CN205293057U - Airship - Google Patents
Airship Download PDFInfo
- Publication number
- CN205293057U CN205293057U CN201521024035.5U CN201521024035U CN205293057U CN 205293057 U CN205293057 U CN 205293057U CN 201521024035 U CN201521024035 U CN 201521024035U CN 205293057 U CN205293057 U CN 205293057U
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- utricule
- draconis
- quick
- bowknot
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Abstract
The utility model provides an airship, it includes utricule (1), a keel (2), interior hoist cable (3), two sets of A quick -releases rings (4), two sets of B quick -releases ring (5) and two sets of bowknot connecting piece (6), the bottom is equipped with two sets of horizontal cloth cover (7) and two sets of vertical cloth cover (8) in utricule (1), two stringers of a set of rib of fossil fragments (2) bottom and two stringers of a set of vertical fossil fragments are placed in respectively in two sets of horizontal cloth cover (7) and two sets of vertical cloth cover (8) of utricule (1) interior bottom, and bind the restraint through cord, this practical advantage is: the shortcoming that this technique is complicated to rigid, semi hard formula airship structure, the big and soft airship bearing capacity of structure weight is not enough, design one kind between the semi hard formula and soft between the airship structure, it has advantages such as simple structure, structure weight is little, bearing capacity is strong.
Description
Technical field
This practicality relates to airship technology field, is specifically related to a kind of dirigible.
Background technology
Tradition dirigible structure is generally divided into rigid, half rigid and soft 3 big type. Rigid airship has the framing structure being similar to aircraft, and exterior skin depends on skeleton, is served only for constituting aerodynamic configuration, and lift is provided by internal ballonet; Blimp forms as typical Germany neat Berlin NT dirigible skeleton is mutually the end to end Os Draconis of certain angle by 3 around dirigible axis,(being similar to the frame of aircraft) is connected every certain fore-and-aft distance by rigid structure between 3 Os Draconis,Exterior skin and utricule are simultaneously used for constituting aerodynamic configuration and providing lift, and aerodynamic configuration is maintained with skeleton jointly by utricule is intrinsic pressure. Rigid or blimp structure is applied to big-and-middle-sized dirigible more, and they maximum features are its rigid skeletons is a complete load-carrying construction, and soft utricule provides only lift. Rigid or half rigid structural design has certain advantage on large-scale load-carrying dirigible, but also inevitably shortcoming served by band, and as construction weight is big, assembling is complicated. Blimp is without large-sized hard structure, and it carries, provides the function such as lift, maintenance aerodynamic configuration to complete by utricule. Blimp structure is generally used for middle-size and small-size dirigible, its lightweight construction, but bearing capacity is limited.
Practical content
This practical purpose is aiming at tradition dirigible structure at present and is generally divided into rigid, half rigid and soft 3 big type. Rigid airship has the framing structure being similar to aircraft, and exterior skin depends on skeleton, is served only for constituting aerodynamic configuration, and lift is provided by internal ballonet; Blimp forms as typical Germany neat Berlin NT dirigible skeleton is mutually the end to end Os Draconis of certain angle by 3 around dirigible axis, exterior skin and utricule are simultaneously used for constituting aerodynamic configuration and providing lift, and aerodynamic configuration is maintained with skeleton jointly by utricule is intrinsic pressure. Rigid or blimp structure is applied to big-and-middle-sized dirigible more, and they maximum features are its rigid skeletons is a complete load-carrying construction, and soft utricule provides only lift. Rigid or half rigid structural design has certain advantage on large-scale load-carrying dirigible, but also inevitably shortcoming served by band, and as construction weight is big, assembling is complicated. Blimp is without large-sized hard structure, and it carries, provides the function such as lift, maintenance aerodynamic configuration to complete by utricule. Blimp structure is generally used for middle-size and small-size dirigible, its lightweight construction, but bearing capacity is limited. Deficiency, and a kind of dirigible is provided.
This practicality includes utricule, Os Draconis, interior hoist cable 3, two groups of A quick-release rings, two groups of B quick-release rings and two groups of bowknot connectors, utricule inner bottom part is provided with two groups of transverse direction cloth sets and two groups of longitudinal direction cloth sets, two stringers of one group of lateral keel bottom Os Draconis and two stringers of one group of longitudinal direction Os Draconis are respectively placed in two groups of transverse direction cloth sets and two groups of longitudinal direction cloth sets of utricule inner bottom part, and by tie string binding constraint, two groups of A quick-release rings and two groups of B quick-release rings are arranged on the both sides, top of Os Draconis respectively through quick-release ring mounting seat, two groups of A quick-release rings are connected with utricule inner top respectively through interior hoist cable 3, two groups of bowknot connectors are separately mounted in utricule bottom, and be distributed along Os Draconis both sides, two groups of B quick-release rings are connected respectively through stay cord and two groups of bowknot connectors.
Cloth set is connected by the mode of heat seal or stitching.
Bowknot connector side is by adhesive and bonding in utricule.
Os Draconis side and opposite side are distributed the bowknot connector having a group or more respectively, and two groups of B quick-release rings are connected with a group or more bowknot connector of Os Draconis both sides respectively through stay cord.
The length of Os Draconis is less than the 1/3 of balloon length, and load is dispersed to utricule by structures such as interior hoist cable 3, bowknot connectors by Os Draconis, and is jointly shared load by utricule and Os Draconis.
This practical advantage is: this technology is for shortcoming rigid, that blimp structure complicated, construction weight big and blimp bearing capacity is not enough, design a kind of rigid and soft between half between dirigible structure, it has the advantages such as simple in construction, construction weight is little, bearing capacity is strong.
Accompanying drawing explanation
Fig. 1 is this utility structure schematic diagram.
Fig. 2 is cloth set installation site structural representation.
Fig. 3 is cloth set installation site side view structural representation.
Fig. 4 is quick-release ring installation site structural representation.
Detailed description of the invention
Such as Fig. 1, 2, 3, shown in 4, this practicality includes utricule 1, Os Draconis 2, interior hoist cable 3, two groups of A quick-release rings 4, two groups of B quick-release rings 5 and two groups of bowknot connectors 6, utricule 1 inner bottom part is provided with two groups of transverse direction cloth sets 7 and two groups of longitudinal direction cloth sets 8, two stringers of one group of lateral keel bottom Os Draconis 2 and two stringers of one group of longitudinal direction Os Draconis are respectively placed in two groups of transverse direction cloth sets 7 and two groups of longitudinal direction cloth sets 8 of utricule 1 inner bottom part, and by tie string binding constraint, two groups of A quick-release rings 4 and two groups of B quick-release rings 5 are arranged on the both sides, top of Os Draconis 2 respectively through quick-release ring mounting seat, two groups of A quick-release rings 4 are connected with utricule 1 inner top respectively through interior hoist cable 3, two groups of bowknot connectors 6 are separately mounted to bottom in utricule 1, and be distributed along Os Draconis 2 both sides, two groups of B quick-release rings 5 are connected respectively through stay cord and two groups of bowknot connectors 6.
Cloth set is connected by the mode of heat seal or stitching.
Bowknot connector 6 side is by adhesive and bonding in utricule 1.
Os Draconis 2 side and opposite side are distributed the bowknot connector 6 having a group or more respectively, and two groups of B quick-release rings 5 are connected with a group or more bowknot connector 6 of Os Draconis 2 both sides respectively through stay cord.
The length of Os Draconis 2 is less than the 1/3 of air bag 1 length, and load is dispersed to utricule 1 by structures such as interior hoist cable 3, bowknot connectors 6 by Os Draconis 2, utricule 1 and Os Draconis 2 jointly share load.
Operation principle: many root lengths Os Draconis of traditional half hard structure are reduced to single short spine arrangement at utricule inner bottom part, and by cloth set, bowknot connector 6, interior hoist cable 3 type of attachment the load on Os Draconis is distributed on utricule to improve the bearing capacity of single short Os Draconis.
Interior hoist cable 3, for connecting Os Draconis with utricule top so that the part mass power of equipment is passed to utricule top, alleviates the load bottom utricule and on Os Draconis.
The effect of cloth set is fixing Os Draconis, transmits the load such as engine power and gear support power.
Little bowknot, for connecting utricule bottom to increase the lateral stability of Os Draconis, is one to cloth set constraint and supplements, it is prevented that Os Draconis occur because of utricule deformation under big rolling momentRelative to utriculeRolling.
Claims (5)
1. a dirigible, it is characterized in that it includes utricule (1), Os Draconis (2), interior hoist cable (3), two groups of A quick-release ring (4), two groups of B quick-release ring (5) and two groups of bowknot connectors (6), utricule (1) inner bottom part is provided with two groups of transverse directions cloth set (7) and two groups of longitudinal directions cloth set (8), two stringers of one group of lateral keel and two stringers of one group of longitudinal direction Os Draconis of Os Draconis (2) bottom are respectively placed in two groups of transverse directions cloth set (7) and two groups of longitudinal directions cloth set (8) of utricule (1) inner bottom part, and by tie string binding constraint, two groups of A quick-release ring (4) and two groups of B quick-release ring (5) are arranged on the both sides, top of Os Draconis (2) respectively through quick-release ring mounting seat, two groups of A quick-release ring (4) are connected with utricule (1) inner top respectively through interior hoist cable (3), two groups of bowknot connectors (6) are separately mounted to utricule (1) interior bottom, and be distributed along Os Draconis (2) both sides, two groups of B quick-release ring (5) are connected respectively through stay cord and two groups of bowknot connectors (6).
2. a kind of dirigible according to claim 1, it is characterised in that cloth set is connected by the mode of heat seal or stitching.
3. a kind of dirigible according to claim 1, it is characterised in that bowknot connector (6) side is by adhesive and bonding in utricule (1).
4. a kind of dirigible according to claim 1, it is characterized in that Os Draconis (2) side and opposite side are distributed the bowknot connector (6) having a group or more respectively, two groups of B quick-release ring (5) are connected with a group or more bowknot connector (6) of Os Draconis (2) both sides respectively through stay cord.
5. a kind of dirigible according to claim 1, it is characterized in that the length of Os Draconis (2) is less than the 1/3 of air bag (1) length, load is dispersed to utricule (1) by structures such as interior hoist cable (3), bowknot connectors (6) by Os Draconis (2), and is jointly shared load by utricule (1) and Os Draconis (2).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201521024035.5U CN205293057U (en) | 2015-12-11 | 2015-12-11 | Airship |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201521024035.5U CN205293057U (en) | 2015-12-11 | 2015-12-11 | Airship |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205293057U true CN205293057U (en) | 2016-06-08 |
Family
ID=56430455
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201521024035.5U Active CN205293057U (en) | 2015-12-11 | 2015-12-11 | Airship |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205293057U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2018122830A1 (en) | 2016-12-31 | 2018-07-05 | Ratti Jayant | High endurance unmanned aerial vehicle |
| CN111746772A (en) * | 2020-07-02 | 2020-10-09 | 上海交通大学 | Rigid-flexible integrated airship nose cone |
-
2015
- 2015-12-11 CN CN201521024035.5U patent/CN205293057U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2018122830A1 (en) | 2016-12-31 | 2018-07-05 | Ratti Jayant | High endurance unmanned aerial vehicle |
| 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 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |