CN103192988A - Airship - Google Patents

Airship Download PDF

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Publication number
CN103192988A
CN103192988A CN2013101622252A CN201310162225A CN103192988A CN 103192988 A CN103192988 A CN 103192988A CN 2013101622252 A CN2013101622252 A CN 2013101622252A CN 201310162225 A CN201310162225 A CN 201310162225A CN 103192988 A CN103192988 A CN 103192988A
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CN
China
Prior art keywords
power
impeller
airship
positive
negative
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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
CN2013101622252A
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Chinese (zh)
Inventor
陈俞任
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陈俞任
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Application filed by 陈俞任 filed Critical 陈俞任
Priority to CN2013101622252A priority Critical patent/CN103192988A/en
Publication of CN103192988A publication Critical patent/CN103192988A/en
Pending legal-status Critical Current

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Abstract

The invention discloses an airship capable of driving on the sea, on the land, in air and in the sky. A semi-olivary outer shell also serves as a ship body; the body of the airship also serves as an aerofoil, and the flying capability is strong with the unfolding wings; the airship can fly on the sea, run on the land, fly in air, and travel in the sky by being matched with an appropriate power device, can run on the sea by being matched with a jet engine or a screw propeller or a power device or other power devices, and because lift force of the unfolding wings is enhanced for the airship wings, the driving resistance is reduced, and the speed is rapid; the airship can fly in air after being matched with the jet engine or a nuclear power device, the load quantity is great, and the airship is invisible; and the airship can run on the land after being equipped with wheels, and can travel in the sky after being matched with the jet engine and a solid rocket or a power cannon, or a nuclear power device, or the nuclear device and the solid rocket or the power cannon, and comes and goes between the earth and the moon, is low in cost, and can achieve interstellar flight.

Description

Airship
Technical field
The present invention relates to a kind of can be in sea, land and sky, the airship that travels of sky.Half olivary shell be the fuselage of hull, aircraft be again wing, add spademan, flight performance is stronger.Mix suitable engine installation, just can marinely go, land race flies in the air, day upstream! Marine row, it is faster than existing ship; Fly in the air, it is bigger than existing aircraft carrying capacity, and is stealthy, and military significance is great; It upstream, it can come and go between the earth and the moon, and cost can also be realized space flight far below liquid-fuel rocket.
Background technology
Can be in sea, land and sky, the airship that travels of sky, also do not have now, the present invention is initiative.
Summary of the invention
For can be in sea, land and sky, day travel, adopted half olivary shell, the fuselage that is hull, aircraft is again wing, adds spademan, flight performance is stronger.Mix suitable engine installation, just can marinely go, land race flies in the air, day upstream.
The technical solution adopted for the present invention to solve the technical problems is: ship is designed to half olive shape, adds spademan, mix suitable engine installation.
The invention has the beneficial effects as follows marine row, it is faster than existing ship; Fly in the air, it is bigger than existing aircraft carrying capacity, and is stealthy, and military significance is great; It upstream, it can come and go between the earth and the moon, and cost is far below liquid-fuel rocket.
Description of drawings
For the embodiment of the invention or technical scheme of the prior art are described better, to do to introduce simply to needed accompanying drawing in embodiment or the description of the Prior Art below, apparently, accompanying drawing in describing below only is one embodiment of the present of invention, for those of ordinary skills, under the prerequisite of not paying creative work, can also obtain other accompanying drawings according to these accompanying drawings.
Fig. 1 is airship and part engine installation scheme drawing, and Fig. 2 is part engine installation scheme drawing.
The parts that mark among the figure are: 1: airship; 2: solid-rocket power airship; 3: the power big gun; 4: the power shell; 5: nuclear power plant; 6: positive and negative impeller jet engine; 7: positive and negative impeller; 8: positive and negative impeller dynaflow letter road; A: jet engine; B: solid-rocket; C: space probe; D: power cavity; E: nuclear reactor; F: cooling dome; G: main pond; H: standby pond; I: separate cleading I; J: separate cleading J; K: power shower nozzle; A: positive impeller a; B: anti-impeller b; C: positive impeller c; D: anti-impeller d; E: positive impeller e; F: anti-impeller f.
The specific embodiment
Below in conjunction with the accompanying drawing in the embodiment of the invention, the technical scheme in the embodiment of the invention is clearly and completely described, obviously, described embodiment only is the present invention's part embodiment, rather than whole embodiment.Based on the embodiment among the present invention, those of ordinary skills belong to the scope of protection of the invention not paying the every other embodiment that obtains under the creative work prerequisite.
Fig. 1 is airship and part engine installation scheme drawing.(1) be airship, half olivary shell be the fuselage of hull, aircraft be again wing, add spademan (it is overhanging to tilt) all around, flight performance is stronger; Mix suitable engine installation, just can marinely go, land race flies in the air, day upstream; Mix jet engine or screw propeller or nuclear power plant or other power part and just can marinely go, because wing adds the lift of spademan, reduced resistance to motion, speed is fast; Mix jet engine or nuclear power plant, just can fly in the air, carrying capacity is big, and is stealthy; Add the just land race of energy of wheel; Mix jet engine and solid-rocket or power big gun, or nuclear power plant, or nuclear power plant and solid-rocket or power big gun; With regard to energy day upstream, cost is low between the round earth and the moon.
(2) be solid-rocket power airship, solid-rocket is divided into power bin and emission storehouse, connects by aperture, can light mutually.A little solid-rocket is being adorned in the emission storehouse, and space probe is being adorned by spacer assembly in the emission storehouse of little solid-rocket.Power bin is separated into more piece by the pressure shell fragment, and each joint connects and can light mutually by aperture.The pressure shell fragment plays pressurization.After the first segment solid gunpowder is lighted, pressure increases to after the setting value first pressure shell fragment penetrated to airship and accelerates and light the second joint solid gunpowder, pressure increases to after the setting value second pressure shell fragment penetrated to airship and accelerates and light the 3rd joint solid gunpowder, the rest may be inferred, until the little solid-rocket of lighting the emission storehouse, launch space probe at last in the emission storehouse of little solid-rocket, airship slows down, and Returning ball turns around.
(3) be the power big gun, the power big gun is divided into power cavity and emission cavity.Emission cavity is being adorned a power shell and space probe, and power cavity is being adorned a plurality of power shells.Each power shell is transmitted to airship by the automatic ignition device igniting and accelerates.Also can copy the principle of automatic gun to make automatic power big gun (only need add heavy caliber), so just can load more power shell, give the bigger speed of airship, realize space flight.
(4) be the power shell, the power shell is made up of shell case, pressure bullet, gunpowder and automatic ignition device.Gunpowder is lighted, and pressure penetrates the pressure bullet and accelerates to airship after being increased to setting value.
Fig. 2 is part engine installation scheme drawing.(5) be nuclear power plant, by nuclear reactor, cooling dome, main pond,, standby pond, power shower nozzle and water, feed channel and valve, separate cleading, automatic water level controller is formed.The water in main pond enters cooling dome, pick up the heat of nuclear reactor and become steam and discharge from gas exhaust duct, divide two-way, one the tunnel enters the power shower nozzle, by the control of valve, can the front, back, left, right, up, down ejection and provide back, preceding, right, left, upper and lower power to airship, and forward and backward same opening or left and right same opening or upper and lower open together or during standard-sized sheet, power is not provided, airship can be flown on request.Connect screw propeller or other power part by positive and negative impeller dynaflow letter road, can realize marine especially big carrying capacity (hundreds of thousands of ton even 1,000,000 tons) navigation.Another road enters main pond or standby pond by the control of valve, do not conduct heat to the Chi Shui pressurization by separating cleading, like this, and the pressure autostable in whole loop, Chi Shui needn't additionaling power equipment because the drop pressurization enters cooling dome automatically.There is automatic water level controller in the pond, when a pond drop to barrier line under water the time automatic open and close related valve enable another pond and give the alarm, prompting adds water.
(6) be positive and negative impeller jet engine, (7) are positive and negative impellers.The positive impeller of positive and negative impeller directly drives axle just to be changeed, and anti-impeller is counter-rotation then, and driving axle again by three of inner gear drives or several free gear just changes, and the result is that positive and negative impeller drives axial direction rotation simultaneously.The direction of the blade of positive and negative impeller is opposite, and when fluid passed through positive and negative impeller, positive and negative impeller rotated simultaneously round about.Positive and negative impeller jet engine has a plurality of positive and negative impellers with rotating shaft, combustion chamber is between positive impeller a and anti-impeller b, the blade installation direction of anti-impeller b is with the difference of other anti-impeller, the high pressure gas of combustion chamber during to preshoot anti-impeller b be counter-rotating rather than just changeing.When fuel produces in combustion chambers burn that high pressure gas promote that positive impeller a is just changeing that anti-impeller b counter-rotating drives that other positive impeller just changes again, the counter-rotating of anti-impeller produces gas from the gas of admission port inspiration and burning the most at last and all advances combustion chamber to heat the pressurization back from the air nozzle ejection and the acquisition onward impulse.Whole letter road is straight, and each wheel rotation also provides onward impulse to final vacuum the time, and is therefore higher than the jet engine efficient of compressing gas boosting.
(8) being positive and negative impeller dynaflow letter road, is to adorn a plurality of positive and negative impellers with rotating shaft in the straight letter road.When fluid during by positive and negative impeller dynaflow letter road, thereby drive each wheel rotation and provide power to drive screw propeller, electrical generator or other needs the machinery of power to rotating shaft.Utilize positive and negative impeller dynaflow letter road to build the power station, just can drive electrical generator as long as in the big place of drop the letter road is installed, save the investment of water project of writing, economic benefit, ecological benefits highly significant particularly can utilize waterfall power generation.Replace steam engine, steam turbine with positive and negative impeller dynaflow letter road, efficient can significantly improve.
One of ordinary skill in the art will appreciate that: accompanying drawing is the scheme drawing of an embodiment, and the module in the accompanying drawing or flow process might not be that enforcement the present invention is necessary.
It should be noted that at last: above embodiment only in order to technical scheme of the present invention to be described, is not intended to limit; Although with reference to previous embodiment the present invention is had been described in detail, those of ordinary skill in the art is to be understood that: it still can be made amendment to the technical scheme that previous embodiment is put down in writing, and perhaps part technical characterictic wherein is equal to replacement; And these modifications or replacement do not make the essence of appropriate technical solution break away from the spirit and scope of embodiment of the invention technical scheme.

Claims (8)

  1. An energy in sea, land and sky, the airship that travels of sky, it is characterized in that: half olivary shell be the fuselage of hull, aircraft be again wing, add spademan, flight performance is stronger; Mix suitable engine installation, just can marinely go, land race flies in the air, day upstream; Mix jet engine or screw propeller or nuclear power plant or other power part and just can marinely go, because wing adds the lift of spademan, reduced resistance to motion, speed is fast; Mix jet engine or nuclear power plant, just can fly in the air, carrying capacity is big, and is stealthy; Add the just land race of energy of wheel; Mix jet engine and solid-rocket or power big gun, or nuclear power plant, or nuclear power plant and solid-rocket or power big gun, with regard to energy day upstream, cost is low between the round earth and the moon, and can realize space flight.
  2. 2. airship according to claim 1 is characterized in that, described solid-rocket is divided into power bin and emission storehouse, connects by aperture, can light mutually; A little solid-rocket is being adorned in the emission storehouse, and space probe is being adorned by spacer assembly in the emission storehouse of little solid-rocket; Power bin is separated into more piece by the pressure shell fragment, and each joint connects and can light mutually by aperture; The pressure shell fragment plays pressurization; After the first segment solid gunpowder is lighted, pressure increases to after the setting value and first pressure shell fragment to be penetrated and to light the second joint solid gunpowder, pressure increases to after the setting value and second pressure shell fragment to be penetrated and to light the 3rd joint solid gunpowder, the rest may be inferred, until the little solid-rocket of lighting the emission storehouse, launch space probe at last in the emission storehouse of little solid-rocket.
  3. 3. airship according to claim 1 is characterized in that, described power big gun is divided into power cavity and emission cavity; Emission cavity is being adorned a power shell and space probe, and power cavity is being adorned a plurality of power shells; Each power shell is transmitted to airship by the automatic ignition device igniting and accelerates; Also can copy the principle of automatic gun to make the automatic power big gun, so just can load more power shell, give the bigger speed of airship, realize space flight.
  4. 4. airship according to claim 1 is characterized in that, described power shell is made up of shell case, pressure bullet, gunpowder and automatic ignition device; Gunpowder is lighted, and pressure penetrates the pressure bullet and accelerates to airship after being increased to setting value.
  5. 5. airship according to claim 1 is characterized in that, described nuclear power plant, by nuclear reactor, cooling dome, main pond, standby pond, power shower nozzle and water, feed channel and valve, separate cleading, automatic water level controller is formed; The water in main pond enters cooling dome, pick up the heat of nuclear reactor and become steam and discharge from gas exhaust duct, divide two-way, one the tunnel enters the power shower nozzle, by the control of valve, can the front, back, left, right, up, down ejection and provide back, preceding, right, left, upper and lower power to airship, and forward and backward same opening or left and right same opening or upper and lower open together or during standard-sized sheet, power is not provided, airship can be flown on request; Connect screw propeller or other power part by positive and negative impeller dynaflow letter road, can realize marine especially big carrying capacity navigation; Another road enters main pond or standby pond by the control of valve, by separating cleading to the Chi Shui pressurization and not conducting heat, like this, and the pressure autostable in whole loop, Chi Shui needn't additionaling power equipment because the drop pressurization enters cooling dome automatically; There is automatic water level controller in the pond, when a pond drop to barrier line under water the time automatic open and close related valve enable another pond and give the alarm, prompting adds water.
  6. 6. airship according to claim 1, it is characterized in that, described positive and negative impeller, positive impeller directly drives axle just to be changeed, anti-impeller is counter-rotation then, driving axle again by three of inner gear drives or several free gear just changes, and the result is that positive and negative impeller drives axial direction rotation simultaneously; The direction of the blade of positive and negative impeller is opposite, and when fluid passed through positive and negative impeller, positive and negative impeller rotated simultaneously round about.
  7. 7. airship according to claim 1, it is characterized in that, described positive and negative impeller jet engine has a plurality of positive and negative impellers with rotating shaft, combustion chamber is between positive impeller a and anti-impeller b, the blade installation direction of anti-impeller b is with the difference of other anti-impeller, the high pressure gas of combustion chamber during to preshoot anti-impeller b be counter-rotating rather than just changeing; When fuel produces in combustion chambers burn that high pressure gas promote that positive impeller a is just changeing that anti-impeller b counter-rotating drives that other positive impeller just changes again, the counter-rotating of anti-impeller produces gas from the gas of admission port inspiration and burning the most at last and all advances combustion chamber to heat the pressurization back from the air nozzle ejection and the acquisition onward impulse; Whole letter road is straight, and each wheel rotation also provides onward impulse to final vacuum the time, and is therefore higher than the jet engine efficient of compressing gas boosting.
  8. 8. airship according to claim 1 is characterized in that, described positive and negative impeller dynaflow letter road is to adorn a plurality of positive and negative impellers with rotating shaft in the straight letter road; When fluid during by positive and negative impeller dynaflow letter road, thereby drive each wheel rotation and provide power to drive screw propeller, electrical generator or other needs the machinery of power to rotating shaft; Utilize positive and negative impeller dynaflow letter road to build the power station, just can drive electrical generator as long as in the big place of drop the letter road is installed, save the investment of water project of writing, economic benefit, ecological benefits highly significant particularly can utilize waterfall power generation; Replace steam engine, steam turbine with positive and negative impeller dynaflow letter road, efficient can significantly improve.
CN2013101622252A 2013-05-06 2013-05-06 Airship Pending CN103192988A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN2013101622252A CN103192988A (en) 2013-05-06 2013-05-06 Airship

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Application Number Priority Date Filing Date Title
CN2013101622252A CN103192988A (en) 2013-05-06 2013-05-06 Airship

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CN103192988A true CN103192988A (en) 2013-07-10

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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103231792A (en) * 2013-03-11 2013-08-07 陈俞任 Precursor fluid power-assisted high-speed craft
CN103693196A (en) * 2013-12-29 2014-04-02 陈俞任 Front-upper air suction and rear-lower air jet type vertical takeoff and landing aircraft
CN105416583A (en) * 2015-12-15 2016-03-23 陆明友 Water and air solar powered airship
RU2748809C1 (en) * 2020-06-01 2021-05-31 Федеральное государственное образовательное учреждение высшего образования "Санкт-Петербургский университет Государственной противопожарной службы Министерства Российской Федерации по делам гражданской обороны, чрезвычайным ситуациям и ликвидации последствий стихийных бедствий" Method for power supply and assembly of facilities in extreme conditions and air mobile unit for implementation thereof

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101327720A (en) * 2008-05-30 2008-12-24 武汉舒居科技有限公司 Triphibian
CN201357727Y (en) * 2009-03-17 2009-12-09 王万琼 Air-sea-land aircraft
CN201456967U (en) * 2009-04-02 2010-05-12 王长林 airship
CN101722806A (en) * 2008-10-24 2010-06-09 刘全文 Vehicle capable of advancing in land, air and/or water
CN102092254A (en) * 2011-01-09 2011-06-15 黄汉洲 Electromagnetic aerodyne
CN102166931A (en) * 2011-06-08 2011-08-31 陈昌志 New energy multifunctional airplane

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101327720A (en) * 2008-05-30 2008-12-24 武汉舒居科技有限公司 Triphibian
CN101722806A (en) * 2008-10-24 2010-06-09 刘全文 Vehicle capable of advancing in land, air and/or water
CN201357727Y (en) * 2009-03-17 2009-12-09 王万琼 Air-sea-land aircraft
CN201456967U (en) * 2009-04-02 2010-05-12 王长林 airship
CN102092254A (en) * 2011-01-09 2011-06-15 黄汉洲 Electromagnetic aerodyne
CN102166931A (en) * 2011-06-08 2011-08-31 陈昌志 New energy multifunctional airplane

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103231792A (en) * 2013-03-11 2013-08-07 陈俞任 Precursor fluid power-assisted high-speed craft
CN103693196A (en) * 2013-12-29 2014-04-02 陈俞任 Front-upper air suction and rear-lower air jet type vertical takeoff and landing aircraft
CN105416583A (en) * 2015-12-15 2016-03-23 陆明友 Water and air solar powered airship
RU2748809C1 (en) * 2020-06-01 2021-05-31 Федеральное государственное образовательное учреждение высшего образования "Санкт-Петербургский университет Государственной противопожарной службы Министерства Российской Федерации по делам гражданской обороны, чрезвычайным ситуациям и ликвидации последствий стихийных бедствий" Method for power supply and assembly of facilities in extreme conditions and air mobile unit for implementation thereof

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Application publication date: 20130710