CN107416233A - Space wind-force cabin - Google Patents
Space wind-force cabin Download PDFInfo
- Publication number
- CN107416233A CN107416233A CN201710568274.4A CN201710568274A CN107416233A CN 107416233 A CN107416233 A CN 107416233A CN 201710568274 A CN201710568274 A CN 201710568274A CN 107416233 A CN107416233 A CN 107416233A
- Authority
- CN
- China
- Prior art keywords
- gas
- nacelle
- negative pressure
- source
- dividing plate
- 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
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/46—Arrangements or adaptations of devices for control of environment or living conditions
Landscapes
- Engineering & Computer Science (AREA)
- Health & Medical Sciences (AREA)
- Life Sciences & Earth Sciences (AREA)
- Biodiversity & Conservation Biology (AREA)
- Environmental & Geological Engineering (AREA)
- Environmental Sciences (AREA)
- General Health & Medical Sciences (AREA)
- Toxicology (AREA)
- Remote Sensing (AREA)
- Aviation & Aerospace Engineering (AREA)
- Wind Motors (AREA)
Abstract
The invention discloses a kind of space wind-force cabin, include cylindrical shape nacelle, it is characterised in that：Is provided with square cavity in the nacelle, nacelle upper wall is provided with the malleation source of the gas down blown, and nacelle lower wall is provided with the negative pressure source of the gas of down air-breathing, and the outside of malleation source of the gas and negative pressure source of the gas is provided with dividing plate, and dividing plate is provided with air-vent, and dividing plate inner side is provided with screen pack；The nacelle side wall is communicated with above malleation source of the gas and the gas circulation channel below negative pressure source of the gas.The present invention overcomes state of weightlessness, makes human body can be freely movable in space capsule by setting wind-force to be oriented to.
Description
Technical field
The present invention relates to a kind of improvement in space wind-force cabin invention.
Background technology
Astronaut in floating state, can not normally walk in the influence of space capsule internal cause weightlessness, influence normal
Live and work.
The content of the invention
The technical problems to be solved by the invention are overcome the deficiencies in the prior art, there is provided a kind of space wind-force cabin.
In order to solve the above-mentioned technical problem, the present invention is adopted the following technical scheme that to realize：This kind of space wind-force cabin,
Include cylindrical shape nacelle, it is characterised in that：Square cavity is provided with the nacelle, nacelle upper wall is provided with the malleation down blown
Source of the gas, nacelle lower wall are provided with the negative pressure source of the gas of down air-breathing, and the outside of malleation source of the gas and negative pressure source of the gas is provided with dividing plate, set on dividing plate
There is air-vent, screen pack is provided with the inside of dividing plate；The nacelle side wall is communicated with above malleation source of the gas and below negative pressure source of the gas
Gas circulation channel.
The malleation source of the gas is the blowing apparatus for being evenly arranged in nacelle upper wall, and negative pressure source of the gas is to be evenly arranged under nacelle
The air draft equipment of wall.
The beneficial effects of the invention are as follows the space wind-force cabin after improvement, by setting wind-force to be oriented to, overcome state of weightlessness, make
Human body can be freely movable in space capsule.
Brief description of the drawings
The embodiment of the present invention is described in further detail below in conjunction with the accompanying drawings.
Fig. 1 is the structural representation of the present invention.
Fig. 2 is the structure front view of the present invention.
Embodiment
Accompanying drawing illustrates the structure of the present invention, further illustrates it about details in conjunction with accompanying drawing below.The space wind-force
Cabin, include cylindrical shape nacelle 1, square cavity is provided with the nacelle 1, the upper wall of nacelle 1 is provided with the malleation source of the gas down blown
2, the lower wall of nacelle 1 is provided with the negative pressure source of the gas 3 of down air-breathing, and the outside of malleation source of the gas 2 and negative pressure source of the gas 3 is provided with dividing plate 4, dividing plate 4
Air-vent is provided with, the inner side of dividing plate 4 is provided with screen pack 5, for Chalk-dust filtering impurity；The side wall of nacelle 1 is communicated with malleation
The gas circulation channel 6 of the top of source of the gas 2 and the lower section of negative pressure source of the gas 3, make to form the continuous field of wind-force down blown in nacelle 1, overcome
Suspension problem caused by state of weightlessness.
The malleation source of the gas 2 is the blowing apparatus for being evenly arranged in the upper wall of nacelle 1, and negative pressure source of the gas 3 is to be evenly arranged in cabin
The air draft equipment of the lower wall of body 1.
In summary, presently preferred embodiments of the present invention is these are only, is not intended to limit the scope of the present invention.
Within the spirit and principles of the invention, any modification, equivalent substitution and improvements made etc., it should be included in the present invention's
Within protection domain.
Claims (2)
1. space wind-force cabin, includes cylindrical shape nacelle, it is characterised in that：Square cavity, nacelle upper wall are provided with the nacelle
Provided with the malleation source of the gas down blown, nacelle lower wall is provided with the negative pressure source of the gas of down air-breathing, and malleation source of the gas is outer with negative pressure source of the gas
Side is provided with dividing plate, and dividing plate is provided with air-vent, screen pack is provided with the inside of dividing plate；The nacelle side wall is communicated with malleation source of the gas
Side and the gas circulation channel below negative pressure source of the gas.
2. space wind-force cabin as claimed in claim 1, it is characterised in that：The malleation source of the gas is to be evenly arranged in nacelle upper wall
Blowing apparatus, negative pressure source of the gas is the air draft equipment for being evenly arranged in nacelle lower wall.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710568274.4A CN107416233A (en) | 2017-07-13 | 2017-07-13 | Space wind-force cabin |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710568274.4A CN107416233A (en) | 2017-07-13 | 2017-07-13 | Space wind-force cabin |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107416233A true CN107416233A (en) | 2017-12-01 |
Family
ID=60427160
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710568274.4A Pending CN107416233A (en) | 2017-07-13 | 2017-07-13 | Space wind-force cabin |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107416233A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108454888A (en) * | 2018-01-31 | 2018-08-28 | 倪惠芳 | A kind of aerospace driving equipment auxiliary device |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5718587A (en) * | 1995-08-28 | 1998-02-17 | Joseph C. Sussingham | Variable gravity simulation system and process |
| JPH11245898A (en) * | 1998-03-03 | 1999-09-14 | Mamoru Yagi | False gravity generator utilizing magnetic force, moving element control device, moving device, stopping device, and adjuster for reinforcing muscle strength, bone, etc. |
| US6206328B1 (en) * | 1998-11-09 | 2001-03-27 | Thomas C. Taylor | Centrifugal gravity habitation torus constructed of salvaged orbital debris |
| CN2908355Y (en) * | 2006-06-22 | 2007-06-06 | 张承祖 | Special toilet for manned spacecraft |
| CN106800098A (en) * | 2015-11-26 | 2017-06-06 | 李宁 | A kind of space capsule structure design of generation acceleration of gravity |
-
2017
- 2017-07-13 CN CN201710568274.4A patent/CN107416233A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5718587A (en) * | 1995-08-28 | 1998-02-17 | Joseph C. Sussingham | Variable gravity simulation system and process |
| JPH11245898A (en) * | 1998-03-03 | 1999-09-14 | Mamoru Yagi | False gravity generator utilizing magnetic force, moving element control device, moving device, stopping device, and adjuster for reinforcing muscle strength, bone, etc. |
| US6206328B1 (en) * | 1998-11-09 | 2001-03-27 | Thomas C. Taylor | Centrifugal gravity habitation torus constructed of salvaged orbital debris |
| CN2908355Y (en) * | 2006-06-22 | 2007-06-06 | 张承祖 | Special toilet for manned spacecraft |
| CN106800098A (en) * | 2015-11-26 | 2017-06-06 | 李宁 | A kind of space capsule structure design of generation acceleration of gravity |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108454888A (en) * | 2018-01-31 | 2018-08-28 | 倪惠芳 | A kind of aerospace driving equipment auxiliary device |
| CN108454888B (en) * | 2018-01-31 | 2021-02-19 | 倪惠芳 | Aerospace drive device auxiliary device |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20171201 |
|
| RJ01 | Rejection of invention patent application after publication |