CN101885379A - Automatically inflatable balloon and hot air balloon parachute - Google Patents
Automatically inflatable balloon and hot air balloon parachute Download PDFInfo
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- CN101885379A CN101885379A CN2010102297438A CN201010229743A CN101885379A CN 101885379 A CN101885379 A CN 101885379A CN 2010102297438 A CN2010102297438 A CN 2010102297438A CN 201010229743 A CN201010229743 A CN 201010229743A CN 101885379 A CN101885379 A CN 101885379A
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- balloon
- parachute
- hot air
- automatically inflatable
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Abstract
The invention provides an automatically inflatable balloon and hot air balloon parachute combining an automatically inflatable balloon, a hot air balloon and a parachute. The automatically inflatable balloon and hot air balloon parachute consists of a sealed (hot air) balloon on the top, automatically inflatable (hot air) balloon in the middle, parachute at the bottom, height direction control wings and a suspended power cockpit, wherein the sealed (hot air) balloon on the top is made of a light thin heat preservation sealing elastic material, is inflated with light gas and is not heated, or inflated with ordinary air and heated by tail gas of a combustor or an internal combustion engine, electric energy or solar energy; the bottom part of the automatically inflatable (hot air) balloon in the middle is provided with a semi-passing valve for impelling air to enter and hold up; the bottom part is provided with the parachute; the height direction control wings are horizontally and vertically connected to a suspension cable or the cockpit respectively; and the lower part of the suspension cable is suspended with the power cockpit. The automatically inflatable balloon and hot air balloon parachute has the advantages of eliminating defects of an ordinary balloon, the hot air balloon and the parachute, and preventing falling accidents because the hot air balloon is burned down or the parachute cannot be opened.
Description
Affiliated technical field
The present invention relates to a kind of lift-off landing flight tool, the especially automatically inflatable balloon and hot air balloon parachute that automatically inflatable balloon, fire balloon and parachute are combined.
Background technology
The fire balloon of prior art uses naked light to add hot air and makes fire balloon go up to the air, cause fire balloon to burn easily and fall; The monolayer umbrella of prior art generally can only utilize the passive landing of air resistance and be difficult for rising, in case parachute is not opened and will be fallen; The balloon of prior art can not be inflated heating aloft automatically.Balloon, fire balloon and parachute three's advantage can not be given full play to, and fatal defective is aloft all arranged separately.
Summary of the invention
In order to give full play to balloon, fire balloon and parachute three's advantage, remedy critical defect separately, the invention provides a kind of with automatically inflatable balloon, the automatically inflatable balloon and hot air balloon parachute that fire balloon and parachute combine, sealed type (heat) balloon by the top, automatic inflation (heat) balloon at middle part, the parachute of bottom, five parts such as Pilotage en Force cabin of the short transverse control wing and suspension are formed, the sealed type at top (heat) balloon adopts frivolous sealing insulation elastic material to make, can fill with light gas and need not heat, also can fill with normal air and adopt burner section, exhaust gases of internal combustion engines, electric energy, solar energy heating; Automatic inflation (heat) the balloon bottom at middle part is adopted half through type valve to impel gas to enter and is detained; Safety when the bottom parachute guarantees landing; The short transverse control wing is connected on suspension cable or the driving compartment respectively horizontally and vertically; The Pilotage en Force cabin that hangs is used for manned loading and active flight is driven.
The technical solution adopted for the present invention to solve the technical problems is: the present invention is the technical solution problem in the following manner.
1, the sealed type at automatically inflatable balloon and hot air balloon parachute top (heat) balloon.The sealed type at top (heat) balloon adopts frivolous sealing warm material to make, as the basic lift support area of aircraft.Can fill with light gas and need not heat, also can fill with normal air and adopt burner section, exhaust gases of internal combustion engines, electric energy, solar energy heating.By covered pipe hot gas is transported in the balloon from driving compartment when adopting the burner section heating, rather than directly heats in the balloon internal combustion.Install automatic and manual exhaust valve on the balloon additional, exhaust decompression when the balloon internal pressure is excessive.
2, automatic inflation (heat) balloon at automatically inflatable balloon and hot air balloon parachute middle part.Automatic inflation (heat) the balloon bottom at middle part is adopted half through type valve to impel gas to enter and is detained: when balloon decline or air-flow rising, the balloon external pressure is greater than air pressure inside, and the valve that can upwardly open is opened, and air-flow enters in the balloon envelope; When balloon rises or air-flow when descending, balloon interior air pressure is greater than external pressure, the valve closure that can not open downwards, and gas is trapped in balloon interior.Also can adopt burner section, exhaust gases of internal combustion engines hot gas to be transported in the balloon from driving compartment, also install automatically and manual exhaust valve exhaust decompression when the balloon internal pressure is excessive on the balloon additional by covered pipe.
3, the parachute of automatically inflatable balloon and hot air balloon parachute bottom.The full skirt that parachute is actual around having only and do not have the umbrella top, the umbrella top is replaced by half through type valve of automatic inflation (heat) balloon bottom, reduces descending speed when balloon descends, the assurance personal security.
4, the short transverse of the automatically inflatable balloon and hot air balloon parachute control wing.Be connected horizontally and vertically respectively on suspension cable or the Pilotage en Force cabin, can controlling level direction and vertical dimension during flight, and can rely on self lifting flight.
5, the Pilotage en Force cabin of automatically inflatable balloon and hot air balloon parachute suspension.The Pilotage en Force cabin hangs by suspension cable, and subsidiary heat power and the horizontal motion engine installation installed is used for manned loading and active flight and drives.
The invention has the beneficial effects as follows that automatically inflatable balloon and hot air balloon parachute can be inflated as common balloon, can heat, can select differing heights and direction flight as aircraft as the slow landing of parachute as fire balloon.Eliminated the defective of general balloon, fire balloon, parachute, prevented, made and take automatically inflatable balloon and hot air balloon parachute flight becoming a kind of safer experience and enjoyment because of the falling accident that fire balloon burns, parachute is not opened to be caused.
Description of drawings
The present invention is further described below in conjunction with drawings and Examples.
Fig. 1 is the layering scheme drawing of automatically inflatable balloon and hot air balloon parachute of the present invention.
Fig. 2 is a balloon gas piping scheme drawing of the present invention.
Fig. 3 is automatic inflation (heat) the balloon bottom half through type valve scheme drawing at the present invention middle part.
Fig. 4 is a full skirt scheme drawing around the parachute of the present invention bottom.
Fig. 5 is a short transverse control wing scheme drawing of the present invention.
Fig. 6 is a suspension Pilotage en Force of the present invention cabin scheme drawing.
Fig. 7 is an exemplary embodiments of the present invention.
The sealed type at 1. tops (heat) balloon among the figure, 2. automatic inflation (heat) balloon at middle part, the 3. parachute of bottom, 4. the short transverse control wing 5. hangs Pilotage en Force cabin, 6. gas piping, 7. half through type valve, 8. full skirt, 9. suspension cable around the parachute, 10. automatic exhaust steam valve, 11. heat powers and horizontal motion engine installation, 12. half through type valve curtains, 13. the control cord bar, 14. propeller, 15. manual exhaust valves, 16. lignilite, 17. inflate (heat) balloon bottom automatically.
The specific embodiment
Among Fig. 1, the sealed type at automatically inflatable balloon and hot air balloon parachute top (heat) balloon (1) connects automatic inflation (heat) balloon (2) at middle part, and automatic inflation (heat) balloon (2) at middle part connects the parachute (3) of bottom.
Among Fig. 2, automatic inflation (heat) balloon (2) at the sealed type at top (heat) balloon (1) and middle part is fed wherein by gas piping (6) respectively, and automanual blow off valve (10) is exhaust decompression when the balloon internal pressure is excessive.
Among Fig. 3, half through type valve (7) is positioned at the bottom (17) of automatic inflation (heat) balloon (2), when balloon decline or air-flow rising, the half through type valve curtain (12) that is fixed on automatic inflation (heat) the balloon bottom (17) by lignilite (16) upwardly opens air admission; When balloon rising or air-flow decline, half through type valve curtain (12) is closed air trapping downwards.
Among Fig. 4, on the external margin of the bottom (17) that half through type valve (7) is arranged of automatic inflation (heat) balloon (2) in the middle part of the top edge of full skirt (8) is sewn to around the parachute of bottom, the bottom of full skirt (8) connects suspension cable (9) around the parachute.
Among Fig. 5, the short transverse control wing (4) is connected on the suspension cable (9), by control cord bar (13), can regulate height and horizontal direction in the process of motion, and can play the safety guard-safeguard effect.
Among Fig. 6, hang Pilotage en Force cabin (5) and be connected suspension cable (9) lower end, heat power and horizontal motion engine installation (11) are installed in the gravity balance position, hot gas is imported sealed type (heat) balloon at top and automatic inflation (heat) balloon interior at middle part is done upward movement by gas piping (6), regulate balloon interior pressure by manual exhaust valve (15), promote to move horizontally by propeller (14).The short transverse control wing (4) also can be connected on the Pilotage en Force cabin (5), awing control height and direction.
Fig. 7 is an exemplary embodiments of the present invention.
Claims (7)
1. automatically inflatable balloon and hot air balloon parachute that automatically inflatable balloon, fire balloon and parachute are combined, it is characterized in that: form by sealed type (heat) balloon at top, automatic inflation (heat) balloon at middle part, the parachute of bottom, five parts such as Pilotage en Force cabin that short transverse is controlled the wing and suspension, the sealed type at top (heat) balloon adopts frivolous sealing insulation elastic material to make, fill with light gas and need not heat, or fill with normal air and adopt burner section, exhaust gases of internal combustion engines, electric energy, solar energy heating; Automatic inflation (heat) the balloon bottom at middle part is adopted half through type valve to impel gas to enter and is detained; The bottom is a parachute; The short transverse control wing is connected respectively on suspension cable or the Pilotage en Force cabin horizontally and vertically; The suspension cable bottom hangs the Pilotage en Force cabin.
2. automatically inflatable balloon and hot air balloon parachute according to claim 1 is characterized in that: by covered pipe hot gas is transported in the balloon from driving compartment when adopting the burner section heating.
3. automatically inflatable balloon and hot air balloon parachute according to claim 1, it is characterized in that: automatic inflation (heat) the balloon bottom at middle part is adopted half through type valve to impel gas to enter and is detained: when balloon decline or air-flow rising, the balloon external pressure is greater than air pressure inside, the valve that can upwardly open is opened, and air-flow enters in the balloon envelope; When balloon rises or air-flow when descending, balloon interior air pressure is greater than external pressure, the valve closure that can not open downwards, and gas is trapped in balloon interior.
4. automatically inflatable balloon and hot air balloon parachute according to claim 1 is characterized in that: install the automatic or manual blow off valve on the balloon additional, exhaust decompression when the balloon internal pressure is excessive.
5. automatically inflatable balloon and hot air balloon parachute according to claim 1 is characterized in that: the full skirt that parachute is actual around having only and do not have the umbrella top, the umbrella top is replaced by half through type valve of automatic inflation (heat) balloon bottom.
6. automatically inflatable balloon and hot air balloon parachute according to claim 1, it is characterized in that: the short transverse control wing is connected respectively on suspension cable or the Pilotage en Force cabin horizontally and vertically, can controlling level direction and vertical dimension during flight, and can rely on self lifting flight.
7. automatically inflatable balloon and hot air balloon parachute according to claim 1 is characterized in that: the Pilotage en Force cabin is suspended on the suspension cable lower end, and heat power and horizontal motion engine installation are installed.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2010102297438A CN101885379A (en) | 2010-07-05 | 2010-07-05 | Automatically inflatable balloon and hot air balloon parachute |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2010102297438A CN101885379A (en) | 2010-07-05 | 2010-07-05 | Automatically inflatable balloon and hot air balloon parachute |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN101885379A true CN101885379A (en) | 2010-11-17 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2010102297438A Pending CN101885379A (en) | 2010-07-05 | 2010-07-05 | Automatically inflatable balloon and hot air balloon parachute |
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| CN (1) | CN101885379A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102009741A (en) * | 2010-12-01 | 2011-04-13 | 航宇救生装备有限公司 | Steam heat aerostat heater |
| CN103043206A (en) * | 2013-01-07 | 2013-04-17 | 四川大学 | Internal combustion engine appliance for fire balloon |
| CN107352013A (en) * | 2017-07-13 | 2017-11-17 | 襄阳宏伟航空器有限责任公司 | It is a kind of to be used for hot gas ball rotation or traversing control structure |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2560562Y (en) * | 2002-04-05 | 2003-07-16 | 李开梅 | Thermodynamic lift-off parachute |
| CN2590868Y (en) * | 2002-12-12 | 2003-12-10 | 苏日东 | High-building life-saving parachute with air-filling protection bag |
| CN2592513Y (en) * | 2002-09-18 | 2003-12-17 | 钟云川 | Lift-off parachute |
-
2010
- 2010-07-05 CN CN2010102297438A patent/CN101885379A/en active Pending
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2560562Y (en) * | 2002-04-05 | 2003-07-16 | 李开梅 | Thermodynamic lift-off parachute |
| CN2592513Y (en) * | 2002-09-18 | 2003-12-17 | 钟云川 | Lift-off parachute |
| CN2590868Y (en) * | 2002-12-12 | 2003-12-10 | 苏日东 | High-building life-saving parachute with air-filling protection bag |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102009741A (en) * | 2010-12-01 | 2011-04-13 | 航宇救生装备有限公司 | Steam heat aerostat heater |
| CN103043206A (en) * | 2013-01-07 | 2013-04-17 | 四川大学 | Internal combustion engine appliance for fire balloon |
| CN107352013A (en) * | 2017-07-13 | 2017-11-17 | 襄阳宏伟航空器有限责任公司 | It is a kind of to be used for hot gas ball rotation or traversing control structure |
| CN107352013B (en) * | 2017-07-13 | 2023-05-02 | 襄阳宏伟航空器有限责任公司 | Control structure for rotation or transverse movement of hot air balloon |
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| C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
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Application publication date: 20101117 |