CN1872620A - Aircraft of seawater air film - Google Patents
Aircraft of seawater air film Download PDFInfo
- Publication number
- CN1872620A CN1872620A CNA2005100436331A CN200510043633A CN1872620A CN 1872620 A CN1872620 A CN 1872620A CN A2005100436331 A CNA2005100436331 A CN A2005100436331A CN 200510043633 A CN200510043633 A CN 200510043633A CN 1872620 A CN1872620 A CN 1872620A
- Authority
- CN
- China
- Prior art keywords
- aircraft
- air film
- seawater
- seawater air
- electrode
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
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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
- Y02T70/00—Maritime or waterways transport
- Y02T70/10—Measures concerning design or construction of watercraft hulls
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- Electrolytic Production Of Non-Metals, Compounds, Apparatuses Therefor (AREA)
Abstract
An air film type marine vehicle including ship, submarine, torpedo, etc features that the positive and negative electrodes of a DC power supply are arranged in the front of the underwater part of its fore-body for electrolyzing seawater to generate an air film layer, which can decrease the navigation resistance effectively.
Description
Technical field:
The present invention relates to a kind of seawater aircraft, specifically a kind of seawater electrolysis is become air film, utilize the air film resistance to be significantly less than the principle of seawater resistance, when improving the aircraft route speed, reduced the aircraft of seawater air film of energy resource consumption.
Background technology:
At present, the seawater aircraft can't increase substantially because of its seawater resistance makes the route speed of aircraft, though the air cushion vehicle of prior art, hydroskis formula speedboat can improve ship's speed, but is cost to consume a large amount of energy, so can not popularize on a large scale.Aircraft wants double ring ahead in traveling process, certainly will will accelerate the rotating speed of screw propeller, facts have proved that the rotating speed of screw propeller wants to improve a times of former speed, its energy-output ratio is about 7 times of former consumption, the consumption of this energy is surprising.At present, also there is not a kind of technology can solve contradiction between aircraft speed and the energy resource consumption effectively.
Summary of the invention:
Technical assignment of the present invention is at the deficiencies in the prior art, and a kind of electrolysis tech that utilizes is provided, and forms the aircraft of seawater air film of one deck air film at the leading section of aircraft.This aircraft is significantly smaller than the principle of seawater resistance according to air resistance, has reduced the running resistance of aircraft effectively, has reduced consumption of power greatly.
The technical solution adopted for the present invention to solve the technical problems is:
This aircraft of seawater air film comprises the aircraft shell, is characterized in that aircraft front end underwater sites is provided with the positive and negative electrode that joins with direct supply.
Above-mentioned aircraft of seawater air film to being equipped with the aircraft of direct supply, only needs to regulate output voltage by pressure regulator, satisfies the seawater electrolysis requirement and gets final product.
Above-mentioned aircraft of seawater air film, to being equipped with source of AC, as the aircraft of alternating current generator, its galvanic obtaining can obtain from source of AC by rectifier.
Above-mentioned aircraft of seawater air film is meant the various devices that move under water such as Submarine, torpedo of sea going various boats and ships and submarine navigation.
Aircraft of seawater air film of the present invention compared with prior art, the beneficial effect that is produced is:
Reasonable in design, simple in structure, be easy to processing, energy conservation and consumption reduction effects is remarkable.
Description of drawings:
Accompanying drawing 1 is a theory structure scheme drawing of the present invention;
Accompanying drawing 2 is the left TV structure scheme drawing of Fig. 1.
Among the figure, 1-aircraft shell, 2-direct supply, 3-electrode, 4-pressure regulator, 5-rectifier, 6-source of AC.
The specific embodiment:
Below in conjunction with explaining below 1,2 pairs of aircraft of seawater air film works of the present invention of accompanying drawing.
Embodiment 1: shown in accompanying drawing 1,2, and aircraft of seawater air film of the present invention, its structure comprises the various aircraft shells 1 of prior art, above-mentioned various aircraft are meant the various devices that move under water such as Submarine, torpedo of sea going various boats and ships and submarine navigation.The front end underwater sites of aircraft shell 1 is provided with the positive and negative electrode 3 that joins with direct supply 2, and direct supply 2 is regulated output voltage by pressure regulator 4.According to the structure of hull, electrode 3 can be fixedly installed, also electrode 3 can be done the moving telescopic setting, bump when reaching port for the electrode 3 that prevents aircraft, cause electrode 3 to damage, when reaching port electrode 3 is contracted in the hull, during the departure from port navigation electrode 3 is stretched out outside the hull.Electrode 3 according to the structure needs of aircraft can be provided with a pair of more than.
Embodiment 2: shown in accompanying drawing 1,2, and aircraft of seawater air film of the present invention, its structure comprises the various aircraft shells 1 of prior art, above-mentioned various aircraft are meant the various devices that move under water such as Submarine, torpedo of sea going various boats and ships and submarine navigation.The front end underwater sites of aircraft shell 1 is provided with the positive and negative electrode 3 that joins with pressure regulator 4, and pressure regulator 4 joins by rectifier 5 and source of AC 6, thereby substitutes direct supply 2 with rectifier 5 and source of AC 6.According to the structure of hull, electrode 3 can be fixedly installed, also electrode 3 can be done the moving telescopic setting, bump when reaching port for the electrode 3 that prevents aircraft, cause electrode 3 to damage, when reaching port electrode 3 is contracted in the hull, during the departure from port navigation electrode 3 is stretched out outside the hull.Electrode 3 according to the structure needs of aircraft can be provided with a pair of more than.For the various devices that move under water of submarine navigations such as Submarine and torpedo, its electrode setting can be with reference to the structure setting of aircraft shell 1 the latter half.
Its processing and fabricating of aircraft of seawater air film of the present invention is simple and convenient, and processing and fabricating gets final product shown in the by specification accompanying drawing.Electrolysis tech is a mature technology, and its decomposition voltage size is determined according to the navigation needs of industry experience and aircraft.
Claims (4)
1, aircraft of seawater air film comprises the aircraft shell, it is characterized in that, the front end underwater sites of aircraft shell is provided with the positive and negative electrode that joins with direct supply.
2, aircraft of seawater air film according to claim 1 is characterized in that, also is provided with the pressure regulator of regulating output voltage between direct supply and the positive and negative electrode.
3, aircraft of seawater air film according to claim 1 and 2 is characterized in that, direct supply obtains from source of AC by rectifier.
4, aircraft of seawater air film according to claim 1 is characterized in that, aircraft is meant the various devices that move under water of sea going various boats and ships and submarine navigation.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CNA2005100436331A CN1872620A (en) | 2005-05-30 | 2005-05-30 | Aircraft of seawater air film |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CNA2005100436331A CN1872620A (en) | 2005-05-30 | 2005-05-30 | Aircraft of seawater air film |
Publications (1)
Publication Number | Publication Date |
---|---|
CN1872620A true CN1872620A (en) | 2006-12-06 |
Family
ID=37483264
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CNA2005100436331A Pending CN1872620A (en) | 2005-05-30 | 2005-05-30 | Aircraft of seawater air film |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN1872620A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9200522B2 (en) | 2007-12-14 | 2015-12-01 | University Of Florida Research Foundation, Inc. | Active film cooling for turbine blades |
-
2005
- 2005-05-30 CN CNA2005100436331A patent/CN1872620A/en active Pending
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9200522B2 (en) | 2007-12-14 | 2015-12-01 | University Of Florida Research Foundation, Inc. | Active film cooling for turbine blades |
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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 |