US3877192A - Assemblage of pieces of a metal frame - Google Patents

Assemblage of pieces of a metal frame Download PDF

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Publication number
US3877192A
US3877192A US360585A US36058573A US3877192A US 3877192 A US3877192 A US 3877192A US 360585 A US360585 A US 360585A US 36058573 A US36058573 A US 36058573A US 3877192 A US3877192 A US 3877192A
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United States
Prior art keywords
upright
end plate
ribs
unit
mast structure
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Expired - Lifetime
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US360585A
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English (en)
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Roger Metailler
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Richier SA
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Richier SA
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B66HOISTING; LIFTING; HAULING
    • B66CCRANES; LOAD-ENGAGING ELEMENTS OR DEVICES FOR CRANES, CAPSTANS, WINCHES, OR TACKLES
    • B66C23/00Cranes comprising essentially a beam, boom, or triangular structure acting as a cantilever and mounted for translatory of swinging movements in vertical or horizontal planes or a combination of such movements, e.g. jib-cranes, derricks, tower cranes
    • B66C23/18Cranes comprising essentially a beam, boom, or triangular structure acting as a cantilever and mounted for translatory of swinging movements in vertical or horizontal planes or a combination of such movements, e.g. jib-cranes, derricks, tower cranes specially adapted for use in particular purposes
    • B66C23/26Cranes comprising essentially a beam, boom, or triangular structure acting as a cantilever and mounted for translatory of swinging movements in vertical or horizontal planes or a combination of such movements, e.g. jib-cranes, derricks, tower cranes specially adapted for use in particular purposes for use on building sites; constructed, e.g. with separable parts, to facilitate rapid assembly or dismantling, for operation at successively higher levels, for transport by road or rail
    • B66C23/28Cranes comprising essentially a beam, boom, or triangular structure acting as a cantilever and mounted for translatory of swinging movements in vertical or horizontal planes or a combination of such movements, e.g. jib-cranes, derricks, tower cranes specially adapted for use in particular purposes for use on building sites; constructed, e.g. with separable parts, to facilitate rapid assembly or dismantling, for operation at successively higher levels, for transport by road or rail constructed to operate at successively higher levels
    • B66C23/283Cranes comprising essentially a beam, boom, or triangular structure acting as a cantilever and mounted for translatory of swinging movements in vertical or horizontal planes or a combination of such movements, e.g. jib-cranes, derricks, tower cranes specially adapted for use in particular purposes for use on building sites; constructed, e.g. with separable parts, to facilitate rapid assembly or dismantling, for operation at successively higher levels, for transport by road or rail constructed to operate at successively higher levels with frameworks composed of assembled elements
    • B66C23/286Cranes comprising essentially a beam, boom, or triangular structure acting as a cantilever and mounted for translatory of swinging movements in vertical or horizontal planes or a combination of such movements, e.g. jib-cranes, derricks, tower cranes specially adapted for use in particular purposes for use on building sites; constructed, e.g. with separable parts, to facilitate rapid assembly or dismantling, for operation at successively higher levels, for transport by road or rail constructed to operate at successively higher levels with frameworks composed of assembled elements with locking devices

Definitions

  • ABSTRACT The present invention concerns the assemblage of the elements of a dismountable metal frame, and more particularly a mast, such as a crane tower which has to be raised by successive superimposed elements or, on the contrary, dismounted.
  • the assemblage devices must be designed in such a manner as to permit the transmission of the components of the stresses in several directions, that is to say in a mast the longitudinal stresses exerted on the uprights placed in prolongation of one another, and the transverse stresses, transmitted more particularly by the cross-braces and resulting from shearing stresses and torques.
  • the assemblage device comprises the combination of parts generally provided with connecting bolts, which receive the longitudinal stresses, and other parts, distinct from the preceding parts, intended for transmitting the transverse stresses, and preferably also for connecting the cross-braces to the uprights, these means projecting with respect to the surface of the joint on each of the pieces to be assembled, externally but tangentially to the perimeter of the said surface.
  • the present invention concerns the assemblage of the elements of a dismountable metal frame, and more particularly a mast, such as a crane tower which has to be raised by successive superimposed elements or, on the contrary, dismounted.
  • the assemblage devices must be designed in such a manner as to permit the transmission of the compo nents of the stresses in several directions, that is to say in a mast the longitudinal stresses exerted on the principal members or the uprights placed in prolongation of one another, and the transverse stresses, transmitted more particularly by the cross-braces and resulting from shearing stresses and torques.
  • the assemblage device comprises the combination of parts generally provided with connecting bolts, which receive the longitudinal stresses, and other parts, distinct from the preceding parts, intended for transmitting the transverse stresses, and preferably also for connecting the cross-braces to the uprights, these means projecting with respect to the surface of the joint on each of the pieces to be assembled, externally but tangentially to the perimeter of the said surface.
  • the invention covers metal frameworks, in particular masts or towers comprising elements assembled by the device concerned.
  • FIG. I is a diagrammatic perspective view showing the upper end of a mast element and the lower end of one of the members of the element above.
  • FIG. 2 shows in perspective on a larger scale the upper end of a member of an element and the lower end of the corresponding member of the element above.
  • FIG. 3 is a view in horizontal projection of the upper end of a member of an element.
  • FIG. 4 is a view in elevation corresponding to FIG. 3
  • FIGS. 10 and 11 show, in elevation and plan, an assemblage device for the panels of a mast element in application of the invention.
  • FIGS. 12 and 13 show on a larger scale, in elevation and in horizontal projection, the detail of the assemblage device before connection of its two portions.
  • FIGS. 14, I5 and 16 correspond respectively to FIGS. 10, I1 and I2 and concern a modification.
  • FIG. I shows in perspective the upper end of the four vertical uprights or members of a metal mast element of square section, and the lower end of one only of the four uprights of the element above, which is to be superimposed and assembled with the first element, while FIG. 2 shows on a slightly larger scale the uprights on the left of FIG. 1.
  • FIGS. 3, 4 and 5 recapitulating the means shown in FIG. 2, show them this time in vertical and horizontal projection.
  • Each of the box uprights of square section such as l, 2, 3, 4 (or 1, 2', 3, 4, the upright 1 only being shown), is provided at each of its ends with a bridle 5 (or 5, see above) provided with two bores 6, 7 for the passage of assemblage bolts, the said bridles being set back with respect to the joint plane.
  • These bridles with their bolts which may or may not be prestressed, serve for transmitting their longitudinal stresses to the uprights, that is to say, the stresses parallel to the arrow A of FIG. 2; as will be seen in FIGS. 3 and 5, the bridles are placed obliquely with respect to the sides of the section of the upright and pass through this section.
  • This arrangement may be modified by providing two long ribs 8, 9 parallel to the axis of the upright and welded respectively to the two faces of the upright which are turned towards the interior of the section of the element formed by the four uprights. On each of the uprights, these ribs project with respect to the joint plane (plane I J in FIG. 4) and are provided with a slight chamfer to facilitate fitting (see FIG. 4).
  • the space 11 between the ribs 8, 9 of the upper end of an upright and the edge a of the upright which is inside the section of the element is less by the thickness of at least one rib than the corresponding space h between the ribs 8' and 9' of the lower end of an upright and the corresponding edge a.
  • the upper end of the uprights is welded to a plate 10 at right-angles to the edges of the uprights and closing the section of the latter.
  • the lower end of the uprights remaining free is supported during assemblage on the plate 10 of the uprights below (FIG. 4).
  • the said plate 10 may project on the faces of the upright, externally of the section of the element as shown in FIGS. 2, 3 and 4, but it is flush with the two faces of the uprights which are inside the section of the element permitting fitting by the ribs and bringing into alignment the edges a and a.
  • the ribs are situated tangentially t the perimeter of the said plate.
  • the joint plane of two successive uprights is the plane marked J] in FIG. 4 or again the plane of FIG. 3.
  • the square cccc shown in dashed lines is the section of the element situated below the plane of the drawing whose respective uprights occupy the squares a h c d, while the squareffff, drawn in chain lines, represents the section of the element situated above the plane of the drawing, whose uprights bear on the plates 10 and have the sections represented by the four squares u e fg.
  • the bridles 5 and 5 are placed in a manner such that the axes of the bores 6, 7 and 6, 7' are in coincidence from one upright to the next, which involves a variation in the position of the bridles with respect to the section of the uprights when the said section itself varies. This will be seen by camparison of FIGS. 3 and 5.
  • the ribs 8, 9, 8', 9' are used for fixing the crossbraces 11 and the ties l2 connecting the uprights together. This fixing may be carried out in any appropriate manner.
  • the drawing shows fixing by plates 13 welded to the ends of the cross-braces or the ties and to the ribs, the latter being shaped to offer edges of suitable inclination such as l4, 14.
  • FIG. 7, 8 and 9 show a modified embodiment of the assemblage, differing from the previously described embodiment in that the bores 6, 7 and 6, 7 for the passage of the assemblage bolts are no longer provided on a bridle crossing the section of the elements, but rather are provided on solid parts l5, 16, 15, 16 fixed to the external faces of the elements, preferably by welding between the ribs 8, 9 and gussets 17, 18, welded to the external faces of the uprights.
  • This arrangement is particularly applicable when the longitudinal stresses to be transmitted become considerable.
  • FIGS. 10 to 12 show a method of applying the invention to the assemblage of panels which are to form a tower.
  • FIG. 11 in which the four panels are represented in horizontal projection, positioned opposite one another for assemblage, shows that each panel comprises an upright I and two pairs ofhalfcross-braces Ila, 11a; 11h, 11h, these pairs being situated in two perpendicular planes passing through the axis of the upright.
  • the half cross-braces are fixed as described in the foregoing to terminal ribs of the uprights and are assembled together to form a triangle, it being possible to provide ties, such as 12, at the apex of the said triangle.
  • each triangle of cross-braces comprises a plate or sole 20 and 20', respectively, which soles are applied against one another during assemblage.
  • These soles are provided with holes 21, 21. in which bolts may be introduced for thus supporting the components of stresses exerted perpendicularly to the said soles.
  • the said soles include at their ends projections 22, 22' adapted to overlap during assemblage, such that the projections 22 of one sole 20 hearing on the edge of the other sole 20 and vice versa so that the projection 22' bears on the edge of the plate 20.
  • This interlocking enables the components of the stresses exerted parallel to the soles to be absorbed and thus enables the shearing stresses on the bolts to be sup pressed.
  • FIGS. 14 to 16 differs from the preceding embodiment in that on each panel the crossbraces 11a extend over almost the entire width of the panel and only in one plane, such that assemblage is effected against one upright.
  • the alignment of the edges (1 a of the uprights, which are in the interior of the superimposed elements, has the advantage of permitting sliding in the tower, from its base to its summit, an important element for raising the tower, as is the case in some types of telescopic cranes.
  • the invention is not, however, limited to this type of alignment of the internal edges.
  • a generally vertical mast structure designed for end-to-end assembly of upright structural units on top of each other in mutual abutting relationship of the adjacent ends of two successive upright units, namely, the upper end of a first upright unit and the lower end of a second upright unit positioned immediately above said first upright unit and extending upwardly, said first and second upright units being fastened endwise to each other by associated bolting means which extend in a longitudinal direction with respect to said mast structure, wherein the improvement comprises the combination of: an end plate fastened with an upright unit end and flanging the same, said end plate having:
  • mast structure as in claim 1 wherein said end plate comprises at least two adjacent rectilinear peripheral sides which are at an angle to each other and connected at an angular corner point, and said end ribs comprise protruding borders which project beyond said end plate at both said adjacent rectilinear sides thereof.
  • said upright structural units comprise coextensive upright elemental struts each having at least two adjacent planar outer faces which are at an angle to each other equal to that of said rectilinear sides and which are connected at respective straight edges, said rectilinear peripheral sides of said end plate and said planar outer faces of said elemental struts being flush with each other and coextensive, and said corner point of said end plate and said straight edges of said elemental struts being likewise colinear thereby forming together a smooth continuous dihedral rail which extends from top to bottom.
  • each upright structural unit comprises a plurality of like upright elemental struts forming corner elements for said unit and provided with end plate and rib systems, and wherein said corner point of the respective end plates and said straight edges of respective elemental struts are directed towards the inside of said upright structural unit whereby said unit comprises inwardly thereof as many Lil smooth continuous dihedral rails as it has upright elemental struts.
  • each upright structural unit further comprises bracing ties interconnecting said upright elemental struts, said bracing ties bearing against buttress sections of said end ribs spaced from said exposed protruding borders thereof.
  • mast structure as in claim 2 wherein said first upright unit comprises at said upper end thereof a pair of end ribs having exposed protruding borders which project upwardly beyond said end plate at said adjacent rectilinear peripheral sides thereof respectively, and said second upright unit comprises likewise at said lower end thereof a further pair of end ribs having exposed protruding borders which project downwardly beyond said end plate at said same rectilinear peripheral sides thereof, respectively, each rib of one pair of said ribs being adjacent to a rib of the other pair of said ribs and associated with the same rectilinear peripheral side of said end plate.
  • each of said pairs of end ribs forms a dihedral of substantially the same angle as the angle between said two adjacent rectilinear peripheral sides of said end plate.

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  • Engineering & Computer Science (AREA)
  • Structural Engineering (AREA)
  • Transportation (AREA)
  • Mechanical Engineering (AREA)
  • Jib Cranes (AREA)
  • Conveying And Assembling Of Building Elements In Situ (AREA)
  • Joining Of Building Structures In Genera (AREA)
US360585A 1972-05-16 1973-05-15 Assemblage of pieces of a metal frame Expired - Lifetime US3877192A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7217427A FR2184418B1 (es) 1972-05-16 1972-05-16

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US3877192A true US3877192A (en) 1975-04-15

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US360585A Expired - Lifetime US3877192A (en) 1972-05-16 1973-05-15 Assemblage of pieces of a metal frame

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US (1) US3877192A (es)
JP (1) JPS545907B2 (es)
AR (1) AR202101A1 (es)
BR (1) BR7303543D0 (es)
CA (1) CA979173A (es)
DE (1) DE2324184C3 (es)
ES (1) ES415153A1 (es)
FR (1) FR2184418B1 (es)
GB (1) GB1427403A (es)
IT (1) IT986325B (es)
SU (1) SU610485A3 (es)

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4620405A (en) * 1982-09-24 1986-11-04 David J. Stainer Structural member
US5406767A (en) * 1992-11-23 1995-04-18 The Manitowoc Company, Inc. Longitudinally divisible crane boom segment
US5487479A (en) * 1992-11-23 1996-01-30 The Manitowoc Company, Inc. Method for nesting longitudinally divisible crane boom segments
US6213318B1 (en) * 1999-03-01 2001-04-10 Manitowoc Crane Group, Inc. Rotatable connection system for crane boom sections
US6296419B1 (en) * 1998-12-21 2001-10-02 Potain (Societe Anonyme) Device providing a connection between a pivot and a mast structure for tower cranes
CN104528543A (zh) * 2014-12-31 2015-04-22 徐州建机工程机械有限公司 一种上引进方式的塔机标准节结构
ITUB20159180A1 (it) * 2015-12-22 2017-06-22 Gp Autolift S R L Elemento modulare a traliccio a montaggio semplificato per torri di gru a torre e torre comprendente tale elemento modulare.
CN109179222A (zh) * 2018-09-29 2019-01-11 温州建设集团有限公司 一种塔式起重机预埋节斜度及水平度控制施工方法
US10392233B2 (en) 2015-03-26 2019-08-27 Liebherr-Werk Biberach Gmbh Crane tower
CN112279120A (zh) * 2020-11-26 2021-01-29 江西省丰和泰重工科技有限公司 一种基座加强型塔式起重机

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1986001848A1 (en) * 1984-09-19 1986-03-27 Gte Products Corporation Space frame
US4562681A (en) * 1985-02-05 1986-01-07 Gte Products Corporation Web section for a space frame
DE4109051A1 (de) * 1991-03-15 1992-09-17 Saalfelder Hebezeugbau Gmbh Stoss- und anschlussausbildung fuer i-artiges leichtbauprofil mit hohlflanschen
FR2903094B1 (fr) * 2006-06-28 2009-02-27 Potain Soc Par Actions Simplif Dispositif d'assemblage demontable pour elements de mat d'une grue a tour
ES2398834B1 (es) * 2011-09-08 2013-12-03 Linden Comansa, S.L. Torre modular.
CN102826463B (zh) * 2012-09-11 2015-05-20 张月梅 塔式起重机组合式基座
CN107010547A (zh) * 2017-05-09 2017-08-04 徐州建机工程机械有限公司 一种塔机新型片节结构

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US712299A (en) * 1901-12-24 1902-10-28 Howland Sherman Mfg Company Column capital and attachment.
US1941952A (en) * 1931-12-26 1934-01-02 Manitowoc Shipbuilding Corp Boom construction
US2086009A (en) * 1933-04-05 1937-07-06 Remington Rand Inc Book stack
US2194810A (en) * 1939-06-20 1940-03-26 Leo A Reiner Scaffold
US2308565A (en) * 1940-08-15 1943-01-19 Kochring Company Structural unit
US2404276A (en) * 1944-07-28 1946-07-16 Cohen Harold Tower construction
US3245188A (en) * 1961-03-17 1966-04-12 Evans Hugh Stanford Scaffolding
US3564802A (en) * 1969-10-07 1971-02-23 Jean Paul L Dreyfus Scaffolding system

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US712299A (en) * 1901-12-24 1902-10-28 Howland Sherman Mfg Company Column capital and attachment.
US1941952A (en) * 1931-12-26 1934-01-02 Manitowoc Shipbuilding Corp Boom construction
US2086009A (en) * 1933-04-05 1937-07-06 Remington Rand Inc Book stack
US2194810A (en) * 1939-06-20 1940-03-26 Leo A Reiner Scaffold
US2308565A (en) * 1940-08-15 1943-01-19 Kochring Company Structural unit
US2404276A (en) * 1944-07-28 1946-07-16 Cohen Harold Tower construction
US3245188A (en) * 1961-03-17 1966-04-12 Evans Hugh Stanford Scaffolding
US3564802A (en) * 1969-10-07 1971-02-23 Jean Paul L Dreyfus Scaffolding system

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4620405A (en) * 1982-09-24 1986-11-04 David J. Stainer Structural member
AU597834B2 (en) * 1982-09-24 1990-06-07 Tristan Guy Melland Structural member
US5406767A (en) * 1992-11-23 1995-04-18 The Manitowoc Company, Inc. Longitudinally divisible crane boom segment
US5487479A (en) * 1992-11-23 1996-01-30 The Manitowoc Company, Inc. Method for nesting longitudinally divisible crane boom segments
US6296419B1 (en) * 1998-12-21 2001-10-02 Potain (Societe Anonyme) Device providing a connection between a pivot and a mast structure for tower cranes
US6213318B1 (en) * 1999-03-01 2001-04-10 Manitowoc Crane Group, Inc. Rotatable connection system for crane boom sections
CN104528543A (zh) * 2014-12-31 2015-04-22 徐州建机工程机械有限公司 一种上引进方式的塔机标准节结构
US10392233B2 (en) 2015-03-26 2019-08-27 Liebherr-Werk Biberach Gmbh Crane tower
ITUB20159180A1 (it) * 2015-12-22 2017-06-22 Gp Autolift S R L Elemento modulare a traliccio a montaggio semplificato per torri di gru a torre e torre comprendente tale elemento modulare.
EP3184479A1 (en) * 2015-12-22 2017-06-28 GP Autolift S.r.l. Simplified assembly trellis-like modular element for towers of tower cranes and tower comprising such modular element
CN109179222A (zh) * 2018-09-29 2019-01-11 温州建设集团有限公司 一种塔式起重机预埋节斜度及水平度控制施工方法
CN109179222B (zh) * 2018-09-29 2020-04-07 温州建设集团有限公司 一种塔式起重机预埋节斜度及水平度控制施工方法
CN112279120A (zh) * 2020-11-26 2021-01-29 江西省丰和泰重工科技有限公司 一种基座加强型塔式起重机

Also Published As

Publication number Publication date
CA979173A (en) 1975-12-09
AR202101A1 (es) 1975-05-15
IT986325B (it) 1975-01-30
FR2184418B1 (es) 1976-03-12
JPS545907B2 (es) 1979-03-22
DE2324184B2 (de) 1978-10-05
ES415153A1 (es) 1976-02-16
SU610485A3 (ru) 1978-06-05
FR2184418A1 (es) 1973-12-28
DE2324184C3 (de) 1979-05-31
GB1427403A (en) 1976-03-10
BR7303543D0 (pt) 1974-07-25
DE2324184A1 (de) 1973-11-29
JPS4955050A (es) 1974-05-28

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