CN105423022B - A kind of major diameter abutted flange structure - Google Patents

A kind of major diameter abutted flange structure Download PDF

Info

Publication number
CN105423022B
CN105423022B CN201410458361.0A CN201410458361A CN105423022B CN 105423022 B CN105423022 B CN 105423022B CN 201410458361 A CN201410458361 A CN 201410458361A CN 105423022 B CN105423022 B CN 105423022B
Authority
CN
China
Prior art keywords
butt joint
ring
groove
circular cone
fixedly connected
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.)
Active
Application number
CN201410458361.0A
Other languages
Chinese (zh)
Other versions
CN105423022A (en
Inventor
彭伟斌
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.)
China Academy of Launch Vehicle Technology CALT
Beijing Institute of Astronautical Systems Engineering
Original Assignee
China Academy of Launch Vehicle Technology CALT
Beijing Institute of Astronautical Systems Engineering
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 China Academy of Launch Vehicle Technology CALT, Beijing Institute of Astronautical Systems Engineering filed Critical China Academy of Launch Vehicle Technology CALT
Priority to CN201410458361.0A priority Critical patent/CN105423022B/en
Publication of CN105423022A publication Critical patent/CN105423022A/en
Application granted granted Critical
Publication of CN105423022B publication Critical patent/CN105423022B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Abstract

The present invention relates to tank major diameter abutted flange technical field, specifically related to a kind of major diameter abutted flange structure, purpose is solved using conventional abutted flange structure, and the stress at flange and store-vessel bottom butt weld is big in surfaces externally and internally gap, the problem of floor loading capability is poor.Characterized in that, it includes butt joint ring (1), weakens groove (2), circular cone reinforcing ring (3) and butt end (4);Circular cone reinforcing ring (3) upper end is fixedly connected with butt end (4), and lower end outside is fixedly connected with weakening groove (2);Butt joint ring (1) is fixedly connected on the outside of weakening groove (2);Docking circumferential weld (5) is fixedly connected on the outside of butt joint ring (1), and flange arrangement is fixedly connected entirely through docking circumferential weld (5) with bottom.After the present invention, abutted flange and bottom to dock circumferential weld (5) surfaces externally and internally stress basically identical, improve the bearing capacity more than 30% of weld seam at this;The present invention also significantly reduces improving cost.

Description

A kind of major diameter abutted flange structure
Technical field
The present invention relates to tank major diameter abutted flange technical field, and in particular to a kind of major diameter abutted flange knot Structure.
Background technology
In tank repropellenting release and gas input discharge etc. be all by the flange on tank to it is related Pipeline joint provides passage.As shown in figure 1, abutted flange refers to that the butt joint ring of flange is identical with the bus of store-vessel bottom, lead to The perforate in bottom is crossed, the connection with abutted flange and store-vessel bottom is realized by the way of butt welding.
Tank bears internal pressure in the course of the work, in abutted flange and bottom joint, there is rigidity effect, opening effect Should, stress is complicated caused by weld material reduction, generally non-membrane stress herein.Using conventional abutted flange structure, Stress at flange with bottom butt weld is larger in surfaces externally and internally gap, there is significant extra bending moment effect, serious shadow Ring floor loading capability.
The content of the invention
Present invention aim to address using conventional abutted flange structure, at flange and store-vessel bottom butt weld Stress is big in surfaces externally and internally gap, and the problem of floor loading capability is poor is eliminated caused by existing abutted flange there is provided a kind of Circumferential weld additional bending moment is docked, the approximate membrane stress state for the commissure that achieves a butt joint improves the major diameter pair of structural-load-carrying capacity Acting flange structure.
What the present invention was realized in:
A kind of major diameter abutted flange structure, including butt joint ring, weakening groove, circular cone reinforcing ring and butt end;Circular cone is strengthened Ring upper end is fixedly connected with butt end, and lower end outside is fixedly connected with weakening groove;Butt joint ring is fixedly connected on the outside of weakening groove;It is right The outside that circumferential weld is fixedly connected on butt joint ring is connect, flange arrangement is fixedly connected entirely through docking circumferential weld with bottom.
Butt joint ring generally annular plate-like as described above, cross section is rectangle, for being connected with docking circumferential weld.
The groove as described above that weakens is that reeded annular slab is opened in upper end, weakens the thickness few 1 of the thickness ratio butt joint ring of groove To 4mm, weakening groove is used to reduce the stress born at docking circumferential weld.
Circular cone reinforcing ring as described above generally ring-type, cross section is taper, and cone angle A is 10 ° to 50 °;Circular cone is strengthened Ring is used to stress concentration caused by opening effect being transferred at circular cone reinforcing ring by docking circumferential weld position, improves flange arrangement Integrated carrying ability.
The thickness of butt joint ring as described above is 6.2mm, and the width La of butt joint ring is 25mm, and the width Lb for weakening groove is 26mm, the thickness for weakening groove is 4.2mm, and the cone angle A of circular cone reinforcing ring is 18.4 °.
Described butt joint ring, weakening groove, circular cone reinforcing ring and butt end uses stainless steel material or aluminum alloy materials system Into.
The beneficial effects of the invention are as follows:
The present invention includes butt joint ring, weakens groove, circular cone reinforcing ring and butt end.After the present invention, abutted flange and case The docking circumferential weld 5 at bottom is basically identical for surfaces externally and internally stress away from significantly improving by original surfaces externally and internally stress difference, approximately realizes Membrane stress state, improves the bearing capacity more than 30% of weld seam at this;The present invention can utilize conventional welding tooling, machining equipment To realize Product processing, improving cost is reduced.
Brief description of the drawings
Fig. 1 is existing store-vessel bottom and abutted flange structural representation;
Fig. 2 is store-vessel bottom and a kind of major diameter abutted flange section of structure of the present invention;
Fig. 3 is a kind of major diameter abutted flange structural representation of the invention;
Fig. 4 is a kind of major diameter abutted flange structure partial view I of the invention;
Fig. 5 is existing abutted flange partial view I.
Wherein:1. butt joint ring, 2. weaken groove, 3. circular cone reinforcing rings, 4. butt ends, 5. docking circumferential welds.
Embodiment
The present invention is described further with reference to the accompanying drawings and examples.
As shown in Figures 2 and 3, a kind of major diameter abutted flange structure, including butt joint ring 1, weakening groove 2, circular cone reinforcing ring 3 With butt end 4.The upper end of circular cone reinforcing ring 3 is fixedly connected with butt end 4, and lower end outside is fixedly connected with weakening groove 2.Butt joint ring 1 It is fixedly connected on the outside of weakening groove 2.Docking circumferential weld 5 is fixedly connected on the outside of butt joint ring 1, and flange arrangement is entirely through butt joint ring Seam 5 is fixedly connected with bottom.
The generally annular plate-like of butt joint ring 1, cross section is rectangle, for being connected with docking circumferential weld 5.
It is that reeded annular slab is opened in upper end to weaken groove 2, weakens the thickness few 1 of thickness ratio butt joint ring 1 of groove 2 to 4mm, cuts Weak groove 2 is used to reduce the stress born at docking circumferential weld 5.
As shown in figure 4, the generally ring-type of circular cone reinforcing ring 3, cross section is taper, cone angle A is 10 ° to 50 °.Circular cone is strengthened Ring 3 is used to stress concentration caused by opening effect being transferred at circular cone reinforcing ring 3 by the position of docking circumferential weld 5, improves flange The integrated carrying ability of structure.
Butt end 4 uses the universal architecture of flange butt end.
Butt joint ring 1, weakening groove 2, circular cone reinforcing ring 3 and butt end 4 are made of stainless steel material or aluminum alloy materials.
By the bottom of 6m diameters exemplified by internal pressure 0.78MPa is born, the outer diameter D of abutted flange is 300mm, and internal diameter d is 180mm, the thickness of butt joint ring 1 is 6.2mm, and the width La of butt joint ring 1 is 25mm, and the width Lb for weakening groove 2 is 26mm, weakens groove 2 thickness is 4.2mm, and the cone angle A of circular cone reinforcing ring 3 is 18.4 °, and this parameter causes the stress docked at circumferential weld 5 approximately to meet Membrane stress requirement.
The present invention includes butt joint ring, weakens groove, circular cone reinforcing ring and butt end.After the present invention, abutted flange and case The docking circumferential weld 5 at bottom is basically identical for surfaces externally and internally stress away from significantly improving by original surfaces externally and internally stress difference, approximately realizes Membrane stress state, improves the bearing capacity more than 30% of weld seam at this;The present invention can utilize conventional welding tooling, machining equipment To realize Product processing, improving cost is reduced.

Claims (4)

1. a kind of major diameter abutted flange structure, it is characterised in that:It includes butt joint ring (1), weakens groove (2), circular cone reinforcing ring And butt end (4) (3);Circular cone reinforcing ring (3) upper end is fixedly connected with butt end (4), and lower end outside is with weakening the fixed company of groove (2) Connect;Butt joint ring (1) is fixedly connected on the outside of weakening groove (2);Docking circumferential weld (5) is fixedly connected on the outside of butt joint ring (1), flange Structure is fixedly connected entirely through docking circumferential weld (5) with bottom;
Described butt joint ring (1) generally annular plate-like, cross section is rectangle, for being connected with docking circumferential weld (5);
Described weakening groove (2) is that reeded annular slab is opened in upper end, weakens the thickness few 1 of the thickness ratio butt joint ring (1) of groove (2) To 4mm, weakening groove (2) is used to reduce the stress that docking circumferential weld (5) place is born.
2. major diameter abutted flange structure according to claim 1, it is characterised in that:Described circular cone reinforcing ring (3) is whole Body is ring-type, and cross section is taper, and cone angle A is 10 ° to 50 °;Circular cone reinforcing ring (3) is used for stress collection caused by opening effect In circular cone reinforcing ring (3) place is transferred to by docking circumferential weld (5) position, improve the integrated carrying ability of flange arrangement.
3. major diameter abutted flange structure according to claim 1, it is characterised in that:The thickness of described butt joint ring (1) For 6.2mm, the width La of butt joint ring (1) is 25mm, and the width Lb for weakening groove (2) is 26mm, and the thickness for weakening groove (2) is 4.2mm, the cone angle A of circular cone reinforcing ring (3) is 18.4 °.
4. the major diameter abutted flange structure according to claim 1-3 any one, it is characterised in that:Described butt joint ring (1), weaken groove (2), circular cone reinforcing ring (3) and butt end (4) to be made of stainless steel material or aluminum alloy materials.
CN201410458361.0A 2014-09-10 2014-09-10 A kind of major diameter abutted flange structure Active CN105423022B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201410458361.0A CN105423022B (en) 2014-09-10 2014-09-10 A kind of major diameter abutted flange structure

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201410458361.0A CN105423022B (en) 2014-09-10 2014-09-10 A kind of major diameter abutted flange structure

Publications (2)

Publication Number Publication Date
CN105423022A CN105423022A (en) 2016-03-23
CN105423022B true CN105423022B (en) 2017-08-25

Family

ID=55501443

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201410458361.0A Active CN105423022B (en) 2014-09-10 2014-09-10 A kind of major diameter abutted flange structure

Country Status (1)

Country Link
CN (1) CN105423022B (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109798203B (en) * 2019-02-18 2023-10-03 北京星际荣耀空间科技有限公司 Storage tank bottom structure and connection structure of storage tank bottom and engine

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2873425A1 (en) * 2004-07-23 2006-01-27 Faurecia Sys Echappement Exhaust gas pipe fixation device for internal combustion engine of motor vehicle, has flange cooperating with stainless steel pipe end, counter flange integrated to cylinder head, and unit assuring flange and counter flange pre-assembling
US7107662B1 (en) * 2000-12-21 2006-09-19 Gene W. Arant, as Trustee Method and a coupler for joining two steel pipes
CN201159351Y (en) * 2008-02-20 2008-12-03 江阴市恒润法兰有限公司 Welding neck flange especially for wind power nuclear power
CN202302429U (en) * 2011-11-08 2012-07-04 徐小玲 Novel flange plate
CN103453252A (en) * 2013-09-17 2013-12-18 江阴中南重工股份有限公司 Flange for pipeline connection
CN203585318U (en) * 2013-11-28 2014-05-07 上海航天精密机械研究所 Sealing flange for low-temperature tank cabin-crossing test

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102008063296A1 (en) * 2008-12-29 2010-07-01 Erhard Gmbh & Co. Kg Method for producing a loose flange and fitting with at least one pipe section and with a loose flange

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7107662B1 (en) * 2000-12-21 2006-09-19 Gene W. Arant, as Trustee Method and a coupler for joining two steel pipes
FR2873425A1 (en) * 2004-07-23 2006-01-27 Faurecia Sys Echappement Exhaust gas pipe fixation device for internal combustion engine of motor vehicle, has flange cooperating with stainless steel pipe end, counter flange integrated to cylinder head, and unit assuring flange and counter flange pre-assembling
CN201159351Y (en) * 2008-02-20 2008-12-03 江阴市恒润法兰有限公司 Welding neck flange especially for wind power nuclear power
CN202302429U (en) * 2011-11-08 2012-07-04 徐小玲 Novel flange plate
CN103453252A (en) * 2013-09-17 2013-12-18 江阴中南重工股份有限公司 Flange for pipeline connection
CN203585318U (en) * 2013-11-28 2014-05-07 上海航天精密机械研究所 Sealing flange for low-temperature tank cabin-crossing test

Also Published As

Publication number Publication date
CN105423022A (en) 2016-03-23

Similar Documents

Publication Publication Date Title
CN201824062U (en) Steel pipe adopting a space curve butt-welded seam
CN105423022B (en) A kind of major diameter abutted flange structure
US9873165B2 (en) Piston rod manufacturing method
CN105033417A (en) X80 steel pipe welding process
US20120160899A1 (en) Piston rod manufacturing method
CN205684968U (en) A kind of pipeline assembly welding docking aid
CN105171347B (en) The field installation process of experimental cabin
JP5538079B2 (en) Clad steel material joining method and structure
CN105179688B (en) Pressure vessel fixture block connection fastening structure
CN110697653A (en) Safety structure for improving reliability of high-temperature collecting furnace tube and operation method
CN206216096U (en) One kind welding back of the body gas shielded device
CN207402004U (en) A kind of lined composite steel tube socket joint welding system
CN102410412A (en) Cu-Al pipe joint
CN103042365A (en) Manufacturing method of spiral wound flange
CN201866431U (en) Concentric reducer
CN205446768U (en) Quick change collection dress disk seat formula material transfer valve
CN202992156U (en) Conical head
CN205978433U (en) Flexible graphite metal ripples tooth composite gasket
CN205446759U (en) Oblique stressed joint loop formula material transfer valve
CN103752996B (en) Two annular workpieces butt-joint process
CN213929839U (en) Gas safety conveying pipeline
CN103133790A (en) Butt welding galvanized elbow
CN103920977A (en) Welding missing control device and welding missing control method for butt welding seams of guide pipes in complicated spatial orientation
CN101954545B (en) Method for welding crimped rim of pipeline connecting piece
WO2012174868A1 (en) Hydraulic test apparatus for large-diameter thick-wall pipe connector and hydraulic test method thereof

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant