• 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:
    A method for forming a domed space frame, comprising assembling and pivotally interconnecting plural longitudinally extensible elongate elements into a planar grid frame array; pivotally anchoring ends of the elongate elements at the grid frame periphery; securing a gas-tight flexible extensible membrane to the grid frame; anchoring the membrane around the periphery of the grid frame in a gas-tight manner; and introducing pressurized gas under the membrane to inflate it and thereby raise the grid frame into a domed configuration, with a consequential extension of the elongate elements. When each elongate element has extended to a predetermined ultimate length, an arresting means associated therewith becomes operative and prevents any further change in the length of that elongate element. When all the elongate elements are so arrested, the gas pressure is released from beneath the membrane, and a self-supporting domed space frame is then available for use.
    公开号:SU1080749A3
    申请号:SU792778051
    申请日:1979-05-30
    公开日:1984-03-15
    发明作者:Бини Данте
    申请人:Данте Бини (Итали )；
    IPC主号:
    专利说明:

    The invention relates to the spatial coverage of buildings and structures and to the method of their formation.
    Closest to the present invention is a spatial coating comprising core elements that are sharnirno interconnected at the nodes with the formation of the lattice lj.
    A disadvantage of the known coating is the complexity of installation, the need to work on connecting the rod elements together at a height in the design position.
    Closest to the present invention is a method of forming a spatial coating, including placing the membrane under the coating, arranging individual core elements and assembling them into a flat grid with a hinged connection of the ends of the elements among themselves, inflating the membrane prior to purchasing the design position with the membrane and dismantling the membrane 2j.
    A disadvantage of the known method is the difficulty of fixing the length of the rods in the design position, including pouring the solution and the need to withstand the pressure under the membrane until the strength of the solution in the system nodes is set.
    The purpose of the invention is to simplify installation.
    The goal is achieved by the fact that in the spatial coverage, which includes separate core elements pivotally interconnected at the nodes to form a grid, each element is equipped with a telescopic headboard, installed with the possibility of longitudinal movement and rotation about the element axis, and a device for fixing its length, and Each grating assembly is equipped with a device for limiting the hinge rotation of elements in two mutually perpendicular planes.
    This goal is achieved in that according to the method of forming a spatial coating, including placing the membrane under the coating, arranging individual core elements and assembling them into a flat grid with a hinged connection of the ends of the elements among themselves, inflating the membrane before acquiring the design position with the membrane and dismantling the membrane after arranging the elements the lower ends of the core elements along the perimeter adjacent to the Contour are hinged, and at 5 times the inflating membrane seals the rod elements prior to purchase of a working position.
    FIG. 1 shows the spatial coverage, general view; figure 2 - coating before installation, top view; FIG. 3 shows the node I in FIGS. 1 and 2, the node in a disassembled state, a domestic view); 4, the same, in the assembled state, is a side view; fig.Z - node II in figure 1 and 2, a general view; figure 6 is a schematic view of the anchoring of the membrane on its periphery, the section.
    0 FIG. 1 shows the coating
    after it is mounted by pressurization. The coating includes separate core elements 1, which are hingedly connected to each other in knots.
    FIG. 2 shows the arrangement of the lattice elements 1 on the membrane 2. In FIG. 3, which shows the means of connecting the lattice elements, a connecting ring 3 is visible, the connecting parts 4, which are short tubes with flat sections 5 in which there are openings 6 for free (with a gap) the placement of the ring 3. Link 7 are tubes in which the shanks 8 of the connecting parts 4 are inserted, and they have the ability to slide into links YAH.7. The connecting piece 4 and the link 7 form the core element 1. In each hole of the link 7 on the inner surface there is an annular recess 9 for accommodating a locking locking spring ring 10 installed in the groove 11 in each of the shank 8 of the connecting piece. Each spring ring 10 is held down, despite the tendency to expand, by placing link 7 in the hole. As soon as the spring ring 10 is aligned with the annular recess (groove) 9 in link 7, it expands and snaps into place, thereby preventing further telescoping the movement of the shank 8 relative to the tube 7 in one way and the other side. In order to
    to allow insertion of the shank 8 with the spring ring 10 into the opening of the link 7 beyond the annular recess 9, there are four openings 12 that are aligned with the annular notch 9. This gives the opportunity to insert the shanks and press on the expansion ring 10 until it goes beyond the limits of the annular recess 9, and also makes it possible to inspect the spring ring and notice that the KOI- is fully engaged in the annular recess 9.
    FIG. 4 shows the assembly I assembled after the installation of the spatially. At the top of the flat part 5 there is a recess 13 which engages with a protrusion 14 on the washer 15. The latter is a part of the fastening means by which the connection of the elements is attached to the membrane 2. In particular, the membrane 2 has an opening 16 which is coaxial with the holes 17 and 18 upper and lower washers 15 and 19. A bolt 20 with an enlarged head 21 passes through the ring 3 between the ends of the flat parts 5 of the connecting elements, the hole 18 of the washer, the hole 16 of the membrane, the hole 17 of the washer, through the elastic waterproof gasket 22 and is screwed a nut 23. In this case, node 1 when the elements are moved from a flat position to a location at an angle, as shown in step of FIG. the protrusions 14 pass over the corners 24 due to the compression of the gaskets 22 until they engage with the recesses 13. This makes it possible to obtain an extra angle, but when the gas pressure under the diaphragm decreases, the spatial frame sits and takes a constant shape. the protrusions 14 are engaged with the recesses 13 of all the connections.
    The hinge connection of the lattice along its periphery to the base (node II in figure 1) can have various forms. One embodiment is illustrated in FIG. Each link 7 has a connecting part 4, made at one end in the form of an eyelet with ears 25. The sheet element 26 is pivotally connected by means of a pin 27. Each sheet element 26 has an enlarged key head 28, which engages with a groove 29. Sleeve 30 and washer 31 is the same as previously described. The sleeve and washer are secured to the base 32, which surrounds the area to be closed, with a bolt 33, the second is embedded in the base 32 and passes through a central hole in the sleeve. The assembly of the assembly is accomplished with a large nut 34, which overlaps the key heads 28 and prevents them from exiting the keyways 29.
    FIG. 6 shows a section of a surface 35 to be coated, a peripheral pit 36 that forms a contour around the surface 35, an anchor bar 37 in the ground, a reinforcement element 38 and bolts 39 that are connected to the sleeves 30 (Fig. 5). The membrane 2 is located in the pit 36, which is filled with concrete in order to secure the membrane circumferentially and form the base 32. The compressed gas is then introduced under the membrane and the blocking of the elements is in fact disengaged in order to provide the final core convex spatial frame. The elements and details of the coating described may be metallic or in many cases may be made of plastic materials.
    The method for forming a spatial coating is as follows.
    The membrane is placed under the lattice, the elements are assembled into a flat lattice with predetermined dimensions around the periphery and a predetermined shape using hinged joints beyond the end elements and anchoring the lattice elements beyond its peripheral points at some distance from each other in order to allow at the anchorage points turn. The membrane is then inflated until all elongated elements are stretched to their respective positions; working lengths, reduce the boost pressure from under the membrane in order to trigger the latching means, and then remove the membrane.
    By the proposed method, the membrane can be placed above the grille. in this case, it is attached to the lattice.
    The application of the invention allows to simplify installation, while installation can be carried out in a limited area and does not require the use of qualified workers, special equipment and precise quality control of the connection of the components.
    /
    J
    ) /
    fie.d G6 P VT- -f "X .-: -. , 4 .. And p ::: 7/5 / / / / "/ I I I Id
    权利要求:
    Claims (2)
    [1]
    1. A spatial coating, including individual rod elements, pivotally connected to each other in nodes to form a lattice, characterized in that, in order to simplify installation, each element is equipped with a telescopic head mounted with the possibility of longitudinal movement and rotation about the axis of the element, and a device for fixing its length, and each node of the lattice is equipped with a device for limiting the articulated rotation of elements in two mutually perpendicular planes,
    [2]
    2. A method of forming a spatial coating, including placing the membrane under the coating, laying out individual core elements and assembling them into a flat grid with articulating ends of the elements together, inflating the membrane until the coating acquires its design position and dismantling the membrane, which means that simplification of installation, after the layout of the elements, the lower ends of the rod elements adjacent to the contour are perpendicularly attached to the contour, and during the inflation of the membrane, the erasers are extended; harvesting elements prior to the acquisition of the coated working position.
    类似技术:
    公开号 | 公开日 | 专利标题
    SU1080749A3|1984-03-15|Three-dimensional roof and method for forming same
    US5634483A|1997-06-03|Canopy support system
    RU2220269C2|2003-12-27|Inflated working shed
    RU2088732C1|1997-08-27|Supporting structure
    US5159948A|1992-11-03|Tent with frame formed by hoops
    US20070084493A1|2007-04-19|Articulating hub assembly
    EP0565629A1|1993-10-20|Collapsible canopy framework having captured scissor ends with non-compressive pivots
    US3973370A|1976-08-10|Method of making a frame assembly
    US2793720A|1957-05-28|Scaffolding and other structural elements
    CA1171756A|1984-07-31|Collapsible building structure
    KR19990022817A|1999-03-25|Collapsible Display Structure for Indoor and Outdoor
    US3269398A|1966-08-30|Convex tents
    US3225413A|1965-12-28|Inflatable form for a concrete building
    WO1981000125A1|1981-01-22|Collapsible structure and method of erecting the same
    US4190990A|1980-03-04|Frame assembly
    US4277922A|1981-07-14|Frame assembly apparatus and method of making same
    CA1215207A|1986-12-16|Cabling system for an inflatable building
    US20060081282A1|2006-04-20|Tent frame and canopy
    JPH06101274A|1994-04-12|Method of constructing roof of cable dome
    WO1989007696A1|1989-08-24|Collapsible frameworks for free standing awnings
    SK130795A3|1996-09-04|Emergency shelter
    KR101845008B1|2018-04-03|Guard fence using band and connector, and method for constructing this same
    SU1546599A1|1990-02-28|High-rise structure
    JP2002081227A|2002-03-22|Tent
    US20060101631A1|2006-05-18|Method and equipment for manufacturing expandable and collapsible structures
    同族专利:
    公开号 | 公开日
    US4296585A|1981-10-27|
    CA1125982A|1982-06-22|
    FR2427439A1|1979-12-28|
    DE2921789A1|1979-12-06|
    BR7903563A|1981-04-28|
    JPS552195A|1980-01-09|
    ES481120A1|1980-02-01|
    IT1118859B|1986-03-03|
    AT372132B|1983-09-12|
    NZ190568A|1983-09-02|
    FR2427439B1|1985-03-01|
    GB2022647B|1982-06-23|
    ATA393879A|1983-01-15|
    GB2022647A|1979-12-19|
    IT7949254D0|1979-05-30|
    JPS6366989B2|1988-12-22|
    ZA792587B|1980-09-24|
    AR225743A1|1982-04-30|
    引用文献:
    公开号 | 申请日 | 公开日 | 申请人 | 专利标题
    RU2665338C1|2017-05-03|2018-08-29|Федеральное государственное бюджетное образовательное учреждение высшего образования "Казанский национальный исследовательский технический университет им. А.Н. Туполева-КАИ" |Grid shell|US2826157A|1953-07-17|1958-03-11|Karl O Vartia|Roof structure|
    US3106772A|1959-08-20|1963-10-15|Gordon B Holcombe|Method of erecting buildings, tanks, domes or similar structures|
    US3057368A|1960-05-03|1962-10-09|Norman R Seaman|Composite air dome structure|
    NL298934A|1962-10-08|
    US3186522A|1963-02-27|1965-06-01|George W Mccauley|Structural surfaces|
    US3315343A|1964-04-13|1967-04-25|Bendix Corp|Method of constructing a building|
    FR1475006A|1966-02-18|1967-03-31|Tent, especially for the beach|
    US3375619A|1966-11-21|1968-04-02|Charles H. Hurkamp|Pneumatic apparatus for erecting structural building components|
    FR1547960A|1967-12-13|1968-11-29|Stromeyer & Co Gmbh L|tent-shaped building, with fabric suspension members|
    JPS5018288B1|1968-11-21|1975-06-27|
    IL34025A|1970-03-08|1971-04-28|Peret Co|Collapsible reticular structures|
    US3675380A|1970-04-27|1972-07-11|Tension Structures Co|Prefabricated dome-type shelter|
    US3676976A|1970-05-27|1972-07-18|Jack G Mcallister|Roof structure|
    US3710806A|1971-10-27|1973-01-16|V Kelly|Erectable building structure|
    US3973370A|1972-05-22|1976-08-10|Mcallister Jack G|Method of making a frame assembly|
    FR2248381B1|1973-10-19|1980-10-03|Chateau Stephane Du|
    US3968808A|1974-11-06|1976-07-13|Zeigler Theodore Richard|Collapsible self-supporting structure|
    DE2454274C2|1974-11-15|1983-09-15|Dante Crows Nest New South Wales Bini|Method for producing a self-supporting dome-like concrete structure and device for carrying out the method|
    US4026313A|1976-07-13|1977-05-31|Zeigler Theodore Richard|Collapsible self-supporting structures|FR2481385B1|1980-02-06|1985-03-08|Schaff Alfred|
    JPH0322515B2|1983-04-13|1991-03-27|Senyo Kogyo Kk|
    IT1190044B|1986-06-05|1988-02-10|Dioguardi Spa Flli|SPATIAL RETICULAR STRUCTURE MADE UP OF TELESCOPIC EXTENSIBLE MODULAR ELEMENTS AND CONTAINED WITH SPHERICAL HINGE KNOTS|
    DE8708053U1|1987-06-06|1988-10-06|Kanya Ag, Duernten, Ch|
    DE3736784A1|1987-10-30|1989-05-24|Friedrich B Grimm|NODE ROD SYSTEM|
    FR2624536B1|1987-12-11|1990-05-25|Thimonier Jean Noel|ARCHITECTONIC STRUCTURE WITH POLYGONAL CELLS ASSEMBLED BY GLUING|
    US5279081A|1990-02-16|1994-01-18|Space Biospheres Ventures|Pressure balancing a closed ecological system|
    US5165207A|1992-01-23|1992-11-24|Harlan Oehlke|Apparatus and method for forming a space frame structure|
    DE19745639C2|1996-11-07|2002-07-18|Franz Dietrich Oeste|Truss supporting structures made of ring elements|
    ES2143382B1|1997-11-27|2000-12-01|Jimenez Rodrigo Ramos|PERFECTED MODULAR STRUCTURE, APPLICABLE AS A POOL COVER AND SIMILAR.|
    DE10119866A1|2001-04-24|2002-11-21|Juergen Graf|Nodal shutter bar join uses center nodal cross linking bars so opposing bars are co-planar and turn around center cross axis for arrestable linking by round bars at ends|
    US20030226319A1|2002-06-06|2003-12-11|Richards Ashton E.|Geodesic dome assemby joint|
    US20050120643A1|2003-12-09|2005-06-09|Siedentopf Robert A.|Primary-geodesic least surface shapes for predetermined ground plots and functions|
    US7779599B2|2004-03-31|2010-08-24|Safway Services, Llc|Articulating work platform support system, work platform system, and methods of use thereof|
    GB2418469A|2004-09-24|2006-03-29|John Moon|Connector assembly|
    DE202005017822U1|2005-11-14|2006-04-06|Schneider, Michael|Washer with keyholes, circlips and rods for constructing geodesic frameworks|
    US7992353B2|2008-12-10|2011-08-09|Athan Stephan P|Space frame hub joint|
    CN103556709B|2013-11-13|2015-04-15|大连博跃科技发展有限公司|Dome frame structure system|
    WO2015070572A1|2013-11-13|2015-05-21|大连博跃科技发展有限公司|Dome frame structural system|
    ES2593270B1|2015-06-05|2017-09-19|Universidade Da Coruña|Double-sided space mesh with lockable joints|
    US20170175378A1|2015-12-16|2017-06-22|Lee Budde|Strut arrangement for a geodesic dome|
    DE102017200039A1|2017-01-03|2018-07-05|Yeon Hee Lee|PREPARED COUPLING|
    CN106836478A|2017-02-24|2017-06-13|荆门创佳机械科技有限公司|One kind inflation prestressing force depression bar|
    ES2630753B2|2017-03-30|2018-06-12|Manuel Fernando BETHENCOURT CRAVID|RETICULAR STRUCTURE|
    EP3807470A1|2018-06-15|2021-04-21|Matilda's Planet Strata Comfort Ltd|Strut connector|
    CN110388006A|2019-06-10|2019-10-29|浙江省建工集团有限责任公司|A kind of membrane structure girder end drip pan of the wooden beam string of assembled Long span|
    CN111502008A|2020-05-07|2020-08-07|中山大学|Membrane-shell composition structure suitable for space base and construction method|
    法律状态:
    优先权:
    申请号 | 申请日 | 专利标题
    AUPD454578|1978-05-30|
    [返回顶部]