CN106542076A - A kind of supporting mechanism of the platform that anchors for captive balloon ground installation - Google Patents
A kind of supporting mechanism of the platform that anchors for captive balloon ground installation Download PDFInfo
- Publication number
- CN106542076A CN106542076A CN201611112059.5A CN201611112059A CN106542076A CN 106542076 A CN106542076 A CN 106542076A CN 201611112059 A CN201611112059 A CN 201611112059A CN 106542076 A CN106542076 A CN 106542076A
- Authority
- CN
- China
- Prior art keywords
- telescopic outrigger
- telescopic
- spindle nose
- captive balloon
- platform
- 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.)
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64B—LIGHTER-THAN AIR AIRCRAFT
- B64B1/00—Lighter-than-air aircraft
- B64B1/66—Mooring attachments
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64B—LIGHTER-THAN AIR AIRCRAFT
- B64B1/00—Lighter-than-air aircraft
- B64B1/40—Balloons
- B64B1/50—Captive balloons
- B64B1/52—Captive balloons attaching trailing entanglements
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Vehicle Cleaning, Maintenance, Repair, Refitting, And Outriggers (AREA)
Abstract
The present invention proposes a kind of supporting mechanism of the platform that anchors for captive balloon ground installation, including elevating rocker arm, lifting slowdown module, automatic leveling module, semitrailer, telescopic outrigger, fulcrum bearing, half spindle nose, road wheel, wheelspan adjusting screw rod and intermediate connecting rod；Telescopic outrigger is divided into telescopic outrigger canned paragraph and telescopic outrigger telescopic section, and elevating rocker arm connects telescopic outrigger by lifting slowdown module；Telescopic outrigger canned paragraph is connected with semitrailer by bolt, supports semi-trailer frame；Automatic leveling module is arranged on telescopic outrigger；Telescopic outrigger lower end is connected with half spindle nose by fulcrum bearing, is connected by cylinder roller bearing between half spindle nose and rail wheel；Half spindle nose is connected with wheelspan adjusting screw rod, and wheelspan adjusting screw rod is threaded connection with intermediate connecting rod, realizes that wheelspan is adjustable.The present invention is used on the anchoring platform of captive balloon so that the scope of application of captive balloon is broader, can be used in fixed position, can be carried out motorized transport again, use in any preliminary position.
Description
Technical field
The present invention relates to the ground installation field of captive balloon (aerostatics), specially one kind are set for captive balloon ground
The supporting mechanism of standby anchoring platform.
Background technology
In the ground installation of captive balloon, need to support anchoring platform using supporting mechanism, while entering the platform that anchors
Row leveling, so that the platform that anchors can smoothly follow captive balloon down wind deflection (along slurry), strengthens the antidumping energy of anchoring platform
Power.Wherein, the supporting mechanism of fixed captive balloon anchoring platform is generally connected on the ground, can bear larger vertical load
Lotus, but it is unable to transition movement.The supporting mechanism of motor driven captive balloon anchoring platform, is generally fixed on anchoring car, Ji Nengshen
Go out to support and leveling anchoring platform, and adaptation vehicle transport can be withdrawn, but the supporting device horizontal load ability to bear is poor, and
It is immovable under holding state, it is impossible to realize dribbling turnover ball storehouse.And in similar support structure, also combined etc. shape
The supporting leg form of formula, although possess elevating function, has both adapted to track, adapts to highway again, but to bear load little for which, does not have
Standby leveling capability, and mechanism is sufficiently complex, is not suitable for the use of captive balloon anchoring platform.
The content of the invention
The anchoring platform support mechanism of existing captive balloon may be only available for fixed captive balloon or may be only available for
Motor driven captive balloon, it is impossible to realize the multiple use of same anchoring platform, constrain the use range of captive balloon system, this
The purpose of invention passes through to design a kind of support mechanism installed in anchoring platform, before good support performance is ensured
Put, captive balloon anchoring platform is used in fixed position, but can motor-driven transition use so that anchoring platform makes
It is expanded with scope.
The technical scheme is that：
A kind of supporting mechanism of the platform that anchors for captive balloon ground installation, it is characterised in that：Shake including lifting
Arm (1), lifting slowdown module (2), automatic leveling module (3), semitrailer (4), telescopic outrigger, fulcrum bearing (7), half spindle nose (8),
Road wheel (10), wheelspan adjusting screw rod (11) and intermediate connecting rod (12)；
Telescopic outrigger is divided into telescopic outrigger canned paragraph (5) and telescopic outrigger telescopic section (6)；
Elevating rocker arm (1) connects telescopic outrigger by lifting slowdown module (2), and can drive telescopic outrigger canned paragraph
(5) with telescopic outrigger telescopic section (6) relative motion；
Telescopic outrigger canned paragraph (5) is connected with semitrailer (4) by bolt, supports semi-trailer frame；
Automatic leveling module (3) when telescopic outrigger ground connection supporting anchoring platform, realizes anchoring on telescopic outrigger
The automatic leveling of platform；
Telescopic outrigger lower end is connected with half spindle nose (8) by fulcrum bearing (7), is led between half spindle nose (8) and rail wheel (10)
Cross cylinder roller bearing (9) connection；When needing anchoring platform to launch, placement activity jacking block below fulcrum bearing (7), as anchoring
The supporting stress point of platform；
Half spindle nose (8) is connected with wheelspan adjusting screw rod (11), and wheelspan adjusting screw rod (11) is with intermediate connecting rod (12) by spiral shell
Stricture of vagina connects, and realizes that wheelspan is adjustable.
Further preferred version, a kind of supporting mechanism of the platform that anchors for captive balloon ground installation, which is special
Levy and be：Telescopic outrigger is processed using bar finish-milling, boring, realizes telescopic outrigger canned paragraph (5) and telescopic outrigger telescopic section (6) essence
Close fit.
Further preferred version, a kind of supporting mechanism of the platform that anchors for captive balloon ground installation, which is special
Levy and be：Half spindle nose (8) is articulated and connected with wheelspan adjusting screw rod (11).
Beneficial effect
The present invention is used on the anchoring platform of captive balloon so that the scope of application of captive balloon is broader, can
Use in fixed position, motorized transport can be carried out again, use in any preliminary position.Design through ball pivot connection so that support
The stressing conditions of mechanism's telescopic outrigger are improved, and the stress deformation of telescopic outrigger is greatly reduced, and the stability of supporting mechanism is obtained
To being significantly increased.Through adding adjustable screw connecting mechanism so that the wheelspan between two supporting legs is adjustable, track width is adapted to
Change.Through adding electric leveling mechanism so that the leveling process efficiency of anchoring platform is higher.Through adding planetary gear speed-reduction
Device, greatly reduces the descending operation difficulty of supporting mechanism, reduces the physical fitness requirement to operator.
The additional aspect and advantage of the present invention will be set forth in part in the description, and partly will become from the following description
Obtain substantially, or recognized by the practice of the present invention.
Description of the drawings
The above-mentioned and/or additional aspect and advantage of the present invention will become from the description with reference to accompanying drawings below to embodiment
It is substantially and easy to understand, wherein：
Fig. 1：Present configuration composition schematic diagram.
Specific embodiment
Embodiments of the invention are described below in detail, the embodiment is exemplary, it is intended to for explaining the present invention, and
It is not considered as limiting the invention.
In describing the invention, it is to be understood that term " " center ", " longitudinal direction ", " horizontal ", " length ", " width ",
" thickness ", " on ", D score, "front", "rear", "left", "right", " vertical ", " level ", " top ", " bottom ", " interior ", " outward ", " up time
The orientation or position relationship of the instruction such as pin ", " counterclockwise " is, based on orientation shown in the drawings or position relationship, to be for only for ease of
The description present invention and simplified description, rather than indicate or imply that the device or element of indication must have specific orientation, Yi Te
Fixed azimuth configuration and operation, therefore be not considered as limiting the invention.
Due to existing captive balloon anchoring platform support mechanism or may be only available for fixed captive balloon or can only fit
For motor driven captive balloon, it is impossible to realize the multiple use of same anchoring platform, constrain the use model of captive balloon system
Enclose, the present invention proposes a kind of support mechanism installed in anchoring platform, on the premise of good support performance is ensured, makes
Captive balloon anchoring platform can be used in fixed position, and the motor-driven transition of energy is used, so that the use range of anchoring platform
It is expanded.
As shown in figure 1, this is used for the supporting mechanism of captive balloon ground installation anchoring platform, including elevating rocker arm (1), liter
Drop slowdown module (2), automatic leveling module (3), semitrailer (4), telescopic outrigger, fulcrum bearing (7), half spindle nose (8), road wheel
(10), wheelspan adjusting screw rod (11) and intermediate connecting rod (12).
Telescopic outrigger is divided into telescopic outrigger canned paragraph (5) and telescopic outrigger telescopic section (6)；Telescopic outrigger is using bar essence
Milling, boring processing, realize telescopic outrigger canned paragraph (5) and telescopic outrigger telescopic section (6) precision-fit, eliminate gap, mutually more conventional
Yue Site supporting legs, its horizontal bearing and vertical bearing ability it is strong, it is ensured that whole bearing requirements of the platform during inbound/outbound process, make
Use security and the reliability.
Elevating rocker arm (1) connects telescopic outrigger by lifting slowdown module (2), and can drive telescopic outrigger canned paragraph
(5) with telescopic outrigger telescopic section (6) relative motion.Lifting slowdown module (2) adopts planetary reduction gear, using its big retarding ratio,
Make lifting (extending and retracting) operation of supporting mechanism lighter.
Telescopic outrigger canned paragraph (5) is connected with semitrailer (4) by high-strength bolt, supports semi-trailer frame.
Automatic leveling module (3) when telescopic outrigger ground connection supporting anchoring platform, realizes anchoring on telescopic outrigger
The automatic leveling of platform.
Telescopic outrigger lower end is connected with half spindle nose (8) by fulcrum bearing (7), is led between half spindle nose (8) and rail wheel (10)
Cross cylinder roller bearing (9) connection；When needing anchoring platform to launch, placement activity jacking block below fulcrum bearing (7), as anchoring
The supporting stress point of platform.Supporting mechanism is walked in orbit by rail wheel, drives anchoring platform to be moved into and out ball along track
Storehouse.
In order to improve stressing conditions when supporting leg is supported in orbit, in half spindle nose of anchoring platform both sides telescopic outrigger
(8) prevent two-side supporting mechanism residing for orbit altitude difference from causing additional bending moment using being articulated and connected with wheelspan adjusting screw rod (11)
Or it is stuck, it is allowed to there is certain difference in height, to adapt to ground or track alignment error that may be present.Wheelspan adjusting screw rod
(11) it is threaded connection with intermediate connecting rod (12), realizes that wheelspan is adjustable, different in width track can be well adapted to, improves system
The adaptability of system.
The anchoring platform support mechanism has been applied on China's model captive balloon, and the model captive balloon has fixation concurrently
Two kinds of use patterns of formula and motor driven, you can use in fixed position, again can transition transport, in the wild preliminary position use, and
And possess good performance, improve the use range of captive balloon system.
Although embodiments of the invention have been shown and described above, it is to be understood that above-described embodiment is example
Property, it is impossible to limitation of the present invention is interpreted as, one of ordinary skill in the art is in the principle and objective without departing from the present invention
In the case of above-described embodiment can be changed within the scope of the invention, change, replace and modification.
Claims (3)
1. it is a kind of for captive balloon ground installation anchor platform supporting mechanism, it is characterised in that：Including elevating rocker arm (1),
Lifting slowdown module (2), automatic leveling module (3), semitrailer (4), telescopic outrigger, fulcrum bearing (7), half spindle nose (8), road wheel
(10), wheelspan adjusting screw rod (11) and intermediate connecting rod (12)；
Telescopic outrigger is divided into telescopic outrigger canned paragraph (5) and telescopic outrigger telescopic section (6)；
Elevating rocker arm (1) by lift slowdown module (2) connect telescopic outrigger, and can drive telescopic outrigger canned paragraph (5) with
Telescopic outrigger telescopic section (6) relative motion；
Telescopic outrigger canned paragraph (5) is connected with semitrailer (4) by bolt, supports semi-trailer frame；
Automatic leveling module (3) when telescopic outrigger ground connection supporting anchoring platform, realizes anchoring platform on telescopic outrigger
Automatic leveling；
Telescopic outrigger lower end is connected with half spindle nose (8) by fulcrum bearing (7), by circle between half spindle nose (8) and rail wheel (10)
Post roller bearing (9) connects；When needing anchoring platform to launch, placement activity jacking block below fulcrum bearing (7), as anchoring platform
Supporting stress point；
Half spindle nose (8) is connected with wheelspan adjusting screw rod (11), and wheelspan adjusting screw rod (11) is connected by screw thread with intermediate connecting rod (12)
Connect, realize that wheelspan is adjustable.
2. according to claim 1 it is a kind of for captive balloon ground installation anchor platform supporting mechanism, it is characterised in that：
Telescopic outrigger is processed using bar finish-milling, boring, realizes telescopic outrigger canned paragraph (5) and telescopic outrigger telescopic section (6) precision-fit.
3. according to claim 1 it is a kind of for captive balloon ground installation anchor platform supporting mechanism, it is characterised in that：
Half spindle nose (8) is articulated and connected with wheelspan adjusting screw rod (11).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611112059.5A CN106542076B (en) | 2016-12-07 | 2016-12-07 | A kind of supporting mechanism for captive balloon ground installation anchoring platform |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611112059.5A CN106542076B (en) | 2016-12-07 | 2016-12-07 | A kind of supporting mechanism for captive balloon ground installation anchoring platform |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN106542076A true CN106542076A (en) | 2017-03-29 |
| CN106542076B CN106542076B (en) | 2018-08-31 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201611112059.5A Active CN106542076B (en) | 2016-12-07 | 2016-12-07 | A kind of supporting mechanism for captive balloon ground installation anchoring platform |
Country Status (1)
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Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108225411A (en) * | 2017-12-13 | 2018-06-29 | 中国特种飞行器研究所 | A kind of multifunction test measuring device |
| CN109229383A (en) * | 2018-10-17 | 2019-01-18 | 中国特种飞行器研究所 | One kind is novel to be tethered at unmanned plane |
| CN111746777A (en) * | 2020-06-01 | 2020-10-09 | 中国科学院空天信息创新研究院 | Collapsible hidden captive balloon holds in palm ball device |
| WO2022143177A1 (en) * | 2020-12-31 | 2022-07-07 | 同方威视技术股份有限公司 | Conveying device used for radiation inspection and radiation inspection system |
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| FR2761456A1 (en) * | 1997-04-01 | 1998-10-02 | Elemia | Mobile aerial lighting installation |
| CN101898633A (en) * | 2010-04-28 | 2010-12-01 | 湖南航天管理局 | All-in-one anchoring trailer |
| KR20110109476A (en) * | 2010-03-31 | 2011-10-06 | 주식회사 에너게일 | Mooring apparatus for aerial wind power generating floating body |
| CN202414173U (en) * | 2011-12-13 | 2012-09-05 | 湖南航天机电设备与特种材料研究所 | Fixed mooring system for tethered balloon |
| CN103482053A (en) * | 2012-11-27 | 2014-01-01 | 中国科学院光电研究院 | Anchoring device for captive balloon |
| CN205707280U (en) * | 2016-04-28 | 2016-11-23 | 湖南航天远望科技有限公司 | A kind of motor driven captive balloon ground tackle |
-
2016
- 2016-12-07 CN CN201611112059.5A patent/CN106542076B/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2761456A1 (en) * | 1997-04-01 | 1998-10-02 | Elemia | Mobile aerial lighting installation |
| KR20110109476A (en) * | 2010-03-31 | 2011-10-06 | 주식회사 에너게일 | Mooring apparatus for aerial wind power generating floating body |
| CN101898633A (en) * | 2010-04-28 | 2010-12-01 | 湖南航天管理局 | All-in-one anchoring trailer |
| CN202414173U (en) * | 2011-12-13 | 2012-09-05 | 湖南航天机电设备与特种材料研究所 | Fixed mooring system for tethered balloon |
| CN103482053A (en) * | 2012-11-27 | 2014-01-01 | 中国科学院光电研究院 | Anchoring device for captive balloon |
| CN205707280U (en) * | 2016-04-28 | 2016-11-23 | 湖南航天远望科技有限公司 | A kind of motor driven captive balloon ground tackle |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108225411A (en) * | 2017-12-13 | 2018-06-29 | 中国特种飞行器研究所 | A kind of multifunction test measuring device |
| CN108225411B (en) * | 2017-12-13 | 2020-08-11 | 中国特种飞行器研究所 | Multifunctional test measuring device |
| CN109229383A (en) * | 2018-10-17 | 2019-01-18 | 中国特种飞行器研究所 | One kind is novel to be tethered at unmanned plane |
| CN111746777A (en) * | 2020-06-01 | 2020-10-09 | 中国科学院空天信息创新研究院 | Collapsible hidden captive balloon holds in palm ball device |
| CN111746777B (en) * | 2020-06-01 | 2021-09-28 | 中国科学院空天信息创新研究院 | Collapsible hidden captive balloon holds in palm ball device |
| WO2022143177A1 (en) * | 2020-12-31 | 2022-07-07 | 同方威视技术股份有限公司 | Conveying device used for radiation inspection and radiation inspection system |
Also Published As
| Publication number | Publication date |
|---|---|
| CN106542076B (en) | 2018-08-31 |
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