CN103640684A - Exhaust flying aircraft - Google Patents
Exhaust flying aircraft Download PDFInfo
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- CN103640684A CN103640684A CN201310675702.5A CN201310675702A CN103640684A CN 103640684 A CN103640684 A CN 103640684A CN 201310675702 A CN201310675702 A CN 201310675702A CN 103640684 A CN103640684 A CN 103640684A
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- air bag
- air sacs
- valve
- aircraft
- blow
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Abstract
The invention provides an exhaust flying aircraft, and relates to the field of flying. The aircraft comprises a buoyancy lift helium ball (1) and air sacs (3). The air sacs are symmetrically installed on two sides of the buoyancy lift helium ball (1), solar power generation thin film batteries (2) are installed on the upper portion and lateral surfaces of the buoyancy lift helium ball (1) and the upper portions and lateral surfaces of the air sacs (3), ascending exhaust valves (6) are installed on the bottoms of the air sacs (3), propulsion exhaust valves (7) are installed at tails of the air sacs (3), descending exhaust valves (8) are installed on upper portions of the air sacs (3), a cockpit (4) is installed at a position, close to the front position, of the buoyancy lift helium ball (1), various control buttons are installed on a manipulation table in the cockpit (4), and an electric inflator pump (5) used for inflating the air sacs (3) is installed in the cockpit (4). The aircraft is simple in piloting, easy to operate, low in manufacturing cost, good in safety, low-carbon and environmentally friendly, and is an ideal low altitude aircraft.
Description
Technical field
The present invention relates to fly the field of wafing, particularly relate to buoyance lift air bag with the exhausting flight device of inflation/deflation power function balloon.
Background technology
Current low flyer is to take the aircraft that helium air bag is main lift, most flying power all adopts fuel power or electric power to realize, the result of doing is like this waste resource and contaminated environment, under the more and more exhausted situation of fuel oil equal energy source, the aviation aircraft that adopts the energy to do power does not meet the requirement of low-carbon economy and environmental protection, and flight cost is also very high.
Summary of the invention
Object of the present invention, is the offline mode that has thoroughly changed orthodox flight power, mainly utilizes natural power to realize air objective and effect, has reached the requirement of environmental protection low-carbon (LC).
The design of exhausting flight device patent of invention is to consider to adopt super light material to make overlength wind energy producer, with nature animal flight structure researchs for referencial use such as bird and honeybee wings.This flight device comprises buoyance lift helium balloon, air bag, the both sides that are arranged on buoyance lift helium balloon of air bag symmetry, and buoyance lift helium balloon and air bag top and side surfaces are provided with solar electrical energy generation hull cell.The bottom of air bag is provided with rising blow off valve, its afterbody is provided with propelling blow off valve, its top is provided with decline blow off valve, the forward position, bottom of buoyance lift helium balloon is provided with driving compartment, various control buttons are installed on the operation bench in driving compartment, in driving compartment, be provided with can be used for to air bag inflation electric inflating pump.
While using this invention, first will in buoyance lift helium balloon, be full of helium, then will in air bag, be full of air.When the present invention rises, first opening installation, at the rising blow off valve of air bag bottom, along with the discharge of air, causes overall weight of the present invention to alleviate, and makes the vivid lift-off of aircraft.When arriving needed height, close bottom rising blow off valve, the afterbody of opening air bag advances blow off valve, now, by the recoil principle of object, makes aircraft do forward sporting flying; In the time of need to turning, a side air bag of turning advances exhaust valve closure, and opposite side continues exhaust, realizes turning object.After turning effect reaches, both sides air bag advances blow off valve exhaust simultaneously again.The propelling blow off valve of turning off afterbody when the present invention completes predetermined flying distance, hovers in the air aircraft; When cockpit gauge panel shows the air deficiency in air bag, be arranged on aircraft cockpit and control knob startup inflation pump, to air bag, inflate.When the present invention prepares to decline, operator assigns open command to the decline blow off valve that is arranged on air bag top, thereby makes the vivid ground that drops to of aircraft.Thereby lift-off of the present invention, flight, hovering, lower degradation basic exercise process have been realized.
Tool of the present invention has the following advantages:
1, because the present invention does not need fuel oil, do not do fuel, utilize the generating of solar power clean energy resource, to electric inflating pump and actuation means supply electric energy.Low therefore consume energy, the obvious safety of low-carbon environment-friendly feature improves greatly;
2, the present invention can be used as express delivery platform, utilizes hovering function, by rope ladder, transports, passes on mail, has greatly improved Mail Express efficiency;
3, the present invention can be used as the instrument of going sightseeing in the air, also can be used for taking photo by plane in the air;
4, the present invention can hang to publicize and waft with coloured silk, as large-scale advertisement promotional platform, uses;
5, the present invention does not almost have mechanical equipment operation, and noise is low;
6, the present invention compares with mechanical aircraft, drives simple, easy to operate;
7, the present invention's main discharge gas control system of filling by buoyance lift helium balloon and air bag in service rises, flies and declines;
8, the present invention is simple in structure, low cost, and suitable popularization, and range of use is wide.
brief Description Of Drawings
Fig. 1 is structural representation of the present invention.
Fig. 2 is the birds-eye view of Fig. 1 structure of the present invention.
As shown in the figure: 1-buoyance lift helium balloon 2-solar electrical energy generation hull cell 3-air bag 4-driving compartment 5-electric inflating pump 6-rising blow off valve 7-advances blow off valve 8-decline blow off valve.
The specific embodiment
Embodiments of the present invention are illustrated by reference to the accompanying drawings.
As shown in Figure 1 and Figure 2, this flight device comprises buoyance lift helium balloon (1), air bag (3), the both sides that are arranged on buoyance lift helium balloon (1) that air bag (3) is symmetrical, buoyance lift helium balloon (1) and air bag (3) top and side surfaces are provided with solar electrical energy generation hull cell (2).The bottom of air bag (3) is provided with rising blow off valve (6), and its afterbody is provided with and advances blow off valve (7), and its top is provided with decline blow off valve (8).The forward position, bottom of buoyance lift helium balloon (1) is provided with driving compartment (4), on the operation bench in driving compartment (4), various control buttons is installed, in driving compartment (4), be provided with can be used for to air bag (3) inflation electric inflating pump (5).Control button in driving compartment is in order to handle the opening and closing of blow off valve (6), (7), (8) and electric inflating pump (5).
Claims (1)
1. an exhausting flight device, this flight device comprises buoyance lift helium balloon (1), air bag (3), it is characterized in that the both sides that are arranged on buoyance lift helium balloon (1) that air bag (3) is symmetrical, buoyance lift helium balloon (1) and air bag (3) top and side surfaces are provided with solar electrical energy generation hull cell (2), the bottom of air bag (3) is provided with rising blow off valve (6), its afterbody is provided with and advances blow off valve (7), its top is provided with decline blow off valve (8), the forward position, bottom of buoyance lift helium balloon (1) is provided with driving compartment (4), on operation bench in driving compartment (4), various control buttons are installed, in driving compartment (4), be provided with can be used for to air bag (3) inflation electric inflating pump (5), control button in driving compartment is in order to handle blow off valve (6), (7), and the opening and closing of electric inflating pump (5) (8).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310675702.5A CN103640684A (en) | 2013-12-13 | 2013-12-13 | Exhaust flying aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310675702.5A CN103640684A (en) | 2013-12-13 | 2013-12-13 | Exhaust flying aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN103640684A true CN103640684A (en) | 2014-03-19 |
Family
ID=50246024
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201310675702.5A Pending CN103640684A (en) | 2013-12-13 | 2013-12-13 | Exhaust flying aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN103640684A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105818955A (en) * | 2016-06-06 | 2016-08-03 | 杨礼诚 | Multi-functional flying and floating platform |
| CN105857611A (en) * | 2016-05-03 | 2016-08-17 | 北方民族大学 | Unmanned aerial vehicle device capable of prolonging flight time and implementation method |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2034745C1 (en) * | 1992-07-15 | 1995-05-10 | Авиационный научно-технический комплекс "Крыло" | Airship |
| US5755402A (en) * | 1994-01-03 | 1998-05-26 | Henry; Roy | Discoid airship |
| JP2003231499A (en) * | 2002-02-07 | 2003-08-19 | Masahiko Hayashi | Air jetting aircraft |
| CN102530231A (en) * | 2010-12-03 | 2012-07-04 | 伊德斯德国股份有限公司 | High-altitude aerial vehicle |
| CN203111492U (en) * | 2013-02-20 | 2013-08-07 | 刘新广 | Air jet flying ball |
| CN103303456A (en) * | 2013-06-13 | 2013-09-18 | 蒲福祥 | Bionic manned airship |
-
2013
- 2013-12-13 CN CN201310675702.5A patent/CN103640684A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2034745C1 (en) * | 1992-07-15 | 1995-05-10 | Авиационный научно-технический комплекс "Крыло" | Airship |
| US5755402A (en) * | 1994-01-03 | 1998-05-26 | Henry; Roy | Discoid airship |
| JP2003231499A (en) * | 2002-02-07 | 2003-08-19 | Masahiko Hayashi | Air jetting aircraft |
| CN102530231A (en) * | 2010-12-03 | 2012-07-04 | 伊德斯德国股份有限公司 | High-altitude aerial vehicle |
| CN203111492U (en) * | 2013-02-20 | 2013-08-07 | 刘新广 | Air jet flying ball |
| CN103303456A (en) * | 2013-06-13 | 2013-09-18 | 蒲福祥 | Bionic manned airship |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105857611A (en) * | 2016-05-03 | 2016-08-17 | 北方民族大学 | Unmanned aerial vehicle device capable of prolonging flight time and implementation method |
| CN105818955A (en) * | 2016-06-06 | 2016-08-03 | 杨礼诚 | Multi-functional flying and floating platform |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20140319 |