CN201494623U - Aerostat mooring lock - Google Patents
Aerostat mooring lock Download PDFInfo
- Publication number
- CN201494623U CN201494623U CN2009203094984U CN200920309498U CN201494623U CN 201494623 U CN201494623 U CN 201494623U CN 2009203094984 U CN2009203094984 U CN 2009203094984U CN 200920309498 U CN200920309498 U CN 200920309498U CN 201494623 U CN201494623 U CN 201494623U
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- CN
- China
- Prior art keywords
- lock
- hollow
- aerostatics
- mooring
- fast
- 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.)
- Expired - Fee Related
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Abstract
The utility model discloses an aerostat mooring lock, wherein a lock bracket bottom board which is provided with through-holes in the middle portion is connected on the upper portion of one mounting plate through angular contact bearings, the upper surface of the lock bracket bottom board is provided with two reversed U-shaped brackets, the top boards of the two reversed U-shaped brackets are respectively provided with a vertical seat bearing, a fast-pulley is arranged between the vertical posts of two reversed U-shaped brackets, a hollow lock tube whose inner pipe diameter is larger than the outer diameter of a head cone is arranged above the fast-pulley, one end on the lower portion of the hollow lock tube is provided with a strip notch for penetrating in the fast-pulley, and one end of the hollow lock tube is a trumpet guide sleeve, and the other end of the hollow lock tube is connected with a lock connector, and a pin hole for fixing the head cone is arranged on the hollow lock tube. The aerostat mooring lock can generate the rotation freedom on two directions through the angular contact bearings and the vertical seat bearings, can realize the fast rotation in vertical direction and pitching direction, enables the guide sleeve to fast align to the head cone, and realizes the fast fixation of the head cone during an aerostat launches and stops.
Description
Technical field
The utility model relates to a kind of aerostatics mooring lock that is applicable to when large and medium-sized aerostatics is parked on ground.
Background technology
Existing large and medium-sized aerostatics is bigger owing to volume, the destruction that is subjected to high wind in the open when park on ground easily.Safety when guaranteeing that aerostatics is parked should reduce the wind area of aerostatics as far as possible, improves the wind resistance of aerostatics ground when parking.The down wind of weather cock formula arranges and can obviously reduce the load that wind produces aerostatics, and therefore, " down wind layouts " is raising aerostatics ground effective measures of wind resistance when parking.Simultaneously, the stage that aerostatics is parked from landing to, be subjected to the influence of wind field easily, need aerostatics is fixing fast.Its fixing means is to be provided with nose cone at the aerostatics head, and nose cone is provided with string for binding a plait, and the mooring mast that the place is equipped with column or truss structure of parking at aerostatics is fixed on the aerostatics nose cone on the mooring mast.The device that is used for fixing nose cone on the mooring mast claims the mooring lock.Existing mooring lock can not rotate, and makes the axis that the aerostatics head can not rotate with the wind as aerostatics, and simultaneously, fixedly the operation of nose cone is more loaded down with trivial details, takes longlyer, and in this process, aerostatics is subjected to the influence of high wind easily, the accident of damage aerostatics occurs.
The utility model content
The purpose of this utility model is to overcome existing mooring and locks the shortcoming that can not rotate with complex operation, a kind of mooring lock with both direction rotational freedom is provided, and the mooring lock that utilizes this device can realize aerostatics when park on the fixing fast and aerostatics ground of nose cone from the parking period that lands is followed the swing of aerostatics and is rotated.
The technical solution of the utility model: the lock frame base plate that is provided with perforation by angular contact bearing and middle part above an adapter plate is connected, on lock frame base plate, be provided with two ∏ type supports, a plummer block housing bearing is housed respectively on the top board of two ∏ type supports, a fixed pulley is housed between the column of two ∏ type supports, the fixed pulley top is provided with the hollow lock pipe that an interior caliber is slightly larger than the nose cone external diameter, end in hollow lock pipe bottom is provided with a strip shape breach that can stretch into fixed pulley, one end of described hollow lock pipe is the toroidal orienting sleeve, the other end of hollow lock pipe is connected with latching connector, is provided with the fixedly pin hole of nose cone on hollow lock pipe.
Described adapter plate is provided with and is used for the through hole that string for binding a plait passes through.
The pulley cylindrical of described fixed pulley and the line of centers of hollow lock pipe are tangent.
Described latching connector is an end osed top hollow tubular, and latching connector is provided with the through hole that can insert the lock tubular axis, and latching connector is connected and fixed by lock tubular axis and plummer block housing bearing.
The outer ring of described angular contact bearing is installed on the adapter plate, and its inner ring is installed on the lock frame base plate.
When aerostatics is reduced to ground, earlier the string for binding a plait on the nose cone is inserted hollow lock pipe from orienting sleeve, and pass the strip shape breach and walk around fixed pulley, and then pass perforation on the lock frame base plate and the through hole on the adapter plate successively.Make aerostatics near mooring mast by pulling string for binding a plait, simultaneously by the rotational freedom of angular contact bearing with the both direction of band plummer block housing bearing introducing, can realize the rotation and the pitch rotation of mooring lock vertical direction, the mooring lock is rotated the rapid alignment nose cone, and enter in the hollow lock pipe with string for binding a plait pulling nose cone, with Fixed latches nose cone is fixed at last.
The utility model produces the rotational freedom of both direction by angular contact bearing and band plummer block housing bearing, can make the mooring lock realize the twirl of vertical direction and pitch orientation, making the mooring lock can follow aerostatics rotates along with the swing of wind direction, make orienting sleeve rapid alignment nose cone, the realization aerostatics is fixed by the quick of nose cone from the parking period that lands.
Description of drawings
Fig. 1 is the utility model structural representation;
Fig. 2 is the structural representation of lock pipe and latch;
Fig. 3 is the assembling scheme drawing of nose cone and mooring lock.
The specific embodiment
The utility model is described in further detail below in conjunction with drawings and Examples.
With reference to accompanying drawing, present embodiment is provided with perforation 3 lock frame base plate 4 by angular contact bearing 2 and middle part and is connected above adapter plate 1, on lock frame base plate, be provided with two ∏ type supports 5, a plummer block housing bearing 6 is housed respectively on the top board of two ∏ type supports, a fixed pulley 7 is housed between the column of two ∏ type supports, the fixed pulley top is provided with the hollow lock pipe 8 that an interior caliber is slightly larger than the nose cone external diameter, end in hollow lock pipe bottom is provided with a strip shape breach 9, the pulley of fixed pulley extend in the breach, the line of centers of its pulley cylindrical and hollow lock pipe is tangent, strip shape breach one end is connected with latching connector 10, the other end at hollow lock pipe is a toroidal orienting sleeve 11, is provided with the fixedly pin hole 12 of nose cone on hollow lock pipe.Described latching connector is an end osed top hollow tubular, and latching connector is provided with through hole, and latching connector is connected and fixed with plummer block housing bearing 6 by lock tubular axis 13.
When aerostatics is reduced to ground, earlier the string for binding a plait on the nose cone 14 15 is inserted hollow lock pipe from orienting sleeve, pass strip shape breach 9 and walk around fixed pulley 7, and then pass perforation 3 on the lock frame base plate and the through hole 16 on the adapter plate successively.Make aerostatics near mooring mast by pulling string for binding a plait, simultaneously by the rotational freedom of angular contact bearing 2 with the both direction of band plummer block housing bearing 6 introducings, can realize the rotation and the pitch rotation of mooring lock vertical direction, make the orienting sleeve rapid alignment nose cone 14 of lock pipe, and enter in the hollow lock pipe 8 with string for binding a plait pulling nose cone, with Fixed latches 12 nose cone is fixed at last.
Claims (4)
1. an aerostatics mooring is locked, it is characterized in that, the lock frame base plate that is provided with perforation by angular contact bearing and middle part above an adapter plate is connected, on lock frame base plate, be provided with two ∏ type supports, a plummer block housing bearing is housed respectively on the top board of two ∏ type supports, a fixed pulley is housed between the column of two ∏ type supports, the fixed pulley top is provided with the hollow lock pipe that an interior caliber is slightly larger than the nose cone external diameter, end in hollow lock pipe bottom is provided with a strip shape breach that can stretch into fixed pulley, one end of described hollow lock pipe is the toroidal orienting sleeve, the other end of hollow lock pipe is connected with latching connector, is provided with the fixedly pin hole of nose cone on hollow lock pipe.
2. aerostatics mooring lock according to claim 1 is characterized in that described adapter plate is provided with and is used for the through hole that string for binding a plait passes through.
3. aerostatics mooring lock according to claim 1 is characterized in that the pulley cylindrical of described fixed pulley and the line of centers of hollow lock pipe are tangent.
4. aerostatics mooring lock according to claim 1 is characterized in that described latching connector is an end osed top hollow tubular, and latching connector is provided with the through hole that can insert the lock tubular axis, and latching connector is connected and fixed by lock tubular axis and plummer block housing bearing.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2009203094984U CN201494623U (en) | 2009-09-02 | 2009-09-02 | Aerostat mooring lock |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2009203094984U CN201494623U (en) | 2009-09-02 | 2009-09-02 | Aerostat mooring lock |
Publications (1)
Publication Number | Publication Date |
---|---|
CN201494623U true CN201494623U (en) | 2010-06-02 |
Family
ID=42437831
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN2009203094984U Expired - Fee Related CN201494623U (en) | 2009-09-02 | 2009-09-02 | Aerostat mooring lock |
Country Status (1)
Country | Link |
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CN (1) | CN201494623U (en) |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103847978A (en) * | 2014-03-24 | 2014-06-11 | 青岛德瑞高机械有限公司 | Nose plug assembly for airship releasing mooring device |
EP2947000A4 (en) * | 2013-01-18 | 2016-01-27 | Altave Indústria Comércio E Exportação De Aeronaves Ltda Me | Airship-mooring device |
CN106477017A (en) * | 2016-12-05 | 2017-03-08 | 中国特种飞行器研究所 | Formula quick-release nose cone opened by a kind of middle-size and small-size unmanned airship umbrella |
CN108263593A (en) * | 2016-12-30 | 2018-07-10 | 东莞前沿技术研究院 | Lock set is tethered at for captive balloon |
CN109263848A (en) * | 2018-09-28 | 2019-01-25 | 中国电子科技集团公司第三十八研究所 | A kind of dirigible nose cone locking device |
CN111055750A (en) * | 2019-12-13 | 2020-04-24 | 中国特种飞行器研究所 | Mooring balloon rapid deployment anchoring system |
CN112429191A (en) * | 2020-11-20 | 2021-03-02 | 中国科学院空天信息创新研究院 | Nose tower end structure, nose tower subassembly and captive balloon of captive balloon anchor mooring facility |
-
2009
- 2009-09-02 CN CN2009203094984U patent/CN201494623U/en not_active Expired - Fee Related
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2947000A4 (en) * | 2013-01-18 | 2016-01-27 | Altave Indústria Comércio E Exportação De Aeronaves Ltda Me | Airship-mooring device |
CN103847978A (en) * | 2014-03-24 | 2014-06-11 | 青岛德瑞高机械有限公司 | Nose plug assembly for airship releasing mooring device |
CN106477017A (en) * | 2016-12-05 | 2017-03-08 | 中国特种飞行器研究所 | Formula quick-release nose cone opened by a kind of middle-size and small-size unmanned airship umbrella |
CN106477017B (en) * | 2016-12-05 | 2018-07-24 | 中国特种飞行器研究所 | A kind of middle-size and small-size unmanned airship umbrella formula quick-release nose cone |
CN108263593A (en) * | 2016-12-30 | 2018-07-10 | 东莞前沿技术研究院 | Lock set is tethered at for captive balloon |
CN109263848A (en) * | 2018-09-28 | 2019-01-25 | 中国电子科技集团公司第三十八研究所 | A kind of dirigible nose cone locking device |
CN111055750A (en) * | 2019-12-13 | 2020-04-24 | 中国特种飞行器研究所 | Mooring balloon rapid deployment anchoring system |
CN111055750B (en) * | 2019-12-13 | 2022-06-28 | 中国特种飞行器研究所 | Mooring balloon rapid deployment anchoring system |
CN112429191A (en) * | 2020-11-20 | 2021-03-02 | 中国科学院空天信息创新研究院 | Nose tower end structure, nose tower subassembly and captive balloon of captive balloon anchor mooring facility |
CN112429191B (en) * | 2020-11-20 | 2022-06-17 | 中国科学院空天信息创新研究院 | Nose tower end structure, nose tower subassembly and captive balloon of captive balloon anchor mooring facility |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
C17 | Cessation of patent right | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20100602 Termination date: 20130902 |