CN106742029A - A kind of anchor launched for small-sized captive balloon automatic inflating puts device - Google Patents

A kind of anchor launched for small-sized captive balloon automatic inflating puts device Download PDF

Info

Publication number
CN106742029A
CN106742029A CN201611201173.5A CN201611201173A CN106742029A CN 106742029 A CN106742029 A CN 106742029A CN 201611201173 A CN201611201173 A CN 201611201173A CN 106742029 A CN106742029 A CN 106742029A
Authority
CN
China
Prior art keywords
anchor
balloon
nose
puts device
captive balloon
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
Application number
CN201611201173.5A
Other languages
Chinese (zh)
Other versions
CN106742029B (en
Inventor
张泰华
张冬辉
何泽青
栗颖思
宋凯
付强
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Academy of Opto Electronics of CAS
Original Assignee
Academy of Opto Electronics of CAS
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Academy of Opto Electronics of CAS filed Critical Academy of Opto Electronics of CAS
Priority to CN201611201173.5A priority Critical patent/CN106742029B/en
Publication of CN106742029A publication Critical patent/CN106742029A/en
Application granted granted Critical
Publication of CN106742029B publication Critical patent/CN106742029B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64FGROUND 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
    • B64F1/00Ground or aircraft-carrier-deck installations
    • B64F1/12Ground or aircraft-carrier-deck installations for anchoring aircraft
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64BLIGHTER-THAN AIR AIRCRAFT
    • B64B1/00Lighter-than-air aircraft
    • B64B1/66Mooring attachments
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64FGROUND 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
    • B64F1/00Ground or aircraft-carrier-deck installations
    • B64F1/12Ground or aircraft-carrier-deck installations for anchoring aircraft
    • B64F1/14Towers or masts for mooring airships or balloons

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Tents Or Canopies (AREA)

Abstract

The present invention relates to the anchoring field of captive balloon, more particularly to a kind of anchor launched for small-sized captive balloon automatic inflating puts device, the mooring guy and the anchoring rope for keeping the empty position high of balloon of lift-off height for adjusting balloon are provided with the captive balloon, the anchor puts device includes the capstan winch of the mooring guy for manipulating captive balloon, nose tower for fixing the anchoring rope of captive balloon, it is characterized in that, the anchor puts device also to be included framework and is arranged on framework top for loading the ball case of captive balloon, the ball case includes ball box main body, the right cover plate being turnably connected with the turnable left cover being connected of the left side wall of ball box main body and with the right side wall of ball box main body.The anchor that the present invention is improved puts device and can realize that captive balloon is inflating expanded, simple to operate, safe and transport transition is convenient.

Description

A kind of anchor launched for small-sized captive balloon automatic inflating puts device
Technical field
It is more particularly to a kind of to be used for small-sized captive balloon automatic inflating exhibition the present invention relates to the anchoring field of captive balloon The anchor opened puts device.
Background technology
Captive balloon belongs to one kind of aerostatics, and aerial buoyance lift is realized using the buoyancy of gas in spheroid.By controlling system The length of balloon bottom mooring guy is stayed, the adjustable height of captive balloon can be controlled, by the pact for controlling captive balloon anchoring rope Beam, makes operation balloon be in anchoring or captive.Hollow panel is risen as one kind, captive balloon can provide larger for balloon borne equipment Vision range over the ground, stagnant outage degree is higher, and coverage is bigger.Therefore, captive balloon can be used for air and environmental monitoring, seize The civil areas such as private, in military domain, are typically used for early warning, electronic countermeasure, technical search and monitoring, myriametric wave communication, letter The aspects such as breath relaying.
No matter it is tethered in the air or anchored condition, in order to stop in atmosphere, it is necessary to pass through heaving pile or ground tackle flat Weighing apparatus air drag.Due to the difference of captive balloon volume, suffered air drag is different, thus required ground tackle is big Small, weight is also not quite similar., it is necessary to the captive balloon of small volume can meet need in sky for the load of lighter in weight Ask.Volume less than hectostere can the small-sized captive balloon that launches of automatic inflating because of it, to transport transition convenient, it is simple to operate, more It is taken seriously and extensive use to get over.But captive balloon is integrally streamlined, the aerodynamic drag very little after inflation shaping, and In gas replenishment process, because utricule is shapeless, aerodynamic drag is big, and surface wind greatly affected operation and safety.
The content of the invention
(1) technical problem to be solved
Device is put it is an object of the invention to provide a kind of anchor launched for small-sized captive balloon automatic inflating, the anchor puts dress Putting can realize that captive balloon is inflating expanded, simple to operate, safe and transport transition is convenient.
(2) technical scheme
In order to solve the above-mentioned technical problem, the invention provides a kind of anchor launched for small-sized captive balloon automatic inflating Device is put, the mooring guy of lift-off height for adjusting balloon and the high-altitude for keeping balloon are provided with the captive balloon The anchoring rope of position, the anchor puts device includes the capstan winch of the mooring guy for manipulating captive balloon, for fixing captive balloon The nose tower of anchoring rope, wherein, the anchor puts device also to be included framework and is arranged on framework top for loading the ball of captive balloon Case, the ball case include the left side wall of ball box main body and ball box main body turnably the left cover of connection and with ball box main body The right cover plate that right side wall is turnably connected.
Wherein, also including the ball support being connected with the ball case under open mode, the ball support include bending separately down the A connection piece and the second connector, front end of first connector respectively with the left cover and the right cover plate are detachable Connection, second connector respectively with the left cover and the rear end detachable connection of the right cover plate.
Wherein, also including lockable mechanism, first connector is respectively by lockable mechanism and the left cover and described Right cover plate locking, second connector passes through lockable mechanism and the left cover and the right cover plate locking respectively.
Wherein, under the ball case open mode, the left cover is 90 ° -150 ° with the angle of the ball case upper surface, The right cover plate is 90 ° -150 ° with the angle of the ball case upper surface.
Wherein, the nose tower is connected with the ball case, and the ball case is connected on the framework in a rotatable manner.
Wherein, the nose tower includes the nose tower crossbeam that one end is connected with the ball case, and the other end with nose tower crossbeam is pivotally connected Nose tower vertical beam, the free end of nose tower vertical beam is provided with nose cone pad, the nose tower also includes diagonal brace, and the two ends of the diagonal brace are distinguished It is connected with nose tower crossbeam and nose tower vertical beam.
Wherein, the nose tower vertical beam is folding.
Wherein, the 3rd connector is additionally provided with the ball case, the nose tower crossbeam of the nose tower is connected with the described 3rd Part detachable connection.
Wherein, the base of frame is provided with height-adjustable supporting leg, and the supporting leg is connected to the frame in a rotatable manner On frame.
Wherein, the base of frame is provided with the movable pulley for aiding in the anchor to put device movement.
(3) beneficial effect
The anchor launched provided by the present invention for small-sized captive balloon automatic inflating puts device and captive balloon anchor is put into device Integrate, fully taken into account expansion folding and unfolding and the transport two states of balloon, and it is simple to operate, it is safe, with pole Big flexibility and versatility higher, can locality for a long time service in sky, it is also possible to by transporting equipment by its Captive carries out transition transport, can be widely used for various load such as earth observation, communication relay, Atmospheric Survey, aerial reconnaissance Rapid deployment.
Brief description of the drawings
Fig. 1 is the structural representation that a kind of anchor launched for small-sized captive balloon automatic inflating according to the present invention puts device Figure;
Fig. 2 is that the anchor in Fig. 1 puts the structural representation that the captive balloon of device carrying is under anchored condition;
Fig. 3 is that the anchor in Fig. 1 puts the structural representation that the captive balloon of device carrying is under captive;
Fig. 4 is that the anchor in Fig. 1 puts structural representation of the device under nose tower deployed condition;And
Fig. 5 is that the anchor in Fig. 1 puts the structural representation that device is under collapsed transportable state.
In figure, 1:Framework;11:Supporting leg;2:Ball case;21:Ball box main body;22:Right cover plate;23:Left cover;3:Ball support;31: First connector;32:Second connector;4:Nose tower;41:Nose tower crossbeam;42:First nose tower vertical beam;43:Second nose tower vertical beam; 44:Nose cone pad;45:Diagonal brace;5:Captive balloon;6:Mooring guy;7:Turntable bearing;8:3rd connector.
Specific embodiment
With reference to the accompanying drawings and examples, specific embodiment of the invention is described in further detail.Following instance For illustrating the present invention, but it is not limited to the scope of the present invention.
In the description of the invention, it is necessary to illustrate, unless otherwise clearly defined and limited, term " installation ", " phase Company ", " connection " should be interpreted broadly, for example, it may be being fixedly connected, or being detachably connected, or be integrally connected;Can Being to mechanically connect, or electrically connect;Can be joined directly together, it is also possible to be indirectly connected to by intermediary, Ke Yishi Two connections of element internal.For the ordinary skill in the art, with concrete condition above-mentioned term can be understood at this Concrete meaning in invention.
Fig. 1 to Fig. 5 shows that a kind of anchor launched for small-sized captive balloon automatic inflating of the invention puts device A preferred embodiment.As illustrated, the lift-off height for adjusting captive balloon 5 is provided with the captive balloon 5 is Rope 6 and the anchoring rope (not shown) for keeping the empty position high of captive balloon 5 are stayed, the anchor puts device to be included being tethered at for manipulation The capstan winch (not shown) of the mooring guy 6 of balloon 5, the nose tower 4 of the anchoring rope for fixing captive balloon 5, nose tower 4 is the anchor of balloon 5 The key equipment of ground windage is resisted under pool state, captive balloon 5 is acted on ground by windage, nose tower 4 will be balanced and constrained Ground windage, it is ensured that the safety of captive balloon 5.The anchor puts device also includes framework 1, and capstan winch is arranged on inside framework 1, is being tethered at gas Balloon 5 is controlled to lift by way of discharging or drawing capstan winch in when ball 5 is lifted;The anchor puts device also to be included being arranged on framework 1 The ball case 2 of side, ball case 2 is mainly used in loading the balloon 5 after deflating, and during the inflation Automatic-expanding of balloon 5, balloon 5 will be whole Body is inflated and Automatic-expanding in ball case 2, and specifically, the ball case 2 includes ball box main body 21, and the left side with ball box main body 21 The right cover plate 22 of the turnable connection of wall and the left cover 23 being turnably connected with the right side wall of ball box main body 21.
When captive balloon 5 needs to launch, gas tube is connected, open helium valve, you can start balloon inflation, balloon 5 In gas replenishment process, will be gradually spread out in ball case 2, until shaping enters anchored condition;Hung to the captive balloon 5 under anchored condition Load is carried, balloon 5 possesses a liter empty condition, according to task needs, can quickly go up to the air;After load has performed task, draw in and twist Disk, just draws captive balloon 5 in from captive, and then switch to anchored condition;After the completion of whole experiment, by captive balloon 5 Helium discharge, after balloon 5 gradually draws in, be folded within ball case 2.During transport, balloon 5 is drawn in ball case 2, whole device In folded state, can be transported by jubilee wagen or picking-up vehicle as needed, can be transported to deployment in Class II highway or hill path Place, and then realize rapid deployment.The anchor that the present invention is provided puts device and can realize that Automatic-expanding is inflated on captive balloon ground, The short distance transition of balloon 5 and long-distance transport can be carried out;Additionally, the apparatus structure is compact, required for balloon is transported and disposed Condition is relatively low, safe, and simple to operate, needs 2 operating personnel to complete balloon inflation and launches deployment.
Specifically, turntable bearing 7 is provided with framework 1, ball case 2 is connected by turntable bearing 7 with capstan winch framework 1, with So that ball case 2 can be rotated freely around turntable bearing 7.In anchored condition, ball case 2 and captive balloon 5 can with the wind around turntable bearing 7 Rotate freely so that captive balloon 5 is in real time in state with the wind.
Additionally, the anchor puts device also includes the ball support 3 for being used to hold up balloon 5, specifically, the ball support includes curved separately down Bent the first connector 31 and the second connector 32, wherein the two ends of the first connector 31 are plugged into the ball under open mode respectively In the hole on the top of the right cover plate 22 of case 2 and the rear end of left cover 23, the two ends of the second connector 32 are plugged into open shape respectively In the hole on the top of the right cover plate 22 of the ball case 2 under state and the front end of left cover 23.Can in order to ensure that ball support 3 is connected with ball case 2 Lean on, the anchor puts device also to be included for the first connector 31 (such as to be inserted with the lockable mechanism of right cover plate 22, the locking of left cover 23 Pin), and for by the second connector 32 and right cover plate 22, the lockable mechanism (such as latch) of the locking of left cover 23.The ball support 3 It is buffer unit that balloon 5 and anchor are put between device, is also support of the balloon 5 in anchored condition, when balloon 5 is subject to ground not Steady air flow, and when causing stern settlement, ball support 3 will hold up the afterbody of balloon 5, it is ensured that balloon 5 is maintained at safe altitude with ground It is interior.
Although showing the first connector 31, the second connector 32 in this embodiment in the form of bend pipe, this area It will be appreciated by the skilled person that the first connector 31, the second connector 32 can also take other form, such as plate-like piece etc..
Nose tower 4 is connected to the nose tower crossbeam 41 of ball case 2 including one end, and the nose tower being pivotally connected with the other end of nose tower crossbeam 41 stands Beam, nose cone pad 44 is provided with the free end of nose tower vertical beam.In order to ensure the steadiness of nose tower 4, the nose tower also includes diagonal brace 45, The two ends of the diagonal brace 45 are connected with nose tower crossbeam 41 and nose tower vertical beam respectively.Specifically, diagonal brace 45 is by pin and nose tower vertical beam Connection, and be turnably connected with nose tower crossbeam 41, the groove for accommodating diagonal brace 45 is provided with nose tower crossbeam 41, as general When nose tower 4 is packed up, diagonal brace 45 can be separated with nose tower vertical beam, and be turned into the groove of nose tower crossbeam 41.Further, Because nose tower vertical beam has larger length, thus nose tower vertical beam include the first nose tower vertical beam 42 and by folding joint (for example Bearing pin) the second nose tower vertical beam 43 for being connected with the first nose tower vertical beam 42, found the first nose tower when device is packed up anchor to be put The nose tower vertical beam 43 of beam 42 and second is folded, so that anchor puts device in collapsed state with minimum size and body Product.In order to ensure the stability in the deployed state of nose tower 4, the nose tower is additionally provided with for by the first nose tower vertical beam 42 and second The spacer pin that nose tower vertical beam 43 is fixed in the deployed state.
It should be noted that, although in this embodiment, nose tower vertical beam includes that the first nose tower that can be folded stands The nose tower vertical beam 43 of beam 42 and second, it should be appreciated to those skilled in the art that nose tower vertical beam may include to fold Multiple nose tower vertical beams so that the anchor puts device in collapsed state with minimum size and volume.
Additionally, in order that nose tower 4 is firm with the connection of ball case 2, the anchor puts device also includes the be arranged on ball case the 3rd Connector 8, nose tower crossbeam 41 is connected by bolt with the 3rd connector 8.In anchored condition, because ball case 2 can with the wind around rotating disk Bearing 7 is rotated freely so that nose tower 4 can also be rotated freely around turntable bearing 7 with the wind, makes captive balloon 5 in real time in shape with the wind State.
In the embodiment shown, capstan winch is driven by motor, and it rotates and causes that the mooring guy 6 of balloon 5 is retracted to capstan winch Or from capstan winch pine oil, so that the length of the mooring guy 6 of modulated in real time balloon 5, and then control the lift-off of balloon 5 highly.In frame The wire-arranging mechanism being connected with capstan winch is additionally provided with inside frame 1, to obtain the length of the mooring guy of balloon 5.
Additionally, framework 1 is provided below movable pulley to facilitate anchor to put the movement of device.When needing to move, pushing meanss, Short-distance movement can be carried out.
In order that framework 1 has more preferable support function, height-adjustable supporting leg 11 is also provided with framework 1, When balloon 5 works, supporting leg 11 is risen, movable pulley is departed from into ground.Such structure is especially suitable for the uneven use environment in ground, Because framework 1 can be made to be in level or other suitable positions by adjusting the height of supporting leg 11.Meanwhile, supporting leg 11 is in level The length in direction can also increase the moment of resistance of toppling of framework 1 so that framework 1 has more preferable stability.The supporting leg 11 with The mode being hinged is connected to the framework 1, so as to when anchoring balloon 5 is needed, launch the supporting leg 11 larger to obtain Topple the moment of resistance, and volume is convenient to transport that can reduce can to pack up the supporting leg 11 when transport is needed.Certainly, the supporting leg 11 Can also be connected on capstan winch framework 1 in other modes of being rotatably connected.
The operating procedure that anchor of the invention puts device includes:
(1) preparatory stage
Supporting leg 11 is launched first, and is flatly put with allowing the anchor to put device according to the height that surface state adjusts supporting leg 11 Put on the ground;Nose tower 4 is launched into connection afterwards, nose cone pad 44 is arranged in the second nose tower vertical beam 43, the second nose tower vertical beam 43 and first are connected between nose tower vertical beam 42 by pivot pin, are spread out, and install spacer pin;The first nose tower after by expansion stands Beam 42 is connected with nose tower crossbeam 41, adjusts the first nose tower vertical beam 42 and nose tower crossbeam 41, it is kept vertical, by the two ends of diagonal brace 45 It is connected between the first nose tower vertical beam 42 and nose tower crossbeam 41;Nose tower crossbeam 41 is bolted with the 3rd connector 8, such as schemes Shown in 4.Then the right cover plate 22 and left cover 23 of ball case 2 are opened, reaches it and open near spacing, by the first of ball support 3 The connector 32 of connector 31 and second is inserted in the end jack of ball case right cover plate 22 and left cover 23 respectively, in place rear locking machine Structure can be locked automatically, as shown in Figure 1.
(2) it is inflating expanded
When weather condition meets the lift-off experiment of captive balloon 5, start balloon 5 and inflate.Now, not deployed captive balloon 5 are in folded state, draw within ball case 2, and the charge valve of captive balloon 5 is connected with helium gas tube, open helium valve, give Captive balloon 5 is inflated, and captive balloon 5 will gradually spread out shaping in ball case 2, and with the utricule of captive balloon 5, helium increases, and is Staying balloon 5 will switch to net light state by net weight, mooring guy 6 will gradually load, and constrain captive balloon 5, keep it in ball case 2 Within the constraint framework of ball support 3, after system inflation is finished, anchored condition is ultimately at.In anchored condition, ball case 2, nose tower 4 Can freely be rotated around turntable bearing 7 with the wind with captive balloon 5, its captive balloon 5 is in real time in state with the wind.
(3) ball is received with transport
Task terminates, it is necessary to when receiving ball, operation order is substantially opposite with expansion order.
The helium gas tube of captive balloon 5 is connected first, after the helium in the utricule of captive balloon 5 is discharged, is folded Within ball case 2, the connection between helium gas tube and captive balloon 5 is then released;Take out the He of the first connector 31 of ball support 3 Latch between second connector 32 and ball case right cover plate 22 and left cover 23, the first connector 31 and second of ball support 3 is connected Fitting 32 takes out from the jack of ball case right cover plate 22 and left cover 23 respectively, closes up ball case right cover plate 22 and left cover 23.So The dismounting of nose tower 4 is carried out afterwards, by the disassembling bolts between nose tower crossbeam 41 and connecting plate 8, nose tower 4 is removed, by diagonal brace 45 and Pin between one nose tower vertical beam 42 is extracted, in diagonal brace 45 is drawn the groove of nose tower crossbeam 41 in;Take out the second nose tower vertical beam 43 and the first spacer pin between nose tower vertical beam 42, drawn in;Remove the company between nose cone pad 44 and the second nose tower vertical beam 43 Connect.Now, anchor puts device and is in collapsed state, and compared with its deployed condition when using, weight and volume is obviously reduced, from And can easily be preserved or be transported.
Presently preferred embodiments of the present invention is the foregoing is only, is not intended to limit the invention, it is all in essence of the invention Within god and principle, any modification, equivalent substitution and improvements made etc. should be included within the scope of the present invention.

Claims (10)

1. a kind of anchor launched for small-sized captive balloon automatic inflating puts device, is provided with for adjusting on the captive balloon The mooring guy and the anchoring rope for keeping the empty position high of balloon of the lift-off height of balloon, the anchor puts device to be included for manipulating The capstan winch of the mooring guy of captive balloon, the nose tower of the anchoring rope for fixing captive balloon, it is characterised in that the anchor puts device also Including framework and it is arranged on framework top and includes ball box main body and ball case master for loading the ball case of captive balloon, the ball case The left cover of the turnable connection of the left side wall of body and the right cover plate being turnably connected with the right side wall of ball box main body.
2. anchor as claimed in claim 1 puts device, it is characterised in that the also ball including being connected with the ball case under open mode Support, the ball support includes the first connector and the second connector that bend separately down, first connector respectively with it is described The front end detachable connection of left cover and the right cover plate, second connector respectively with the left cover and the right cover The rear end detachable connection of plate.
3. anchor as claimed in claim 2 puts device, it is characterised in that also including lockable mechanism, the first connector difference By lockable mechanism and the left cover and the right cover plate locking, second connector respectively by lockable mechanism with it is described Left cover and the right cover plate locking.
4. anchor according to claim 1 puts device, it is characterised in that under the ball case open mode, the left cover It it is 90 ° -150 ° with the angle of the ball case upper surface, the right cover plate is 90 ° -150 ° with the angle of the ball case upper surface.
5. anchor according to claim 1 puts device, it is characterised in that the nose tower is connected with the ball case, the ball case It is connected in a rotatable manner on the framework.
6. anchor according to claim 1 puts device, it is characterised in that the nose tower includes what one end was connected with the ball case Nose tower crossbeam, the nose tower vertical beam being pivotally connected with the other end of nose tower crossbeam, is provided with nose cone pad, the nose in the free end of nose tower vertical beam Tower also includes diagonal brace, and the two ends of the diagonal brace are connected with nose tower crossbeam and nose tower vertical beam respectively.
7. anchor according to claim 6 puts device, it is characterised in that the nose tower vertical beam is folding.
8. anchor according to claim 6 puts device, it is characterised in that be additionally provided with the 3rd connector on the ball case, The nose tower crossbeam of the nose tower and the 3rd connector detachable connection.
9. the anchor according to any one of claim 1-8 puts device, it is characterised in that the base of frame is provided with adjustable The supporting leg of height, the supporting leg is connected on the framework in a rotatable manner.
10. the anchor according to any one of claim 1-8 puts device, it is characterised in that the base of frame be provided with for The anchor is aided in put the movable pulley of device movement.
CN201611201173.5A 2016-12-22 2016-12-22 Anchor device for automatic inflation and deployment of small tethered balloon Active CN106742029B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201611201173.5A CN106742029B (en) 2016-12-22 2016-12-22 Anchor device for automatic inflation and deployment of small tethered balloon

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201611201173.5A CN106742029B (en) 2016-12-22 2016-12-22 Anchor device for automatic inflation and deployment of small tethered balloon

Publications (2)

Publication Number Publication Date
CN106742029A true CN106742029A (en) 2017-05-31
CN106742029B CN106742029B (en) 2023-10-27

Family

ID=58899717

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201611201173.5A Active CN106742029B (en) 2016-12-22 2016-12-22 Anchor device for automatic inflation and deployment of small tethered balloon

Country Status (1)

Country Link
CN (1) CN106742029B (en)

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107873351A (en) * 2017-12-12 2018-04-06 程鹏 A kind of weather modification is tethered at plume and is tethered at cigarette stove
CN109515678A (en) * 2018-10-17 2019-03-26 中国特种飞行器研究所 Platform and method of deploying is unfolded in the small-sized automatic fast aeration of spindle spheric captive balloon
CN110194428A (en) * 2018-02-26 2019-09-03 东莞前沿技术研究院 A kind of captive balloon utricule dimension inspection high altitude operation control system
CN111114736A (en) * 2019-12-27 2020-05-08 中国特种飞行器研究所 Captive balloon, ground equipment and helium-filled automatic unfolding method
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
CN111776193A (en) * 2020-07-30 2020-10-16 青岛德瑞高机械有限公司 Mooring balloon anchoring device
CN112478123A (en) * 2020-11-27 2021-03-12 中国科学院空天信息创新研究院 Nose tower end structure of mooring balloon anchoring facility
CN112550657A (en) * 2020-11-06 2021-03-26 中国特种飞行器研究所 Tethered balloon integrated comprehensive operation guarantee platform and use method thereof
CN112591070A (en) * 2020-11-23 2021-04-02 中国科学院空天信息创新研究院 Ball supporting frame and ball supporting frame assembly of captive balloon anchoring facility
CN112703154A (en) * 2018-07-23 2021-04-23 Adf集团 System and method for mooring an aircraft or airship balloon-type aerial vehicle
CN112722230A (en) * 2021-03-02 2021-04-30 湖南航天远望科技有限公司 Marine type captive balloon system and using method thereof

Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB213607A (en) * 1923-03-31 1924-06-05 Enrico Forlanini Improvements in anchoring devices for airships
US3976268A (en) * 1975-04-08 1976-08-24 The United States Of America As Represented By The Secretary Of The Air Force Tethered balloon mooring means
EP0781703A1 (en) * 1995-12-29 1997-07-02 Aerophile S.A. Balloon ground anchoring method and ground infrastructure therefor
CN201553299U (en) * 2009-09-03 2010-08-18 深圳市安托山特种机械有限公司 Weight balancing trolley for mooring ball
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
US20160200235A1 (en) * 2013-09-11 2016-07-14 Silicis Technologies, Inc. Trailer for autonomous vehicle
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
CN206336443U (en) * 2016-12-22 2017-07-18 中国科学院光电研究院 A kind of anchor deployed for small-sized captive balloon automatic inflating puts device

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB213607A (en) * 1923-03-31 1924-06-05 Enrico Forlanini Improvements in anchoring devices for airships
US3976268A (en) * 1975-04-08 1976-08-24 The United States Of America As Represented By The Secretary Of The Air Force Tethered balloon mooring means
EP0781703A1 (en) * 1995-12-29 1997-07-02 Aerophile S.A. Balloon ground anchoring method and ground infrastructure therefor
CN201553299U (en) * 2009-09-03 2010-08-18 深圳市安托山特种机械有限公司 Weight balancing trolley for mooring ball
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
US20160200235A1 (en) * 2013-09-11 2016-07-14 Silicis Technologies, Inc. Trailer for autonomous vehicle
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
CN206336443U (en) * 2016-12-22 2017-07-18 中国科学院光电研究院 A kind of anchor deployed for small-sized captive balloon automatic inflating puts device

Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107873351A (en) * 2017-12-12 2018-04-06 程鹏 A kind of weather modification is tethered at plume and is tethered at cigarette stove
CN110194428A (en) * 2018-02-26 2019-09-03 东莞前沿技术研究院 A kind of captive balloon utricule dimension inspection high altitude operation control system
CN110194428B (en) * 2018-02-26 2024-04-30 深圳光启空间技术有限公司 High-altitude operation control system for tethered balloon body maintenance
CN112703154A (en) * 2018-07-23 2021-04-23 Adf集团 System and method for mooring an aircraft or airship balloon-type aerial vehicle
CN112703154B (en) * 2018-07-23 2023-12-05 Adf集团 System and method for mooring an aircraft or airship balloon-type aeronautical vehicle
CN109515678A (en) * 2018-10-17 2019-03-26 中国特种飞行器研究所 Platform and method of deploying is unfolded in the small-sized automatic fast aeration of spindle spheric captive balloon
CN109515678B (en) * 2018-10-17 2022-04-19 中国特种飞行器研究所 Automatic quick inflation and deployment platform and deployment method for small spindle-shaped captive balloon
CN111114736A (en) * 2019-12-27 2020-05-08 中国特种飞行器研究所 Captive balloon, ground equipment and helium-filled automatic unfolding method
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
CN111776193A (en) * 2020-07-30 2020-10-16 青岛德瑞高机械有限公司 Mooring balloon anchoring device
CN112550657A (en) * 2020-11-06 2021-03-26 中国特种飞行器研究所 Tethered balloon integrated comprehensive operation guarantee platform and use method thereof
CN112591070A (en) * 2020-11-23 2021-04-02 中国科学院空天信息创新研究院 Ball supporting frame and ball supporting frame assembly of captive balloon anchoring facility
CN112478123A (en) * 2020-11-27 2021-03-12 中国科学院空天信息创新研究院 Nose tower end structure of mooring balloon anchoring facility
CN112722230A (en) * 2021-03-02 2021-04-30 湖南航天远望科技有限公司 Marine type captive balloon system and using method thereof
CN112722230B (en) * 2021-03-02 2023-02-28 湖南航天远望科技有限公司 Ocean type captive balloon system and using method thereof

Also Published As

Publication number Publication date
CN106742029B (en) 2023-10-27

Similar Documents

Publication Publication Date Title
CN106742029A (en) A kind of anchor launched for small-sized captive balloon automatic inflating puts device
US20190217969A1 (en) Portable balloon launch rig
CN103482053B (en) A kind of ground tackle for captive balloon
CN205707280U (en) A kind of motor driven captive balloon ground tackle
US4402479A (en) Small tethered aerostat relocatable system
CN108557051B (en) Tethered balloon sphere, guaranteeing shelter and tethered balloon system thereof
US7690596B2 (en) Apparatus for lighter-than-air aircraft
US20070102570A1 (en) Aircraft
CN106585743A (en) Vehicle-mounted mooring system for large and medium-sized captive balloon
CN111055750B (en) Mooring balloon rapid deployment anchoring system
US11697509B2 (en) Aircraft retrieval system and method
CN206336443U (en) A kind of anchor deployed for small-sized captive balloon automatic inflating puts device
CN110481753B (en) Motorized rapid aerial balloon issuing system
CN105322879B (en) Motorized high-power extension photovoltaic power station
CN206446783U (en) A kind of ground tackle and anchoring car
CN210417008U (en) Unmanned aerial vehicle takes off and retrieves integration operation car
CN111746774B (en) High-altitude balloon issuing system and method
CN219601042U (en) Pull type emergency communication vehicle
CN107585285A (en) A kind of aerostatics dispensing apparatus and its distribution method
RU2339548C1 (en) Mobil device for lighter-than-air craft holding
CN208377040U (en) A kind of ground tackle for captive balloon
CN116394827A (en) Pull type emergency communication vehicle
CN109515678B (en) Automatic quick inflation and deployment platform and deployment method for small spindle-shaped captive balloon
WO2014194341A2 (en) Containment assembly
CN114313208B (en) Quick automatic inflation of captive balloon is put and is flown off streamlined anchoring platform

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