CN2752175Y - Man power dynamic light-gas airship - Google Patents
Man power dynamic light-gas airship Download PDFInfo
- Publication number
- CN2752175Y CN2752175Y CN 200420055479 CN200420055479U CN2752175Y CN 2752175 Y CN2752175 Y CN 2752175Y CN 200420055479 CN200420055479 CN 200420055479 CN 200420055479 U CN200420055479 U CN 200420055479U CN 2752175 Y CN2752175 Y CN 2752175Y
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- CN
- China
- Prior art keywords
- body skin
- dirigible
- manpowered
- storehouse
- airship
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
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Abstract
The utility model discloses a light-gas airship with manpower used as motive power, which comprises an outer housing, an air bag arranged in the external shell, a suspension chamber arranged under the outer housing, outer housing screw propellers connected with the outer housing, a propulsion device thereof and a driving device for the airship, wherein lateral wings of the airship are arranged on both sides of the outer housing, accumulator cells which supply electrical energy to each part are arranged in the suspension chamber, and the input ends of the accumulator cells are respectively connected with the output end of a solar power supply device and the output end of an electric generator; the input end of the electric generator is connected with the output end of a pedal driving device, an air storage tank is arranged in the suspension chamber and is connected with the air bag through an air pipe. The utility model has the advantages of simple structure, small size, safe use and easy operation, solar energy and manpower resources are adopted for supplying energy to the power section of the airship, light weight air is adopted and is used circularly, and the utility model has energy saving and environment protection; besides, the airship can be guaranteed to stay in the air for a long time and the utility model has high elevation and falling speed and flexible reaction.
Description
Technical field
The utility model relates to a kind of dirigible, relates in particular to a kind of manpowered light gas airship that industries such as family, tourism and military affairs are used that is suitable for.
Background technology
Dirigible is a kind of aircraft of light filling gas, and it can aloft suspend, vertical takeoff and landing, and not resembling needs facilities such as airfield runway the aircraft such as other aircraft.The noise of dirigible is low, can be in low-latitude flying, so dirigible also is suitable for going sightseeing except that the transportation means that is used for as aerial shipping goods, but present dirigible major part all is to be used for bearing goods, and do not see promising going sightseeing and the dirigible developed.Also there is following weak point in present dirigible: the manufacturing cost height, bulky, poor stability, the operating sequence complexity, sensitivity is low since propulsion source to be limited in aerial length of the halt shorter.
The utility model content
The utility model provides a kind of rational in infrastructure in order to solve the problems of the technologies described above exactly, safe in operation, reliable, and volume is little, and processing ease is beneficial to the manpowered light gas airship that people use.
In order to solve the problems of the technologies described above, the utility model is achieved in that a kind of manpowered light gas airship, it comprises body skin, be arranged on the air bag in the body skin, body skin below is provided with hangs the storehouse, body skin screw propeller that is connected with body skin and propelling unit thereof and dirigible actuating device, the both sides that it is characterized in that body skin are provided with the dirigible flank, for providing the storage battery of electric energy to be arranged on, hangs in the storehouse each several part, the input end of storage battery is connected with the mouth of solar power supply apparatus and the mouth of electrical generator respectively, the input end of electrical generator is connected with the mouth of foot drive device, hangs and is provided with gaholder in the storehouse, gaholder is connected with air bag by tracheae.
Described manpowered light gas airship, it also comprises the tail big shield that is connected with the rear end of body skin.
Described air bag is made up of a plurality of ballonets, and each ballonet is connected with gaholder by tracheae respectively.
Described manpowered light gas airship, it also comprise with hang that the storehouse is connected hang storehouse screw propeller and propelling unit thereof.
Dirigible flank and body skin flexibly connect, and are rotary structure.
Described dirigible flank is captiveed joint with body skin, and the dirigible flank is made of the blinds that is provided with in support and the support.
The top of described body skin is provided with the optical fiber observing instrument, and the optical fiber observing instrument is connected with read out instrument in hanging the storehouse by cable.
Advantage of the present utility model and effect are as follows:
The utility model is simple in structure, and volume is little, and is safe in utilization, processing ease adopts solar power and human resources to provide the energy for the power pack section of dirigible, adopts light gas to recycle, energy-conserving and environment-protective, and guaranteed that dirigible can stop for a long time aloft, it is produced material and is easy to get, make easily, rising or falling speed is fast, and reaction is fit to industries such as family, tourism and military affairs and uses flexibly, be beneficial to enforcement, have extensive market prospects.
Below in conjunction with the drawings and specific embodiments the utility model is described in further details.
Description of drawings
Fig. 1 is a structural representation of the present utility model.
Fig. 2 is a birds-eye view of the present utility model.
Among the figure, 1. body skin, 2. air bag, 3. solar power supply apparatus, 4. optical fiber observing instrument, 5. body skin screw propeller and propelling unit thereof, 6. the dirigible flank 7. hangs storehouse screw propeller and propelling unit thereof, 8. foot drive device, 9. motor, 10. gas compressor, 11. freeing pipes, 12. gaholder, 13. hang the storehouse, 14. air inlet pipes, 15. electrical generator, 16. storage batterys, 17. tails are sculled.
The specific embodiment
Embodiment one
A kind of manpowered light gas airship, it is to be made of following structure: body skin 1; Be arranged on the air bag 2 in the body skin 1; Body skin 1 below is provided with hangs storehouse 13; The body skin screw propeller and the propelling unit 5 thereof that are connected with the front end face of body skin 1; What be connected with the front end face that hangs storehouse 13 hangs storehouse screw propeller and propelling unit 7 thereof; The dirigible actuating device; The both sides of body skin 1 are provided with dirigible flank 6, dirigible flank 6 flexibly connects with body skin 1, is rotary structure, and the rotation of dirigible flank 6 is controlled by being arranged on the dirigible flank hand-control device that hangs in the storehouse, control part is a prior art, is not described in detail its concrete structure; The tail that is connected with the rear end of body skin 1 sculls 17, and the structure of tail big shield 17 and ship are sculled basic identical, and its front end is that rigid material is made, and the rear end is made by flexible material; For providing the storage battery 16 of electric energy to be arranged on, hangs in the storehouse 13 each several part, the input end of storage battery 16 is connected with the mouth of solar power supply apparatus 3 and the mouth of electrical generator 15 respectively, the input end of electrical generator 15 is connected with the mouth of foot drive device 8, the input shaft junction of the output shaft of foot drive device 8 and electrical generator 15 is provided with power-transfer clutch, motor 9 is by storage battery 16 power supplies, and solar power supply apparatus 3 is arranged on the upper surface of body skin 1; Hang and be provided with gaholder 12 in the storehouse, gaholder 12 is connected with air bag 2 with freeing pipe 11 by air inlet pipe 14, air inlet pipe 14 is provided with control cock, freeing pipe 11 is provided with gas compressor 10, gas compressor 10 links to each other with the mouth of motor 9, and gas compressor 10 is provided with power-transfer clutch with the adapter shaft of motor 9; The top of body skin 1 is provided with optical fiber observing instrument 4, and optical fiber observing instrument 4 is connected with read out instrument in hanging storehouse 13 by cable, and optical fiber observing instrument 4 and read out instrument are not described in detail for prior art the utility model.
Embodiment two
Embodiment one described air bag 2 is made up of a plurality of ballonets, and each ballonet air inlet pipe by separately respectively is connected with gaholder 12 with freeing pipe.Other is with embodiment one.
Embodiment three
Embodiment one described dirigible flank 6 is captiveed joint with body skin 1, and dirigible flank 6 is made of the blinds that is provided with in support and the support.Hanging of dirigible is provided with dirigible flank control setup in the storehouse, be used to control the folding direction of dirigible flank 6 blinds, and control setup is a prior art, is not described in detail its concrete structure, and other is with embodiment one.
Claims (7)
1. manpowered light gas airship, it comprises body skin (1), be arranged on the air bag (2) in the body skin (1), body skin (1) below is provided with hangs storehouse (13), the body skin screw propeller that is connected with body skin (1) and propelling unit (5) and dirigible actuating device, the both sides that it is characterized in that body skin (1) are provided with dirigible flank (6), for providing the storage battery (16) of electric energy to be arranged on, hangs in the storehouse (13) each several part, the input end of storage battery (16) is connected with the mouth of solar power supply apparatus (3) and the mouth of electrical generator (15) respectively, the input end of electrical generator (15) is connected with the mouth of foot drive device (8), hangs and is provided with gaholder (12) in the storehouse, gaholder (12) is connected with air bag (2) by tracheae.
2. manpowered light gas airship according to claim 1 is characterized in that it also comprises the tail big shield (17) that is connected with the rear end of body skin (1).
3. manpowered light gas airship according to claim 1 and 2 is characterized in that described air bag (2) is made up of a plurality of ballonets, and each ballonet is connected with gaholder (12) by tracheae respectively.
4. manpowered light gas airship according to claim 1, it is characterized in that it also comprise with hang that the storehouse is connected hang storehouse screw propeller and propelling unit (7) thereof.
5. manpowered light gas airship according to claim 1 and 2 is characterized in that described dirigible flank (6) and body skin (1) flexibly connect, and are rotary structure.
6. manpowered light gas airship according to claim 1 and 2 is characterized in that described dirigible flank (6) captives joint with body skin (1), and dirigible flank (6) is made of the blinds that is provided with in support and the support.
7. manpowered light gas airship according to claim 1 is characterized in that the top of described body skin (1) is provided with optical fiber observing instrument (4), and optical fiber observing instrument (4) is connected by the cable read out instrument interior with hanging storehouse (13).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 200420055479 CN2752175Y (en) | 2004-12-08 | 2004-12-08 | Man power dynamic light-gas airship |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 200420055479 CN2752175Y (en) | 2004-12-08 | 2004-12-08 | Man power dynamic light-gas airship |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN2752175Y true CN2752175Y (en) | 2006-01-18 |
Family
ID=35913584
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 200420055479 Expired - Fee Related CN2752175Y (en) | 2004-12-08 | 2004-12-08 | Man power dynamic light-gas airship |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN2752175Y (en) |
Cited By (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101860088A (en) * | 2010-05-27 | 2010-10-13 | 中国电子科技集团公司第三十八研究所 | Microwave wireless energy transfer system for airship |
| CN101885378A (en) * | 2010-07-06 | 2010-11-17 | 张朝林 | Inflation airship |
| CN101913425A (en) * | 2010-08-07 | 2010-12-15 | 吴泽峰 | Airship |
| CN102424104A (en) * | 2011-12-31 | 2012-04-25 | 沈阳航空航天大学 | Four-rotor-wing indoor airship |
| CN102874400A (en) * | 2012-10-22 | 2013-01-16 | 湖南航天机电设备与特种材料研究所 | Airship tail vectored thrust device |
| CN104640767A (en) * | 2012-04-24 | 2015-05-20 | 拉斯卡尔有限公司 | Neutral buoyancy craft |
| CN105015754A (en) * | 2014-04-17 | 2015-11-04 | 杨礼诚 | Flying system moving by natural wind |
| CN105059524A (en) * | 2015-07-29 | 2015-11-18 | 骆银成 | Micropower hovering recreational vehicle |
| CN105667754A (en) * | 2015-12-31 | 2016-06-15 | 上海交通大学 | Airship valve flow optimal control method |
| CN106428505A (en) * | 2016-11-14 | 2017-02-22 | 杨礼诚 | Flying aircraft with jet propeller |
| CN107117303A (en) * | 2017-05-31 | 2017-09-01 | 佛山市神风航空科技有限公司 | A kind of man-powered aircraft that can be generated electricity |
| CN108248809A (en) * | 2018-01-10 | 2018-07-06 | 北京天恒长鹰科技股份有限公司 | Stratosphere powered balloon |
| CN108945383A (en) * | 2018-09-12 | 2018-12-07 | 重庆交通职业学院 | The kayak body of more unmanned hot air dirigible airships of rotor |
| CN111994268A (en) * | 2020-08-20 | 2020-11-27 | 武汉大学 | Low-power consumption unmanned vehicles based on developments are glided |
-
2004
- 2004-12-08 CN CN 200420055479 patent/CN2752175Y/en not_active Expired - Fee Related
Cited By (17)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101860088A (en) * | 2010-05-27 | 2010-10-13 | 中国电子科技集团公司第三十八研究所 | Microwave wireless energy transfer system for airship |
| CN101860088B (en) * | 2010-05-27 | 2012-10-03 | 中国电子科技集团公司第三十八研究所 | Microwave wireless energy transfer system for airship |
| CN101885378A (en) * | 2010-07-06 | 2010-11-17 | 张朝林 | Inflation airship |
| CN101913425A (en) * | 2010-08-07 | 2010-12-15 | 吴泽峰 | Airship |
| CN102424104A (en) * | 2011-12-31 | 2012-04-25 | 沈阳航空航天大学 | Four-rotor-wing indoor airship |
| CN104640767A (en) * | 2012-04-24 | 2015-05-20 | 拉斯卡尔有限公司 | Neutral buoyancy craft |
| CN102874400A (en) * | 2012-10-22 | 2013-01-16 | 湖南航天机电设备与特种材料研究所 | Airship tail vectored thrust device |
| CN105015754A (en) * | 2014-04-17 | 2015-11-04 | 杨礼诚 | Flying system moving by natural wind |
| CN105059524A (en) * | 2015-07-29 | 2015-11-18 | 骆银成 | Micropower hovering recreational vehicle |
| CN105667754A (en) * | 2015-12-31 | 2016-06-15 | 上海交通大学 | Airship valve flow optimal control method |
| CN106428505A (en) * | 2016-11-14 | 2017-02-22 | 杨礼诚 | Flying aircraft with jet propeller |
| CN107117303A (en) * | 2017-05-31 | 2017-09-01 | 佛山市神风航空科技有限公司 | A kind of man-powered aircraft that can be generated electricity |
| CN108248809A (en) * | 2018-01-10 | 2018-07-06 | 北京天恒长鹰科技股份有限公司 | Stratosphere powered balloon |
| CN108248809B (en) * | 2018-01-10 | 2024-02-13 | 北京天恒长鹰科技股份有限公司 | Stratosphere dynamic balloon |
| CN108945383A (en) * | 2018-09-12 | 2018-12-07 | 重庆交通职业学院 | The kayak body of more unmanned hot air dirigible airships of rotor |
| CN108945383B (en) * | 2018-09-12 | 2021-10-22 | 重庆交通职业学院 | Hull of unmanned steam airship with multiple rotors |
| CN111994268A (en) * | 2020-08-20 | 2020-11-27 | 武汉大学 | Low-power consumption unmanned vehicles based on developments are glided |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C19 | Lapse of patent right due to non-payment of the annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |