CN102431641A - Air energy hot air balloon - Google Patents
Air energy hot air balloon Download PDFInfo
- Publication number
- CN102431641A CN102431641A CN2010105792687A CN201010579268A CN102431641A CN 102431641 A CN102431641 A CN 102431641A CN 2010105792687 A CN2010105792687 A CN 2010105792687A CN 201010579268 A CN201010579268 A CN 201010579268A CN 102431641 A CN102431641 A CN 102431641A
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- balloon
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- air
- hot air
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Abstract
The invention discloses an air energy hot air balloon which is used for low-altitude manned flight. The air energy hot air balloon consists of a balloon body, a heat exchanger 1, a conduit, a compressor, an expansion valve, a heat exchanger 2, a storage battery, a control switch, a person carrying cabin and a tow rope, wherein the volume of the balloon body is determined according to rated carrying capacity of the hot air balloon; the entire balloon body is not provided with a large opening, but the bottom of the balloon body is provided with a plurality of small open holes for ventilation; the heat exchanger 1 is arranged in the balloon body and is connected to the compressor and the expansion valve, which are arranged in the person carrying cabin, through the conduit and is then connected with the heat exchanger 2 outside the cabin wall; in addition, the person carrying cabin is connected with the balloon body through the tow rope; the storage battery is arranged in the cabin, so that the compressor can be operated; when the hot air balloon ascends, a working medium (R134a and the like) is driven by the compressor to circularly and reciprocally evaporate in the heat exchanger 2 to absorb heat and then is liquefied in the heat exchanger 1 to release heat, so that the temperature of the air in the balloon body is continuously raised to slowly ascend the hot air balloon; when the hot air balloon descends, the compressor reversely works through the control switch, and then, the temperature of the air in the balloon body is continuously reduced, so that the hot air balloon slowly descends; during work, the compressor, the expansion valve, the heat exchanger 1 and the heat exchanger 2 form a reversible heat engine system; and according to a Carnot principle, the electro-thermal efficiency of the hot air balloon is about 300-500 percent. The air energy hot air balloon can effectively sail in air; and less energy consumption and no pollution are guaranteed.
Description
Affiliated technical field
The present invention relates to a kind of can the navigation and can fire balloon, especially power consumption lack in aerial air, free of contamination air can fire balloon.
Background technology
Fire balloon is that the balloon that a kind of utilization is full of hot gas drags the device that rises on the manned storehouse, and its principle is: hot air density is less than balloon external cooling density of air in the balloon, and the suffered atmospheric buoyancy force of balloon is greater than the gross weight in balloon and manned storehouse; Thereby whole device rises, and common fire balloon generally adopts the mode of fuel oil or combustion gas to heat; This type of heating directly converts chemical power into heat energy; It is bigger to consume energy, and can produce a large amount of greenhouse gases, and air is had pollution.
Summary of the invention
Adopt the mode of fuel oil or combustion gas to heat in order to overcome present fire balloon; The big and relatively large deficiency of aerial contamination of power consumption, the present invention provides a kind of air ability fire balloon, and this air can not only can navigate by water in the air by fire balloon effectively; And power consumption is few, pollution-free.
The technical solution adopted for the present invention to solve the technical problems is: this air can fire balloon by spheroid, H Exch one, conduit, compressor and expansion valve; H Exch two, storage battery, master cock, manned capsule; Towline is formed, and wherein the spheroid volume is decided according to the fire balloon nominal payload, and whole spheroid does not have big opening, only in its bottom some small-sized perforates is arranged; Be used for ventilation, there is H Exch one spheroid inside, is connected to compressor and the expansion valve that is installed in the manned capsule through conduit, connects the H Exch two in the bulkhead outside again; In addition, manned capsule links to each other through towline with spheroid, and storage battery is arranged in the cabin, can supply compressor operation; When fire balloon rose, compressor ordered about working medium (R134a etc.) evaporation heat absorption in H Exch two circularly, liquefaction heat release in H Exch one again, and air themperature constantly raises in the spheroid thereby make; Fire balloon is slowly risen, when fire balloon descends, make the compressor reverse operation through master cock, then; Air themperature constantly reduces in the spheroid, thereby fire balloon is slowly descended, in the work; Compressor, expansion valve, H Exch one, H Exch two are formed a reversible heat engine system, and according to Carnot's principle, its electrothermal efficiency is about 300%-500%.
The invention has the beneficial effects as follows: not only can navigate by water effectively, and power consumption is few, pollution-free in the air.
Description of drawings
Below in conjunction with accompanying drawing and embodiment the present invention is further specified.
Accompanying drawing is the structural representation of this air ability fire balloon.
In the accompanying drawing: 1, spheroid; 2, H Exch one; 3, conduit; 4, compressor and expansion valve; 5, H Exch two; 6, storage battery; 7, master cock; 8, manned capsule; 9, towline.
The specific embodiment
In specific embodiment shown in the accompanying drawing, this air can fire balloon by spheroid (1), H Exch one (2), conduit (3); Compressor and expansion valve (4), H Exch two (5), storage battery (6), master cock (7); Manned capsule (8), towline (9) is formed, and wherein spheroid (1) volume is decided according to the fire balloon nominal payload, and whole spheroid (1) does not have big opening; Only in its bottom some small-sized perforates are arranged, be used for ventilation, there is H Exch one (2) spheroid (1) inside, is connected to compressor and the expansion valve (4) that is installed in the manned capsule (8) through conduit (3); Connect the H Exch two (5) in the bulkhead outside again, in addition, manned capsule (8) links to each other through towline (9) with spheroid (1), and storage battery (6) is arranged in the cabin; Can supply compressor and expansion valve (4) running, when fire balloon rose, compressor ordered about working medium (R134a etc.) evaporation heat absorption in H Exch two (5) circularly, liquefaction heat release in H Exch one (2) again; Thereby the interior air themperature of spheroid (1) is constantly raise, fire balloon is slowly risen, when fire balloon descends, make the compressor reverse operation through master cock (7); Then the interior air themperature of spheroid (1) constantly reduces, thereby fire balloon is slowly descended, in the work; Compressor and expansion valve (4), H Exch one (2), H Exch two (5) are formed a reversible heat engine system, and according to Carnot's principle, its electrothermal efficiency is about 300%-500%.
Claims (1)
1. an air can fire balloon, is made up of spheroid, manned capsule, towline, heating arrangement etc., it is characterized in that: this air can fire balloon by spheroid, H Exch one; Conduit, compressor and expansion valve, H Exch two, storage battery; Master cock, manned capsule, towline is formed, and wherein the spheroid volume is decided according to the fire balloon nominal payload; Whole spheroid does not have big opening, only in its bottom some small-sized perforates is arranged, and is used for ventilation, and there is H Exch one spheroid inside; Be connected to compressor and the expansion valve that is installed in the manned capsule through conduit, connect the H Exch two in the bulkhead outside again, in addition, manned capsule links to each other through towline with spheroid; Storage battery is arranged in the cabin, can supply compressor operation, when fire balloon rose, compressor ordered about working medium (R134a etc.) evaporation heat absorption in H Exch two circularly; Liquefaction heat release in H Exch one again, air themperature constantly raises in the spheroid thereby make, and fire balloon is slowly risen, when fire balloon descends; Make the compressor reverse operation through master cock, then, air themperature constantly reduces in the spheroid, thereby fire balloon is slowly descended; In the work, compressor, expansion valve, H Exch one, H Exch two are formed a reversible heat engine system, and according to Carnot's principle, its electrothermal efficiency is about 300%-500%.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2010105792687A CN102431641A (en) | 2010-12-08 | 2010-12-08 | Air energy hot air balloon |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2010105792687A CN102431641A (en) | 2010-12-08 | 2010-12-08 | Air energy hot air balloon |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN102431641A true CN102431641A (en) | 2012-05-02 |
Family
ID=45980076
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2010105792687A Pending CN102431641A (en) | 2010-12-08 | 2010-12-08 | Air energy hot air balloon |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN102431641A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102991664A (en) * | 2012-12-03 | 2013-03-27 | 航宇救生装备有限公司 | Automatic control method for tethered hot air airship |
| CN115783226A (en) * | 2022-11-25 | 2023-03-14 | 中国特种飞行器研究所 | Multi-energy complementary hot air balloon |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20050269442A1 (en) * | 2004-06-05 | 2005-12-08 | Phu Nguyen | Device and method for sealing and lighting a balloon |
| CN2915675Y (en) * | 2006-05-22 | 2007-06-27 | 江宁 | Solar energy hot air balloon |
| CN201254288Y (en) * | 2008-06-20 | 2009-06-10 | 金玉 | Electric energy hot air balloon |
-
2010
- 2010-12-08 CN CN2010105792687A patent/CN102431641A/en active Pending
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20050269442A1 (en) * | 2004-06-05 | 2005-12-08 | Phu Nguyen | Device and method for sealing and lighting a balloon |
| CN2915675Y (en) * | 2006-05-22 | 2007-06-27 | 江宁 | Solar energy hot air balloon |
| CN201254288Y (en) * | 2008-06-20 | 2009-06-10 | 金玉 | Electric energy hot air balloon |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102991664A (en) * | 2012-12-03 | 2013-03-27 | 航宇救生装备有限公司 | Automatic control method for tethered hot air airship |
| CN102991664B (en) * | 2012-12-03 | 2015-05-13 | 航宇救生装备有限公司 | Automatic control method for tethered hot air airship |
| CN115783226A (en) * | 2022-11-25 | 2023-03-14 | 中国特种飞行器研究所 | Multi-energy complementary hot air balloon |
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| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| DD01 | Delivery of document by public notice |
Addressee: Ge Bo Document name: Notification that Application Deemed to be Withdrawn |
|
| C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20120502 |