CN88102214A - A kind of manufacture method of trusses - Google Patents
A kind of manufacture method of trusses Download PDFInfo
- Publication number
- CN88102214A CN88102214A CN8888102214A CN88102214A CN88102214A CN 88102214 A CN88102214 A CN 88102214A CN 8888102214 A CN8888102214 A CN 8888102214A CN 88102214 A CN88102214 A CN 88102214A CN 88102214 A CN88102214 A CN 88102214A
- Authority
- CN
- China
- Prior art keywords
- flexible piece
- skeleton
- extension
- dividing plate
- make
- 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
Images
Classifications
-
- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04C—STRUCTURAL ELEMENTS; BUILDING MATERIALS
- E04C3/00—Structural elongated elements designed for load-supporting
- E04C3/02—Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces
- E04C3/29—Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces built-up from parts of different material, i.e. composite structures
-
- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04C—STRUCTURAL ELEMENTS; BUILDING MATERIALS
- E04C3/00—Structural elongated elements designed for load-supporting
- E04C3/02—Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces
- E04C3/29—Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces built-up from parts of different material, i.e. composite structures
- E04C3/291—Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces built-up from parts of different material, i.e. composite structures with apertured web
-
- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04C—STRUCTURAL ELEMENTS; BUILDING MATERIALS
- E04C3/00—Structural elongated elements designed for load-supporting
- E04C3/02—Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces
- E04C3/04—Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal
- E04C3/08—Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal with apertured web, e.g. with a web consisting of bar-like components; Honeycomb girders
-
- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04C—STRUCTURAL ELEMENTS; BUILDING MATERIALS
- E04C3/00—Structural elongated elements designed for load-supporting
- E04C3/02—Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces
- E04C3/04—Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal
- E04C2003/0404—Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal beams, girders, or joists characterised by cross-sectional aspects
- E04C2003/0408—Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal beams, girders, or joists characterised by cross-sectional aspects characterised by assembly or the cross-section
- E04C2003/0413—Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal beams, girders, or joists characterised by cross-sectional aspects characterised by assembly or the cross-section being built up from several parts
-
- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04C—STRUCTURAL ELEMENTS; BUILDING MATERIALS
- E04C3/00—Structural elongated elements designed for load-supporting
- E04C3/02—Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces
- E04C3/04—Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal
- E04C2003/0404—Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal beams, girders, or joists characterised by cross-sectional aspects
- E04C2003/0426—Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal beams, girders, or joists characterised by cross-sectional aspects characterised by material distribution in cross section
- E04C2003/0434—Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal beams, girders, or joists characterised by cross-sectional aspects characterised by material distribution in cross section the open cross-section free of enclosed cavities
-
- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04C—STRUCTURAL ELEMENTS; BUILDING MATERIALS
- E04C3/00—Structural elongated elements designed for load-supporting
- E04C3/02—Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces
- E04C3/04—Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal
- E04C2003/0404—Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal beams, girders, or joists characterised by cross-sectional aspects
- E04C2003/0443—Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal beams, girders, or joists characterised by cross-sectional aspects characterised by substantial shape of the cross-section
- E04C2003/0465—Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal beams, girders, or joists characterised by cross-sectional aspects characterised by substantial shape of the cross-section square- or rectangular-shaped
-
- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04C—STRUCTURAL ELEMENTS; BUILDING MATERIALS
- E04C3/00—Structural elongated elements designed for load-supporting
- E04C3/02—Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces
- E04C3/04—Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal
- E04C2003/0486—Truss like structures composed of separate truss elements
-
- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04C—STRUCTURAL ELEMENTS; BUILDING MATERIALS
- E04C3/00—Structural elongated elements designed for load-supporting
- E04C3/02—Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces
- E04C3/04—Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of metal
- E04C2003/0486—Truss like structures composed of separate truss elements
- E04C2003/0495—Truss like structures composed of separate truss elements the truss elements being located in several non-parallel surfaces
Landscapes
- Engineering & Computer Science (AREA)
- Architecture (AREA)
- Civil Engineering (AREA)
- Structural Engineering (AREA)
- Composite Materials (AREA)
- Chemical & Material Sciences (AREA)
- Rod-Shaped Construction Members (AREA)
- Laminated Bodies (AREA)
- External Artificial Organs (AREA)
- Glass Compositions (AREA)
- Inorganic Insulating Materials (AREA)
- Diaphragms For Electromechanical Transducers (AREA)
- Slide Fasteners, Snap Fasteners, And Hook Fasteners (AREA)
- Electrical Discharge Machining, Electrochemical Machining, And Combined Machining (AREA)
- Mechanical Treatment Of Semiconductor (AREA)
- Superconductors And Manufacturing Methods Therefor (AREA)
- Lining Or Joining Of Plastics Or The Like (AREA)
- Manufacture Of Motors, Generators (AREA)
- Moulding By Coating Moulds (AREA)
- Electronic Switches (AREA)
- Control Of El Displays (AREA)
- Ropes Or Cables (AREA)
Abstract
A kind of manufacture method of trusses.At first will make skeleton 1 around a plurality of dividing plates 2 with a plurality of extensions 4 that composite material is made.Then around skeleton twine the line 5,5 of many tensionings ', make each extension 4 in the plane of each dividing plate 2 with wherein single line contact.Line can be bonded on the skeleton subsequently, and the thermoplasticity shell of the most handy fusing line also makes the method for its cementation.In light weight and the intensity height of the beam of this manufactured.
Description
The present invention relates to a kind of manufacture method of trusses.
Trusses is made with steel or composite material usually.Girder steel intensity is high but very heavy, therefore transportation inconvenience.The higher composite material beam of intensity will be made with the instrument division system, and this will increase producing cost inevitably.And this composite material beam is solid, makes beam become overweight.The present invention attempts to provide a kind of intensity height, and is in light weight, and easy to manufacture, the trusses that cost is low.
The invention provides a kind of manufacture method of trusses, it is characterized in that may further comprise the steps:
(a) make a skeleton that comprises a plurality of extensions that separate by a plurality of plane clapboards; With
(b) then around the flexible piece of backbone winding,, extension fixes thereby being contacted in the plane of each dividing plate with one of flexible piece with many tensionings.
Preferably on skeleton, the free margins of the dividing plate between the adjacent extension is contacted with flexible piece some flexible pieces.
Preferably each flexibility is fixed on its contact point with skeleton.
Extension is preferably hollow.
The most handy thermosetting or the resin of pad plasticity and the composite material of fiber of comprising of extension is made.
Used material is advantageously selected to the modulus of elasticity that makes them, and the numerical value of Poisson's ratio and proportion belongs to the same order of magnitude.
Each flexible piece is preferably all made with conductive material, and preferably covers thereon with one deck thermoplastic.
Preferably usefulness sticks to flexible piece on the skeleton by the way of electric current thereon.
The extension spaced-apart beams made from said method is made the beam of the very light in weight of unit length.Flexible piece is pressed to dividing plate with extension and is made with extension contact in the plane of each dividing plate and keeps between them closely cooperating.The beam of making so just can be used as solid memder and is used for machinery: flexible piece bears the most of stress that acts on the beam.Therefore this beam strength is high and in light weight.And it can do quite longly, without the segmentation manufacturing.
One embodiment of the present of invention are shown in accompanying drawing, wherein:
Fig. 1 is the phantom drawing along a pipe or three dividing plates of axle arrangement;
Fig. 2 is one and comprises Fig. 1 dividing plate and axle and by giving the phantom drawing of deciding the skeleton that adds pipe that mode arranges;
Fig. 3 has the phantom drawing that first line is wrapped in Fig. 2 skeleton on the pipe;
Fig. 4 has the phantom drawing that second line is wrapped in Fig. 3 skeleton on the pipe.
From accompanying drawing as can be seen, method of the present invention is from making skeleton 1.The dividing plate made from the composite material of glass fiber and thermalplastic resin 2 is along axis or manage 3 and install with same intervals.Axle or manage 3 and be placed on the vertical rotating turntable so that be easy to approaching during fabrication.To place by its allocation that gives with the extension pipe 4 that the same compound material is made then with respect to dividing plate 2.
Then many lines 5 are decided pattern and are wrapped on the skeleton 1 by giving.This pattern can be a spirality.Every pipe 4 collinear 5 contacts in the plane of each dividing plate 2.Each limit of each dividing plate 2 is crossed by the line between the adjacent pipe 45.And then add more line 5 ' to increase the stability and the intensity of beam.After the line 5 ' also that adds twine by spirality, but preferably the direction of spiral is opposite with the direction of first line 5.After the line 5 ' also that adds in the plane of each dividing plate 2 with pipe 4 contacts, each limit of each dividing plate 2 is also by the line between the adjacent pipe 45 ' cross.
The fuse that each bar line 5,5 ' all have conductive material is done and the shell of thermoplastic.Thereby make thermoplasticity shell fusing with line 5,5 ' be bonded on the skeleton 1 by energising on fuse.Thermoplastic resin in the composite material of pipe 4 and dividing plate 2 also is melted in the contiguous zone of collinear 5,5 ' contact point.At failure of current, line 5,5 ' cooling, thermoplastic resin just stick together line 5,5 ' same pipe 4 and dividing plate 2.
Though extension recited above is hollow, the solid bar of the solid bar that operating weight is lighter or filling also are acceptable with the hollow object of foam or synthetic materials.Extension around dividing plate can be made different arrangement, and the arrangement shown in the present embodiment is an example.The present invention is not restricted to the extension with composite material, it is contemplated that the extension of thin-wall steel tube or aluminum pipe also is suitable.
Flexible piece can be with steel or other metals, or comprises the line that high-tensile nonmetallic materials such as carbon or glass fiber reinforced epoxy are made, bar or band. Flexible piece can have a plastic casing, and can be bonded on the skeleton with being different from above-mentioned method, for example, directly heats to the pad plastic housing. Flexible piece also can be fixed on the two ends of skeleton or fix by periodic interval. Fixing method can be taked any suitable mode, such as binding, welds or repeats and twine. Pattern also can adopt non-helical shape, contacts with flexible piece as long as extend in the plane of each dividing plate.
A kind ofly be applicable to that the thermoplastic resin of the shell of extension and line is to be referred to as " I is close " material (Aramid) in Sweden. Also can adopt nylon. But these just for example.
Be appreciated that with such as the single flexible spare of line and so on from one of beam around to the other end. But also can be one by one the head of flexible piece being coupled together makes it twine back and forth along its beam length.
Claims (15)
1, a kind of manufacture method of trusses is characterized in that may further comprise the steps:
(a) make a skeleton 1 that comprises a plurality of extensions 4 that separate by a plurality of plane clapboards 2 and
(b) then around skeleton 1 wind flexible piece 5,5 with many tensionings ', make extension 4 with flexible piece 5,5 ', make extension 4 with flexible piece 5, thus 5 ' one of in the plane of each dividing plate 2, contact and fix.
2, the method for claim 1 is characterized in that, flexible piece 5,5 ' in some with the contact of the free margins of the dividing plate 4 between the adjacent extension 4.
3, as the method for claim 1 or 2, it is characterized in that flexible piece 5,5 ' be fixed on the skeleton at each contact point place with skeleton 1.
4, the method for any one claim as described above is characterized in that extension 4 is hollow.
5, the method for any one claim as described above is characterized in that the material of beam should so be selected, even their modulus of elasticity (Eij), the numerical value of Poisson's ratio (Vij) and proportion (ρ) belongs to the same order of magnitude.
6, method as claimed in claim 5 is characterized in that, the material of beam should be chosen to make them to have the modulus of elasticity (Eij) of roughly the same numerical value, Poisson's ratio (Vij) and proportion (ρ).
7, method as claimed in claim 6 is characterized in that, extension 4, dividing plate 2 and flexible piece 5,5 ' all have identical materials.
8, the method for any one claim as described above is characterized in that, extension 4 is with comprising that the composite material of heat fixing character or thermoplastic resin and fiber makes.
9, the method for any one claim as described above is characterized in that, dividing plate 2 is roughly arranged equidistantly along skeleton 1.
10, the method for any one claim as described above is characterized in that each flexible piece (5,5 ') is an electric conductor.
11, the method for any one claim as described above is characterized in that, flexible piece 5,5 ' and skeleton 1 at its for the place's spot heating that crosses one another with the melting heat plastic housing, thereby with flexible piece 5,5 ' cement on the skeleton 1.
12, as any one described method in the claim 1 to 10, it is characterized in that flexible piece 5,5 ' stick on the skeleton 1 by galvanization thereon.
13, the method for any one claim as described above is characterized in that, each flexible piece 5,5 ' have shell of thermoplastic.
14, the method for any one claim as described above is characterized in that, beam is made with being installed in a dividing plate 2 on the rotatable shaft 3.
15, the produced trusses of method of aforementioned any one claim of a kind of usefulness.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB8708500 | 1987-04-09 | ||
GB08708500A GB2204614A (en) | 1987-04-09 | 1987-04-09 | Manufacture of a truss beam of composite materials |
Publications (1)
Publication Number | Publication Date |
---|---|
CN88102214A true CN88102214A (en) | 1988-10-26 |
Family
ID=10615530
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN8888102214A Pending CN88102214A (en) | 1987-04-09 | 1988-04-09 | A kind of manufacture method of trusses |
Country Status (13)
Country | Link |
---|---|
EP (1) | EP0355103B1 (en) |
JP (1) | JPH03500068A (en) |
KR (1) | KR890700726A (en) |
CN (1) | CN88102214A (en) |
AT (1) | ATE70877T1 (en) |
AU (1) | AU616887B2 (en) |
BR (1) | BR8807454A (en) |
DE (1) | DE3867235D1 (en) |
DK (1) | DK496589D0 (en) |
FI (1) | FI894791A0 (en) |
GB (1) | GB2204614A (en) |
NO (1) | NO885476L (en) |
WO (1) | WO1988008064A1 (en) |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE9312391U1 (en) * | 1993-08-14 | 1993-10-21 | Menzel, Hans-Claus, Dr., 70619 Stuttgart | Bracing the center pillar of a composite pillar |
DE29907874U1 (en) * | 1999-05-04 | 2000-09-14 | Hupperich, Werner, 53804 Much | Assembly device for building purposes |
AU782363B2 (en) * | 1999-10-21 | 2005-07-21 | Onesteel Reinforcing Pty Limited | A rollable mesh apparatus |
AUPQ356699A0 (en) * | 1999-10-21 | 1999-11-11 | Bhp Steel (Rp) Pty Ltd | A rollable mesh apparatus |
US8919071B2 (en) * | 2012-12-19 | 2014-12-30 | Patco, Llc | Truss configuration |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3501880A (en) * | 1967-11-08 | 1970-03-24 | Lawrence R Bosch | Captive column structure |
CH636929A5 (en) * | 1979-04-18 | 1983-06-30 | Pantex Stahl Ag | Lattice girder for the underground track and shaft expansion. |
US4566247A (en) * | 1983-08-03 | 1986-01-28 | Overbo Gordon I | Captive column |
DE3436882A1 (en) * | 1984-07-27 | 1986-01-30 | Burger, Frank, 8000 München | FRAME SYSTEM, ESPECIALLY FOR FRAMES AND INTERIORS |
-
1987
- 1987-04-09 GB GB08708500A patent/GB2204614A/en active Pending
-
1988
- 1988-04-09 CN CN8888102214A patent/CN88102214A/en active Pending
- 1988-04-11 DE DE8888903297T patent/DE3867235D1/en not_active Expired - Fee Related
- 1988-04-11 JP JP63503063A patent/JPH03500068A/en active Pending
- 1988-04-11 AU AU15779/88A patent/AU616887B2/en not_active Ceased
- 1988-04-11 WO PCT/GB1988/000279 patent/WO1988008064A1/en active IP Right Grant
- 1988-04-11 EP EP88903297A patent/EP0355103B1/en not_active Expired - Lifetime
- 1988-04-11 BR BR888807454A patent/BR8807454A/en unknown
- 1988-04-11 AT AT88903297T patent/ATE70877T1/en not_active IP Right Cessation
- 1988-12-08 KR KR1019880701625A patent/KR890700726A/en not_active Application Discontinuation
- 1988-12-09 NO NO88885476A patent/NO885476L/en unknown
-
1989
- 1989-10-06 DK DK496589A patent/DK496589D0/en not_active Application Discontinuation
- 1989-10-09 FI FI894791A patent/FI894791A0/en not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
GB8708500D0 (en) | 1987-05-13 |
NO885476L (en) | 1989-02-01 |
DK496589A (en) | 1989-10-06 |
AU616887B2 (en) | 1991-11-14 |
JPH03500068A (en) | 1991-01-10 |
BR8807454A (en) | 1990-05-15 |
NO885476D0 (en) | 1988-12-09 |
EP0355103B1 (en) | 1991-12-27 |
DK496589D0 (en) | 1989-10-06 |
WO1988008064A1 (en) | 1988-10-20 |
DE3867235D1 (en) | 1992-02-06 |
FI894791A0 (en) | 1989-10-09 |
GB2204614A (en) | 1988-11-16 |
EP0355103A1 (en) | 1990-02-28 |
ATE70877T1 (en) | 1992-01-15 |
AU1577988A (en) | 1988-11-04 |
KR890700726A (en) | 1989-04-27 |
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C06 | Publication | ||
PB01 | Publication | ||
C10 | Entry into substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
C01 | Deemed withdrawal of patent application (patent law 1993) | ||
WD01 | Invention patent application deemed withdrawn after publication |