CN105015754A - Flying system moving by natural wind - Google Patents
Flying system moving by natural wind Download PDFInfo
- Publication number
- CN105015754A CN105015754A CN201410154233.7A CN201410154233A CN105015754A CN 105015754 A CN105015754 A CN 105015754A CN 201410154233 A CN201410154233 A CN 201410154233A CN 105015754 A CN105015754 A CN 105015754A
- Authority
- CN
- China
- Prior art keywords
- air
- connection support
- air bag
- passenger cabin
- support frame
- 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.)
- Pending
Links
Abstract
The invention provides a flying system moving by natural wind, and relates to a flying system moving by natural wind. The technical scheme is that the flying system comprises helium buoyancy lift air bags, a cockpit, and air air-sacs. Two symmetric helium buoyancy lift air bags are installed and fixed on an upper connection support framework. The upper connection support framework is connected with the cockpit. The bottom layer of the cockpit is connected and provided with a lower connection support framework. The two symmetric air air-sacs are installed and fixed on the lower connection support framework. One end of the air air-sac is provided with an air inlet, and the other end of the air air-sac is provided with a vent valve. The cockpit is internally provided with an air pump, a pedal belt drive unit providing power for thrust propellers, and a pedal belt drive unit providing power for the air pump. The gas tubes communicated with the air pump are communicated with the air air-sacs. The system is characterized by high flight security, and can be used for sightseeing above a tourist attraction, and also can be used for advertising media, and meets development trend of environmental protection and energy conversation.
Description
Technical field
The present invention relates to and fly the field of wafing, particularly relate to utilize natural wind to move fly the system of wafing.
Background technology
Existing aircraft, roughly there are three kinds: aircraft, dirigible and fire balloon, most of aviation aircraft all adopts fuel oil equal energy source power to start aircraft, under the situation that fuel oil equal energy source is more and more exhausted, the aviation aircraft adopting the energy to do power does not meet the requirement of low-carbon economy and environmental protection, and flight cost is also very high.Aircraft flight speed is very fast, but safety problem is always troubling; Existing low flyer, as fire balloon, dirigible etc., because wind resistance is poor, cannot go up to the air or fly in the larger situation of wind-force, even if go up to the air reluctantly, air security is difficult to ensure.
Summary of the invention
The object of the invention is to fly with air bag the weak point that row wind resistance is poor, safety is difficult to guarantee of wafting for existing, propose a kind of by using multiple helium buoyance lift air bag and air buoyance lift air bag combination symmetric form, according to aerodynamic principle, by to the utilization of natural wind and conversion, poor to solve wind resistance, safety is difficult to the problem ensured.
Technical scheme of the present invention is: this flies the system of wafing and comprises helium buoyance lift air bag, passenger cabin and air bag, two symmetrical helium buoyance lift air bags are fixed on connection support frame, upper connection support frame is connected with passenger cabin, the bottom of passenger cabin is connected and installed with lower connection support frame, two symmetrical air bags are fixed on lower connection support frame, one end of air bag is provided with air inlet, is provided with air intake valve in admission port.The other end of air bag is provided with aie escape valve, in passenger cabin, inflation pump is housed, and the rear side of passenger cabin is provided with thrust screw propeller, and the coconnected appendix of inflation pump communicates with air bag.The power of inflation pump and thrust screw propeller is all from the foot-operated belt transmission by artificial realization.
When using of the present invention, first two symmetrical helium buoyance lift air bags are full of helium, then two air bags be positioned at below passenger cabin are full of air, when this flies to waft system lift-off, the aie escape valve opened on air bag bleeds off portion of air, make overall weight be relieved to a certain degree, when being less than the carrying force of helium buoyance lift air bag, this flies the system of wafing and starts lift-off.After lift-off, constantly inflate with under the effect of the continuous suck air of air bag admission port at inflation pump, make the present invention maintain certain altitude, under the effect of thrust screw propeller, maintain the low-latitude flying originally flying the system of wafing.When needing in-flight to change direction, realize turning to by the aie escape valve folding on the air bag of the left and right sides.When the present invention declines, inflation pump strengthens inflation dynamics, closes aie escape valve simultaneously, and when air bag and passenger cabin and the weight being connected support frame are greater than helium buoyance lift air bag carrying force, this flies the system of wafing and slowly declines, until landing.
The present invention has following remarkable result:
1, because the present invention mainly leans on natural wind energy as power, do not need electric energy and fuel completely, meet the requirement of energy-saving and environmental protection and low-carbon economy;
2, the present invention has the high feature of flight safety;
3, the present invention can go sightseeing to use above tourist attraction, also may be used for advertising media;
4, the present invention can be used as aerial sports item;
5, the present invention can be used as large-scale aerial amusement platform;
6, the present invention also can be used as low latitude transport facility.
Brief Description Of Drawings
Fig. 1 is structural representation of the present invention.
Fig. 2 is the structural representation of Fig. 1 left view of the present invention.
As shown in the figure: connect support frame 13-under connecting support frame base plate 11-air inlet 12-under 1-helium buoyance lift air bag 2-connecting support frame 3-passenger cabin 4-inflation pump 5-appendix 6-pulling force rope 7-aie escape valve 8-spring device 9-air bag 10-and ride belt transmission 14 thrust screw propeller 15-and ride connection support frame top board 17-air intake valve belt transmission 16-on
Detailed description of the invention
The specific embodiment of the present invention is illustrated by reference to the accompanying drawings: as shown in the figure, and this flies the system of wafing and comprises helium buoyance lift air bag (1), passenger cabin (3) and air bag (9).Two symmetrical helium buoyance lift air bags (1) are fixed on connection support frame (2), upper connection support frame (2) is connected with passenger cabin (3), the bottom of passenger cabin (3) is connected and installed with lower connection support frame (12), two symmetrical air bags (9) are fixed on lower connection support frame (12), one end of air bag (9) is provided with air inlet (11), air intake valve (17) is installed in air inlet (11), automatically open at Action of Wind pressure lower inlet valve door (17), when blast is little or windless condition, air intake valve is closed automatically.The other end of air bag (9) is provided with aie escape valve (7), aie escape valve (7) is provided with spring device (8), spring device (8) is connected with in passenger cabin (3) by pulling force rope (6), and control staff can be facilitated according to declining or turning to situation to handle the folding of aie escape valve.With inflation pump (4), foot-operated belt transmission (13) and foot-operated belt transmission (15) are housed in passenger cabin (3), inflation pump (4) coconnected appendix (5) communicates with air bag (9).Foot-operated belt transmission (13) provides power for thrust screw propeller (14), promotes the present invention and moves ahead.Foot-operated belt transmission (15) provides power for inflation pump (4), is inflated to air bag (9) by appendix (5).
Claims (1)
1. one kind utilize natural wind to move fly the system of wafing, this flies the system of wafing and comprises helium buoyance lift air bag (1), passenger cabin (3) and air bag (9), it is characterized in that: two symmetrical helium buoyance lift air bags (1) are fixed on connection support frame (2), upper connection support frame (2) is connected with passenger cabin (3), the bottom of passenger cabin (3) is connected and installed with lower connection support frame (12), the rear portion of passenger cabin (3) is provided with thrust screw propeller (14), two symmetrical air bags (9) are fixed on lower connection support frame (12), one end of air bag (9) is provided with air inlet (11), air intake valve (17) is installed in air inlet (11), the other end of air bag (9) is provided with aie escape valve (7), aie escape valve (7) is provided with spring device (8), spring device (8) is connected with in passenger cabin (3) by pulling force rope (6), inflation pump (4) is housed in passenger cabin (3), there is provided the foot-operated belt transmission (13) of power for thrust screw propeller and provide the foot-operated belt transmission (15) of power for inflation pump, inflation pump (4) coconnected appendix (5) communicates with air bag (9).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410154233.7A CN105015754A (en) | 2014-04-17 | 2014-04-17 | Flying system moving by natural wind |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410154233.7A CN105015754A (en) | 2014-04-17 | 2014-04-17 | Flying system moving by natural wind |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN105015754A true CN105015754A (en) | 2015-11-04 |
Family
ID=54406151
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410154233.7A Pending CN105015754A (en) | 2014-04-17 | 2014-04-17 | Flying system moving by natural wind |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105015754A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106428505A (en) * | 2016-11-14 | 2017-02-22 | 杨礼诚 | Flying aircraft with jet propeller |
| CN111616091A (en) * | 2020-07-01 | 2020-09-04 | 山东省水生生物资源养护管理中心 | Platform that tourism fishing and box with a net breed combine |
| CN111994268A (en) * | 2020-08-20 | 2020-11-27 | 武汉大学 | Low-power consumption unmanned vehicles based on developments are glided |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2005081680A2 (en) * | 2003-09-09 | 2005-09-09 | Universtiy Of Massachusetts | System and method for altitude control |
| CN2752175Y (en) * | 2004-12-08 | 2006-01-18 | 李鱼飞 | Man power dynamic light-gas airship |
| CN101913425A (en) * | 2010-08-07 | 2010-12-15 | 吴泽峰 | Airship |
| CN102407932A (en) * | 2011-10-08 | 2012-04-11 | 杨礼诚 | Air-propelled multistage separating type flying system |
| CN203246581U (en) * | 2013-03-21 | 2013-10-23 | 郭瀚宁 | Light-gas buoyancy carrier |
| CN203975214U (en) * | 2014-04-17 | 2014-12-03 | 杨礼诚 | A kind of system of wafing that flies of utilizing natural wind motion |
-
2014
- 2014-04-17 CN CN201410154233.7A patent/CN105015754A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2005081680A2 (en) * | 2003-09-09 | 2005-09-09 | Universtiy Of Massachusetts | System and method for altitude control |
| CN2752175Y (en) * | 2004-12-08 | 2006-01-18 | 李鱼飞 | Man power dynamic light-gas airship |
| CN101913425A (en) * | 2010-08-07 | 2010-12-15 | 吴泽峰 | Airship |
| CN102407932A (en) * | 2011-10-08 | 2012-04-11 | 杨礼诚 | Air-propelled multistage separating type flying system |
| CN203246581U (en) * | 2013-03-21 | 2013-10-23 | 郭瀚宁 | Light-gas buoyancy carrier |
| CN203975214U (en) * | 2014-04-17 | 2014-12-03 | 杨礼诚 | A kind of system of wafing that flies of utilizing natural wind motion |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106428505A (en) * | 2016-11-14 | 2017-02-22 | 杨礼诚 | Flying aircraft with jet propeller |
| CN111616091A (en) * | 2020-07-01 | 2020-09-04 | 山东省水生生物资源养护管理中心 | Platform that tourism fishing and box with a net breed combine |
| CN111994268A (en) * | 2020-08-20 | 2020-11-27 | 武汉大学 | Low-power consumption unmanned vehicles based on developments are glided |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN201678037U (en) | Natural power levitation platform | |
| CN108058802A (en) | A kind of variable density unmanned airship based on solar energy | |
| CN201367113Y (en) | Lifting and floating integrated semirigid airship | |
| CN203975214U (en) | A kind of system of wafing that flies of utilizing natural wind motion | |
| CN106005394A (en) | Rescue aircraft | |
| CN108501639A (en) | A kind of hovercar | |
| CN105015754A (en) | Flying system moving by natural wind | |
| CN203410624U (en) | Small-sized hand-thrown unmanned aerial vehicle | |
| CN102730179A (en) | Combined lifting force deformation airship | |
| CN104192301B (en) | A kind of manpower variable wing plane | |
| CN209209028U (en) | One kind is verted three rotor VTOL all-wing aircraft of type | |
| CN202609074U (en) | Wind power air transportation system | |
| CN205524948U (en) | Unmanned autogyro | |
| CN204737021U (en) | Solar energy dirigible of double dynamical dual fail -safe | |
| CN109319083A (en) | A kind of axis change soft lighter-than-air flight device of buoyancy | |
| CN201086826Y (en) | Back pushing type veil opening device of minitype pilotless plane | |
| CN205044987U (en) | Aircraft goes up and down to assist flying platform | |
| CN106965934A (en) | The landing modes and device of a kind of aircraft | |
| CN103640684A (en) | Exhaust flying aircraft | |
| CN102730180A (en) | Fly floating aerial island chain system | |
| CN106965933A (en) | The launching apparatus and mode of a kind of aircraft | |
| CN206518880U (en) | Remote control amphibious aircraft | |
| CN105818955A (en) | Multi-functional flying and floating platform | |
| CN104890850A (en) | Dual-power dual-insurance solar airship | |
| CN104992586A (en) | Airplane system capable of realizing flight experience |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20151104 |
|
| WD01 | Invention patent application deemed withdrawn after publication |