CN102050411A - Ground lifting machine for aerial remote sensor - Google Patents
Ground lifting machine for aerial remote sensor Download PDFInfo
- Publication number
- CN102050411A CN102050411A CN 201010615565 CN201010615565A CN102050411A CN 102050411 A CN102050411 A CN 102050411A CN 201010615565 CN201010615565 CN 201010615565 CN 201010615565 A CN201010615565 A CN 201010615565A CN 102050411 A CN102050411 A CN 102050411A
- Authority
- CN
- China
- Prior art keywords
- remote sensor
- understructure
- bracing frame
- reduction gearing
- worm type
- 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.)
- Pending
Links
Images
Landscapes
- Forklifts And Lifting Vehicles (AREA)
Abstract
The invention relates to the field of aerial machinery, in particular to a ground lifting machine for an aerial remote sensor. The ground lifting machine for the aerial remote sensor comprises a horizontal two-degree-of-freedom adjusting platform and a vertical adjusting platform, wherein the horizontal two-degree-of-freedom adjusting platform is arranged on the vertical adjusting platform. The ground lifting machine can be convenient to realize short-distance transportation of the aerial remote sensor, and can be rapid and reliable to realize accurate butt joint between an aerial remote sensor interface and an airplane interface in the direction X, the direction Y and the direction Z in the process of assembly and disassembly.
Description
Technical field
The present invention relates to the aviation machine field, particularly a kind of ground rise or fall machine that is used for aero remote sensor.
Background technology
In the use of aero remote sensor, need safely, realize and the charge and discharge operations of aircraft interface having good working order fast and exactly with the guarantee aero remote sensor.Because the non-common apparatus of aero remote sensor, and lack necessary accessory equipment in the outfield, so, develop and a kind ofly can realize that the ground rise or fall machine that is used for aero remote sensor of above-mentioned functions is imperative.
Summary of the invention
At above-mentioned situation, in order to solve prior art problems, purpose of the present invention just is to provide a kind of ground rise or fall machine that is used for aero remote sensor, can regulate aero remote sensor by three directions.
The technical scheme that technical solution problem of the present invention adopts is, a kind of ground rise or fall machine that is used for aero remote sensor comprises that horizontal two-freedom adjusts platform and vertical adjustment platform, and said horizontal two-freedom is adjusted platform and is contained on the vertical adjustment platform.
Said horizontal two-freedom is adjusted platform and is comprised superstructure, middle level structure, understructure and worm type of reduction gearing, between superstructure and the middle level structure, all connect between middle level structure and the understructure by the linear bearing parafacies, worm type of reduction gearing is contained in a side of understructure, and links to each other with the middle level structure with understructure by rack-and-pinion.
Said vertical adjustment platform comprises bracing frame, four screw mandrel screw pairs, driving chain and worm type of reduction gearings, both sides are housed on the bracing frame two screw mandrel screw pairs respectively are housed, the lower end of screw mandrel screw pair links to each other with worm type of reduction gearing by driving chain, and worm type of reduction gearing is contained in a side of bracing frame.
The present invention can realize aero remote sensor ground short-distance transportation easily; Can in handling process, realize aero remote sensor interface and of accurate the docking of aircraft interface rapidly, reliably in X, Y, three directions of Z.
Description of drawings
Fig. 1 is the three-dimensional structure diagram that is used for the ground rise or fall machine of aero remote sensor of the present invention.
Fig. 2 is the three-dimensional structure diagram that the horizontal two-freedom that is used for the ground rise or fall machine of aero remote sensor of the present invention is adjusted platform.
Fig. 3 is the constructional drawing of the linear bearing pair of the ground rise or fall machine that is used for aero remote sensor of the present invention.
Fig. 4 is the constructional drawing of the rack-and-pinion of the ground rise or fall machine that is used for aero remote sensor of the present invention.
Fig. 5 is the constructional drawing of the worm type of reduction gearing of the ground rise or fall machine that is used for aero remote sensor of the present invention.
Fig. 6 is the three-dimensional structure diagram of vertical adjustment platform of the present invention.
Among the figure, 1, horizontal two-freedom adjusts platform, 2, the vertical adjustment platform, 3, superstructure, 4, the middle level structure, 5, understructure, 6, worm type of reduction gearing, 7, linear bearing pair, 8, rack-and-pinion, 9, the remote sensor bracing frame, 10, bracing frame, 11, screw mandrel screw pair, 12, driving chain, 13, cardan wheel.
The specific embodiment
Below in conjunction with accompanying drawing the specific embodiment of the present invention is elaborated.
By shown in Figure 1, a kind of ground rise or fall machine that is used for aero remote sensor of the present invention is characterized in that, comprises horizontal two-freedom adjustment platform 1 and vertical adjustment platform 2, and said horizontal two-freedom is adjusted platform 1 and is contained in vertical adjustment platform 2.
Shown in Fig. 1-5, said horizontal two-freedom is adjusted platform 1 and is comprised superstructure 3, middle level structure 4, understructure 5 and worm type of reduction gearing 6, between superstructure 3 and the middle level structure 4, all link to each other between middle level structure 4 and the understructure 5 by linear bearing secondary 7, worm type of reduction gearing 6 is contained in a side of understructure 5, and links to each other with middle level structure 4 with understructure 5 by rack-and-pinion 8.
Shown in Fig. 1,2, said superstructure 3 is provided with remote sensor bracing frame 9.
By shown in Figure 2, said superstructure 3, middle level structure 4 and understructure 5 all are shaped as frame.
By shown in Figure 6, said vertical adjustment platform 2 comprises bracing frame 10, four screw mandrel screw pairs 11, driving chain 12 and worm type of reduction gearings 6, both sides are housed on the bracing frame 10 two screw mandrel screw pairs 11 respectively are housed, the lower end of screw mandrel screw pair 11 links to each other with worm type of reduction gearing 6 by driving chain 12, and worm type of reduction gearing 6 is contained in a side of bracing frame 10.
Said bracing frame is equipped with cardan wheel 13 10 times.
By shown in Figure 1, said understructure 5 is contained on the bracing frame 10
Worm type of reduction gearing 6 casings among the present invention adopt ZL114, and worm screw is adopted 40Cr, and worm gear adopts albronze QAl9-4; Horizontal two-freedom is adjusted platform 1, vertical adjustment platform 2 frameworks are welded by square steel tube and sheet material, and material is Q235, has both alleviated weight, has guaranteed enough intensity again; Leading screw adopts 40Cr in the leading screw screw pair 11, and screw adopts albronze QAl9-4; Other driving parts adopts common charcoal steel, and non-welding exposes part and adopts corrosion-resistant steel.
When the present invention worked, by four leading screw screw pairs 11 of handwheel driving of rotation worm type of reduction gearing 6, the horizontal two-freedom of drive was adjusted platform 1 and is risen to upper limit position.After aero remote sensor correctly was placed on the remote sensor bearing surface, the horizontal two-freedom of driving was adjusted platform 1 and is reduced to the lower position, and utilize the ground rise or fall car that aero remote sensor is transported to installation site correct under the machine this moment.After using the ground rise or fall car that remote sensor is risen to correct position, drive horizontal two-freedom adjustment platform 1 by worm type of reduction gearing 6 and realize that the remote sensor interface docks X, the accurate of Y both direction with the aircraft interface, is interfaced to and the complete docking location of aircraft interface with vertical adjustment platform 2 lifting aero remote sensors again.After using corresponding screw fastening, the horizontal two-freedom of driving is adjusted platform 1 and is reduced to the lower position, makes the ground rise or fall car leave aircraft to correct position again.At this moment, finished use ground rise or fall car the operation of aero remote sensor to aircraft has been installed.Can be considered the inverse process of said process from the operation of aircraft dismounting remote sensor.
The present invention can realize reliable, the rapid descending operation of aero remote sensor; In the installation process, can realize aero remote sensor interface and the accurate adjustment function of docking of aircraft interface in X, Y, three directions of Z; Can realize the short distance delivery functions of aero remote sensor.
Claims (7)
1. a ground rise or fall machine that is used for aero remote sensor is characterized in that, comprises horizontal two-freedom adjustment platform (1) and vertical adjustment platform (2), and said horizontal two-freedom is adjusted platform (1) and is contained on the vertical adjustment platform (2).
2. a kind of ground rise or fall machine that is used for aero remote sensor according to claim 1, it is characterized in that, said horizontal two-freedom is adjusted platform (1) and is comprised superstructure (3), middle level structure (4), understructure (5) and worm type of reduction gearing (6), between superstructure (3) and the middle level structure (4), all link to each other between middle level structure (4) and the understructure (5) by linear bearing pair (7), worm type of reduction gearing (6) is contained in a side of understructure (5), and links to each other with middle level structure (4) with understructure (5) by rack-and-pinion (8).
3. a kind of ground rise or fall machine that is used for aero remote sensor according to claim 2 is characterized in that said superstructure (3) is provided with remote sensor bracing frame (9).
4. a kind of ground rise or fall machine that is used for aero remote sensor according to claim 2 is characterized in that said superstructure (3), middle level structure (4) and understructure (5) all are shaped as frame.
5. a kind of ground rise or fall machine that is used for aero remote sensor according to claim 1, it is characterized in that, said vertical adjustment platform (2) comprises bracing frame (10), four screw mandrel screw pairs (11), driving chain (12) and worm type of reduction gearing (6), four screw mandrel screw pairs (11) are installed in the both sides of bracing frame (10) respectively, the lower end of screw mandrel screw pair (11) links to each other with worm type of reduction gearing (6) by driving chain (12), and worm type of reduction gearing (6) is contained in a side of bracing frame (10).
6. a kind of ground rise or fall machine that is used for aero remote sensor according to claim 5 is characterized in that, cardan wheel (13) is housed under the said bracing frame (10).
7. according to claim 2 or 5 described a kind of ground rise or fall machines that are used for aero remote sensor, it is characterized in that said understructure (5) is contained on the bracing frame (10).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201010615565 CN102050411A (en) | 2010-12-30 | 2010-12-30 | Ground lifting machine for aerial remote sensor |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201010615565 CN102050411A (en) | 2010-12-30 | 2010-12-30 | Ground lifting machine for aerial remote sensor |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN102050411A true CN102050411A (en) | 2011-05-11 |
Family
ID=43955285
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201010615565 Pending CN102050411A (en) | 2010-12-30 | 2010-12-30 | Ground lifting machine for aerial remote sensor |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN102050411A (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103672320A (en) * | 2013-11-18 | 2014-03-26 | 北京空间机电研究所 | Auxiliary supporting mechanism of spaceflight optical remote sensor |
| CN106276704A (en) * | 2016-10-24 | 2017-01-04 | 中国兵器装备集团自动化研究所 | A kind of vehicle-mounted Two axle drive lifting device |
| CN108100968A (en) * | 2017-12-19 | 2018-06-01 | 华中科技大学无锡研究院 | A kind of scissor type telescopic arm |
| CN109132933A (en) * | 2018-09-26 | 2019-01-04 | 云南电网有限责任公司红河供电局 | A kind of hoistable platform for mending gap impact test apparatus for carrying string |
| CN114278072A (en) * | 2021-12-23 | 2022-04-05 | 通州建总集团有限公司 | Construction work platform for building engineering |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO1999054190A1 (en) * | 1998-04-17 | 1999-10-28 | Maxmove Ab | Arrangement for vehicles |
| CN2598866Y (en) * | 2002-12-31 | 2004-01-14 | 华兴航空机轮公司模具厂 | Machine wheel loading and unloading ground surface engineering car |
| CN2828000Y (en) * | 2005-09-16 | 2006-10-18 | 中国南车集团株洲电力机车有限公司 | Hydraulic lifting moving trolley |
| CN101318616A (en) * | 2007-06-05 | 2008-12-10 | 江苏长虹涂装机械有限公司 | Multidimensional movement horizontal plane working vehicle |
| CN101475102A (en) * | 2009-01-23 | 2009-07-08 | 浙江理工大学 | Hand-operated elevation type tank transportation loading and unloading frame |
| CN201442831U (en) * | 2008-12-24 | 2010-04-28 | 贵阳黔江机械厂 | Hydraulic lifting work ladder with extendable platform |
| CN101708816A (en) * | 2009-11-13 | 2010-05-19 | 鄂州市合强机械发展有限公司 | Fully automatic mobile hydraulic lifting platform machine |
-
2010
- 2010-12-30 CN CN 201010615565 patent/CN102050411A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO1999054190A1 (en) * | 1998-04-17 | 1999-10-28 | Maxmove Ab | Arrangement for vehicles |
| CN2598866Y (en) * | 2002-12-31 | 2004-01-14 | 华兴航空机轮公司模具厂 | Machine wheel loading and unloading ground surface engineering car |
| CN2828000Y (en) * | 2005-09-16 | 2006-10-18 | 中国南车集团株洲电力机车有限公司 | Hydraulic lifting moving trolley |
| CN101318616A (en) * | 2007-06-05 | 2008-12-10 | 江苏长虹涂装机械有限公司 | Multidimensional movement horizontal plane working vehicle |
| CN201442831U (en) * | 2008-12-24 | 2010-04-28 | 贵阳黔江机械厂 | Hydraulic lifting work ladder with extendable platform |
| CN101475102A (en) * | 2009-01-23 | 2009-07-08 | 浙江理工大学 | Hand-operated elevation type tank transportation loading and unloading frame |
| CN101708816A (en) * | 2009-11-13 | 2010-05-19 | 鄂州市合强机械发展有限公司 | Fully automatic mobile hydraulic lifting platform machine |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103672320A (en) * | 2013-11-18 | 2014-03-26 | 北京空间机电研究所 | Auxiliary supporting mechanism of spaceflight optical remote sensor |
| CN103672320B (en) * | 2013-11-18 | 2015-10-21 | 北京空间机电研究所 | A kind of space flight optical remote sensor auxiliary support mechanism |
| CN106276704A (en) * | 2016-10-24 | 2017-01-04 | 中国兵器装备集团自动化研究所 | A kind of vehicle-mounted Two axle drive lifting device |
| CN108100968A (en) * | 2017-12-19 | 2018-06-01 | 华中科技大学无锡研究院 | A kind of scissor type telescopic arm |
| CN109132933A (en) * | 2018-09-26 | 2019-01-04 | 云南电网有限责任公司红河供电局 | A kind of hoistable platform for mending gap impact test apparatus for carrying string |
| CN114278072A (en) * | 2021-12-23 | 2022-04-05 | 通州建总集团有限公司 | Construction work platform for building engineering |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN104259830B (en) | A kind of high-tension battery assembly equipment | |
| CN102050411A (en) | Ground lifting machine for aerial remote sensor | |
| CN205220756U (en) | Building machine was climbed to thing in electronic year | |
| CN104132591B (en) | A kind of rocket portion section rolling posture adjusting device on a large scale | |
| CN107262572B (en) | Numerical control I-steel cold bending machine | |
| CN204867888U (en) | Three degree of freedom mobile welding robot of hoist box girder | |
| CN202033093U (en) | Billet on-line weighing device | |
| CN105417114B (en) | Lift conveyor | |
| CN109226345A (en) | Plate unit structural member straightening machine | |
| CN103787203B (en) | For installing the bracing frame of precast beam jack | |
| CN103215955A (en) | Airborne hydraulic spiral pile driver | |
| CN103803422B (en) | A kind of hoisting device for nuclear station and installation method thereof | |
| CN202116033U (en) | Tire transfer mechanism | |
| CN103662704A (en) | Rail-spanning transportation assembly wagon | |
| CN201560101U (en) | Fork tool structure and arm frame structure applying same | |
| CN204043530U (en) | A kind of rocket portion section rolling posture adjusting device on a large scale | |
| CN203654705U (en) | Slideable hanging basket apparatus for steel skeleton assembling | |
| CN104925721A (en) | Automatic overturning device applied to tank container | |
| CN206343805U (en) | Positioner for lower frame of excavator | |
| CN203268959U (en) | Glass frame moving device applied to full-automatic glass batch-out machine | |
| CN206358797U (en) | One kind conveying handling device | |
| CN206241567U (en) | A kind of base plate welds deflection machine | |
| CN104627823B (en) | Driving peculiar to vessel | |
| CN202462729U (en) | Tire post-inflated device | |
| CN204022416U (en) | The device of liftable and rolling coil of strip |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20110511 |