CN201396347Y - Tension joint of circular section composite material pultruded sectional material - Google Patents

Tension joint of circular section composite material pultruded sectional material Download PDF

Info

Publication number
CN201396347Y
CN201396347Y CN2009200133224U CN200920013322U CN201396347Y CN 201396347 Y CN201396347 Y CN 201396347Y CN 2009200133224 U CN2009200133224 U CN 2009200133224U CN 200920013322 U CN200920013322 U CN 200920013322U CN 201396347 Y CN201396347 Y CN 201396347Y
Authority
CN
China
Prior art keywords
composite material
circular section
section bar
material drawing
extruding
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.)
Expired - Fee Related
Application number
CN2009200133224U
Other languages
Chinese (zh)
Inventor
祁锦明
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.)
ANSHAN YUANDA GRID ENGINEERING Co Ltd
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to CN2009200133224U priority Critical patent/CN201396347Y/en
Application granted granted Critical
Publication of CN201396347Y publication Critical patent/CN201396347Y/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Landscapes

  • Moulding By Coating Moulds (AREA)

Abstract

The utility model provides a tension joint of a circular section composite material pultruded sectional material, which comprises a circular section composite material pultruded sectional material anda tubular joint sheath, and is characterized in that a fibrous layer is uniformly arranged on the outer surface of the end part of the circular section composite material pultruded sectional material, the fibrous layer has the maximum thickness at the end of the circular section composite material pultruded sectional material, the thickness of the fibrous layer presents a tapered decreasing trendalong the axial direction of the circular section composite material pultruded sectional material, the inner diameter of the tubular joint sheath has taper, and the taper is matched with that of thefibrous layer arranged on the outer surface of the end part of the circular section composite material pultruded sectional material. The utility model has the advantages that the structure can make the inner hole of the joint sheath tightly combined with the fibrous layer uniformly arranged on the outer surface of the end part of the circular section composite material pultruded sectional material, the reliability is good, and the tensile strength is high.

Description

The tension joint of circular section composite material drawing and extruding section bar
Technical field
The utility model relates to the section bar processing technique field, the tension joint of particularly a kind of circular section composite material drawing and extruding section bar.
Background technique
The tension joint of circular section composite material drawing and extruding section bar is mainly used in the transmission longitudinal pulling force, thus to performance demands such as its intensity, endurance, reliabilities than higher.Traditional tension joint all is to adopt joint overcoat and drawing and extruding section bar crimping or bonding method to be connected the bad control of its reliability.
Summary of the invention
The purpose of this utility model is to provide a kind of good reliability, the tension joint of the circular section composite material drawing and extruding section bar that tensile strength is high.
The purpose of this utility model realizes by following technical proposals:
The tension joint of circular section of the present utility model composite material drawing and extruding section bar, comprise circular section composite material drawing and extruding section bar, the tubular configured joint overcoat, the outer surface that it is characterized in that composite material drawing and extruding section bar end, described circular section evenly is provided with layer of fibers, this layer of fibers is in the thickness maximum of composite material drawing and extruding section bar termination, circular section, its thickness successively decreases along the tapering that axially is of circular section composite material drawing and extruding section bar, the internal diameter of described tubular configured joint overcoat is the internal diameter that has tapering, and the fibrolaminar tapering of its tapering and circular section composite material drawing and extruding section bar end outer surface setting is complementary.
The outer surface of described tubular configured joint overcoat is provided with the boss in outside thread or strap bolt hole.
The hole taper of described tubular configured joint overcoat is 1: 10-1: 50, and the end diameter of this tubular configured joint overcoat endoporus is slightly larger than the external diameter of circular section composite material drawing and extruding section bar.
The layer of fibers that is arranged on the outer surface of circular section composite material drawing and extruding section bar can be that the shop is applied, and also can be to twine, and described layer of fibers is for soaking into resin fibre or fibre cloth, and its minimum thickness is 0-2mm, and maximum ga(u)ge is 4-7mm.
The material of described tubular configured joint overcoat is metal or composite material.
The utility model has the advantages that:
Owing to adopted said structure, composite material drawing and extruding section bar end outer surface is provided with the layer of fibers that has tapering in the circular section, and its tubular configured joint overcoat also is provided with the internal diameter of band tapering, and both taperings are complementary.The circular section fibrolaminar minimum thickness of composite material drawing and extruding section bar end outer surface equals the gap width between tubular configured joint overcoat internal taper hole small end and drawing and extruding section bar, its maximum ga(u)ge equals the gap width between big end of tubular configured joint overcoat internal taper hole and drawing and extruding section bar, both are combined closely, good reliability, the tensile strength height.
Description of drawings
Fig. 1 is provided with externally threaded structural representation for the outer surface of the utility model tension joint jacket tube.
Fig. 2 is provided with the structural representation of the boss in strap bolt hole for the outer surface of the utility model tension joint jacket tube.
Embodiment
The embodiment who provides below in conjunction with accompanying drawing further specifies embodiment of the present utility model.
As Fig. 1, shown in Figure 2, the tension joint of circular section of the present utility model composite material drawing and extruding section bar, comprise circular section composite material drawing and extruding section bar 1, tubular configured joint overcoat 2, the outer surface that it is characterized in that composite material drawing and extruding section bar 1 end, described circular section evenly is provided with layer of fibers 4, this layer of fibers 4 is in the thickness maximum of composite material drawing and extruding section bar termination, circular section, its thickness successively decreases along the tapering that axially is of circular section composite material drawing and extruding section bar, the internal diameter of described tubular configured joint overcoat 2 is the internal diameter that has tapering, and the tapering of the layer of fibers 4 of its tapering and circular section composite material drawing and extruding section bar 1 end outer surface setting is complementary.
The outer surface of tubular configured joint overcoat 2 described in the utility model is provided with outside thread 5, as shown in Figure 1, or the boss 3 in strap bolt hole, as shown in Figure 2, can also make other shape, its outer surface is provided with outside thread or is provided with the boss in strap bolt hole, and the tension joint of being convenient to this circular section composite material drawing and extruding section bar is connected with other member.
The hole taper of described tubular configured joint overcoat 2 is 1: 10~1: 50, and the end diameter of these tubular configured joint overcoat 2 endoporus is slightly larger than the external diameter of circular section composite material drawing and extruding section bar.
The layer of fibers 4 that is arranged on the outer surface of circular section composite material drawing and extruding section bar 1 can be that the shop is applied, and also can be to twine, and described layer of fibers is for soaking into resin fibre or fibre cloth, and its minimum thickness is 0-2mm, and maximum ga(u)ge is 4-7mm.The material of described joint overcoat 2 is metal or composite material.
Bonding firm for the infiltration resin fibre or the fibre cloth that make the shop apply or twine with drawing and extruding section bar, pretreatment can be carried out in the bonding position of drawing and extruding section bar, as adopt methods such as surperficial hacking or boring.

Claims (5)

1, the tension joint of a kind of circular section composite material drawing and extruding section bar, comprise circular section composite material drawing and extruding section bar, tubular configured joint overcoat, the outer surface that it is characterized in that composite material drawing and extruding section bar end, described circular section evenly is provided with layer of fibers, this layer of fibers is in the thickness maximum of composite material drawing and extruding section bar termination, circular section, its thickness successively decreases along the tapering that axially is of circular section composite material drawing and extruding section bar, the internal diameter of described tubular configured joint overcoat is the internal diameter that has tapering, and the fibrolaminar tapering of its tapering and circular section composite material drawing and extruding section bar end outer surface setting is complementary.
2, the tension joint of circular section according to claim 1 composite material drawing and extruding section bar is characterized in that the outer surface of described tubular configured joint overcoat is provided with the boss in outside thread or strap bolt hole.
3, the tension joint of circular section according to claim 1 and 2 composite material drawing and extruding section bar, the hole taper that it is characterized in that described tubular configured joint overcoat is 1: 10-1: 50, and the end diameter of this tubular configured joint overcoat endoporus is slightly larger than the external diameter of circular section composite material drawing and extruding section bar.
4, the tension joint of circular section according to claim 1 composite material drawing and extruding section bar, the layer of fibers that it is characterized in that being arranged on the outer surface of circular section composite material drawing and extruding section bar can be that the shop is applied, also can be to twine, described layer of fibers is for soaking into resin fibre or fibre cloth, its minimum thickness is 0-2mm, and maximum ga(u)ge is 4-7mm.
5, the tension joint of circular section according to claim 1 composite material drawing and extruding section bar, the material that it is characterized in that described joint overcoat is metal or composite material.
CN2009200133224U 2009-04-29 2009-04-29 Tension joint of circular section composite material pultruded sectional material Expired - Fee Related CN201396347Y (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN2009200133224U CN201396347Y (en) 2009-04-29 2009-04-29 Tension joint of circular section composite material pultruded sectional material

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN2009200133224U CN201396347Y (en) 2009-04-29 2009-04-29 Tension joint of circular section composite material pultruded sectional material

Publications (1)

Publication Number Publication Date
CN201396347Y true CN201396347Y (en) 2010-02-03

Family

ID=41618856

Family Applications (1)

Application Number Title Priority Date Filing Date
CN2009200133224U Expired - Fee Related CN201396347Y (en) 2009-04-29 2009-04-29 Tension joint of circular section composite material pultruded sectional material

Country Status (1)

Country Link
CN (1) CN201396347Y (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102815210A (en) * 2012-08-30 2012-12-12 同济大学 Composite-material automobile transmission shaft formed by pulling, squeezing and winding and preparation method thereof

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102815210A (en) * 2012-08-30 2012-12-12 同济大学 Composite-material automobile transmission shaft formed by pulling, squeezing and winding and preparation method thereof
CN102815210B (en) * 2012-08-30 2015-06-03 同济大学 Composite-material automobile transmission shaft formed by pulling, squeezing and winding and preparation method thereof

Similar Documents

Publication Publication Date Title
US10612568B2 (en) Connector
US9482266B2 (en) Connector for a tubular composite shaft
EP1639270B1 (en) Rope terminator
CN105143592B (en) Tube elements with composite material tube and metal connector
CN102802925A (en) Method for manufacturing composite connecting rods, and connecting rods produced according to the method
US20100122606A1 (en) Tie rod and force transmitting assembly for a tie rod
WO2017130928A1 (en) Assembly component of compressive anchor clamp, anchor structure for power-transmission line, and method for constructing compressive anchor clamp
CN101603353A (en) A kind of composite anchorage that is used for anchoring multiple fibre reinforced plastic twisted wire muscle or drag-line
CN102410153A (en) Rotor blade or rotor blade segment for a wind turbine
JP2014074655A (en) Tensile strength testing method of filament-reinforced metal matrix composite material and tensile test piece
CN101567537A (en) Strain clamp for JRLX/T carbon fiber leads
CN107447757B (en) A kind of Extruded anchoring tool and anchoring process of FRP tendons
CN201396347Y (en) Tension joint of circular section composite material pultruded sectional material
CN211714375U (en) Steel bar connecting joint of prefabricated concrete structure
CN1975185A (en) Nut assembly member for reinforced glassfiber whole-thread rockbolt
AU2011271206B2 (en) Thermoplastic composite tension member and method of manufacturing of the latter
JP3160110U (en) Retention end structure of twisted wires
RU2309848C1 (en) Composite threaded joining member
CN207234348U (en) A kind of aluminium coats carbon fiber conductor strain clamp
CN206220625U (en) The attachment structure of fibre reinforced composites transmission & distribution electric pole
CN111043115A (en) Carbon fiber composite material bearing rod and manufacturing method thereof
CN212360417U (en) Rod piece connecting end
CN218616065U (en) High-strength high-modulus spoke and rim assembly
CN105034412A (en) Connection joint between high-effective anti-fatigue composite material and metal and connection method thereof
US20230231370A1 (en) Termination arrangement for an overhead electrical cable including a tensile strain sheath

Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
ASS Succession or assignment of patent right

Owner name: ANSHAN YUANDA POWER GRID ENGINNERING CO., LTD.

Free format text: FORMER OWNER: QI JINMING

Effective date: 20110315

C41 Transfer of patent application or patent right or utility model
TR01 Transfer of patent right

Effective date of registration: 20110315

Address after: Anshan City, Liaoning Province, China Road 114031 North 337 Lishan District No. 1

Patentee after: Anshan Yuanda Grid Engineering Co., Ltd.

Address before: Anshan City, Liaoning Province, China Road 114031 North 337 Lishan District No. 1

Patentee before: Qi Jinming

C17 Cessation of patent right
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20100203

Termination date: 20120429