CN106477017A - Formula quick-release nose cone opened by a kind of middle-size and small-size unmanned airship umbrella - Google Patents
Formula quick-release nose cone opened by a kind of middle-size and small-size unmanned airship umbrella Download PDFInfo
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- CN106477017A CN106477017A CN201611099793.2A CN201611099793A CN106477017A CN 106477017 A CN106477017 A CN 106477017A CN 201611099793 A CN201611099793 A CN 201611099793A CN 106477017 A CN106477017 A CN 106477017A
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- Prior art keywords
- cone
- cap
- cone cap
- size
- pipe joint
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Classifications
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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
Abstract
The present invention proposes a kind of middle-size and small-size unmanned airship umbrella and opens formula quick-release nose cone, including boring cap, pipe joint and strut；Pipe joint leading portion has nose cone and is tethered at hole, and middle part has packing hole, and there is the connection ring of two circles difference drift angle at rear portion；Inner cone cap and rear cone cap are the head hollow conic structure that is processed using sheet metal, and inner cone cap is enclosed connection ring with pipe joint rear portion two respectively with the inner of rear cone cap and is fixedly connected by rivet；Outer end is molded by rivet；Many struts curve the umbrella-shaped structure that fits with airship envelope head outline, and strut rear end is fixedly connected by removable mode with dirigible utricule, and front end is fixedly connected by removable mode with the fixing device in cone cap outside wall surface.The present invention compared to existing nose cone structure, lightweight, simple structure, facilitate quick detachable, be easy to outfield operate；Strut quantity, multi-directionally load, strong adaptability are adjusted according to magnitude of load.
Description
Technical field
The present invention relates to middle-size and small-size unmanned airship technical field, formula quick-release head opened by specially a kind of middle-size and small-size unmanned airship umbrella
Cone.
Background technology
Dirigible nose cone is mounted to the structure member of airship envelope head, is mainly used in the Ground Mooring of dirigible and auxiliary is led
Draw, and the rigidity of dirigible head is improved, strengthen its wind loading rating.Dirigible head can deform weak when air pressure is not enough, and impact flies
The normal flight of ship, so dirigible nose cone is indispensable rigid structure part on dirigible utricule.At present, dirigible is typically adopted
Nose cone complex structure, weight weight, affect flight attitude and the exterior appearance of dirigible.Secondly, existing nose cone takes up room greatly, dirigible
When transition is transported, it is required for for nose cone disassembling separation, to facilitate transport.At present, dirigible nose cone is fastened by standard component connection,
So that dirigible nose cone assembly and disassembly are bothered very much, erection and the transition times of dirigible are extended, have impact on airship flight operation
Operating efficiency.
Content of the invention
For solving the problems, such as prior art, the present invention proposes a kind of middle-size and small-size unmanned airship umbrella and opens formula quick-release head
Cone, is fastened by the cone cap and pipe joint of two different angles, then be stained with the quick-release type umbrella strut molding assembly of velcro,
Make dirigible head possess certain rigidity, facilitate the traction of dirigible while head configuration is maintained and be tethered at.
The technical scheme is that：
Formula quick-release nose cone opened by a kind of middle-size and small-size unmanned airship umbrella, it is characterised in that：Including boring cap, pipe joint and support
Bar；Cone cap is divided into inner cone cap and rear cone cap；
The pipe joint leading portion has nose cone and is tethered at hole, after in pipe joint insertion mooring mast, can join with latch
Close and nose cone is fixed on mooring mast；Packing hole is had in the middle part of the pipe joint, for nose cone is fastened with air bag head；Described
There is the connection ring of two circles difference drift angle at pipe joint rear portion, is respectively used to be connected with inner cone cap and rear cone cap；
The inner cone cap and rear cone cap are the head hollow conic structure that is processed using sheet metal, inner cone cap and rear cone
The cone angle of cap is different, and the circle of pipe joint rear portion two connection ring drift angle is consistent respectively；The inner of inner cone cap and rear cone cap is connect with pipe respectively
Back of head 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 many struts curve the umbrella-shaped structure that fits with airship envelope head outline, and strut rear end can be with dirigible
Utricule is fixedly connected by removable mode, and strut front end fixes company with the fixing device in cone cap outside wall surface by removable mode
Connect.
Further preferred version, a kind of middle-size and small-size unmanned airship umbrella open formula quick-release nose cone, it is characterised in that：Strut
Front end side wall has annular spacing groove；Fixing device in cone cap outside wall surface is by mounting seat, slide block, poke rod, base, stage clip group
Become；Base is fixed in cone cap outside wall surface, and with the hollow cylindrical structure for inserting strut front end, hollow circuit cylinder on base
Structure side wall has spacing hole；Mounting seat is fixedly mounted on the side that base has spacing hole, is provided with slide block inside mounting seat
And stage clip, stage clip heads into slide block in base spacing hole, can be with the strut front end of inserted base hollow cylindrical structure annular limit
Position groove coordinates；Slide block side is connected with poke rod, can move slide position by poke rod.
Further preferred version, a kind of middle-size and small-size unmanned airship umbrella open formula quick-release nose cone, it is characterised in that：Strut
Rear end has velcro face, can put corresponding matte bonding with dirigible utricule cloth.
Beneficial effect
The present invention compared to existing nose cone structure, lightweight, simple structure, facilitate quick detachable, be easy to outfield operate；According to
Magnitude of load adjusts strut quantity, multi-directionally load, strong adaptability.
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
Substantially and easy to understand, wherein：
Fig. 1 is combining structure schematic diagram of the present invention；
Fig. 2 is scheme of installation at pipe joint of the present invention；
Fig. 3 is to rivet schematic diagram at present invention cone cap outer rim；
Fig. 4 is quick-release structural representation of the present invention；
Fig. 5 is quick-release structure erection support part sectioned view of the present invention；
In figure：1st, inner cone cap；2nd, cap is bored afterwards；3rd, pipe joint；4th, strut；5th, hole is tethered at；6th, packing hole；7th, mounting seat；8、
Slide block；9th, poke rod；10th, base；11st, stage clip.
Specific embodiment
Embodiments of the invention are described below in detail, the example of the embodiment is shown in the drawings, wherein from start to finish
Same or similar label represents same or similar element or the element with same or like function.Below with reference to attached
The embodiment of figure description is exemplary, it is intended to for explaining the present invention, and be 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 of instruction such as pin ", " counterclockwise " or position relationship are based on orientation shown in the drawings or position relationship, are for only for ease of
The description present invention and simplification description, rather than the device or element of instruction or hint indication must be with specific orientation, Yi Te
Fixed azimuth configuration and operation, are therefore not considered as limiting the invention.
As illustrated, formula quick-release nose cone opened by middle-size and small-size unmanned airship umbrella proposed by the present invention, mainly by two different angles
Cone cap and pipe joint fasten, then be stained with the quick-release type umbrella strut molding assembly of velcro.Its Main Function is to make to fly
Deflection arch portion possesses certain rigidity, facilitates the traction of dirigible and be tethered at while head configuration is maintained.
As shown in figure 1, formula quick-release nose cone opened by a kind of middle-size and small-size unmanned airship umbrella, including boring cap, pipe joint 3 and strut 4；Cone
Cap is divided into inner cone cap 1 and rear cone cap 2.
As shown in Fig. 23 leading portion of the pipe joint has nose cone and is tethered at hole, in Ground Mooring, pipe joint 3 being inserted
After entering in the corresponding lasso trick of mooring mast, can coordinate with latch and nose cone is fixed on mooring mast.Have in the middle part of the pipe joint
Packing hole, for fastening nose cone with air bag head.There is the connection ring of two circles difference drift angle at the pipe joint rear portion, is respectively used to
It is connected with inner cone cap and rear cone cap.
As shown in Figures 2 and 3, the inner cone cap and rear cone cap are the technology mode processing using thin aluminum sheet panel beating with riveting
Head hollow conic structure, inner cone cap is different with the cone angle of rear cone cap, and connection ring drift angle one is enclosed at pipe joint rear portion two respectively
Cause；Inner cone cap is enclosed connection ring with pipe joint rear portion two respectively with the inner of rear cone cap and is fixedly connected by rivet；Inner cone cap and after
The outer end of cone cap is molded by rivet；Nose cone weight can be so reduced to minimum, and is still possessed higher strong
Degree.
As shown in figure 1, many struts curve the umbrella-shaped structure that fits with airship envelope head outline, strut rear end
With velcro face, corresponding matte bonding can be put with dirigible utricule cloth, be fastened nose cone.Strut front
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 cone cap outside wall surface is by mounting seat, slide block, poke rod, base, stage clip group
Become；Base is fixed in cone cap outside wall surface, and with the hollow cylindrical structure for inserting strut front end, hollow circuit cylinder on base
Structure side wall has spacing hole；Mounting seat is fixedly mounted on the side that base has spacing hole, is provided with slide block inside mounting seat
And stage clip, stage clip heads into slide block in base spacing hole, can be with the strut front end of inserted base hollow cylindrical structure annular limit
Position groove coordinates, to fix nose cone stay；Slide block side is connected with poke rod, can move slide position by poke rod, will be sliding
Block removes stopper slot makes stay separate with cone cap, convenient dismounting.
When nose cone is attached on utricule, first nose cone is fastened by packing hole 6 with air bag head, then by strut 4 and capsule
The set bonding of body cloth, 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 of body head puts, and the situation for destroying utricule so as to avoid pulling force from concentrating occurs, it is ensured that the safety of dirigible traction.
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 without departing from the present invention and objective
In the case of above-described embodiment can be changed within the scope of the invention, change, replace and modification.
Claims (3)
1. formula quick-release nose cone opened by a kind of middle-size and small-size unmanned airship umbrella, it is characterised in that：Including boring cap, pipe joint and strut；
Cone cap is divided into inner cone cap and rear cone cap；
The pipe joint leading portion has nose cone and is tethered at hole, and after in pipe joint insertion mooring mast, can coordinate with latch will
Nose cone is fixed on mooring mast；Packing hole is had in the middle part of the pipe joint, for nose cone is fastened with air bag head；The pipe connects
Back of head has the connection ring of two circles difference drift angle, is respectively used to be connected with inner cone cap and rear cone cap；
The inner cone cap and rear cone cap are the head hollow conic structure that is processed using sheet metal, inner cone cap and rear cone cap
Cone angle is different, and the circle of pipe joint rear portion two connection ring drift angle is consistent respectively；The inner of inner cone cap and rear cone cap respectively with pipe joint after
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 many struts curve the umbrella-shaped structure that fits with airship envelope head outline, and strut rear end can be with dirigible utricule
It is fixedly connected by removable mode, strut front end is fixedly connected by removable mode with the fixing device in cone cap outside wall surface.
2. formula quick-release nose cone opened by a kind of middle-size and small-size unmanned airship umbrella according to claim 1, it is characterised in that：Strut front
Wall has annular spacing groove；Fixing device in cone cap outside wall surface is made up of mounting seat, slide block, poke rod, base, stage clip；Bottom
Seat is fixed in cone cap outside wall surface, and with the hollow cylindrical structure for inserting strut front end, hollow cylindrical structure on base
Side wall has spacing hole；Mounting seat is fixedly mounted on the side that base has spacing hole, is provided with slide block and pressure inside mounting seat
Spring, stage clip head into slide block in base spacing hole, can be with the strut front end annular spacing groove of inserted base hollow cylindrical structure
Coordinate；Slide block side is connected with poke rod, can move slide position by poke rod.
3. formula quick-release nose cone opened by a kind of middle-size and small-size unmanned airship umbrella according to claim 1 or claim 2, it is characterised in that：After strut
End can put corresponding matte bonding with dirigible utricule cloth with velcro face.
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 true CN106477017A (en) | 2017-03-08 |
| CN106477017B 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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Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111746772A (en) * | 2020-07-02 | 2020-10-09 | 上海交通大学 | Rigid-flexible integrated airship nose cone |
| 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 |
| CN114132480A (en) * | 2021-12-03 | 2022-03-04 | 中国特种飞行器研究所 | Foldable flexible device for three-dimensional nose cone comparison and using method and preparation method thereof |
| CN115042989A (en) * | 2022-06-21 | 2022-09-13 | 青岛飞宇航空科技有限公司 | Automatic anchor tower of putting of exhibition of dirigible |
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| JPH0333000A (en) * | 1989-06-30 | 1991-02-13 | Kimito Tanaka | Automatic anchoring ballast adjusting device of airship |
| 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 |
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Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
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| JPH0333000A (en) * | 1989-06-30 | 1991-02-13 | Kimito Tanaka | Automatic anchoring ballast adjusting device of airship |
| 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 |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111746772A (en) * | 2020-07-02 | 2020-10-09 | 上海交通大学 | Rigid-flexible integrated airship nose cone |
| CN111746772B (en) * | 2020-07-02 | 2022-07-19 | 上海交通大学 | Rigid-flexible integrated airship nose cone |
| 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 |
| CN114132480A (en) * | 2021-12-03 | 2022-03-04 | 中国特种飞行器研究所 | Foldable flexible device for three-dimensional nose cone comparison and using method and preparation method thereof |
| 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 |
| CN115042989A (en) * | 2022-06-21 | 2022-09-13 | 青岛飞宇航空科技有限公司 | Automatic anchor tower of putting of exhibition of dirigible |
Also Published As
| Publication number | Publication date |
|---|---|
| CN106477017B (en) | 2018-07-24 |
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