CN106114788A - A kind of aircraft push structure - Google Patents
A kind of aircraft push structure Download PDFInfo
- Publication number
- CN106114788A CN106114788A CN201610589546.4A CN201610589546A CN106114788A CN 106114788 A CN106114788 A CN 106114788A CN 201610589546 A CN201610589546 A CN 201610589546A CN 106114788 A CN106114788 A CN 106114788A
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- CN
- China
- Prior art keywords
- nacelle
- passage
- aircraft
- inner hollow
- rotating assembly
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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.)
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63H—MARINE PROPULSION OR STEERING
- B63H1/00—Propulsive elements directly acting on water
- B63H1/02—Propulsive elements directly acting on water of rotary type
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Ocean & Marine Engineering (AREA)
- Wind Motors (AREA)
Abstract
The invention discloses a kind of aircraft push structure, this structure includes the first nacelle, the second nacelle and passage；Wherein, described first nacelle is airtight and the spheroidal nacelle of inner hollow, and described second nacelle is internal is formed with spherical inner chamber by dividing plate isolation；Described passage is the cylindrical channel of inner hollow；Described first nacelle is fixedly linked with described passage and turns on；This structure has thoroughly overturned the thrust power source of aircraft in prior art, it is different from existing any propulsion mode, this structure need not the propulsive elements such as propeller, and the thrust produced that self rotates directly utilizing outer nacelle (the second nacelle) promotes aircraft entirety to move ahead.This structure has the advantages such as speed-raising is fast, energy-efficient performance is good.Stability in the large when aircraft moves ahead can be increased, by reasonably designing the contour structures of the second nacelle, relatively big to the propulsive thrust of water, headway can be increased.
Description
Technical field
The present invention relates to propeller technical field, particularly relate to a kind of aircraft push structure.
Background technology
Steamer facilitates the change of human lives, causes the mankind to have a dream the countries in the world mutual dependence for existence that also I had never expected in the past
Relation.Today, the steamer of modernization, wherein there are passenger steamer, cargo ship and an oil tanker, are working on the various fate of human beings that is related to
Global business shipping.Such as the U.S. of developed country maximum in the world, in phase early 1970s, import of transporting by sea every year
More than 300,000,000 tons, total value is more than 30,000,000,000 dollars.Some of them luxury goods such as Swiss Watch, Russia's fur, Scotch whisky,
Italy footwear, Denmark's furniture, batard-montrachet, only account for the sub-fraction of import total value；Main import is
Raw material, indispensable including the crude oil of more than 400,000,000 barrels, 40,000,000 tons of iron ores, more than 1,500 ten thousand tons of bauxitic ores and national life
Other few article.In prior art, steamer operationally steam promotes piston to do work in cylinder, and the steam of cooling is by pipe
It is re-condensed into water to being introduced into condenser.This process constantly repeats when steam engine moves.General steam engine has three
Cylinder one group of composition.The up and down motion of piston is directly converted into the rotary motion of ship axle by steam engine.Before final promotion steamer
Enter.The steam engine of modern steamer also has other to improve the mechanism of its efficiency.For example, it is possible to multiple cylinders are connected together.Steam
Next cylinder it is also input into the most afterwards from a cylinder.The diameter of these cylinders one than upper one big.Although so steam
Pressure often by constantly reducing after a cylinder, but total power that each piston is applied by it is identical.Make existing
The steamer in technology is had to promote inefficient.
Summary of the invention
The invention provides a kind of aircraft push structure.
The invention provides following scheme:
A kind of aircraft push structure, this structure includes the first nacelle, the second nacelle and passage；
Wherein, described first nacelle is airtight and the spheroidal nacelle of inner hollow, described second nacelle internal by every
Plate isolation is formed with spherical inner chamber；Described passage is the cylindrical channel of inner hollow；Described first nacelle is solid with described passage
Determine to be connected and conducting；
Described first nacelle is positioned at inside described spherical inner chamber, and described second nacelle is by turning of being set on described passage
Shaft assembly is rotatable with described passage to be connected；Described rotating assembly is connected with the Power Component being positioned at described passage, described dynamic
Power assembly is used for driving described second nacelle to rotate around described passage.
Preferred: described rotating assembly includes bearing.
Preferred: described rotating assembly includes axle sleeve.
Preferred: between mainboard and the described dividing plate of described second nacelle, to be provided with load-carrying members securing plate.
Preferred: described second nacelle outer surface is provided with multiple drying slurry.
The specific embodiment provided according to the present invention, the invention discloses techniques below effect:
By the invention it is possible to realize a kind of aircraft push structure, under a kind of implementation, this structure can be wrapped
Include the first nacelle, the second nacelle and passage；Wherein, described first nacelle is airtight and the spheroidal nacelle of inner hollow, institute
State the second nacelle inside and be formed with spherical inner chamber by dividing plate isolation；Described passage is the cylindrical channel of inner hollow；Described
First nacelle is fixedly linked with described passage and turns on；Described first nacelle is positioned at inside described spherical inner chamber, described second cabin
Body is connected by the rotating assembly that is set on described passage is rotatable with described passage；Described rotating assembly be positioned at described logical
Power Component in road is connected, and described Power Component is used for driving described second nacelle to rotate around described passage.This structure is thorough
The thrust power source of aircraft in prior art has been overturned at the end, is different from existing any propulsion mode, and this structure is not
Needing the propulsive elements such as propeller, the thrust produced that self rotates directly utilizing outer nacelle (the second nacelle) promotes aircraft whole
Body moves ahead.This structure has the advantages such as speed-raising is fast, energy-efficient performance is good.Stability in the large when aircraft moves ahead can be increased, logical
Cross the contour structures reasonably designing the second nacelle, relatively big to the propulsive thrust of water, headway can be increased.
Certainly, the arbitrary product implementing the present invention it is not absolutely required to reach all the above advantage simultaneously.
Accompanying drawing explanation
In order to be illustrated more clearly that the embodiment of the present invention or technical scheme of the prior art, below will be to institute in embodiment
The accompanying drawing used is needed to be briefly described, it should be apparent that, the accompanying drawing in describing below is only some enforcements of the present invention
Example, for those of ordinary skill in the art, on the premise of not paying creative work, it is also possible to obtains according to these accompanying drawings
Obtain other accompanying drawing.
Fig. 1 is the structural representation of a kind of aircraft push structure that the embodiment of the present invention provides；
Fig. 2 is another structural representation of a kind of aircraft push structure that the embodiment of the present invention provides.
In figure: first nacelle the 1, second nacelle 2, passage 3, dividing plate 4, rotating assembly 5, power assembly 6, drying slurry 7.
Detailed description of the invention
Below in conjunction with the accompanying drawing in the embodiment of the present invention, the technical scheme in the embodiment of the present invention is carried out clear, complete
Describe, it is clear that described embodiment is only a part of embodiment of the present invention rather than whole embodiments wholely.Based on
Embodiment in the present invention, the every other embodiment that those of ordinary skill in the art are obtained, broadly fall into present invention protection
Scope.
Embodiment
See Fig. 1, Fig. 2, a kind of aircraft push structure provided for the embodiment of the present invention, as shown in Figure 1 and Figure 2, should
Structure includes the first nacelle the 1, second nacelle 2 and passage 3；
Wherein, described first nacelle 1 is airtight and the spheroidal nacelle of inner hollow, and described second nacelle 2 is internal to be passed through
Dividing plate 4 isolation is formed with spherical inner chamber；Described passage 3 is the cylindrical channel of inner hollow；Described first nacelle 1 is logical with described
Road 3 is fixedly linked and turns on；
Described first nacelle 1 is positioned at inside described spherical inner chamber, and described second nacelle 2 is by being set on described passage 3
Rotating assembly 5 rotatable with described passage be connected；Described rotating assembly 5 and Power Component 6 phase being positioned at described passage 3
Even, described Power Component 6 is used for driving described second nacelle to rotate around described passage 3.
In use, the first nacelle can use this structure as carrying storehouse, and passenger can be passed in and out by this passage
First nacelle, this first nacelle is when advancing, and this channel position relatively is constant, it is ensured that the comfortableness of passenger.When advancing,
Power Component output power, drives this runner assembly to rotate, thus drives this second nacelle to rotate entirely around this passage, and second
Nacelle is during rotating, and the water being in contact with it can produce deboost to it and then drive total to move ahead.Specifically
When selecting this rotating assembly, described rotating assembly includes bearing.Described rotating assembly can also include axle sleeve.Specifically chosen permissible
Overall dimensions according to this structure is determined.For further promoting the robustness of this structure, the mainboard of described second nacelle
And it is provided with load-carrying members securing plate between described dividing plate.In order to improve the drying performance of this structure, the embodiment of the present application also may be used
To provide described second nacelle outer surface to be provided with multiple drying slurry 7.
This structure has thoroughly overturned the thrust power source of aircraft in prior art, is different from existing any one and pushes away
Entering mode, this structure need not the propulsive elements such as propeller, and directly utilize outer nacelle (the second nacelle) self rotates generation
Thrust promotes aircraft entirety to move ahead.This structure has the advantages such as speed-raising is fast, energy-efficient performance is good.Aircraft can be increased when moving ahead
Stability in the large, by reasonably designing the contour structures of the second nacelle, relatively big to the propulsive thrust of water, navigation speed can be increased
Degree.It will, of course, be appreciated that, this structure, can according to the least of aircraft and application scenario not when specifically applying
With, can select to organize this structure more and use simultaneously.
It should be noted that in this article, the relational terms of such as first and second or the like is used merely to a reality
Body or operation separate with another entity or operating space, and deposit between not necessarily requiring or imply these entities or operating
Relation or order in any this reality.And, term " includes ", " comprising " or its any other variant are intended to
Comprising of nonexcludability, so that include that the process of a series of key element, method, article or equipment not only include that those are wanted
Element, but also include other key elements being not expressly set out, or also include for this process, method, article or equipment
Intrinsic key element.In the case of there is no more restriction, statement " including ... " key element limited, it is not excluded that
Including process, method, article or the equipment of described key element there is also other identical element.
The foregoing is only presently preferred embodiments of the present invention, be not intended to limit protection scope of the present invention.All
Any modification, equivalent substitution and improvement etc. made within the spirit and principles in the present invention, are all contained in protection scope of the present invention
In.
Claims (5)
1. an aircraft push structure, it is characterised in that described structure includes the first nacelle, the second nacelle and passage；
Wherein, described first nacelle is airtight and the spheroidal nacelle of inner hollow, described second nacelle internal by dividing plate every
From being formed with spherical inner chamber；Described passage is the cylindrical channel of inner hollow；Described first nacelle fixes phase with described passage
Connect and conducting；
Described first nacelle is positioned at inside described spherical inner chamber, and described second nacelle is by the rotating shaft group being set on described passage
Part is rotatable with described passage to be connected；Described rotating assembly is connected with the Power Component being positioned at described passage, described power packages
Part is used for driving described second nacelle to rotate around described passage.
Structure the most according to claim 1, it is characterised in that described rotating assembly includes bearing.
Structure the most according to claim 1, it is characterised in that described rotating assembly includes axle sleeve.
Structure the most according to claim 1, it is characterised in that arrange between mainboard and the described dividing plate of described second nacelle
There is load-carrying members securing plate.
Structure the most according to claim 1, it is characterised in that described second nacelle outer surface is provided with multiple drying
Slurry.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610589546.4A CN106114788A (en) | 2016-07-26 | 2016-07-26 | A kind of aircraft push structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610589546.4A CN106114788A (en) | 2016-07-26 | 2016-07-26 | A kind of aircraft push structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106114788A true CN106114788A (en) | 2016-11-16 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610589546.4A Pending CN106114788A (en) | 2016-07-26 | 2016-07-26 | A kind of aircraft push structure |
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|---|---|
| CN (1) | CN106114788A (en) |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0125799A1 (en) * | 1983-04-14 | 1984-11-21 | John Wright Ingle | Shape of a marine craft, in particular of a life-boat |
| FR2598672B1 (en) * | 1985-11-07 | 1991-04-12 | Legoy Auguste | ROTARY FLOAT AND MACHINES EQUIPPED WITH SUCH A FLOAT |
| FR2680149B1 (en) * | 1991-08-08 | 1993-11-26 | Hauser Jean Luc | TURBO-FLOAT. |
| TWI280931B (en) * | 2003-07-29 | 2007-05-11 | Schmitt Kugelantriebe Gmbh | Vessel propulsion system |
| CN101337572A (en) * | 2008-01-10 | 2009-01-07 | 马启义 | Globular shape ship |
| CN105196814A (en) * | 2015-10-13 | 2015-12-30 | 宋建国 | Ball-shaped rolling land and water scooter |
| CN205837155U (en) * | 2016-07-26 | 2016-12-28 | 刘朝凡 | A kind of aircraft push structure |
-
2016
- 2016-07-26 CN CN201610589546.4A patent/CN106114788A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0125799A1 (en) * | 1983-04-14 | 1984-11-21 | John Wright Ingle | Shape of a marine craft, in particular of a life-boat |
| FR2598672B1 (en) * | 1985-11-07 | 1991-04-12 | Legoy Auguste | ROTARY FLOAT AND MACHINES EQUIPPED WITH SUCH A FLOAT |
| FR2680149B1 (en) * | 1991-08-08 | 1993-11-26 | Hauser Jean Luc | TURBO-FLOAT. |
| TWI280931B (en) * | 2003-07-29 | 2007-05-11 | Schmitt Kugelantriebe Gmbh | Vessel propulsion system |
| CN101337572A (en) * | 2008-01-10 | 2009-01-07 | 马启义 | Globular shape ship |
| CN105196814A (en) * | 2015-10-13 | 2015-12-30 | 宋建国 | Ball-shaped rolling land and water scooter |
| CN205837155U (en) * | 2016-07-26 | 2016-12-28 | 刘朝凡 | A kind of aircraft push structure |
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| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
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| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20161116 |
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| RJ01 | Rejection of invention patent application after publication |