CN107757672B - A kind of adjustable aircraft wing handling device for supporting and lifting position and height - Google Patents
A kind of adjustable aircraft wing handling device for supporting and lifting position and height Download PDFInfo
- Publication number
- CN107757672B CN107757672B CN201710989655.XA CN201710989655A CN107757672B CN 107757672 B CN107757672 B CN 107757672B CN 201710989655 A CN201710989655 A CN 201710989655A CN 107757672 B CN107757672 B CN 107757672B
- Authority
- CN
- China
- Prior art keywords
- trailing arm
- gear
- slideway
- wheel
- aircraft wing
- 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
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B62—LAND VEHICLES FOR TRAVELLING OTHERWISE THAN ON RAILS
- B62B—HAND-PROPELLED VEHICLES, e.g. HAND CARTS OR PERAMBULATORS; SLEDGES
- B62B3/00—Hand carts having more than one axis carrying transport wheels; Steering devices therefor; Equipment therefor
- B62B3/02—Hand carts having more than one axis carrying transport wheels; Steering devices therefor; Equipment therefor involving parts being adjustable, collapsible, attachable, detachable or convertible
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B62—LAND VEHICLES FOR TRAVELLING OTHERWISE THAN ON RAILS
- B62B—HAND-PROPELLED VEHICLES, e.g. HAND CARTS OR PERAMBULATORS; SLEDGES
- B62B3/00—Hand carts having more than one axis carrying transport wheels; Steering devices therefor; Equipment therefor
- B62B3/10—Hand carts having more than one axis carrying transport wheels; Steering devices therefor; Equipment therefor characterised by supports specially adapted to objects of definite shape
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B62—LAND VEHICLES FOR TRAVELLING OTHERWISE THAN ON RAILS
- B62B—HAND-PROPELLED VEHICLES, e.g. HAND CARTS OR PERAMBULATORS; SLEDGES
- B62B5/00—Accessories or details specially adapted for hand carts
- B62B5/0006—Bumpers; Safety devices
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B62—LAND VEHICLES FOR TRAVELLING OTHERWISE THAN ON RAILS
- B62B—HAND-PROPELLED VEHICLES, e.g. HAND CARTS OR PERAMBULATORS; SLEDGES
- B62B2206/00—Adjustable or convertible hand-propelled vehicles or sledges
- B62B2206/02—Adjustable or convertible hand-propelled vehicles or sledges adjustable in length or width
- B62B2206/04—Adjustable or convertible hand-propelled vehicles or sledges adjustable in length or width only the load support being adjustable
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B62—LAND VEHICLES FOR TRAVELLING OTHERWISE THAN ON RAILS
- B62B—HAND-PROPELLED VEHICLES, e.g. HAND CARTS OR PERAMBULATORS; SLEDGES
- B62B2206/00—Adjustable or convertible hand-propelled vehicles or sledges
- B62B2206/06—Adjustable or convertible hand-propelled vehicles or sledges adjustable in height
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Transportation (AREA)
- Mechanical Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
A kind of adjustable aircraft wing handling device for supporting and lifting position and height, belong to aircraft wing and carries field, including saddle, a kind of saddle one end connection rubber pad of the adjustable aircraft wing handling device for supporting and lifting position and height, the upper trailing arm of other end connection, connecting rod is connected between the upper trailing arm, plays stable effect.Wheel is bolted by pneumatically pushing up the lower trailing arm of plug connection, the lower trailing arm fifth wheel platform, the Luntai in the upper trailing arm.The rubber pad upper end connects equally distributed upper convex rubber convex point, and lower end connects saddle.The present invention can be buffered in the degree of jolting in the handling process of aircraft wing by the high pressure gas in control air cavity, so that handling process is more steady smooth, mitigation is jolted and adversely affected to wing itself is generated.
Description
Technical field
The present invention relates to a kind of aircraft wing handling device more particularly to a kind of adjustable aircrafts for supporting and lifting position and height
Wing handling device belongs to aircraft wing and carries field.
Background technology
In recent years, China is continued to increase in the investment of aircraft circles, and account is investigated and analysed according to civil aviaton's industry market
Bright, civil aviaton of China is to advance by leaps and bounds in nearly development in 25 years, and it is public that initial stage nineties civil aviaton realizes that passenger has enough to meet the need 230.48 hundred million people
In, open 437 course lines.By 2015, whole people's boat volume of passenger transportation turned over 30 times, and it is public to realize that passenger has enough to meet the need 7270.7 hundred million people
In, annual compound growth rate reaches 15%.Total course line reaches 3142, wherein domestic air route 2652.Civil aviaton of China it is many-sided all
Realize General Promotion.
And wing, since its length is longer, is being removed the wing of different type of machines as one of the important component on aircraft
There are different degrees of difficulties in fortune and installation process, how to resolve removing for the fast and steady of aircraft wing during the installation process
Fortune, which is to continue with, to be solved the problems, such as, this is not only related to the production efficiency of aircraft, the life to the Civil Aviation Industry or even military aircraft in China
Production can all generate significant impact.
Invention content
A kind of adjustable aircraft wing handling device for supporting and lifting position and height, its object is to：Promote aircraft wing
Installation speed and its existing since length is long and generates carrying is unstable or carries slower problem in the handling process,
Promote the safety coefficient of wing handling process.
The present invention to achieve the above object, has provided following technical scheme：A kind of adjustable position and height of supporting and lifting
Aircraft wing handling device, including saddle, upper trailing arm, pneumatic top plug, stage body, air pump I, lower trailing arm, Luntai, wheel, air pump II,
Motor, rubber pad, connecting rod, slideway, slideway gear grooved, slideway gear, the gear teeth, rubber stopper, locking nut, air flue, air cavity, positioning
Gasket, lower trailing arm wall, scroll wheel, Luntai support plate, scroll wheel support arm, movable pulley wheel track, gear, motor gear, motor shaft,
Rubber salient point, is particularly limited as：A kind of saddle one of the adjustable aircraft wing handling device for supporting and lifting position and height
End connection rubber pad, the other end connect upper trailing arm, connect connecting rod between the upper trailing arm, play stable effect.The pop-up
Wheel is bolted by pneumatically pushing up the lower trailing arm of plug connection, the lower trailing arm fifth wheel platform, the Luntai in arm.The rubber
It pads upper end and connects equally distributed upper convex rubber convex point, lower end connects saddle.The lower trailing arm connects stage body, institute by slideway
State stage body connection air pump I, air pump II and motor.There are slideway gear grooved, the slideway gear grooved to supply on the outside of the slideway of the stage body
The rotation of slideway gear is used.The slideway gear connects lower trailing arm and carries the gear teeth, and the gear teeth connect slideway gear grooved.It is described
Slideway gear and the coaxially connected lower trailing arm of gear.The gear is engaged with motor gear, and is driven and rotated by motor gear.It is described
Motor gear passes through motor axis connection motor.
The present invention has carried out specific restriction to above-mentioned technical proposal, is particularly limited as：A kind of be adjusted supports and lifts position
It sets and the pneumatic top of the aircraft wing handling device of height plug includes rubber stopper, locking nut, air flue, air cavity, locating shim.Institute
The upper trailing arm of rubber stopper upper end connection is stated, lower end connects locating shim.The locating shim upper end connects rubber stopper, lower end connection lock
Tight nut.The locking nut is connected through a screw thread trailing arm.Described air flue one end connects air cavity, and the other end connects air pump.
The present invention has carried out specific restriction to above-mentioned technical proposal, is particularly limited as：A kind of be adjusted supports and lifts position
It sets and the Luntai of the aircraft wing handling device of height includes scroll wheel, Luntai support plate, scroll wheel support arm, movable pulley wheel
Rail.Movable pulley wheel track one end connects stage body, and the other end connects scroll wheel.The scroll wheel is connected by scroll wheel support arm
Luntai support plate.Luntai support plate upper end connects scroll wheel support arm and lower trailing arm simultaneously, and lower end connects wheel.
The present invention advantageous effects be：When in use, control can be passed through according to the wing length to be carried first
Motor and air pump holder for regulating platform position processed and height, the pneumatic top in connection between trailing arm and lower trailing arm are filled in due to being by high pressure gas
Body is filled in air cavity and the support force of generation, so the high pressure gas in air cavity can rise in the handling process of aircraft wing
The effect jolted to buffering so that handling process is more steady smooth, while can substantially reduce aircraft wing and carry
Due to jolting and to adverse effect caused by wing itself in journey.
Description of the drawings
Fig. 1 is the overall structure front view of the present invention；
Fig. 2 is the overall structure left view of the present invention；
Fig. 3 is the slideway structure vertical view of the present invention；
Fig. 4 is the slideway gear engagement structure schematic diagram of the present invention；
Fig. 5 is the pneumatic top plug structure schematic diagram of the present invention；
Fig. 6 is the Luntai structural schematic diagram of the present invention；
Fig. 7 is the lower trailing arm screw gear drive mechanism schematic diagram of the present invention；
Fig. 8 is the gantry structure schematic diagram of the present invention；
Fig. 9 is the rubber gasket structure vertical view of the present invention.
In figure：1, saddle, 2, upper trailing arm, 3, pneumatic top plug, 4, stage body, 5, air pump I, 6, lower trailing arm, 7, Luntai, 8, wheel
Son, 9, air pump II, 10, motor, 11, rubber pad, 12, connecting rod, 13, slideway, 14, slideway gear grooved, 15, slideway gear, 16, wheel
Tooth, 17, rubber stopper, 18, locking nut, 19, air flue, 20, air cavity, 21, locating shim, 22, lower trailing arm wall, 23, scroll wheel,
24, Luntai support plate, 25, scroll wheel support arm, 26, movable pulley wheel track, 27, gear, 28, motor gear, 29, motor shaft, 30,
Rubber salient point.
Specific implementation mode
In order to better understand the present invention, the specific implementation mode of the present invention is described in detail below in conjunction with the accompanying drawings.
A kind of adjustable aircraft wing handling device for supporting and lifting position and height, including saddle 1, upper trailing arm 2, pneumatic top plug
3, stage body 4, air pump I 5, lower trailing arm 6, Luntai 7, wheel 8, air pump II 9, motor 10, rubber pad 11, connecting rod 12, slideway 13, slideway
Gear grooved 14, slideway gear 15, the gear teeth 16, rubber stopper 17, locking nut 18, air flue 19, air cavity 20, locating shim 21, subiculum
Arm wall 22, scroll wheel 23, Luntai support plate 24, scroll wheel support arm 25, movable pulley wheel track 26, gear 27, motor gear 28, electricity
Arbor 29, rubber salient point 30.
A kind of 1 one end of saddle connection rubber pad of the adjustable aircraft wing handling device for supporting and lifting position and height
11, the other end connects upper trailing arm 2, connects connecting rod 12 between described two upper trailing arms 2, plays stable effect.The upper trailing arm 2
By pneumatically pushing up the lower trailing arm 6 of 3 connection of plug, the lower trailing arm 6 connects Luntai 7, and wheel 8 is bolted in the Luntai 7.It is described
11 upper end of rubber pad connects equally distributed upper convex rubber convex point 30, and lower end connects saddle 1.The lower trailing arm 6 passes through slideway
13 connection stage bodies 4, the stage body 4 connect air pump I 5, air pump II 9 and motor 10.There is slideway tooth in 13 outside of slideway of the stage body 4
Race 14, the slideway gear grooved 14 are used for the rotation of slideway gear 15.The slideway gear 15 connects lower trailing arm 6 and with wheel
Tooth 16, the gear teeth 16 connect slideway gear grooved 14.The coaxially connected lower trailing arm of the slideway gear 15 and gear 27 6.The tooth
Wheel 27 is engaged with motor gear 28, and is driven and rotated by motor gear 28.The motor gear 28 connects electricity by motor shaft 29
Machine 10.
A kind of pneumatic top plug 3 of adjustable aircraft wing handling device for supporting and lifting position and height includes rubber stopper
17, locking nut 18, air flue 19, air cavity 20, locating shim 21.The upper trailing arm 2 of 17 upper end of rubber stopper connection, lower end connection are fixed
Position gasket 21.21 upper end of the locating shim connects rubber stopper 17, and lower end connects locking nut 18.The locking nut 18 passes through
Trailing arm 2 in threaded connection.19 one end of the air flue connects air cavity 20, and the other end connects air pump.
A kind of Luntai 7 of adjustable aircraft wing handling device for supporting and lifting position and height includes scroll wheel 23, wheel
Platform support plate 24, scroll wheel support arm 25, movable pulley wheel track 26.Described 26 one end of movable pulley wheel track connects stage body 4, and the other end connects
Connect scroll wheel 23.The scroll wheel 23 connects Luntai support plate 24 by scroll wheel support arm 25.In the Luntai support plate 24
Scroll wheel support arm 25 and lower trailing arm 6 are held while connecting, lower end connects wheel 8.
Operation principle：When in use, first according to the wing length to be carried, wheel 8 is driven by controlling motor 10
The position of saddle 1 is adjusted, the sliding in slideway 13 under the drive of slideway gear 15 of lower trailing arm 6 at this time, until saddle 1 is adjusted
To suitable position.Behind the position for regulating saddle 1, booster air pump I 5 and air pump II 9, high pressure gas at this time by air flue 19 into
Enter air cavity 20, upper trailing arm 2 is gradually held up, plays the role of adjusting 1 height of saddle, until saddle by the entrance of high pressure gas upwards
1 can stablize when lifting aircraft wing, and air pump I 5 and air pump II 9 are stopped and keep pressure.Following wheel 8 is in motor 10
Aircraft wing is lifted under effect realizes carrying.It simultaneously in the handling process, the problems such as uneven such as ground, can be by controlling air pump
I 5 and air pump II 9 adjust the height of saddle 1 to control the high pressure gas scale of construction entered in air cavity 20 by air flue 19, reach buffering top
The purpose stablized and carried is realized in the effect winnowed with a dustpan.
Technical characteristic of the present invention without description can be achieved by the prior art, and details are not described herein.Certainly, it above states
Bright is not limitation of the present invention, and the present invention is also not limited to the example above, and those skilled in the art exist
The variations, modifications, additions or substitutions made in the essential scope of the present invention, should also belong to the scope of protection of the present invention.
Claims (3)
1. a kind of adjustable aircraft wing handling device for supporting and lifting position and height, including saddle, upper trailing arm, pneumatic top plug, platform
Body, air pump I, lower trailing arm, Luntai, wheel, air pump II, motor, rubber pad, connecting rod, slideway, slideway gear grooved, slideway gear, wheel
Tooth, lower trailing arm wall, gear, motor gear, motor shaft, rubber salient point, wherein pneumatic top plug includes rubber stopper, locking nut, gas
Road, air cavity, locating shim；Luntai includes scroll wheel, Luntai support plate, scroll wheel support arm, movable pulley wheel track, and feature exists
In：A kind of saddle one end connection rubber pad of adjustable aircraft wing handling device for supporting and lifting position and height, the other end
Trailing arm in connection connects connecting rod between the upper trailing arm, plays stable effect, the upper trailing arm is by pneumatically pushing up under plug connection
Wheel is bolted in trailing arm, the lower trailing arm fifth wheel platform, the Luntai, and the rubber pad upper end connection is equally distributed
Upper convex rubber convex point, lower end connect saddle；The lower trailing arm connects stage body, the stage body connection air pump I, air pump by slideway
II and motor, there is slideway gear grooved on the outside of the slideway of the stage body, the slideway gear grooved is used for the rotation of slideway gear, described
The lower trailing arm of slideway gear connection simultaneously carries the gear teeth, and the gear teeth connect slideway gear grooved, and the slideway gear coaxially connects with gear
Lower trailing arm is connect, the gear is engaged with motor gear, and is driven and rotated by motor gear, and the motor gear is connected by motor shaft
Connect motor.
2. a kind of adjustable aircraft wing handling device for supporting and lifting position and height as described in claim 1, it is characterised in that：
The upper trailing arm of rubber stopper upper end connection, lower end connect locating shim, and the locating shim upper end connects rubber stopper, lower end connection
Locking nut, the locking nut are connected through a screw thread trailing arm, and described air flue one end connects air cavity, and the other end is separately connected gas
Pump I and air pump II.
3. a kind of adjustable aircraft wing handling device for supporting and lifting position and height as described in claim 1, it is characterised in that：
Movable pulley wheel track one end connects stage body, and the other end connects scroll wheel, and the scroll wheel passes through scroll wheel support arm fifth wheel
Platform support plate, Luntai support plate upper end connect scroll wheel support arm and lower trailing arm simultaneously, and lower end connects wheel.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710989655.XA CN107757672B (en) | 2017-10-23 | 2017-10-23 | A kind of adjustable aircraft wing handling device for supporting and lifting position and height |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710989655.XA CN107757672B (en) | 2017-10-23 | 2017-10-23 | A kind of adjustable aircraft wing handling device for supporting and lifting position and height |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN107757672A CN107757672A (en) | 2018-03-06 |
| CN107757672B true CN107757672B (en) | 2018-10-12 |
Family
ID=61268401
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710989655.XA Active CN107757672B (en) | 2017-10-23 | 2017-10-23 | A kind of adjustable aircraft wing handling device for supporting and lifting position and height |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107757672B (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108860376B (en) * | 2018-03-22 | 2019-11-29 | 河南科技大学 | It is a kind of for transmitting the spare wheel device of power |
Family Cites Families (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106342042B (en) * | 2009-04-10 | 2013-07-24 | 中航贵州飞机有限责任公司 | A kind of aircraft dispatch car |
| US9327751B2 (en) * | 2013-05-03 | 2016-05-03 | Embraer S.A. | Assemblies and methods for handling, transporting and/or positioning component parts |
| CN203698077U (en) * | 2013-12-23 | 2014-07-09 | 南京中航特种装备有限公司上海技术中心 | Aircraft wing transport cart |
| KR20160117948A (en) * | 2015-04-01 | 2016-10-11 | 주식회사 대명엔지니어링 | Wing component rack for aircraft |
| CN205589263U (en) * | 2016-03-21 | 2016-09-21 | 吴为阳 | Special article deposit flow box |
| CN206158943U (en) * | 2016-11-15 | 2017-05-10 | 舟山市晶源船舶设备制造有限公司 | Marine pump |
-
2017
- 2017-10-23 CN CN201710989655.XA patent/CN107757672B/en active Active
Also Published As
| Publication number | Publication date |
|---|---|
| CN107757672A (en) | 2018-03-06 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN204237510U (en) | A kind of die assembly transport trolley | |
| CN107757672B (en) | A kind of adjustable aircraft wing handling device for supporting and lifting position and height | |
| CN203612877U (en) | Floating-conveying assembling wagon | |
| CN106378755A (en) | Aircraft engine maintaining platform | |
| CN207873928U (en) | A kind of steel plate polishing machine | |
| CN206705185U (en) | A kind of feeding turning device | |
| CN201543907U (en) | Tool retracting device of cutting machine with double bevels | |
| CN104476342B (en) | Ductile iron pipe cement lining polisher | |
| CN206179830U (en) | Solar cell panel appearance detection device | |
| CN205257225U (en) | But feed elevator of self -modulation elasticity | |
| CN206382868U (en) | A kind of nitrogen balance cylinder system | |
| CN205521389U (en) | Multiaxis formula swing arm robot | |
| CN203129205U (en) | Movable arm counter weight follow-up excavator | |
| CN205096831U (en) | Balanced flywheel installation of reciprocating compressor and shaft coupling alignment specialized tool | |
| CN104175740B (en) | A kind of paper-pressing mechanism for the machine of binding | |
| CN210305770U (en) | Turning integral type gyro wheel frame | |
| CN207915676U (en) | One kind can pull liftable planing tool mechanism | |
| CN205257787U (en) | Lift hoist with retinue function that opens and shuts | |
| CN207058256U (en) | Glass grinding apparatus | |
| CN205602542U (en) | Special conveyer of building material | |
| CN205086034U (en) | Motor drive formula sponge circle cutting device | |
| CN220705654U (en) | Workover hydraulic pressure lifts quick-witted travelling bogie of pipe | |
| CN207243361U (en) | A kind of auto spiral lifting device | |
| CN221007150U (en) | Drop hammer type collision experiment accelerating tower | |
| CN219031639U (en) | Construction material conveyer |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20210419 Address after: No.198, Jianghai West Road, Haian Town, Haian City, Nantong City, Jiangsu Province Patentee after: Hengcheng Aviation Technology (Nantong) Co.,Ltd. Address before: 448000 Jingmen province Hubei city Zhanghe District Aviation Industrial Park No. 1 love to fly Patentee before: ALOONG AIRCRAFT (JINGMEN) Co.,Ltd. |
|
| TR01 | Transfer of patent right |