CN104002958A - Airship with auxiliary wings - Google Patents
Airship with auxiliary wings Download PDFInfo
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- CN104002958A CN104002958A CN201410198047.3A CN201410198047A CN104002958A CN 104002958 A CN104002958 A CN 104002958A CN 201410198047 A CN201410198047 A CN 201410198047A CN 104002958 A CN104002958 A CN 104002958A
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- aileron
- dirigible
- sail
- control
- flexible cover
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Abstract
The invention relates to an airship with auxiliary wings. The airship comprises a flexible cover and a pod, wherein the flexible cover is filled with gas lighter than air, the pod is connected with the lower portion of the flexible cover, the auxiliary wings which are used for controlling the direction and enabling the airship to fly with the help of wind are arranged on the two sides of the flexible cover, the auxiliary wings are fin-shaped sailboards, and the auxiliary wings are composed of fin-shaped sail frames, sail faces laid in the sail frames, a sail supporting frame for supporting the sail faces and auxiliary wing supports connected with the airship. Rotating shafts for controlling the sail faces to rotate, unfold and fold are arranged on the auxiliary wing supports. Compared with the prior art, by means of the wind catching performance of the auxiliary wings, a plurality of folding and unfolding fin-shaped structures are arranged on the airship, wind resources are utilized for providing auxiliary power for the airship, or unpowered flight is achieved, and even the wind energy catching and rotating technology is utilized for storing electric energy converted from wind energy, so that the electric energy can be used for meeting the requirements of the airship for lighting, heat supply and mechanical energy output.
Description
Technical field
The present invention relates to a kind of dirigible, especially relate to a kind of have aileron with controlling party to dirigible.
Background technology
Since 20 beginning of the century dirigibles are brought into play strategy function in the World War I, with and substitute the revolutionary change of hydrogen through helium after, at present because of its heavy－duty, low cost, be more and more subject to the attention of research institution of various countries and government without infrastructure constructions such as runways, although dirigible has the negative existence such as bulky, flying speed is relatively slow as aircraft, but, for processing the commercial market demand of non-military scope, the value of dirigible is far away higher than fixed wing aircraft and autogyro.
For a long time, this vehicle that move about in air of dirigible are all to exist with oval-shaped airflow design, and this design has reduced the effect of air resistance to dirigible greatly, and dirigible can be flown with desirable speed under the effect of screw propeller.
This design has reduced greatly really windage against the wind in the situation that, has improved flying speed.But this design is for dirigible, the flight in situation with the wind helps but to have reduced greatly.
Application number is that the Chinese patent of 200810114792.x discloses airship empennage of tail rotor type, comprises stabilator, rudder face, rotating shaft.On structure fabrication, stabilator and rudder face are first barricaded as after skeleton by floor, wall, cover covering sizing outward and form, and between stabilator and rudder face, are connected with rotating shaft; Stabilator is fixedly connected with ship capsule; Wherein, establish a through hole on stabilator, the rotatable mechanism that is connected in through hole, is provided with vector tail-rotor in mechanism, and rotating mechanism and vector tail-rotor are with respect to stabilator synchronous rotary, and the anglec of rotation is ± 180 °, but this empennage cannot freely be received or launch.
Summary of the invention
Object of the present invention is exactly to provide a kind of in order to overcome the defect that above-mentioned prior art exists can utilize wind resource to provide power to carry out unpowered flight to dirigible and facilitate controlled motion direction and the dirigible with aileron of height.
Object of the present invention can be achieved through the following technical solutions:
A kind of dirigible with aileron, comprise and be filled with the flexible cover of lighter-than-air gas and be connected to the gondola under flexible cover, controlling party is installed to also making the aileron of dirigible by wind-force flight in the both sides of flexible cover, this aileron is fin shape windsurfing, by the sail face framework that is fin shape, the sail face being laid in sail face framework, the sail face bracing frame of support sail face and the aileron of connection dirigible prop up and are configured to, and described aileron support is provided with the turning cylinder of controlling the rotation of sail face, storage or expansion.
Described aileron is concertina type structure, by electronic or manual control storage or expansion.
Described aileron is folded form structure, by electronic or manual control storage or expansion.
Utilize storage or the expansion of pulley and hawser control aileron.
Described aileron is provided with two pairs four or more multipair, be symmetricly set on the both sides of dirigible, the junction of each aileron and dirigible is equipped with a pulley, controls hawser and reefing control hawser and synchronously or respectively control storage or the expansion of aileron through lifting a sail of pulley control linkage aileron.
In motion process or under wind-force effect, obtain the motion of buoyancy control dirigible in the vertical direction upwards at the angle control dirigible of vertical direction by changing aileron.
Described aileron is connected with dirigible through mast, and lift a sail control hawser and reefing control hawser are along the setting of mast direction.
Described mast is connected with bolster, on this bolster, is provided with capstan winch, is lift a sail and is controlled the folding and unfolding of hawser and reefing control hawser by this winch control.
Described gondola can also be located at flexible cover inside, or is located at flexible cover top as ship's deck.
Compared with prior art, what the present invention utilized aileron catches wind performance, load onto the aileron of several fin structures that can launch and draw in to dirigible, control the folding of aileron and form different angles from sense of motion and vertical direction, thereby can control sense of motion and the flying height of dirigible, can utilize like this wind resource to provide power to carry out unpowered flight to dirigible, or even the electric energy that utilizes wind energy seizure and conversion technique storage wind energy to change is exported demand for illumination, heat supply, refrigeration and the mechanical energy of dirigible.
Brief description of the drawings
Fig. 1 is structural representation of the present invention in embodiment 1;
Fig. 2 is structural representation of the present invention in embodiment 2;
Fig. 3 is the structural representation of aileron.
In figure, 1 for aileron, 11 for sail face framework, 12 for sail face, 13 for sail face bracing frame, 14 for aileron support, 15 for turning cylinder, 2 for pulley, 3 for lift a sail control hawser, 4 for reefing control hawser, 5 for mast, 6 for bolster, 7 for capstan winch, 8 for dirigible, 9 for screw propeller, 10 be flexible cover.
Detailed description of the invention
Below in conjunction with the drawings and specific embodiments, the present invention is described in detail.
Embodiment 1
There is the dirigible of aileron, its structure as shown in Figure 1, comprise and be filled with the flexible cover 10 of lighter-than-air gas and be connected to the gondola under flexible cover 10, controlling party is installed to also making the aileron of dirigible by wind-force flight in the both sides of flexible cover 10, the structure of the dirigible aileron using as shown in Figure 3, for fin shape windsurfing, by the sail face framework 11 that is fin shape, the sail face 12 being laid in sail face framework 11, the sail face bracing frame 13 of support sail face 12 and the aileron support 14 of connection dirigible form, on aileron support 14, be provided with and control the rotation of sail face, storage or the turning cylinder 15 launching.Aileron 1 in the present embodiment is folded form structure, by electronic or manual control storage or expansion.In the present embodiment, aileron 1 is provided with two pairs four or more, be symmetricly set on the both sides of dirigible 8, each aileron 1 is equipped with a pulley 2 with the junction of dirigible 8, controls hawser 3 and reefing control hawser 4 and synchronously or respectively control storage or the expansion of aileron 1 through lifting a sail of pulley 2 control linkage ailerons 1.Aileron 1 is connected with dirigible 8 through mast 5, lift a sail and control hawser 3 and reefing control hawser 4 along the direction setting of mast 5 also, mast 5 is connected with bolster 6, on this bolster 6, is provided with capstan winch 7, controls to lift a sail control the folding and unfolding of hawser 3 and reefing control hawser 4 by this capstan winch 7.
Dirigible 8 is in the time advancing, the screw propeller 9 of afterbody can provide power forward, what the present invention utilized aileron 1 catches wind performance, load onto several fin structures that can launch and draw in to dirigible, sense of motion by change aileron 1 with the angle control dirigible of working direction, obtains the motion of buoyancy control dirigible in the vertical direction upwards at the angle control dirigible of vertical direction by changing aileron 1.Thereby can conveniently utilize wind resource to provide power to carry out unpowered flight to dirigible, can also be that the electric energy that utilizes wind energy seizure and conversion technique storage wind energy to change is exported demand for illumination, heat supply, refrigeration and the mechanical energy of dirigible in addition.
Embodiment 2
There is the dirigible of aileron, its structure as shown in Figure 2, comprise and be filled with the flexible cover 10 of lighter-than-air gas and be connected to the gondola under flexible cover 10, controlling party is installed to also making the aileron of dirigible by wind-force flight in the both sides of flexible cover 10, the structure of the dirigible aileron using as shown in Figure 3, for fin shape windsurfing, by the sail face framework 11 that is fin shape, the activity sail face 12 in sail face framework 11 that is laid in, the sail face bracing frame 13 of support sail face 12 and the aileron support 14 of connection dirigible form, on aileron support 14, be provided with and control the rotation of sail face, storage or the turning cylinder 15 launching.Aileron 1 in the present embodiment is concertina type structure, by electronic or manual control storage or expansion.In the present embodiment, aileron 1 is provided with two pairs four or more multipair, be symmetricly set on the both sides of dirigible 8, the top of each aileron 1 and be equipped with a pulley 2 with the junction of dirigible 8, controls hawser 3 and reefing control hawser 4 and synchronously or respectively controls storage or the expansion of aileron 1 through lifting a sail of pulley 2 control linkage ailerons 1.Aileron 1 is connected with dirigible 8 through mast 5, lift a sail and control hawser 3 and reefing control hawser 4 along the direction setting of mast 5 also, mast 5 is connected with bolster 6, on this bolster 6, is provided with capstan winch 7, controls to lift a sail control the folding and unfolding of hawser 3 and reefing control hawser 4 by this capstan winch 7.
Dirigible 8 is in the time advancing, the screw propeller 9 of afterbody can provide power forward, what the present invention utilized aileron 1 catches wind performance, load onto several fin structures that can launch and draw in to dirigible, sense of motion by change aileron 1 with the angle control dirigible of working direction, obtains the motion of buoyancy control dirigible in the vertical direction upwards at the angle control dirigible of vertical direction by changing aileron 1.Thereby can conveniently utilize wind resource to provide power to carry out unpowered flight to dirigible, can also be that the electric energy that utilizes wind energy seizure and conversion technique storage wind energy to change is exported demand for illumination, heat supply, refrigeration and the mechanical energy of dirigible in addition.
One of ordinary skill in the art will appreciate that: the foregoing is only the preferred embodiments of the present invention, although being not limited to the present invention has been described in detail the present invention with reference to previous embodiment, for a person skilled in the art, its technical scheme that still can record aforementioned each embodiment be modified, or part technical characterictic is wherein equal to replacement.Within the spirit and principles in the present invention all, to do any amendments, are equal to replacement, improve etc., within all should being included in protection scope of the present invention.
Claims (10)
1. one kind has the dirigible of aileron, comprise and be filled with the flexible cover of lighter-than-air gas and be connected to the gondola under flexible cover, it is characterized in that, controlling party is installed to also making the aileron of dirigible by wind-force flight in the both sides of flexible cover, this aileron is fin shape windsurfing, by the sail face framework that is fin shape, the sail face being laid in sail face framework, the sail face bracing frame of support sail face and the aileron of connection dirigible prop up and are configured to, and described aileron support is provided with the turning cylinder of controlling the rotation of sail face, storage or expansion.
2. a kind of dirigible with aileron according to claim 1, is characterized in that, described aileron is concertina type structure, by electronic or manual control storage or expansion.
3. a kind of dirigible with aileron according to claim 1, is characterized in that, described aileron is folded form structure, by electronic or manual control storage or expansion.
4. according to a kind of dirigible with aileron described in claim 2 or 3, it is characterized in that, utilize storage or the expansion of pulley and hawser control aileron.
5. a kind of dirigible with aileron according to claim 4, it is characterized in that, described aileron is provided with two pairs four or more multipair, be symmetricly set on the both sides of dirigible, the junction of each aileron and dirigible is equipped with a pulley, controls hawser and reefing control hawser and synchronously or respectively control storage or the expansion of aileron through lifting a sail of pulley control linkage aileron.
6. a kind of dirigible with aileron according to claim 5, is characterized in that, by changing the sense of motion of angle control dirigible of aileron and working direction.
7. a kind of dirigible with aileron according to claim 5, it is characterized in that, in motion process or under wind-force effect, obtain the motion of buoyancy control dirigible in the vertical direction upwards at the angle control dirigible of vertical direction by changing aileron.
8. a kind of dirigible with aileron according to claim 5, is characterized in that, described aileron is connected with dirigible through mast, and lift a sail control hawser and reefing control hawser are along the setting of mast direction.
9. a kind of dirigible with aileron according to claim 8, is characterized in that, described mast is connected with bolster, on this bolster, is provided with capstan winch, is lift a sail and is controlled the folding and unfolding of hawser and reefing control hawser by this winch control.
10. according to a kind of dirigible with aileron described in claims, it is characterized in that, described gondola can also be located at flexible cover inside, or is located at flexible cover top as ship's deck.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410198047.3A CN104002958A (en) | 2014-05-12 | 2014-05-12 | Airship with auxiliary wings |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410198047.3A CN104002958A (en) | 2014-05-12 | 2014-05-12 | Airship with auxiliary wings |
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| Publication Number | Publication Date |
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| CN104002958A true CN104002958A (en) | 2014-08-27 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410198047.3A Pending CN104002958A (en) | 2014-05-12 | 2014-05-12 | Airship with auxiliary wings |
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| CN (1) | CN104002958A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106335623A (en) * | 2015-12-11 | 2017-01-18 | 中国特种飞行器研究所 | Compact type tethered balloon |
| CN110171556A (en) * | 2019-05-17 | 2019-08-27 | 中国电子科技集团公司第三十八研究所 | A kind of vane type tail gear and the spheric captive balloon with the device |
| CN113371174A (en) * | 2021-05-18 | 2021-09-10 | 北京流体动力科学研究中心 | Regional resident floating system based on sail helps navigation |
| CN114379761A (en) * | 2022-02-17 | 2022-04-22 | 青岛飞宇航空科技有限公司 | Structure of rigid support of air bag |
Citations (6)
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|---|---|---|---|---|
| CN1105329A (en) * | 1994-01-14 | 1995-07-19 | 邝赤科 | Air craft |
| CN101602402A (en) * | 2008-06-11 | 2009-12-16 | 中国科学院光电研究院 | Airship empennage of tail rotor type |
| CN201484655U (en) * | 2009-07-31 | 2010-05-26 | 杨克成 | Power flying and floating aircraft |
| CN101830279A (en) * | 2010-05-28 | 2010-09-15 | 朱明华 | Optical and air energies complementary aerial airship |
| CN201721614U (en) * | 2009-12-10 | 2011-01-26 | 曹斌 | Micro maneuvering airship |
| CN202609074U (en) * | 2012-01-04 | 2012-12-19 | 杨礼诚 | Wind power air transportation system |
-
2014
- 2014-05-12 CN CN201410198047.3A patent/CN104002958A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1105329A (en) * | 1994-01-14 | 1995-07-19 | 邝赤科 | Air craft |
| CN101602402A (en) * | 2008-06-11 | 2009-12-16 | 中国科学院光电研究院 | Airship empennage of tail rotor type |
| CN201484655U (en) * | 2009-07-31 | 2010-05-26 | 杨克成 | Power flying and floating aircraft |
| CN201721614U (en) * | 2009-12-10 | 2011-01-26 | 曹斌 | Micro maneuvering airship |
| CN101830279A (en) * | 2010-05-28 | 2010-09-15 | 朱明华 | Optical and air energies complementary aerial airship |
| CN202609074U (en) * | 2012-01-04 | 2012-12-19 | 杨礼诚 | Wind power air transportation system |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106335623A (en) * | 2015-12-11 | 2017-01-18 | 中国特种飞行器研究所 | Compact type tethered balloon |
| CN110171556A (en) * | 2019-05-17 | 2019-08-27 | 中国电子科技集团公司第三十八研究所 | A kind of vane type tail gear and the spheric captive balloon with the device |
| CN113371174A (en) * | 2021-05-18 | 2021-09-10 | 北京流体动力科学研究中心 | Regional resident floating system based on sail helps navigation |
| CN113371174B (en) * | 2021-05-18 | 2024-05-10 | 北京流体动力科学研究中心 | Regional resident floating system based on sail navigation assistance |
| CN114379761A (en) * | 2022-02-17 | 2022-04-22 | 青岛飞宇航空科技有限公司 | Structure of rigid support of air bag |
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Application publication date: 20140827 |