GB2216218A - Space frame - Google Patents

Space frame Download PDF

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Publication number
GB2216218A
GB2216218A GB8904083A GB8904083A GB2216218A GB 2216218 A GB2216218 A GB 2216218A GB 8904083 A GB8904083 A GB 8904083A GB 8904083 A GB8904083 A GB 8904083A GB 2216218 A GB2216218 A GB 2216218A
Authority
GB
United Kingdom
Prior art keywords
bolt
strut
collar
shank
strut body
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.)
Granted
Application number
GB8904083A
Other versions
GB2216218B (en
GB8904083D0 (en
Inventor
Siew Kwong Wong
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
NEW YORK PLASTIC CO Pte Ltd
Original Assignee
NEW YORK PLASTIC CO Pte Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by NEW YORK PLASTIC CO Pte Ltd filed Critical NEW YORK PLASTIC CO Pte Ltd
Publication of GB8904083D0 publication Critical patent/GB8904083D0/en
Publication of GB2216218A publication Critical patent/GB2216218A/en
Application granted granted Critical
Publication of GB2216218B publication Critical patent/GB2216218B/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04BGENERAL BUILDING CONSTRUCTIONS; WALLS, e.g. PARTITIONS; ROOFS; FLOORS; CEILINGS; INSULATION OR OTHER PROTECTION OF BUILDINGS
    • E04B1/00Constructions in general; Structures which are not restricted either to walls, e.g. partitions, or floors or ceilings or roofs
    • E04B1/18Structures comprising elongated load-supporting parts, e.g. columns, girders, skeletons
    • E04B1/19Three-dimensional framework structures
    • E04B1/1903Connecting nodes specially adapted therefor
    • E04B1/1906Connecting nodes specially adapted therefor with central spherical, semispherical or polyhedral connecting element
    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04BGENERAL BUILDING CONSTRUCTIONS; WALLS, e.g. PARTITIONS; ROOFS; FLOORS; CEILINGS; INSULATION OR OTHER PROTECTION OF BUILDINGS
    • E04B1/00Constructions in general; Structures which are not restricted either to walls, e.g. partitions, or floors or ceilings or roofs
    • E04B1/18Structures comprising elongated load-supporting parts, e.g. columns, girders, skeletons
    • E04B1/19Three-dimensional framework structures
    • E04B2001/1924Struts specially adapted therefor
    • E04B2001/1927Struts specially adapted therefor of essentially circular cross section
    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04BGENERAL BUILDING CONSTRUCTIONS; WALLS, e.g. PARTITIONS; ROOFS; FLOORS; CEILINGS; INSULATION OR OTHER PROTECTION OF BUILDINGS
    • E04B1/00Constructions in general; Structures which are not restricted either to walls, e.g. partitions, or floors or ceilings or roofs
    • E04B1/18Structures comprising elongated load-supporting parts, e.g. columns, girders, skeletons
    • E04B1/19Three-dimensional framework structures
    • E04B2001/1957Details of connections between nodes and struts
    • E04B2001/196Screw connections with axis parallel to the main axis of the strut

Abstract

A space frame consists of nodes with screw threaded sockets and interconnecting struts (6, 7) each having at each end a bolt (9), which can be turned by a surrounding collar (11), to which it is keyed by a ball which is seated in a recess (17) in the bolt and works in a keyway groove (18) in the collar. The bolt may be retracted into the end of the strut against the action of a spring (13) to enable the strut to be inserted closely between an adjacent pair of nodes. <IMAGE>

Description

DESCRIPTION IMPROVEMENTS RELATING TO SPACE FRAMES The invention relates to a space frame of the kind, hereinafter referred to as of the kind described, comprising a plurality of nodes, each provided with a plurality of screw threaded sockets; and a plurality of elongate struts for linking respective pairs of nodes. Each end of each strut is provided with a longitudinally extending bolt which is freely rotatable relatively to a strut body and which has a shank with a screw threaded portion extending from the end of the strut body for engagement of the screw threaded portion with a respective node socket, whereby rotation of the bolt draws the end of the strut body towards the node.
Each shank is surrounded by a collar having a non-circular external surface to which a turning tool can be applied, the collar and the shank each having one a key and the other a complementary longitudinal keyway whereby the shank is constrained to rotate with the collar but is movable axially therethrough a and the collar is gripped between the end of the strut body and the node when the bolt has been fully tightened.
A space frame of this kind is disclosed for example is EP-B-0044057, and in GB-B-2002482. In 0044057, the complementary key and keyway are provided a pin which extends diametrically through, and is fixed in, the bolt, the ends of the pin engaging in axial slots through the collar. This is costly to produce and the exposed slots in the collar are unsightly and may accumulate dirt. In 2002482 the key and keyway are provided by a hexagonal section of the bolt shank, and a surrounding complementarily shaped inner surface of a hub of the collar. Although this connection is concealed, it is again expensive to produce.
In accordance with a first aspect of the present invention, in a strut for a space frame of the kind described, the key and key way are provided by a ball partly nesting in a recess in the bolt shank, and a complementary groove extending axially along the inner surface of the collar. This is a very simple arrangement both to produce and assemble. To assist assembly the groove in the collar will normally be open at the end of the collar nearer to the strut body, and closed at its other end.
A further problem with space frames of the kind described, is that when two nodes are rigidly positioned relatively to one another, as a result of complete, or near complete, assembly of the frame, it is difficult to insert or replace a strut between the two nodes which are at a fixed distance from one another. This is because it is necessary for the screw threaded ends of the bolt shanks to extend from the strut collars, so that they can engage the screw threads in the node sockets, upon rotation of the collars and bolts. However, if the shanks extend, even marginally, from the ends of the strut collars, the strut body, with the collars at its ends, cannot be inserted between two nodes which are spaced by no more than the total length of the strut body and collars.Consequently, some clearance to accommodate the projecting bolt shank, is necessary between the end of each collar and the respective node, so that when the bolts are subsequently tightened into the node sockets, either the collars will not be drawn up closely against the nodes, or the frame will be deflected and stressed by drawing of the nodes towards one another.
In accordance with a second, independent, aspect of the invention, in a strut for a space frame of the kind described, each bolt is retractable against a spring within the strut body to a position in which the tip of the shank is flush with the outer end of the respective collar, whereby a strut body with collars at each end can be inserted between two fixed nodes having a spacing substantially equal to the combined length of the strut body and two collars whereupon the springs will extend the bolt shanks so that the screw threaded portions will be pushed into the entrances to the respective node sockets ready for engagement with the socket screw threads when the bolts are turned by a torque applied to the collars.
In one construction each strut body is provided by a tube, each end of which receives a reduced diameter portion of a member which houses the head of the bolt and, behind the bolt an abutment for a compression spring which is located between the abutment and bolt head.
An example of a space frame constructed in accordance with the present invention is illustrated in the accompanying drawings, in which: Figure 1 is a side elevation of the end of one strut; FIgure 2 is a section taken on the line II-II in Figure It Figure 3 is a perspective view of a strut bolt; Figure 4 is a perspective view of a strut collar; and, Figure 5 is a perspective view of a node.
Each strut comprises a body in the form of a steel tube 6, each end of which receives as a force fit a reduced diameter end portion of a tapered housing 7. Captive by its head 8 within the housing is a bolt having a shank 9, which extends out of the housing and is provided at its end with a screw threaded portion 10. The shank is closely surrounded by a collar 11 having a hexagonal tool engaging portion 12. The bolt is urged out of the housing 7 by a helically coiled compression spring, which abuts at one end a washer 14, engaging the head 8, and at its other end, a washer 15, which is held in position by a circlip 16. The clearance within the housing 7 is such that the bolt can be retracted against the action of the spring 13 until the tip of the screw threaded portion 10 is flush with the outer end of the collar 11.
The shank 9 of the bolt is provided with a hemispherical recess 17, in which is seated a steel ball, the ball being slidable within a complementary groove 18 within the interior of the collar 11.
In addition to a number of the struts, the frame comprises a number of nodes, such as that shown in Figure 5. Each node comprises a generally spherical body 19 formed with a symmetrical array of internally screw threaded sockets 20, each complementary to the screw threaded portion 10 of a strut bolt.
A strut may be assembled between two fixed nodes by retracting the bolts within the housing 7 and collars 11, inserting the strut between the nodes, in alignment with two of the sockets 20, whereupon the springs 13 will advance the bolts so that the screw threaded portions 10 of the bolts are urged into the respective sockets 20. Rotation of respective collars 11, by application of a spanner or similar tool to the portions 12, will then screw the bolts into the respective sockets, until the collars 11 are clamped between the ends of the strut body and the nodes. This results from each ball, acting between a respective recess 17 and groove 18, transmitting the rotation of the respective collar 11 to the respective bolt, whilst allowing axial movement of the bolt through the collar. As shown in Figure 2, each groove 18 opens at the strut body end of the respected collars, so that the collar can be assembled on to the bolt shank over the screw threaded portion 10.

Claims (7)

1. A strut for a space frame of the kind comprising a plurality of nodes (19), each provided with a plurality of screw threaded sockets (20); and a plurality of elongate struts for linking respective pairs of nodes; the strut having, at each end, a longitudinally extending bolt which is freely rotatable relatively to a strut body (6) and which has a shank (9) with a screw threaded portion (10) extending from the end of the strut body for engagement of the screw threaded portion, in use, with a respective node socket (20), whereby rotation of the bolt draws the end of the strut body towards the node; each shank (9) being surrounded by a collar (11) having a non-circular external surface (12) to which a turning tool can be applied, the collar and shank each having one a key (17) and the other a complementary longitudinal keyway (18) whereby the shank is constrained to rotate with the collar but is movable axially therethrough and the collar is gripped between the end of the strut body and the node when the bolt has been fully tightened; wherein the key and keyway are provided by a ball partly nesting in a recess (17) in the bolt shank (9), and a complementary groove (18) extending axially along the inner surface of the collar (11).
2. A strut according to claim 1, wherein the groove (18) in the collar (11) is open at the end of the collar nearer to the strut body (6), and closed at its other end.
3. A strut according to claim 1 or claim 2, wherein each bolt is retractable against a spring (13) within the strut body (6) to a position in which the tip of the shank (9) is flush with the outer end of the respective collar (11), whereby a strut body with collars at each end can, in use, be inserted between two fixed nodes (19) having a spacing substantially equal to the combined length of the strut body (6) and two collars (11) whereupon the springs will extend the bolt shanks so that the screw threaded portions will be pushed into the entrances to the respective node sockets (20) ready for engagement with the socket screw threads when the bolts are turned by a torque applied to the collars.
4. A strut according to claim 3, wherein each strut body (6) is provided by a tube, each end of which receives a reduced diameter portion of a member (7) which houses the head (8) of the bolt and, behind the bolt, an abutment (16) for a compression spring (13) which is located between the abutment and bolt head.
5. A strut for a space frame of the kind comprising a plurality of nodes (19), each provided with a plurality of screw threaded sockets (20); and a plurality of elongate struts for linking respective pairs of nodes; the strut having, at each end, a longitudinally extending bolt which is freely rotatable relatively to a strut body (6) and which has a shank (9) with a screw threaded portion (10) extending from the end of the strut body for engagement of the screw threaded portion, in use, with a respective node socket (20), whereby rotation of the bolt draws the end of the strut body towards the node; each shank (9) being surrounded by a collar (11) having a non-circular external surface (12) to which a turning tool can be applied, the collar and shank each having one a key (17) and the other a complementary longitudinal keyway (18) whereby the shank is constrained to rotate with the collar but is movable axially therethrough and the collar is gripped between the end of the strut body and the node when the bolt has been fully tightened; wherein each bolt is retractable against a spring (13) within the strut body (6) to a position in which the tip of the shank (9) is flush with the outer end of the respective collar (11), whereby a strut body with collars at each end can, in use, be inserted between two fixed nodes (19) having a spacing substantially equal to the combined length of the strut body (6) and two collars (11) whereupon the springs will extend the bolt shanks so that the screw threaded portions will be pushed into the entrances to the respective node sockets (20) ready for engagement with the socket screw threads when the bolts are turned by a torque applied to the collars.
6. 4. A strut according to claim 5, wherein each strut body (6) is provided by a tube, each end of which receives a reduced diameter portion of a member (7) which houses the head (8) of the bolt and, behind the bolt, an abutment (16) for a compression spring (13) which is located between the abutment and bolt head.
7. A space frame, comprising a plurality of nodes (19), each provided with a plurality of screw threaded sockets (20); and a plurality of elongate struts, each according to any one of the preceding claims, for linking respective pairs of nodes.
GB8904083A 1988-02-23 1989-02-22 Improvements relating to space frames Expired - Fee Related GB2216218B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB888804127A GB8804127D0 (en) 1988-02-23 1988-02-23 Space frame

Publications (3)

Publication Number Publication Date
GB8904083D0 GB8904083D0 (en) 1989-04-05
GB2216218A true GB2216218A (en) 1989-10-04
GB2216218B GB2216218B (en) 1992-09-02

Family

ID=10632172

Family Applications (2)

Application Number Title Priority Date Filing Date
GB888804127A Pending GB8804127D0 (en) 1988-02-23 1988-02-23 Space frame
GB8904083A Expired - Fee Related GB2216218B (en) 1988-02-23 1989-02-22 Improvements relating to space frames

Family Applications Before (1)

Application Number Title Priority Date Filing Date
GB888804127A Pending GB8804127D0 (en) 1988-02-23 1988-02-23 Space frame

Country Status (2)

Country Link
CN (1) CN1032024C (en)
GB (2) GB8804127D0 (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2241997A (en) * 1990-03-15 1991-09-18 Victor Mfg Ltd Joining together counter modules
GR1001160B (en) * 1992-02-20 1993-05-24 Georgios Gkamanis Mechanism for the connection of a pipe to a node of a three-dimensional structure.
GB2274142A (en) * 1993-01-07 1994-07-13 P T Rangka Ruang Joint for space frames
WO2010130099A1 (en) * 2009-05-15 2010-11-18 Abb Technology Ltd. Lock device for restricting rotational movement

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104373804B (en) * 2014-11-13 2017-03-15 江苏明福钢结构有限公司 A kind of functional steel truss
CN105350640A (en) * 2015-11-19 2016-02-24 李全民 A machinery connecting device between assembly type concrete prefabricated units and an operation method
CN109208764B (en) * 2018-11-02 2020-05-29 叶祺 Bracing piece connection structure of steel house room
CN113235818B (en) * 2021-05-27 2022-12-02 依格安顾问(香港)有限公司 Connection structure and framework
CN114592711A (en) * 2022-03-08 2022-06-07 中交第四公路工程局有限公司 Device and method for replacing pull rod in steel grid structure

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1001812A (en) * 1962-02-07 1965-08-18 David Ashley Pears Improvements in scaffolding and like structures
GB2002482A (en) * 1977-08-13 1979-02-21 Mero Raumstruktur Gmbh & Co Screw connection between tubular bars and attachment connectors in space frameworks
GB2013832A (en) * 1978-02-04 1979-08-15 Uni Cardan Ag Telescopic drive shaft
EP0044057A1 (en) * 1980-07-15 1982-01-20 MERO-Raumstruktur GmbH & Co. Nodal joint for wood bars of trusses, in particular three-dimensional trusses

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1001812A (en) * 1962-02-07 1965-08-18 David Ashley Pears Improvements in scaffolding and like structures
GB2002482A (en) * 1977-08-13 1979-02-21 Mero Raumstruktur Gmbh & Co Screw connection between tubular bars and attachment connectors in space frameworks
GB2013832A (en) * 1978-02-04 1979-08-15 Uni Cardan Ag Telescopic drive shaft
EP0044057A1 (en) * 1980-07-15 1982-01-20 MERO-Raumstruktur GmbH & Co. Nodal joint for wood bars of trusses, in particular three-dimensional trusses

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2241997A (en) * 1990-03-15 1991-09-18 Victor Mfg Ltd Joining together counter modules
GR1001160B (en) * 1992-02-20 1993-05-24 Georgios Gkamanis Mechanism for the connection of a pipe to a node of a three-dimensional structure.
GB2274142A (en) * 1993-01-07 1994-07-13 P T Rangka Ruang Joint for space frames
WO2010130099A1 (en) * 2009-05-15 2010-11-18 Abb Technology Ltd. Lock device for restricting rotational movement

Also Published As

Publication number Publication date
GB2216218B (en) 1992-09-02
GB8904083D0 (en) 1989-04-05
CN1032024C (en) 1996-06-12
CN1036612A (en) 1989-10-25
GB8804127D0 (en) 1988-03-23

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Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee

Effective date: 19970222