CN106477017B - A kind of middle-size and small-size unmanned airship umbrella formula quick-release nose cone - Google Patents
A kind of middle-size and small-size unmanned airship umbrella formula quick-release nose cone Download PDFInfo
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- CN106477017B CN106477017B CN201611099793.2A CN201611099793A CN106477017B CN 106477017 B CN106477017 B CN 106477017B CN 201611099793 A CN201611099793 A CN 201611099793A CN 106477017 B CN106477017 B CN 106477017B
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- cone
- cone cap
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- pipe fitting
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64B—LIGHTER-THAN AIR AIRCRAFT
- B64B1/00—Lighter-than-air aircraft
- B64B1/66—Mooring attachments
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mutual Connection Of Rods And Tubes (AREA)
- Refuge Islands, Traffic Blockers, Or Guard Fence (AREA)
Abstract
The present invention proposes a kind of middle-size and small-size unmanned airship umbrella formula quick-release nose cone, including cone cap, pipe fitting and strut；Pipe fitting leading portion is provided with nose cone and is tethered at hole, and middle part is provided with packing hole, and there is the connection ring of the different drift angles of two circles at rear portion；Inner cone cap and rear cone cap are the head hollow conic structure processed using sheet metal, and inner cone cap and the rear inner end for boring cap are enclosed connection ring with pipe fitting rear portion two respectively and be fixedly connected by rivet；Outer end is molded by rivet；More struts curve the umbrella-shaped structure being bonded with airship envelope head outer profile, and strut rear end is fixedly connected with dirigible utricule by removable mode, and front end is fixedly connected with the fixing device in cone cap outside wall surface by removable mode.The present invention is light-weight compared to existing nose cone structure, simple in structure, facilitates quick detachable, is operated convenient for outfield；Strut quantity is adjusted according to magnitude of load, multi-directionally load is adaptable.
Description
Technical field
The present invention relates to middle-size and small-size unmanned airship technical field, specially a kind of middle-size and small-size unmanned airship umbrella formula quick-release head
Cone.
Background technology
Dirigible nose cone is mounted to the structure member on airship envelope head, and the Ground Mooring and auxiliary for being mainly used for dirigible are led
Draw, and improve the rigidity on dirigible head, enhances its wind loading rating.Dirigible head can deform weak in air pressure deficiency, influence to fly
The normal flight of ship, so dirigible nose cone is indispensable rigid structure component on dirigible utricule.Currently, what dirigible generally used
Nose cone is complicated, weight weight, influences the flight attitude and exterior appearance of dirigible.Secondly, existing nose cone occupied space is big, dirigible
When transition is transported, it is required for nose cone disassembling separation, with convenience in transport.Currently, dirigible nose cone is to connect to fasten by standard component,
So that the assembly and disassembly of dirigible nose cone are very troublesome, erection and the transition times of dirigible are extended, airship flight operation is affected
Working efficiency.
Invention content
In order to solve the problems existing in the prior art, the present invention proposes a kind of middle-size and small-size unmanned airship umbrella formula quick-release head
Cone is fastened by cone cap and the pipe fitting of two different angles, then with the quick-release type umbrella strut molding assembly that is stained with velcro,
So that dirigible head is had certain rigidity, facilitate the traction of dirigible while maintaining head configuration and is tethered at.
The technical scheme is that：
A kind of middle-size and small-size unmanned airship umbrella formula quick-release nose cone, it is characterised in that：Including cone cap, pipe fitting and support
Bar；Cone cap is divided into inner cone cap and rear cone cap；
The pipe fitting leading portion is provided with nose cone and is tethered at hole, for that after pipe fitting is inserted into mooring mast, can match with bolt
Nose cone is fixed on mooring mast by conjunction；It is provided with packing hole in the middle part of the pipe fitting, for fastening nose cone and air bag head；It is described
There is the connection ring of the different drift angles of two circles at pipe fitting rear portion, is respectively used to connect with inner cone cap and rear cone cap；
The inner cone cap and rear cone cap are the head hollow conic structure processed using sheet metal, inner cone cap and rear cone
The cone angle of cap is different, and it is consistent to enclose connection ring drift angle for pipe fitting rear portion two respectively；The inner end of inner cone cap and rear cone cap connects with pipe respectively
Back of head two encloses connection ring and is fixedly connected by rivet；The outer end of inner cone cap and rear cone cap is molded by rivet；
The more struts curve the umbrella-shaped structure being bonded with airship envelope head outer profile, and strut rear end can be with dirigible
Utricule is fixedly connected by removable mode, and company is fixed in strut front end with the fixing device in cone cap outside wall surface by removable mode
It connects.
Further preferred embodiment, a kind of middle-size and small-size unmanned airship umbrella formula quick-release nose cone, it is characterised in that：Strut
Front end side wall has annular spacing groove；The fixing device in cap outside wall surface is bored by mounting base, sliding block, poke rod, pedestal, compression spring group
At；Pedestal is fixed in cone cap outside wall surface, and has the hollow cylindrical structure for being inserted into strut front end, hollow circuit cylinder on pedestal
Structure side wall is provided with limit hole；Mounting base, which is fixedly mounted on pedestal, has the side of limit hole, and sliding block is equipped with inside mounting base
And compression spring, compression spring head into sliding block in pedestal limit hole, can be limited with the strut front end annular of inserted base hollow cylindrical structure
Position slot cooperation；Sliding block side is connect with poke rod, and slide position can be moved by poke rod.
Further preferred embodiment, a kind of middle-size and small-size unmanned airship umbrella formula quick-release nose cone, it is characterised in that：Strut
Rear end has velcro face, and corresponding matte bonding can be put on dirigible utricule cloth.
Advantageous effect
The present invention is light-weight compared to existing nose cone structure, simple in structure, facilitates quick detachable, is operated convenient for outfield；According to
Magnitude of load adjusts strut quantity, and multi-directionally load is adaptable.
The additional aspect and advantage of the present invention will be set forth in part in the description, and will partly become from the following description
Obviously, or practice through the invention is recognized.
Description of the drawings
The above-mentioned and/or additional aspect and advantage of the present invention will become in the description from combination following accompanying drawings to embodiment
Obviously and it is readily appreciated that, wherein：
Fig. 1 is combining structure schematic diagram of the present invention；
Fig. 2 is scheme of installation at pipe fitting of the present invention；
Fig. 3 is to rivet schematic diagram at present invention cone cap outer rim；
Fig. 4 is quick-release structural schematic diagram of the present invention；
Fig. 5 is quick-release structure erection support partial cutaway view of the present invention；
In figure：1, inner cone cap；2, cap is bored afterwards；3, pipe fitting；4, strut；5, it is tethered at hole；6, packing hole；7, mounting base；8、
Sliding block；9, poke rod；10, pedestal；11, compression spring.
Specific implementation mode
The embodiment of the present invention is described below in detail, examples of the embodiments are shown in the accompanying drawings, wherein from beginning to end
Same or similar label indicates same or similar element or element with the same or similar functions.Below with reference to attached
The embodiment of figure description is exemplary, it is intended to for explaining the present invention, and is not considered as limiting the invention.
In the description of the present invention, it is to be understood that, term "center", " longitudinal direction ", " transverse direction ", " length ", " width ",
" thickness ", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outside", " up time
The orientation or positional relationship of the instructions such as needle ", " counterclockwise " is to be based on the orientation or positional relationship shown in the drawings, and is merely for convenience of
The description present invention and simplified description, do not indicate or imply the indicated device or element must have a particular orientation, with spy
Fixed azimuth configuration and operation, therefore be not considered as limiting the invention.
As shown, middle-size and small-size unmanned airship umbrella proposed by the present invention formula quick-release nose cone, mainly by two different angles
Cone cap and pipe fitting fasten, then with the quick-release type umbrella strut molding assembly that is stained with velcro.Its main function is to make to fly
Deflection arch portion has certain rigidity, facilitates the traction of dirigible while maintaining head configuration and is tethered at.
As shown in Figure 1, a kind of middle-size and small-size unmanned airship umbrella formula quick-release nose cone, including cone cap, pipe fitting 3 and strut 4；Cone
Cap is divided into inner cone cap 1 and rear cone cap 2.
As shown in Fig. 2, 3 leading portion of the pipe fitting is provided with nose cone and is tethered at hole, in Ground Mooring, pipe fitting 3 to be inserted
After entering in the corresponding lasso trick of mooring mast, it can coordinate with bolt and nose cone is fixed on mooring mast.It is provided in the middle part of the pipe fitting
Packing hole, for fastening nose cone and air bag head.There is the connection ring of the different drift angles of two circles at the pipe fitting rear portion, is respectively used to
It is connect with inner cone cap and rear cone cap.
As shown in Figures 2 and 3, the inner cone cap and rear cone cap are to be processed using thin aluminum sheet metal plate and the technology mode of riveting
Head hollow conic structure, inner cone cap and the rear cone cone angle of cap are different, respectively two circle connection ring drift angle one of pipe fitting rear portion
It causes；The inner end of inner cone cap and rear cone cap is enclosed connection ring with pipe fitting rear portion two respectively and is fixedly connected by rivet；Inner cone cap is with after
The outer end of cone cap is molded by rivet；Nose cone weight can in this way reduced to minimum, and is still had higher strong
Degree.
As shown in Figure 1, the more struts curve the umbrella-shaped structure being bonded with airship envelope head outer profile, strut rear end
With velcro face, corresponding matte bonding can be put on dirigible utricule cloth, nose cone is made to be fastened.Strut front end side
Wall has annular spacing groove, is fixedly connected by removable mode with the fixing device in cone cap outside wall surface.
As shown in Figure 4 and Figure 5, the fixing device in cap outside wall surface is bored by mounting base, sliding block, poke rod, pedestal, compression spring group
At；Pedestal is fixed in cone cap outside wall surface, and has the hollow cylindrical structure for being inserted into strut front end, hollow circuit cylinder on pedestal
Structure side wall is provided with limit hole；Mounting base, which is fixedly mounted on pedestal, has the side of limit hole, and sliding block is equipped with inside mounting base
And compression spring, compression spring head into sliding block in pedestal limit hole, can be limited with the strut front end annular of inserted base hollow cylindrical structure
Position slot cooperation, to fix nose cone strut；Sliding block side is connect with poke rod, can be moved slide position by poke rod, will be slided
Block, which removes limiting slot, makes strut be detached with cone cap, easy to disassemble.
When nose cone is installed to utricule, first nose cone is fastened with air bag head by packing hole 6, then by strut 4 and capsule
Body cloth set bonds, and strut quantity can be adjusted according to needed for load, and the pulling force for drawing string for binding a plait is evenly distributed to capsule by nose cone
The cloth on body head is put on, and to avoid pulling force that the case where destroying utricule is concentrated to occur, ensures the safety of dirigible traction.
Although the embodiments of the present invention has been shown and described above, it is to be understood that above-described embodiment is example
Property, it is not considered as limiting the invention, those skilled in the art are not departing from the principle of the present invention and objective
In the case of can make changes, modifications, alterations, and variations to the above described embodiments within the scope of the invention.
Claims (3)
1. a kind of middle-size and small-size unmanned airship umbrella formula quick-release nose cone, it is characterised in that：Including cone cap, pipe fitting and strut；
Cone cap is divided into inner cone cap and rear cone cap；
The pipe fitting leading portion is provided with nose cone and is tethered at hole, for after pipe fitting is inserted into mooring mast, can coordinate with bolt will
Nose cone is fixed on mooring mast；It is provided with packing hole in the middle part of the pipe fitting, for fastening nose cone and air bag head；The pipe connects
Back of head has the connection ring of the different drift angles of two circles, is respectively used to connect with inner cone cap and rear cone cap；
The inner cone cap and rear cone cap are the head hollow conic structure processed using sheet metal, inner cone cap and afterwards cone cap
Cone angle is different, and it is consistent to enclose connection ring drift angle with pipe fitting rear portion two respectively；The inner end of inner cone cap and rear cone cap respectively with pipe fitting
Rear portion two is enclosed connection ring and is fixedly connected by rivet；The outer end of inner cone cap and rear cone cap is molded by rivet；
The more struts curve the umbrella-shaped structure being bonded with airship envelope head outer profile, and strut rear end can be with dirigible utricule
It is fixedly connected by removable mode, strut front end is fixedly connected with the fixing device in cone cap outside wall surface by removable mode.
2. a kind of middle-size and small-size unmanned airship umbrella formula quick-release nose cone according to claim 1, it is characterised in that：Strut front end side
Wall has annular spacing groove；Fixing device in cone cap outside wall surface is made of mounting base, sliding block, poke rod, pedestal, compression spring；Bottom
Seat is fixed in cone cap outside wall surface, and has the hollow cylindrical structure for being inserted into strut front end, hollow cylindrical structure on pedestal
Side wall is provided with limit hole；Mounting base, which is fixedly mounted on pedestal, has the side of limit hole, and sliding block and pressure are equipped with inside mounting base
Spring, compression spring head into sliding block in pedestal limit hole, can be with the strut front end annular spacing groove of inserted base hollow cylindrical structure
Cooperation；Sliding block side is connect with poke rod, and slide position can be moved by poke rod.
3. a kind of middle-size and small-size unmanned airship umbrella according to claim 1 or claim 2 formula quick-release nose cone, it is characterised in that：After strut
End has velcro face, and corresponding matte bonding can be put on dirigible utricule cloth.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611099793.2A CN106477017B (en) | 2016-12-05 | 2016-12-05 | A kind of middle-size and small-size unmanned airship umbrella formula quick-release nose cone |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611099793.2A CN106477017B (en) | 2016-12-05 | 2016-12-05 | A kind of middle-size and small-size unmanned airship umbrella formula quick-release nose cone |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN106477017A CN106477017A (en) | 2017-03-08 |
| CN106477017B true CN106477017B (en) | 2018-07-24 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201611099793.2A Active CN106477017B (en) | 2016-12-05 | 2016-12-05 | A kind of middle-size and small-size unmanned airship umbrella formula quick-release nose cone |
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Families Citing this family (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111746772B (en) * | 2020-07-02 | 2022-07-19 | 上海交通大学 | Rigid-flexible integrated airship nose cone |
| 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 |
| CN114132480B (en) * | 2021-12-03 | 2023-08-04 | 中国特种飞行器研究所 | Three-dimensional nose cone comparison foldable flexible device, and use method and preparation method thereof |
| CN115042989B (en) * | 2022-06-21 | 2023-06-27 | 青岛飞宇航空科技有限公司 | Automatic exhibition of airship is put anchor tower |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5429325A (en) * | 1993-09-28 | 1995-07-04 | Tcom, L. P. | Lightweight nose cone assembly |
| CN201350971Y (en) * | 2008-12-27 | 2009-11-25 | 中国特种飞行器研究所 | Tethered balloon nose cone stay device |
| CN201494623U (en) * | 2009-09-02 | 2010-06-02 | 湖南航天近空间飞行器研发中心 | Aerostat mooring lock |
| CN201914455U (en) * | 2011-01-27 | 2011-08-03 | 中国电子科技集团公司第三十八研究所 | Mooring lock for ground mooring of captive balloon |
| CN203946271U (en) * | 2014-06-16 | 2014-11-19 | 江苏捷诚车载电子信息工程有限公司 | The dirigible mooring gear that anchors fast |
| CN104627352A (en) * | 2013-11-06 | 2015-05-20 | 青岛飞宇航空科技有限公司 | Novel device of tethered balloon |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2913408B2 (en) * | 1989-06-30 | 1999-06-28 | 公人 田中 | Airship automatic mooring ballast adjustment device |
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2016
- 2016-12-05 CN CN201611099793.2A patent/CN106477017B/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5429325A (en) * | 1993-09-28 | 1995-07-04 | Tcom, L. P. | Lightweight nose cone assembly |
| CN201350971Y (en) * | 2008-12-27 | 2009-11-25 | 中国特种飞行器研究所 | Tethered balloon nose cone stay device |
| CN201494623U (en) * | 2009-09-02 | 2010-06-02 | 湖南航天近空间飞行器研发中心 | Aerostat mooring lock |
| CN201914455U (en) * | 2011-01-27 | 2011-08-03 | 中国电子科技集团公司第三十八研究所 | Mooring lock for ground mooring of captive balloon |
| CN104627352A (en) * | 2013-11-06 | 2015-05-20 | 青岛飞宇航空科技有限公司 | Novel device of tethered balloon |
| CN203946271U (en) * | 2014-06-16 | 2014-11-19 | 江苏捷诚车载电子信息工程有限公司 | The dirigible mooring gear that anchors fast |
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| CN106477017A (en) | 2017-03-08 |
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