CN1872620A - Aircraft of seawater air film - Google Patents

Aircraft of seawater air film Download PDF

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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
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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
Application number
CNA2005100436331A
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Chinese (zh)
Inventor
王宝民
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to CNA2005100436331A priority Critical patent/CN1872620A/en
Publication of CN1872620A publication Critical patent/CN1872620A/en
Pending legal-status Critical Current

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    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T70/00Maritime or waterways transport
    • Y02T70/10Measures 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

Aircraft of seawater air film
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.
CNA2005100436331A 2005-05-30 2005-05-30 Aircraft of seawater air film Pending CN1872620A (en)

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)

* Cited by examiner, † Cited by third party
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

Cited By (1)

* Cited by examiner, † Cited by third party
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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C06 Publication
PB01 Publication
C02 Deemed withdrawal of patent application after publication (patent law 2001)
WD01 Invention patent application deemed withdrawn after publication