CN201633917U - Energy-saving air sightseeing device - Google Patents
Energy-saving air sightseeing device Download PDFInfo
- Publication number
- CN201633917U CN201633917U CN2010201041913U CN201020104191U CN201633917U CN 201633917 U CN201633917 U CN 201633917U CN 2010201041913 U CN2010201041913 U CN 2010201041913U CN 201020104191 U CN201020104191 U CN 201020104191U CN 201633917 U CN201633917 U CN 201633917U
- Authority
- CN
- China
- Prior art keywords
- cabinet
- energy
- hydrogen
- conservation
- aerial
- 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
Links
Images
Abstract
The utility model relates to a travelling device, in particular to an energy-saving air sightseeing device; the energy-saving air sightseeing device comprises a suspension device and a case; the energy-saving air sightseeing device is characterized in that: the suspension device is a fan-shaped structure formed by connecting a plurality of hydrogen balloons by a large net, the suspension device is communicated with hydrogen in the case by a hydrogen supplying pipe, a steady rod is arranged on the suspension device in the case, the suspension device and the steady rod are connected by an upper steady rope, and a lower steady rope is arranged between the steady rod and the case; a driving operation room is arranged in the case, and a power device, a balance board and a rudder are arranged in the case, and a screw propeller is arranged outside the case and at the periphery of the hydrogen supplying pipe; the energy-saving air sightseeing device is manufactured with low cost, is easy to drive and is easy to control in the air for realizing sightseeing effect.
Description
Technical field
The utility model relates to a kind of travelling device, particularly a kind of energy-conservation aerial tour device.
Background technology
Along with improving constantly of people's living standard, the essence variation has also taken place to the mode of going sightseeing, travel in people, and along with development of science and technology, people have also begun exploitation space, moon trip when exploring space, moon secret.But to space, moon tourism, with the ordinary people, cost is too high, so that is difficult to realize.As the air transit instrument, though aircraft can be implemented in aerial navigation, it is in the nature the vehicle, but not for sightseeing usefulness, thus its speed soon, highly high, be not suitable for as the travelling device.2003.05.28 Patent Office of the People's Republic of China discloses the utility model patent of a kind of by name " aircraft ", and (notification number: CN1420829), an aircraft preferably span does not have fuselage or yaw rudder from cargo-carring flight wing.This aircraft is with the flight of lower speed, and has 200 feet the span, in the major part of this aerofoil surface photovoltaic element is housed.This aircraft utilizes the difference of its eight angle of rake thrusts to turn.Each of five parts of wing has one or more driving engine and photocell matrix, and is independent of other parts and produces the lift of himself, to avoid that other part is produced load.Whole five photocell matrixs are received from the photoelectric energy of wing top incident by transparent surface, and from the photoelectric energy of wing bottom incident.This aircraft comprises hinge means and actuating device, is used to wing to form adjustable dihedral.This actuating device can be driving engine or control surface.As selection, this actuating device can be can be movably material block in the wing, and its shape that can change wing to be changing the aerodynamic force educational level of this wing, and therefore activates this hinge means.Because utilized the dihedral of wing, this aircraft is included in the driving engine on the drag center and under the drag center, this aircraft uses the thrust difference to come the pitching of controlling aircraft.This Flight Vehicle Structure complexity, cost is very high, is unsuitable for applying, and uses difficulty complicated, and the ordinary people is not easy to control; In addition, this aircraft does not have yaw rudder, can not control its heading.
Summary of the invention
For overcoming the above-mentioned deficiency of prior art, the utility model provides a kind of energy-conservation aerial tour device, cheap, the easy effect of driving, can control arbitrarily its realization sightseeing that flies aloft that this device is made.
The utility model adopts following technical scheme:
A kind of energy-conservation aerial tour device, comprise levitation device and cabinet, it is characterized in that: described levitation device connects the sector structure that several hydrogen balloons form for big net, levitation device is communicated with by the interior sources of hydrogen of hydrogen supply pipe and cabinet, levitation device is provided with firm bar in cabinet, connect by last firm rope between described levitation device and the firm bar, firm rope is set down between firm bar and the cabinet; Be provided with between driver behavior in the described cabinet, simultaneously, power plant, balance plate and yaw rudder be set in the cabinet; Outside cabinet, reach hydrogen supply pipe periphery screw propeller is set.
Described cabinet is made of light material.
Described cabinet periphery is provided with guardrail.
Described cabinet bottom is provided with castor.
Be connected by spring between described castor and the cabinet.
On last firm rope, also be provided with the advertisement width of cloth.
Hydrogen balloon has buoyancy, will big online holder, and firmly rope, hydrogen supply pipe, firm bar and firm down rope in the pull-up, several hydrogen balloons at ordinary times can not be higher than the total weight of whole device toward total power that floats.
Cabinet of the present utility model is used to hold the visitor goes sightseeing, and cabinet does not seal, and is made by light material, with expendable weight.Levitation device is that net connects the sector structure that several hydrogen balloons form greatly, and levitation device is communicated with by the interior sources of hydrogen of hydrogen supply pipe and cabinet, can guarantee and will draw high sky on the cabinet; Sources of hydrogen can be guaranteed the unsettled of levitation device energy longer time; Firm bar firmly levitation device is used between driver behavior control the sightseeing device in cabinet, and balance plate plays equilibrium activity, and yaw rudder can guarantee that the visitor controls the touring line of sightseeing device arbitrarily; Guardrail increases the safety of cabinet, and castor and spring can make steadily landing of safety of sightseeing device.When people's tour, the equipment that turns on the power, sources of hydrogen is started working, fill up hydrogen toward top hydrogen balloon by the hydrogen supply pipe, whole tour device just slowly rises, and behind certain altitude, opens screw propeller, under the effect at yaw rudder and the movable place of yaw rudder, chaufeur can selection schemer aloft be gone sight-seeing, according to the height needs, and plus-minus hydrogen total volume, be hydrogen balloon under the effect of hydrogen supply pipe, the hydrogen supply pipe just produces under the effect of sources of hydrogen.Owing to be not aircraft, tourism business does not need too fast speed, and slowly visit gets final product, and therefore, under the situation of simplicity of design own, resistance is also little, and screw propeller rotates, and yaw rudder is adjusted direction, travels to predetermined circuit at leisure, reaches the effect of sightseeing.Cut energy savings, compare, have energy-conservation effect with other aircraft.
Description of drawings
Fig. 1 is a structural representation of the present utility model.
Wherein 1 be cabinet, 2 for guardrail, 3 between driver behavior, 4 be the hydrogen supply pipe for hydrogen balloon, 17 for last firm rope, 16 for firm rope down, 15 for big net, 14 for firm bar, 13 for the movable place of yaw rudder, 12 for yaw rudder, 11 for balance plate, 10 for spring, 9 for castor, 8 for sources of hydrogen, 7 for power plant, 6 for screw propeller, 5.
The specific embodiment
Below in conjunction with accompanying drawing the utility model is further described.As shown in Figure 1, the utility model provides a kind of energy-conservation aerial tour device, cheap, the easy effect of driving, can control arbitrarily its realization sightseeing that flies aloft that this device is made.The tour device comprises levitation device and cabinet 1, the described levitation device big net 13 of serving as reasons connects the sector structure that several hydrogen balloons 16 form, levitation device is communicated with by hydrogen supply pipe 17 and cabinet 1 interior sources of hydrogen, firm bar 12 is set between levitation device and the cabinet 1, connect by last firm rope 15 between described levitation device and the firm bar 12, firm rope 14 is set down between firm bar 12 and the cabinet 1; Be provided with between driver behavior 3 in the described cabinet 1, simultaneously, power plant 5, balance plate 9 and yaw rudder be set in the cabinet 1; 10 reach hydrogen supply pipe 17 peripheries outside cabinet 1 is provided with screw propeller 4.Cabinet 1 is made of light material, is provided with guardrail 2 in cabinet 1 periphery, and the bottom is provided with castor 7, is connected by spring 8 between described castor 7 and the cabinet 1, also is provided with advertisement 18 on last firm rope 15.Hydrogen balloon 16 has buoyancy, with big net 13 pop-ups, and firm rope 15, hydrogen supply pipe 17, firm bar 12 and down firm rope 14 in the pull-up, several hydrogen balloons 16 at ordinary times can not be higher than the total weight of whole device toward the total power of come-up.Wherein cabinet 1 is used to hold the visitor and goes sightseeing, and cabinet 1 does not seal, and is made by light material, with expendable weight.The levitation device big net 13 of serving as reasons connects the sector structure that several hydrogen balloons 16 form, and levitation device is communicated with by hydrogen supply pipe 17 and cabinet 1 interior sources of hydrogen, can guarantee and will draw high sky on the cabinet 1; Sources of hydrogen can be guaranteed the unsettled of levitation device energy longer time; Firm bar 12 is levitation device and cabinet 1 firmly, and 3 are used to control the sightseeing device between driver behavior, 9 equilibrium activitys of balance plate, and yaw rudder 10 can guarantee that the visitor controls the touring line of sightseeing device arbitrarily; Guardrail 2 increases the safety of cabinet, and castor 7 and spring 8 can make steadily landing of safety of sightseeing device.When people's tour, the equipment 5 that turns on the power, sources of hydrogen is started working, fill up hydrogen toward top hydrogen balloon 16 by hydrogen supply pipe 17, whole tour device just slowly rises, and behind certain altitude, opens screw propeller 4, under the effect at yaw rudder 10 and the movable place 11 of yaw rudder, chaufeur can selection schemer aloft be gone sight-seeing, according to the height needs, and plus-minus hydrogen total volume, be hydrogen balloon 16 under 17 effects of hydrogen supply pipe, hydrogen supply pipe 17 produces under the effect of sources of hydrogen.Owing to be not aircraft, tourism business does not need too fast speed, and slowly visit gets final product, and therefore, under the situation of simplicity of design own, resistance is also little, and screw propeller 4 rotates, and yaw rudder 10 is adjusted direction, travels to predetermined circuit at leisure, reaches the effect of sightseeing.Being provided with of the advertisement width of cloth can be provided with advertisement on the sightseeing device, the sky writing effect is better.The utility model can also energy savings, compares with other aircraft, has energy-conservation effect.
Claims (6)
1. energy-conservation aerial tour device, comprise levitation device and cabinet (1), it is characterized in that: the described levitation device big net (13) of serving as reasons connects the sector structure that several hydrogen balloons (16) form, levitation device is communicated with by the interior sources of hydrogen of hydrogen supply pipe (17) and cabinet (1), firm bar (12) is set between levitation device and the cabinet (1), connect by last firm rope between described levitation device and the firm bar (12), between firm bar (12) and the cabinet (1) firm rope (14) is set down; Be provided with in the described cabinet (1) (3) between driver behavior, simultaneously, power plant (5), balance plate (9) and yaw rudder (10) be set in the cabinet (1); Outside cabinet (1), reach hydrogen supply pipe (17) periphery screw propeller (4) is set respectively.
2. energy-conservation aerial tour device according to claim 1, it is characterized in that: described cabinet (1) is made of light material.
3. energy-conservation aerial tour device according to claim 1 is characterized in that: described cabinet (1) periphery is provided with guardrail (2).
4. energy-conservation aerial tour device according to claim 1 is characterized in that: described cabinet (1) bottom is provided with castor (7).
5. energy-conservation aerial tour device according to claim 4 is characterized in that: be connected by spring (8) between described castor (7) and the cabinet (1).
6. energy-conservation aerial tour device according to claim 1 is characterized in that: also be provided with the advertisement width of cloth (18) on last firm rope (15).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2010201041913U CN201633917U (en) | 2010-01-29 | 2010-01-29 | Energy-saving air sightseeing device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2010201041913U CN201633917U (en) | 2010-01-29 | 2010-01-29 | Energy-saving air sightseeing device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201633917U true CN201633917U (en) | 2010-11-17 |
Family
ID=43078401
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2010201041913U Expired - Fee Related CN201633917U (en) | 2010-01-29 | 2010-01-29 | Energy-saving air sightseeing device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN201633917U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106218853A (en) * | 2016-09-30 | 2016-12-14 | 德保县实验小学 | A kind of hot air balloon device |
-
2010
- 2010-01-29 CN CN2010201041913U patent/CN201633917U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106218853A (en) * | 2016-09-30 | 2016-12-14 | 德保县实验小学 | A kind of hot air balloon device |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US8894002B2 (en) | System and method for solar-powered airship | |
| CN101778759B (en) | Lenticular airship and associated controls | |
| CN101157383B (en) | A novel V-shaped sopiler airship | |
| US20150360775A1 (en) | Vertical take-off and landing flight vehicle | |
| CN102717887B (en) | A kind of inflatable wing and can the near space dirigible of tilted propeller of adopting | |
| CN104290906B (en) | A kind of vertically taking off and landing flyer | |
| CN104925243B (en) | A kind of variable inflated type buoyance lift integration stratospheric airship of span | |
| CN102186723A (en) | Aircraft system that enables ground traveling | |
| CN102730183B (en) | Novel solar airplane | |
| CN102730192B (en) | A kind of can the aircraft of vertical takeoff and landing | |
| CN102673787B (en) | Small-sized combined type air vehicle adopting layout combining disk swing with variable wings and airbag | |
| CN106628099A (en) | Tethered and autonomous flight dual-purpose solar aerostat | |
| CN206265280U (en) | A kind of dirigible without rudder face structure | |
| CN103991534A (en) | Vertical take-off and landing safety aircraft | |
| CN205686600U (en) | The aircraft that a kind of dirigible is combined with many rotors | |
| CN201633917U (en) | Energy-saving air sightseeing device | |
| CN201484655U (en) | Power flying and floating aircraft | |
| CN105329441B (en) | A kind of four axis all-wing aircraft aircraft of combined type | |
| CN207403919U (en) | A kind of new unmanned airship | |
| CN105564647A (en) | Low-altitude aircraft | |
| CN202089231U (en) | Aerial rotary restaurant | |
| CN201158456Y (en) | Solar energy electric airship | |
| US20060049301A1 (en) | Solar-Powered Floatation Device for all types of vehicles (air, land and sea) | |
| CN104229130A (en) | Four-rotor wing unmanned aerial vehicle with pneumatic structure | |
| CN204056295U (en) | Pneumatic structure four rotor unmanned aircraft |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20101117 Termination date: 20110129 |