CN102040001A - Solar hydrogen lithium battery unmanned reconnaissance aircraft - Google Patents
Solar hydrogen lithium battery unmanned reconnaissance aircraft Download PDFInfo
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- CN102040001A CN102040001A CN2009101972758A CN200910197275A CN102040001A CN 102040001 A CN102040001 A CN 102040001A CN 2009101972758 A CN2009101972758 A CN 2009101972758A CN 200910197275 A CN200910197275 A CN 200910197275A CN 102040001 A CN102040001 A CN 102040001A
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- hydrogen
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- bag
- garden shape
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Abstract
The invention relates to a solar hydrogen lithium battery unmanned reconnaissance aircraft. The unmanned reconnaissance aircraft comprises an elliptic semicircular hydrogen bag, wherein the surface of the elliptic semicircular hydrogen bag is attached with a solar energy receiving film; a flight direction aerial rudder and a flight thruster are arranged on the rear part of the elliptic semicircular hydrogen bag; and a reconnaissance aircraft, a satellite navigation receiver, a computer program control system, and a system which combines a lithium battery with a solar electricity and is used as a power source are arranged on the lower part of the elliptic semicircular hydrogen bag. The solar hydrogen lithium battery unmanned reconnaissance aircraft has the advantages of better completing reconnaissance missions.
Description
Technical field
The present invention relates to a kind of scounting aeroplane, relate in particular to the structure of this scounting aeroplane.
Background technology
Scounting aeroplane has very big effect in modern war, bear reconnaissance mission better in order to make scounting aeroplane, designs a kind of performance and is more preferably that technical personnel will consider.
Summary of the invention
The technical issues that need to address of the present invention have provided a kind of solar hydrogen and have risen lithium electricity scounting aeroplane, are intended to solve the above problems.
In order to solve the problems of the technologies described above, the present invention is achieved by the following technical solutions:
The present invention includes: a hydrogen bag of falling half garden shape; Post solar power on the surface of the hydrogen bag of the half garden shape of falling and receive film; Settle heading air rudder and a flight propelling unit at the rear portion of the hydrogen bag of the half garden shape of falling; Falling, instrument settle to be scouted in the bottom of hydrogen bag of half garden shape, the satellite navigation receptor combines as the system of the energy with solar-electricity with computer program control system and lithium cell.
Compared with prior art, the invention has the beneficial effects as follows: can better bear reconnaissance mission.
Description of drawings
Fig. 1 is a structural representation of the present invention.
The specific embodiment
Below in conjunction with the accompanying drawing and the specific embodiment the present invention is described in further detail:
As seen from Figure 1: the present invention includes: a hydrogen bag 1 of falling half garden shape; Post solar power on the surface of the hydrogen bag 1 of the half garden shape of falling and receive film 2; Settle heading air rudder 3 and a flight propelling unit 4 at the rear portion of the hydrogen bag 1 of the half garden shape of falling; Falling, instrument 5 settle to be scouted in the bottom of hydrogen bag 1 of half garden shape, the satellite navigation receptor combines with solar-electricity as the system 7 of the energy with computer program control system 6 and lithium cell;
The hydrogen bag 1 afterbody place of the described half garden shape of falling is higher than chain-drive section 8.
The present invention adopts the hydrogen bag of the half garden shape of falling to make fuselage, and the garden streamline arc of falling is slightly high at the afterbody place, is the streamline arcuation to chain-drive section, slides.Hydrogen bag fuselage makes the weight of scout lighter, and hydrogen has the lift effect in atmospheric envelope, has reduced the energy expenditure that scout climbs.Be the streamline arc from tail to head and glide, make scounting aeroplane reduce the resistance of air, favourable flight awing.
The outside of streamline arc half garden shape scout hydrogen bag is posted solar power and is received film, and the electric energy that receives can also can be stored in the poultry electrical equipment under the fuselage directly as the machine electric energy on the one hand, as the preparation electric energy, strengthens the flying power of scounting aeroplane.The hydrogen bag sticks solar power outward and receives film in addition, and hydrogen bag fuselage is shielded.
Be equipped with satellite navigation receptor and computer program control system, electric energy driving engine flight system under the half garden shape fuselage of scounting aeroplane.Adopt lithium cell to combine with solar-electricity as the energy of scounting aeroplane, the afterbody of scounting aeroplane is equipped with heading air rudder and flight propelling unit, adopts above method design-calculated solar hydrogen to rise the electric scounting aeroplane of lithium and stealthy ability is arranged.
Claims (2)
1. a solar hydrogen is risen lithium electricity scounting aeroplane, it is characterized in that comprising: a hydrogen bag of falling half garden shape; Post solar power on the surface of the hydrogen bag of the half garden shape of falling and receive film; Settle heading air rudder and a flight propelling unit at the rear portion of the hydrogen bag of the half garden shape of falling; Falling, instrument settle to be scouted in the bottom of hydrogen bag of half garden shape, the satellite navigation receptor combines as the system of the energy with solar-electricity with computer program control system and lithium cell.
2. solar hydrogen according to claim 1 is risen lithium electricity scounting aeroplane, and it is characterized in that: the hydrogen bag afterbody place of the described half garden shape of falling is higher than chain-drive section.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2009101972758A CN102040001A (en) | 2009-10-16 | 2009-10-16 | Solar hydrogen lithium battery unmanned reconnaissance aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2009101972758A CN102040001A (en) | 2009-10-16 | 2009-10-16 | Solar hydrogen lithium battery unmanned reconnaissance aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN102040001A true CN102040001A (en) | 2011-05-04 |
Family
ID=43906620
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2009101972758A Pending CN102040001A (en) | 2009-10-16 | 2009-10-16 | Solar hydrogen lithium battery unmanned reconnaissance aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN102040001A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103241380A (en) * | 2012-02-03 | 2013-08-14 | 伊德斯德国股份有限公司 | Surveillance and/or weapons system and method for objects on land or sea |
-
2009
- 2009-10-16 CN CN2009101972758A patent/CN102040001A/en active Pending
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103241380A (en) * | 2012-02-03 | 2013-08-14 | 伊德斯德国股份有限公司 | Surveillance and/or weapons system and method for objects on land or sea |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20110504 |