11) and described platform II (12) gradually draw close, described cylinder block (22) is along described
Cylinder block slideway (14) is to two side shiftings；Control described halfpace device (3) to hoist, according to described middle upper mounting plate
(31) sensor feedback information, when the skid of described middle upper mounting plate (31) contact helicopter, stops hoisting；Reduce described
The height of the described oil cylinder cylinder rod (23) of lifting device (2), controls described halfpace device (3) and carries out back fall, return fall stable
Rear described halfpace lock I is sealed with described halfpace lock II, and described scalable connecting rod (52) is elongated to described platform II
(12) in；Described control system controls the comprehensive automatic walking of described Mecanum wheel (4) of described driving means；It is transported to machine
Behind storehouse, described halfpace lock I is opened with described halfpace lock II, controls described halfpace device (3) and hoist,
Regulating the described cylinder block (22) position described cylinder block slideway (14), the base regulating described lifting bracket (21) exists
The position of lifting bracket slideway (15), makes the top of described oil cylinder cylinder rod (23) withstand in the lifting hole of fuselage, control described in
Between stage apparatus (3) carry out back fall, control to be gradually disengaged between described platform I (11) and described platform II (12) simultaneously, until
Helicopter skid completely disengages from described middle upper mounting plate (31), regulates the height of described oil cylinder cylinder rod (23), makes the skid of fuselage
Contact with ground；Finally control whole device and leave hangar.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610643686.5A CN106114897B (en) | 2016-08-08 | 2016-08-08 | A kind of slide-type helicopter Intelligent lifting conveying arrangement |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610643686.5A CN106114897B (en) | 2016-08-08 | 2016-08-08 | A kind of slide-type helicopter Intelligent lifting conveying arrangement |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN106114897A true CN106114897A (en) | 2016-11-16 |
| CN106114897B CN106114897B (en) | 2018-04-17 |
Family
ID=57257335
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610643686.5A Active CN106114897B (en) | 2016-08-08 | 2016-08-08 | A kind of slide-type helicopter Intelligent lifting conveying arrangement |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106114897B (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108609197A (en) * | 2018-06-25 | 2018-10-02 | 青岛科技大学 | A kind of ski type helicopter ground omnidirectional mobile device |
| CN109665115A (en) * | 2018-12-29 | 2019-04-23 | 飞智控（天津）科技有限公司 | Helicopter transport system and transportation resources |
| CN110406454A (en) * | 2019-06-29 | 2019-11-05 | 芜湖航翼集成设备有限公司 | Aircraft emergency management and rescue fast removal equipment |
| CN113147560A (en) * | 2021-04-22 | 2021-07-23 | 江阴秋钧机电设备有限公司 | Road transport vehicle for airplane fuselage parts |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH1149490A (en) * | 1997-07-29 | 1999-02-23 | Tamagawa Seiki Co Ltd | Carrying device |
| DE202007006340U1 (en) * | 2006-09-28 | 2007-09-06 | Bünning, Thorsten | Universal tow bar for the helicopter Sea Lynx |
| WO2011030140A1 (en) * | 2009-09-10 | 2011-03-17 | Tlc Handling Ltd | Transport cradle for a skid-supported helicopter |
| US20130062128A1 (en) * | 2011-05-13 | 2013-03-14 | Dan Johnson | Apparatus For Moving Wheeled Loads |
| CN203684118U (en) * | 2013-12-04 | 2014-07-02 | 海丰通航科技有限公司 | Lifting platform for ascending and descending of helicopter |
| CN205931304U (en) * | 2016-08-08 | 2017-02-08 | 青岛科技大学 | Skid formula helicopter intelligence promotes conveyer |
-
2016
- 2016-08-08 CN CN201610643686.5A patent/CN106114897B/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH1149490A (en) * | 1997-07-29 | 1999-02-23 | Tamagawa Seiki Co Ltd | Carrying device |
| DE202007006340U1 (en) * | 2006-09-28 | 2007-09-06 | Bünning, Thorsten | Universal tow bar for the helicopter Sea Lynx |
| WO2011030140A1 (en) * | 2009-09-10 | 2011-03-17 | Tlc Handling Ltd | Transport cradle for a skid-supported helicopter |
| US20130062128A1 (en) * | 2011-05-13 | 2013-03-14 | Dan Johnson | Apparatus For Moving Wheeled Loads |
| CN203684118U (en) * | 2013-12-04 | 2014-07-02 | 海丰通航科技有限公司 | Lifting platform for ascending and descending of helicopter |
| CN205931304U (en) * | 2016-08-08 | 2017-02-08 | 青岛科技大学 | Skid formula helicopter intelligence promotes conveyer |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108609197A (en) * | 2018-06-25 | 2018-10-02 | 青岛科技大学 | A kind of ski type helicopter ground omnidirectional mobile device |
| CN108609197B (en) * | 2018-06-25 | 2023-12-15 | 青岛科技大学 | Skid type helicopter ground omnidirectional moving device |
| CN109665115A (en) * | 2018-12-29 | 2019-04-23 | 飞智控（天津）科技有限公司 | Helicopter transport system and transportation resources |
| CN110406454A (en) * | 2019-06-29 | 2019-11-05 | 芜湖航翼集成设备有限公司 | Aircraft emergency management and rescue fast removal equipment |
| CN110406454B (en) * | 2019-06-29 | 2022-04-01 | 芜湖航翼集成设备有限公司 | Quick carrying equipment for emergency rescue of airplane |
| CN113147560A (en) * | 2021-04-22 | 2021-07-23 | 江阴秋钧机电设备有限公司 | Road transport vehicle for airplane fuselage parts |
| CN113147560B (en) * | 2021-04-22 | 2022-05-20 | 江阴秋钧机电设备有限公司 | Road transport vehicle for airplane fuselage parts |
Also Published As
| Publication number | Publication date |
|---|---|
| CN106114897B (en) | 2018-04-17 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN106114897A (en) | A kind of slide-type helicopter Intelligent lifting conveying arrangement | |
| CN106394711B (en) | A kind of toter based on gravity center adjusting mechanism | |
| CN104310009B (en) | A kind of charging and discharging mechanism | |
| CN105668383B (en) | A kind of adjustable double-deck large-tonnage lift car of car height and adjusting method | |
| CN103144975B (en) | Pipe loading-unloading machine | |
| CN205840820U (en) | Fluid cylinder direct-drive type dynamic catwalk | |
| CN205931304U (en) | Skid formula helicopter intelligence promotes conveyer | |
| CN205312915U (en) | Double -beam portal crane | |
| CN208485176U (en) | A kind of adjustable climbing conveyer | |
| CN104163340B (en) | Mobile loader | |
| CN206187142U (en) | Carrying device based on focus adjustment mechanism | |
| CN106143943A (en) | A kind of tailored version helicopter automatically moves storehouse device | |
| CN109436056A (en) | A kind of liftable logistics device | |
| CN205417709U (en) | From uninstallation handling trolley | |
| JP2010269870A (en) | Elevating/lowering device and method for controlling the same | |
| CN105217413B (en) | Become the oblique operation container self-level(l)ing device of the gradient and method | |
| CN205931303U (en) | Full -automatic storehouse device that moves of tailored version helicopter | |
| CN104495277B (en) | A kind of central hydraulic lowering or hoisting gear and the hydraulic pressure transportation system using the device | |
| CN206278594U (en) | A kind of intelligent mobile instrument with lift and conveyer structure | |
| CN204161996U (en) | A kind of charging and discharging mechanism | |
| CN207105230U (en) | The walking blank truck device of high-pressure forming machine | |
| CN106477452B (en) | A kind of raising beam mechanism of elevator for the laying of tunnel inner cable | |
| CN101249892A (en) | Boarding moving staircase | |
| CN208006827U (en) | A kind of vehicle dragging system, ray detection system and its vehicle drag trolley | |
| CN108407704A (en) | Vehicle dragging system, ray detection system and its vehicle drag trolley |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20231114 Address after: 1337, 13th Floor, Building 2, No. 38 Kechuangwu Street, Beijing Economic and Technological Development Zone, Daxing District, Beijing, 100000 (Yizhuang Cluster, High end Industrial Zone, Beijing Pilot Free Trade Zone) Patentee after: Beifei Blueprint (Beijing) Aeronautical Engineering Technology Research Institute Co.,Ltd. Address before: 230000 floor 1, building 2, phase I, e-commerce Park, Jinggang Road, Shushan Economic Development Zone, Hefei City, Anhui Province Patentee before: Dragon totem Technology (Hefei) Co.,Ltd. Effective date of registration: 20231114 Address after: 230000 floor 1, building 2, phase I, e-commerce Park, Jinggang Road, Shushan Economic Development Zone, Hefei City, Anhui Province Patentee after: Dragon totem Technology (Hefei) Co.,Ltd. Address before: 266000 Qingdao University of Science & Technology, 99 Songling Road, Laoshan District, Qingdao, Shandong Patentee before: QINGDAO University OF SCIENCE AND TECHNOLOGY |
|
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20240314 Address after: 335400 Fazhan Road, economic development zone, Guixi City, Yingtan City, Jiangxi Province intersects National Highway 320 (in Guixi science and Technology Innovation Center) Patentee after: Beifei blueprints Aviation Technology Co.,Ltd. Country or region after: China Address before: 1337, 13th Floor, Building 2, No. 38 Kechuangwu Street, Beijing Economic and Technological Development Zone, Daxing District, Beijing, 100000 (Yizhuang Cluster, High end Industrial Zone, Beijing Pilot Free Trade Zone) Patentee before: Beifei Blueprint (Beijing) Aeronautical Engineering Technology Research Institute Co.,Ltd. Country or region before: China |