CN102464105A - Solar energy three-arc uninhabited combat air vehicle - Google Patents
Solar energy three-arc uninhabited combat air vehicle Download PDFInfo
- Publication number
- CN102464105A CN102464105A CN2010105339254A CN201010533925A CN102464105A CN 102464105 A CN102464105 A CN 102464105A CN 2010105339254 A CN2010105339254 A CN 2010105339254A CN 201010533925 A CN201010533925 A CN 201010533925A CN 102464105 A CN102464105 A CN 102464105A
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- hydrogen
- skeleton
- arc
- bags
- air vehicle
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T90/00—Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02T90/40—Application of hydrogen technology to transportation, e.g. using fuel cells
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Abstract
The invention relates to a solar energy three-arc uninhabited combat air vehicle, comprising a skeleton made of plastic and three segments of arcs and also five hydrogen bags. The five hydrogen bags are respectively arranged on lower ends of a left side and a right side of the skeleton, on a lower end of the middle of the skeleton and on lower ends of joints of the three arcs; a screw propeller is arranged in front of each hydrogen bag, and a minisize missile is arranged under each hydrogen bag; air rudders are arranged on the three middle hydrogen bags; a computer chip GPS satellite receiver is arranged on the upper middle part of the skeleton. The invention has beneficial effect that the uninhabited combat air vehicle can fight and be on duty in upper air for months both day and night and begin fight once receiving an order, so as to play an important role in protecting our airspace and marginal sea.
Description
Technical field
The present invention relates to a kind of UCAV, relate in particular to the physical structure of this machine.
Background technology
Along with military development of science and technology, UCAV will play a part increasing in future war.UCAV of the prior art is different, how to design that a kind of to adopt the UCAV of hydrogen bag be the problem that technical personnel will solve.
Summary of the invention
The technical issues that need to address of the present invention have provided a kind of solar power three arc UCAVs, are intended to solve the above problems.
In order to solve the problems of the technologies described above, the present invention realizes through following technical scheme:
The present invention includes: by gently mould process, three sections skeletons that arc is formed; Also comprise: 5 hydrogen bags; Described 5 hydrogen bags are placed in the lower end of the left and right sides of skeleton, the middle lower end of skeleton and the lower end, junction of three sections arcs respectively; Settle a propeller in the place ahead of said hydrogen bag, below the hydrogen bag, micro missile is installed; An air rudder is settled at rear at middle 3 hydrogen bags; Also settle a computer chip gps satellite receptor at the middle upper part of said skeleton.
Compared with prior art, the invention has the beneficial effects as follows: can be day and night in the high-altitude, continuous some months is alert aloft, goes into battle once receiving instruction, for playing very big effect in the territorial waters, territorial sky of protection China.
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:
Visible by Fig. 1: as to the present invention includes: by gently mould process, three sections skeletons 1 that arc is formed; Also comprise: 5 hydrogen bags 2; Described 5 hydrogen bags 2 are placed in the lower end of the left and right sides of skeleton 1, the middle lower end of skeleton 1 and the lower end, junction of three sections arcs respectively; Settle a propeller 3 in the place ahead of said hydrogen bag 2, micro missile 5 is installed below hydrogen bag 2; An air rudder 4 is settled at rear at middle 3 hydrogen bags 2; Also settle a computer chip gps satellite receptor 6 at the middle upper part of said skeleton 1;
On skeleton 1, go back sticker and solar power reception film 7.
The present invention adopts gently to mould and processes skeleton, becomes three arcs, 6 meters of each radian circumferences, and totally 18 meters long of three radians, width is 1 meter, arc forms 8 ° of arc chord angles.Radian makes the wind in high-altitude little to the influence of UCAV for a short time, and arc plays lifting to UCAV.Light moulding material not only gently but also be rich in toughness and can bear the gravity of whole unmanned plane fully.Gently moulding three radian circumferences of skeleton and be 18 meters wide is that sticker solar power and received film on 1 meter the skeleton; The electric power that solar power reception film receives is the power of conduct flight propeller air rudder directly; Most remaining electric power is stored in the electric storage means on the machine, is computer chip gps satellite receptor on the machine and the usefulness of being hung the MISSILE LAUNCHING igniting.
The present invention's fixed in position on UCAV has 5 hydrogen bags, is equipped with propeller engine under the hydrogen bag, and engine lower has micro missile.5 double helix slurry driving engine can be opened simultaneously, makes the speed of a ship or plane very fast.A driving engine makes the speed of a ship or plane very slow in the middle of also can opening separately.Owing to be equipped with the hydrogen bagging apparatus, the unmanned plane of not starting shooting also can be trapped in the high-altitude, carries out alert.
The present invention has air rudder after the propeller under three hydrogen bags on the middle radian, air rudder is accepted computer instruction and made unmanned plane up lifting or Fu Chong down, toward turning left or toward turning right.Unmanned plane toward turn left or toward another method of right-hand rotation be about the acceleration or the deceleration of two limit propeller engines.Quicken left side driving engine, make the unmanned plane right-hand turning to; Deceleration left side propeller engine, make the unmanned plane left-handed turning to; Otherwise with the quadrat method operation, the right propeller engine plays the effect of turning left to turn right too.
Be equipped with gps satellite receptor and ground signal receptor on the supercentral hydrogen bag of medial arc of the present invention; And be equipped with the program control facility of computer chip; UCAV is received instruction and is started for the front; Guided missile igniting emission is to aircraft, the guided missile that the enemy attacks, the surprise attack that ground and naval target are with lightning speed.
In sum, that UCAV of the present invention has is in light weight, power consumption less, manoevreability is big and attack is strong, will greatly strengthen the aerial anti-aggression ability of China.
Claims (2)
1. solar power three arc UCAVs is characterized in that comprising: by gently mould process, three sections skeletons that arc is formed; Also comprise: 5 hydrogen bags; Described 5 hydrogen bags are placed in the lower end of the left and right sides of skeleton, the middle lower end of skeleton and the lower end, junction of three sections arcs respectively; Settle a propeller in the place ahead of said hydrogen bag, below the hydrogen bag, micro missile is installed; An air rudder is settled at rear at middle 3 hydrogen bags; Also settle a computer chip gps satellite receptor at the middle upper part of said skeleton.
2. solar power three arc UCAVs according to claim 1 is characterized in that: on described skeleton, go back sticker and solar power reception film.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2010105339254A CN102464105A (en) | 2010-11-05 | 2010-11-05 | Solar energy three-arc uninhabited combat air vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2010105339254A CN102464105A (en) | 2010-11-05 | 2010-11-05 | Solar energy three-arc uninhabited combat air vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN102464105A true CN102464105A (en) | 2012-05-23 |
Family
ID=46068285
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2010105339254A Pending CN102464105A (en) | 2010-11-05 | 2010-11-05 | Solar energy three-arc uninhabited combat air vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN102464105A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105416565A (en) * | 2014-05-20 | 2016-03-23 | 波音公司 | Solar powered aircraft |
-
2010
- 2010-11-05 CN CN2010105339254A patent/CN102464105A/en active Pending
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105416565A (en) * | 2014-05-20 | 2016-03-23 | 波音公司 | Solar powered aircraft |
| US10807728B2 (en) | 2014-05-20 | 2020-10-20 | The Boeing Company | Solar powered airplane |
| CN105416565B (en) * | 2014-05-20 | 2021-06-18 | 波音公司 | Solar airplane |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | 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: 20120523 |