• 专利附录
  • 专利说明
  • 权利要求
  • 类似技术
  • 同族专利
  • 引用文献
  • 法律状态
  • 优先权
    • 专利摘要:
    This invention relates to a space flying object having a structure wherein dwelling facility of astronauts or various equipement and machines (2) are sealed inside the innermost film (1c) of a multi-layered film balloon consisting of a large number of spherical films (1a, 1b, 1c) that are disposed concentrically. A gas in a state suitable for human activity or for operations of various equipment and machines (2) is sealed in the innermost film (1c), and gases having progressively decreasing pressures are sealed in the spaces between the films from the innermost film to the outermost film. In comparison with a balloon consisting of a single film, the multi-layered film balloon can insure more reliably protection against the space environment and prevention of scattering of articles, and the difference between internal and external pressures of each film is small. This is advantageous in terms of strength. To prevent the mutual contact of the films, support members such as strings (3a, 3b) are preferably disposed between the films.
    公开号:SU1709899A3
    申请号:SU884613067
    申请日:1988-11-16
    公开日:1992-01-30
    发明作者:Кода Манабу
    申请人:Manabu Koda；
    IPC主号:
    专利说明:

    The invention relates to the design of space technology, namely, devices for protecting objects in outer space.
    The aim of the invention is to improve the conditions for the functioning of an object in outer space by bringing these conditions closer to those on Earth.
    1 shows a device for protecting an object in outer space; 2 shows the construction of a shell layer.
    The security device is made in a Bmda shell consisting of several layers 1a, 16, 1c and covering the protected object 2. The object being protected, for example, may be a communication satellite. Each layer of the sheath is connected to the adjacent layer of at least four connecting elements, Over, 36, which prevent mutual contact of the layers. Fixed cables, racks or rigid struts should be used as mop / t connecting elements. Each layer can be made in the form of glued outer films 4 and carrier fabric 5 arranged between them. Films can be made of polyvinylidene fluoride and polytetrafluoroethylene. Internal fabric can be made of fiberglass. The space between the cladding layers is filled with gas with decreasing pressure rio as the gas moves from the gas surrounding the object to the gas surrounded by the outer layer. The calculations show that the correspondence between the diameter of each layer (a spherical shape is considered) and the pressure of the gas, the corresponding layer, can be as follows: 1.33 4 1 atm. 13.3 m - 0.1 atm, 133 m - 0.01 atm. those. with the diameter of the inner layer of 10 m, the gas pressure will be 0.2 atm, which corresponds to the partial pressure of oxygen on the ground. Such a size allows a large communication satellite, a laboratory or a manned spacecraft to be blasted inside the shell, and a person and living organisms can be in an oxygen atmosphere with a pressure of 0.2 atm. In addition to oxygen, in other cases, the spaces between the layers can be filled with inert gas, nitrogen or carbon dioxide. Perhaps in; The layer surrounding the protective object adds carbon dioxide (to ensure plant photosynthesis), nitrogen (to approach the earth's atmosphere), etc. The layers of the containment can be made of a material that does not interfere with the transmission of electromagnetic waves. This will ensure the functioning inside the containment of such objects as a communication satellite, as well as
    how is it possible to pass through the layers of the shell of radio waves and sunlight. To control the position of satellites inside the envelope, they can be used.
    a flywheel base orientation system or a gas ventilation system between the layers and through the cladding layers. The last system includes a fan which, by moving the gas around the target object
    through layers, by maintaining the total amount of the amount of movement, controls the loopback of the protected object. The use of these systems makes it possible to eliminate the expenditure of materials for
    control the position of the object.
    The proposed device provides not only protection against adverse factors of outer space (cosmic radiation, meteorites, etc.), but also
    creates around the protected object favorable conditions close to the earth. Pho. rmula of invention
    权利要求:
    Claims (5)
    [1]
    1. A device for protecting an object in outer space, containing
    p-layer inflatable shell surrounding the object, characterized in that. in order to improve the conditions for the functioning of an object in outer space by bringing these conditions closer to terrestrial,
    the spaces between the cladding layers are filled with gas with a decrease in pressure along the .vjepe transition from the gas surrounding the object and the gas bounded by the outer cladding layer, with each layer of the cladding
    connected to the adjacent layer of the shell at least four connecting elements.
    [2]
    2. The device according to claim 1, characterized in that each layer of the shell is made of a material that does not interfere with the transmission of electromagnetic waves.
    [3]
    3. The device according to claim 1, in accordance with the fact that one of the layers of the shell is made of a material that prevents the passage of electromagnetic waves.
    [4]
    4. Device pop. 1, characterized in that each layer of the shell is made of 8 types of outer films and the supporting tissue located by them.
    [5]
    5. Device pop. 1, characterized in that the spaces between the object / I, the inner layer of the shell and between the layers of the shells are filled with an inert gas.
    b. The device pop. 1, characterized by that. that in the space between object 1, the shell is located a fan for moving gas around the object or through the layers of the shell.
    four
    FIG 2
    类似技术:
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    OKRESS et al.1980|Solar thermal aerostat research station
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    Graham1990|Extraterrestrial life in the universe
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    Corliss1971|Earth Orbital Science, Space in the Seventies.
    Brown1997|Inflating hopes for a lunar base
    Johnson et al.1996|Architectural Considerations In Design of Lunar-Based Astronomical Observatories
    Amrine et al.1992|Project Ares: a systems engineering and operations architecture for the exploration of Mars
    Hansen et al.1998|Degradation of Hubble Space Telescope Metallized Teflon | FEP Thermal Control Materials
    同族专利:
    公开号 | 公开日
    WO1988007002A1|1988-09-22|
    JP2520250B2|1996-07-31|
    US4971269A|1990-11-20|
    JPS63227500A|1988-09-21|
    引用文献:
    公开号 | 申请日 | 公开日 | 申请人 | 专利标题
    RU2528756C1|2013-04-09|2014-09-20|Федеральное государственное автономное образовательное учреждение высшего профессионального образования "Белгородский государственный национальный исследовательский университет" |Method of construction of shelter on space object|US1001892A|1910-07-05|1911-08-29|Julius Rund|Balloon-envelop material.|
    US1900744A|1931-06-15|1933-03-07|Zeppelin Luftschiffbau|Airship|
    DE1158848B|1961-08-05|1963-12-05|Maxson Electronics Corp|Carrier device|
    FR1344260A|1962-05-24|1963-11-29|Cie D Ingenieurs Et Technicien|Prestressed enclosures, and method of manufacturing such enclosures|
    US3369770A|1965-05-20|1968-02-20|Bernard F. Cohlan|Drag free spacecraft|
    US4166598A|1974-05-30|1979-09-04|The United States Of America As Represented By The Secretary Of The Air Force|Vehicle enshrouding apparatus|CH666235A5|1987-06-24|1988-07-15|Contraves Ag|INFLATABLE FOLDING STRUCTURE AND METHOD FOR PRODUCING FOLDING STRUCTURES.|
    US5115998A|1990-06-29|1992-05-26|The United States Of America As Represented By The Secretary Of The Air Force|Annular balloon|
    US5568902A|1994-08-01|1996-10-29|Hurley, Jr.; Rupert B.|Descent, travel, and protection apparatus, method of making and using same|
    FR2727506B1|1994-11-30|1997-01-24|Giat Ind Sa|DEVICE FOR PROTECTING A VEHICLE OR A STRUCTURE|
    US5743786A|1996-05-30|1998-04-28|Lindsey; Alan|Balloon face polyhedra|
    US7780118B2|2004-07-29|2010-08-24|Bigelow Aerospace|Radiation shield|
    US20100314280A1|2009-06-16|2010-12-16|Zulu 2|Apparatus for the protection of a package, plant, animal, or human|
    EP2517473B1|2009-12-22|2013-04-03|Abb As|Wireless sensor device and method for wirelessly communicating a sensed physical parameter|
    DE102010043086A1|2010-10-28|2012-05-03|Deutsches Zentrum für Luft- und Raumfahrt e.V.|Casing for protecting equipment against high-energy radiation in space, has heat insulation layer, gas diffusion-proof layer and radiation protection layers that are positioned between mechanical protection layers|
    CN112693635A|2021-01-26|2021-04-23|北京航空航天大学|Spacecraft cabin pressure protection system for deep space exploration task|
    法律状态:
    优先权:
    申请号 | 申请日 | 专利标题
    JP62060855A|JP2520250B2|1987-03-16|1987-03-16|Protected structures in outer space|
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