CN201793013U - Automatic inflatable balloon and hot balloon parachute - Google Patents
Automatic inflatable balloon and hot balloon parachute Download PDFInfo
- Publication number
- CN201793013U CN201793013U CN2010202609581U CN201020260958U CN201793013U CN 201793013 U CN201793013 U CN 201793013U CN 2010202609581 U CN2010202609581 U CN 2010202609581U CN 201020260958 U CN201020260958 U CN 201020260958U CN 201793013 U CN201793013 U CN 201793013U
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- balloon
- parachute
- hot
- hot air
- automatically inflatable
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Abstract
The utility model provides an automatic inflatable balloon and hot balloon parachute, which combines an automatic inflatable balloon, a hot balloon and a parachute, comprising five parts such as a seal type (hot) balloon at the top, an automatic inflatable (hot) balloon at the middle, the parachute at the bottom, height and direction control wings and a suspended control cabin and the like, wherein the seal type (hot) balloon at the top is made of light and thin sealing insulating elastic material, is inflated with light gas without heating, or is inflated with common air and adopts a burner, an internal combustion engine tail gas, electric energy and solar energy for heating; the bottom of the automatic inflatable (hot) balloon at the middle adopts a semi-passing type valve to enhance entering and retention of gas; the bottom is a parachute; the height and direction control wings are respectively connected on a suspended rope or the control cabin horizontally and vertically; and the lower part of the suspended rope is suspended with a power control cabin. The automatic inflatable balloon and hot balloon parachute eliminates the defects of the common balloon, the hot balloon and the parachute, prevents the falling accidents as the hot balloon is burnt and the parachute can not be opened.
Description
Affiliated technical field
The utility model 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.
The utility model content
In order to give full play to balloon, fire balloon and parachute three's advantage, remedy critical defect separately, it is a kind of with automatically inflatable balloon that the utility model provides, 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 scheme that its technical matters that solves the utility model adopts is: the utility model 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 beneficial effects of the utility model are that automatically inflatable balloon and hot air balloon parachute can be inflated as common balloon, can heat as fire balloon, can select differing heights and direction flight as aircraft as the slow landing of parachute.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
Below in conjunction with drawings and Examples the utility model is further specified.
Fig. 1 is the layering scheme drawing of the utility model automatically inflatable balloon and hot air balloon parachute.
Fig. 2 is the utility model balloon gas piping scheme drawing.
Fig. 3 is automatic inflation (heat) the balloon bottom half through type valve scheme drawing at the utility model middle part.
Fig. 4 is a full skirt scheme drawing around the parachute of the utility model bottom.
Fig. 5 is a short transverse control wing scheme drawing of the present utility model.
Fig. 6 is a suspension Pilotage en Force of the present utility model cabin scheme drawing.
Fig. 7 is an exemplary embodiments of the present utility model.
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 utility model.
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: be made up of the sealed type balloon at top, the automatic inflation fire 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 balloon at top adopts frivolous sealing insulation elastic material to make; Half through type valve is adopted in the automatic inflation fire balloon bottom at middle part; 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: have hot gas is transported to covered pipe in the balloon from driving compartment.
3. automatically inflatable balloon and hot air balloon parachute according to claim 1 is characterized in that: the half through type valve that impels gas to enter and be detained is adopted in the automatic inflation fire balloon bottom at middle part.
4. automatically inflatable balloon and hot air balloon parachute according to claim 1 is characterized in that: the automatic or manual blow off valve that installs exhaust decompression when the balloon internal pressure is excessive on the balloon additional.
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 fire 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 |
|---|---|---|---|
| CN2010202609581U CN201793013U (en) | 2010-07-05 | 2010-07-05 | Automatic inflatable balloon and hot balloon parachute |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2010202609581U CN201793013U (en) | 2010-07-05 | 2010-07-05 | Automatic inflatable balloon and hot balloon parachute |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201793013U true CN201793013U (en) | 2011-04-13 |
Family
ID=43847934
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2010202609581U Expired - Fee Related CN201793013U (en) | 2010-07-05 | 2010-07-05 | Automatic inflatable balloon and hot balloon parachute |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN201793013U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103112579A (en) * | 2012-12-12 | 2013-05-22 | 樊荣 | Balloon driving force manual control flying machine |
| CN103171767A (en) * | 2011-12-25 | 2013-06-26 | 山东科技职业学院 | Airplane protective ejection air bag |
| WO2013120357A1 (en) * | 2012-02-17 | 2013-08-22 | Sun Lei | Airplane anti-falling and self-rescuing device |
| CN111498079A (en) * | 2020-05-01 | 2020-08-07 | 梅向瑾 | Multi-shell safety landing structure and method capable of steering local climbing for air force meteorological observation |
-
2010
- 2010-07-05 CN CN2010202609581U patent/CN201793013U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103171767A (en) * | 2011-12-25 | 2013-06-26 | 山东科技职业学院 | Airplane protective ejection air bag |
| WO2013120357A1 (en) * | 2012-02-17 | 2013-08-22 | Sun Lei | Airplane anti-falling and self-rescuing device |
| CN103112579A (en) * | 2012-12-12 | 2013-05-22 | 樊荣 | Balloon driving force manual control flying machine |
| CN111498079A (en) * | 2020-05-01 | 2020-08-07 | 梅向瑾 | Multi-shell safety landing structure and method capable of steering local climbing for air force meteorological observation |
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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: 20110413 Termination date: 20110705 |