CN203567924U - Novel helium airship bag structure - Google Patents
Novel helium airship bag structure Download PDFInfo
- Publication number
- CN203567924U CN203567924U CN201320776275.5U CN201320776275U CN203567924U CN 203567924 U CN203567924 U CN 203567924U CN 201320776275 U CN201320776275 U CN 201320776275U CN 203567924 U CN203567924 U CN 203567924U
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- China
- Prior art keywords
- balloonet
- gas bag
- hanging
- hawser
- main gasbag
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- Expired - Lifetime
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- 239000001307 helium Substances 0.000 title claims abstract description 22
- 229910052734 helium Inorganic materials 0.000 title claims abstract description 22
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 title claims abstract description 22
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 claims abstract description 6
- 230000009286 beneficial effect Effects 0.000 abstract description 2
- 239000007789 gas Substances 0.000 abstract 14
- 230000000149 penetrating effect Effects 0.000 abstract 2
- 230000005484 gravity Effects 0.000 description 5
- 230000008901 benefit Effects 0.000 description 4
- 230000008859 change Effects 0.000 description 4
- 238000005516 engineering process Methods 0.000 description 4
- 238000010586 diagram Methods 0.000 description 3
- 239000000203 mixture Substances 0.000 description 3
- 239000002775 capsule Substances 0.000 description 2
- 230000007812 deficiency Effects 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 238000004064 recycling Methods 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
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- Air Bags (AREA)
Abstract
The utility model discloses a novel helium airship bag structure. The novel helium airship bag structure comprises a main gas bag, a hanging rope and an auxiliary gas bag, wherein the main gas bag is connected with a pod at the lower part of a bag body through the hanging rope, the hanging rope comprises an outer hanging cable and an inner hanging cable, the outer hanging cable is located at the outer side of the main gas bag, the inner hanging cable is located at the inner side of the main gas bag, the auxiliary gas bag is arranged at the inner part of the main gas bag, the auxiliary gas bag is provided with a flexible sleeve in a penetrating way, one end of the inner hanging cable is fixedly arranged at the top part of the inner side of the main gas bag, and the other end of the inner hanging cable extends to the bottom part of the main gas bag by penetrating through the auxiliary gas bag through the sleeve and is connected with the outer hanging cable; the inner hanging cable is provided with an electric resistance wire, the top part of the auxiliary gas bag is provided with an electric slip ring which is sleeved on the electric resistance wire, the electric slip ring is electrically connected with the electric resistance wire, voltage is applied to two ends of the electric resistance wire, and the electric slip ring is connected with a flight control system through an electric cable. The novel helium airship bag structure disclosed by the utility model has the beneficial effects that the problems that the inner hanging cable and the auxiliary gas bag can not coexist and the volume of the auxiliary gas bag is difficult to be effectively measured are solved, the attitude control of the airship is convenient, the structure is simple, and the cost is low.
Description
Technical field
The utility model relates to Helium Airship field, is specifically related to a kind of novel helium dirigible utricule structure.
Background technology
Helium Airship, in order to keep inside and outside utricule reasonably pressure reduction, is all designed with in the main gasbag inside of filling helium the balloonet that fills air, and balloonet can have one or more; The gondola of utricule bottom is fastened on utricule by the hanging rope being fixed on utricule, and what hanging rope was positioned at utricule inside is hanging, and what hanging rope was positioned at utricule outside is outer hanging.Due to the needs of Helium Airship balanced design, the utricule of single balloonet, balloonet must design in position, utricule centre of buoyancy, and gondola is also positioned near position, utricule centre of buoyancy, if adopt single balloonet will cause and the interference of interior hanging simultaneously.
At present, if existing Helium Airship use in hanging design, balloonet is general adopts 2 above balloonets, adopts the outer hanging structure of employing of single balloonet, to avoid interior hanging and single balloonet mutually to interfere.
In addition, existing Helium Airship adopts laser rangefinder to measure balloonet volume, in the bottom of balloonet, laser rangefinder is installed, and measures the height at balloonet top by laser rangefinder, and recycling altitude information calculates balloonet volume.Adopt this kind of infrastructure cost high, technology is more complicated also, only on Large Airship, uses, and is difficult to promote.
Summary of the invention
The technical problems to be solved in the utility model is that in existing for existing Helium Airship, hanging and single balloonet can not coexist in same utricule and the high deficiency of balloonet cubing cost, and a kind of novel helium dirigible utricule structure is provided.
The utility model for solving the problems of the technologies described above adopted technical scheme is:
Novel helium dirigible utricule structure, comprise main gasbag, hanging rope, described main gasbag is connected with the gondola of utricule bottom by hanging rope, described hanging rope comprises the outer hanging hawser that is positioned at main gasbag outside and the hanging hawser that is positioned at main gasbag inner side, it is characterized in that: this utricule also comprises the balloonet that is arranged at main gasbag inside, on described balloonet, be equipped with flexible sleeve, one end of described interior hanging hawser is fixed on the inside top of main gasbag, the other end of interior hanging hawser passes balloonet by sleeve and extends to main gasbag bottom, and be connected with the outer hanging hawser in main gasbag outside.
Press such scheme, described sleeve is identical with the quantity of interior hanging hawser.
Press such scheme, the quantity of described sleeve and interior hanging hawser is 4～8.
Press such scheme, on described interior hanging hawser, resistor wire is installed, the top of described balloonet is provided with the electric slip ring being enclosed within on resistor wire, and electric slip ring is electrically connected with resistor wire, resistor wire two ends on load voltage, and electric slip ring is also connected with flight control system by cable.
Principle of work of the present utility model: balloonet and interior hanging hawser are arranged on main gasbag inside, the flexible sleeve that design can be passed for interior hanging hawser on balloonet, both kept the integraty of balloonet, guarantee that again interior hanging hawser can pass balloonet from utricule top by sleeve smoothly and reach main gasbag bottom, because sleeve is flexible, during balloonet volume change, flexible sleeve can not hinder balloonet top along the rise and fall of interior hanging hawser; Due to the restriction of interior hanging hawser, balloonet top also can only be moved along interior hanging hawser, can not swing to front portion or rear portion completely due to the pitching of dirigible utricule, can avoid significantly changing because airship's posture changes the center of gravity causing simultaneously.Adopt the balloonet of this structure to coexist in the ship capsule of Helium Airship with interior hanging hawser, make this utricule structure have the advantage of single balloonet and interior hanging concurrently, and when dirigible wide-angle pitching flying, can reduce balloonet and move forward and backward the gravity center shift causing.Simultaneously, due to the resistor wire moving contact on electric slip ring and the interior hanging hawser at balloonet top, a rheostat of common composition, at resistor wire two ends making alive, when balloonet top moves up and down, electric slip ring punishment is pressed and is changed thereupon, and flight control system utilizes electric slip ring to gather the voltage division signal of position, balloonet top on resistor wire, obtain the height at balloonet top, thereby calculate balloonet volume (capacity).
The utlity model has following beneficial effect:
1, tube-in-tube structure has solved interior hanging hawser and the incompatible problem of single balloonet, utricule not only possessed interior hanging cable stress evenly, utricule forming, the advantage such as windage is little, the life-span is long, also possessed single balloonet and be easy to carry out bag pressure control, the advantage that simple in structure, cost is low, easy to use;
2, because interior hanging hawser restriction balloonet top can only be moved in short transverse along interior hanging hawser, can also be when dirigible dives and climbs, avoid balloonet to swing to utricule front portion or rear portion causes utricule center of gravity significantly to change, be conducive to the attitude control of dirigible;
3, a rheostat of the common composition of the resistor wire on the electric slip ring at balloonet top and interior hanging hawser, solve balloonet volume and be difficult to a difficult problem of effectively measuring, while utilizing balloonet volume change, the relative position of top and hawser changes to obtain balloonet overhead height, thereby calculate balloonet volume, with low cost, technology realizes and being very easy to.
Accompanying drawing explanation
Fig. 1 is structure constructional drawing of the present utility model;
Fig. 2 is the lateral plan of Fig. 1;
Fig. 3 be Fig. 1 along A ?A to cutaway view;
Fig. 4 is the structure for amplifying schematic diagram at C place in Fig. 3;
Fig. 5 be Fig. 2 along B ?B to cutaway view;
Fig. 6 is the schematic circuit diagram that the utility model is measured balloonet height;
In figure, 1 ?main gasbag, 2 ?balloonet, 3 ?in hanging hawser, 4 ?sleeve, 5 ?resistor wire, 6 ?slip ring, 7 ?cable.
The specific embodiment
Below in conjunction with drawings and Examples, the utility model is elaborated.
Shown in Fig. 1～Fig. 5, novel helium dirigible utricule structure described in the utility model, comprise main gasbag 1, hanging rope, described main gasbag 1 is connected with the gondola of utricule bottom by hanging rope, described hanging rope comprises the outer hanging hawser that is positioned at main gasbag 1 outside and the hanging hawser 3 that is positioned at main gasbag 1 inner side, this utricule also comprises the balloonet 2 that is arranged at main gasbag 1 inside, on described balloonet 2, be equipped with flexible sleeve 4, one end of described interior hanging hawser 3 is fixed on the inside top of main gasbag 1, the other end of interior hanging hawser 3 extends to main gasbag 1 bottom by sleeve 4 through balloonet 2, and be connected with the outer hanging hawser in main gasbag 1 outside.
Described sleeve 4 is identical with the quantity of interior hanging hawser 3, and sleeve 4 is made in the cavity of offering on balloonet 2.
Described sleeve 4 is 4～8 with the quantity of interior hanging hawser 3.
On described interior hanging hawser 3, resistor wire 5 is installed, the top of described balloonet 2 is provided with the electric slip ring 6 being enclosed within on resistor wire 5, and electric slip ring 6 is electrically connected with resistor wire 5, resistor wire 5 two ends on load voltages, and electric slip ring 6 is also connected with flight control system by cable 7.
During the utility model work, balloonet 2 and interior hanging hawser 3 are arranged on main gasbag 1 inside, the flexible sleeve 4 that design can be passed for interior hanging hawser 3 on balloonet 2, both kept the integraty of balloonet 2, guarantee that again interior hanging hawser 3 can reach main gasbag 1 bottom from utricule top by sleeve 4 through balloonet 2 smoothly, because sleeve 4 is flexible, during balloonet 2 volume change, flexible sleeve 4 can not hinder balloonet 2 tops along interior hanging hawser 3 rise and fall; Due to the restriction of interior hanging hawser 3, balloonet 2 tops also can only be moved along interior hanging hawser 3, can not swing to front portion or rear portion completely due to the pitching of dirigible utricule, can avoid significantly changing because airship's posture changes the center of gravity causing simultaneously.Adopt the balloonet 2 of this structure to coexist in the ship capsule of Helium Airship with interior hanging hawser 3, make this utricule structure have the advantage of single balloonet and interior hanging concurrently, and when dirigible wide-angle pitching flying, can reduce balloonet and move forward and backward the gravity center shift causing.
Simultaneously, with reference to schematic circuit diagram shown in Fig. 6, due to resistor wire 5 moving contacts on electric slip ring 6 and the interior hanging hawser 3 at balloonet 2 tops, a rheostat of common composition, at resistor wire 5 two ends making alives, when balloonet 2 tops move up and down, electric slip ring 6 punishment are pressed and are changed thereupon, flight control system utilizes electric slip ring 6 to gather the voltage division signal of balloonet 2 positions, top on resistor wire 5, obtains the height at balloonet 2 tops, thereby calculates balloonet 2 volumes (capacity).
The foregoing is only preferred embodiment of the present utility model; not in order to limit the utility model; all any modifications of doing within spirit of the present utility model and principle, be equal to and replace and improvement etc., within all should being included in protection domain of the present utility model.
Claims (4)
1. novel helium dirigible utricule structure, comprise main gasbag (1), hanging rope, described main gasbag (1) is connected with the gondola of utricule bottom by hanging rope, described hanging rope comprises the outer hanging hawser that is positioned at main gasbag (1) outside and the hanging hawser (3) that is positioned at main gasbag (1) inner side, it is characterized in that: this utricule also comprises the balloonet (2) that is arranged at main gasbag (1) inside, on described balloonet (2), be equipped with flexible sleeve (4), one end of described interior hanging hawser (3) is fixed on the inside top of main gasbag (1), the other end of interior hanging hawser (3) extends to main gasbag (1) bottom by sleeve (4) through balloonet (2), and be connected with the outer hanging hawser in main gasbag (1) outside.
2. novel helium dirigible utricule structure as claimed in claim 1, is characterized in that: described sleeve (4) is identical with the quantity of interior hanging hawser (3).
3. novel helium dirigible utricule structure as claimed in claim 1, is characterized in that: described sleeve (4) is 4～8 with the quantity of interior hanging hawser (3).
4. novel helium dirigible utricule structure as claimed in claim 1, it is characterized in that: resistor wire (5) is installed on described interior hanging hawser (3), the top of described balloonet (2) is provided with the electric slip ring (6) being enclosed within on resistor wire (5), electric slip ring (6) is electrically connected with resistor wire (5), resistor wire (5) two ends on load voltage, electric slip ring (6) is also connected with flight control system by cable (7).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320776275.5U CN203567924U (en) | 2013-11-29 | 2013-11-29 | Novel helium airship bag structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320776275.5U CN203567924U (en) | 2013-11-29 | 2013-11-29 | Novel helium airship bag structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203567924U true CN203567924U (en) | 2014-04-30 |
Family
ID=50535669
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201320776275.5U Expired - Lifetime CN203567924U (en) | 2013-11-29 | 2013-11-29 | Novel helium airship bag structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203567924U (en) |
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 |
| CN112078774A (en) * | 2020-07-04 | 2020-12-15 | 毛雷杰 | Solar energy does not have multiaxis unmanned aerial vehicle structure of dead weight power consumption |
| RU2763322C1 (en) * | 2020-11-05 | 2021-12-28 | Екатерина Дмитриевна Мухина | Method for stiffening airshipe shell with semi-rigid structure |
-
2013
- 2013-11-29 CN CN201320776275.5U patent/CN203567924U/en not_active Expired - Lifetime
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 |
| CN112078774A (en) * | 2020-07-04 | 2020-12-15 | 毛雷杰 | Solar energy does not have multiaxis unmanned aerial vehicle structure of dead weight power consumption |
| RU2763322C1 (en) * | 2020-11-05 | 2021-12-28 | Екатерина Дмитриевна Мухина | Method for stiffening airshipe shell with semi-rigid structure |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CX01 | Expiry of patent term |
Granted publication date: 20140430 |
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| CX01 | Expiry of patent term |