CN105276310A - Hoop type connecting structure for composite thin-walled circular pipes - Google Patents
Hoop type connecting structure for composite thin-walled circular pipes Download PDFInfo
- Publication number
- CN105276310A CN105276310A CN201510699420.8A CN201510699420A CN105276310A CN 105276310 A CN105276310 A CN 105276310A CN 201510699420 A CN201510699420 A CN 201510699420A CN 105276310 A CN105276310 A CN 105276310A
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- Prior art keywords
- draw
- groove
- flanges
- width
- flange
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16L—PIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
- F16L21/00—Joints with sleeve or socket
- F16L21/06—Joints with sleeve or socket with a divided sleeve or ring clamping around the pipe-ends
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16L—PIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
- F16L23/00—Flanged joints
- F16L23/04—Flanged joints the flanges being connected by members tensioned in the radial plane
Abstract
The invention provides a hoop type connecting structure for composite thin-walled circular pipes, and belongs to the technical field of composite connection. The problems existing in connection of the composite thin-walled circular pipes at present are solved. The hoop type connecting structure comprises the two pipes to be connected, and is characterized in that butt-joint ports of the two pipes to be connected are each provided with a flange, and the two flanges are in butt joint; two opposite hoops are arranged around the flanges, and the two hoops are connected through two or more bolts; clamping grooves in tight fit with the two flanges are formed in the inner sides of the two hoops respectively, two parallel planes are arranged on the two opposite sides of each flange respectively, and the two ends of each clamping groove are matched with the planes in shape. The hoop type connecting structure is used for connecting the composite thin-walled circular pipes.
Description
Technical field
The invention belongs to composite material interconnection technique field, be specifically related to a kind of clamp band type linkage structure for composite material thin wall pipe.
Background technique
Composite material is widely used in high-tech areas such as aircraft manufacturings, and along with the continuous progress of composite material theoretical research and moulding process, the overall performance of composite material is greatly improved.But, due to by composite products shaping technical merit restriction and practical application need, composite products certainly exists certain structure parting surface and production breakdown interface, so inevitably there is a large amount of connection parts in composite structure, and the connection part of composite material is the integrally-built weak link of composite products always, affect giving full play to of composite material excellent specific property, therefore according to function and the service condition of composite products, analyse in depth the connection performance of composite material, rationally and neatly apply Connecting format and the method for composite material, improve composite products overall construction intensity, alleviate composite products overall weight, give full play to one of important channel of composite material excellent specific property.
The connection of current composite material thin wall pipe adopts bolt flange formula to connect, and it is that the flange being fastened by bolts two thin-wall circular tube ports connects to realize pipe that bolt flange formula connects, and this Placement exists following shortcoming:
1. have different strategies when mounting and dismounting bolt, needed time is long, and therefore installing/dismounting efficiency is lower;
2. need to carry out the secondary mechanical processing process such as perforate, except increasing labor intensity and except man-hour, also easy thin-wall circular tube to be caused damage, the reduction of thin-wall circular tube performance is even damaged;
3. flange width needed for is comparatively large, in the confined spaces such as wing, need could realize the connection of bolt flange formula, reduce the performances such as thin-wall circular tube flexural rigidity, and weight accounting is also large by reducing thin-wall circular tube diameter.
Visible, the joint efficiency of current composite material thin wall pipe is low, and effect is undesirable, needs to improve.
Summary of the invention
The object of the invention is the problems referred to above that the connection in order to solve current composite material thin wall pipe exists, provide a kind of clamp band type linkage structure for composite material thin wall pipe, its technological scheme is as follows:
A kind of clamp band type linkage structure for composite material thin wall pipe, it comprises two and waits to take over, flange is respectively arranged with at two craft port places to be taken over, two flange docking, around two flanges, two relative clips are set, two clips are connected by two or more bolt, are provided with and two friction tight draw-in grooves of flange inside two clips; In order to improve the anti-twisting property of linkage structure, arrange a plane be parallel to each other respectively in the relative both sides of each flange, accordingly, the shape at each draw-in groove two ends matches with described plane.
Beneficial effect of the present invention is: be connected firmly, and anti-twisting property is strong; Each parts can time processing shaping, avoid the secondary operations process such as perforate, connect simple and convenient, can not cause damage to thin-wall circular tube, make pipe fitting keep primary characteristic, improve dismounting efficiency and Security; Obviously can reduce the width of flange, the more current Placement of integral diameter obviously reduces, and is applicable in wing or other confined spaces.
accompanying drawing illustrates:
Fig. 1 is overall structure schematic diagram of the present invention;
Fig. 2 is the exploded view of Fig. 1;
Fig. 3 is the side view of Fig. 1;
Fig. 4 is the schematic cross-section of flange;
Fig. 5 is the schematic cross-section of clip;
Fig. 6 is the schematic diagram of embodiment one;
Fig. 7 is the schematic diagram of embodiment two;
Fig. 8 is the schematic diagram of embodiment three;
Fig. 9 is the schematic diagram of optimal way one.
embodiment:
Below in conjunction with accompanying drawing, technological scheme of the present invention is further described; but be not limited thereto; everyly technical solution of the present invention modified or equivalent to replace, and not departing from the spirit and scope of technical solution of the present invention, all should be encompassed in protection scope of the present invention.
Referring to figs. 1 through Fig. 9, a kind of clamp band type linkage structure for composite material thin wall pipe, it comprises two and treats adapter 1, treat that the craft port place of adapter 1 is respectively arranged with flange 2 at two, two flanges 2 dock, arrange two relative clip 3, two clips 3 around two flanges 2 to be connected by two or more bolt 4, be provided with inside two clips 3 and two friction tight draw-in groove 3-1 of flange 2; In order to improve the anti-twisting property of linkage structure, arrange a plane 2-1 be parallel to each other respectively in the relative both sides of each flange 2, accordingly, the shape at each draw-in groove 3-1 two ends matches with described plane 2-1.
Embodiment one, the apparent surface 2-2 of described two flanges 2 all with the axes normal of two flanges 2, described two flanges 2 are gradually thin to edge 2-4 by root 2-3, namely when the edge 2-4 thickness of two flanges 2 is all greater than zero, the cross section of two flanges 2 is right-angled trapezium, and the transverse cross-sectional combinations of two flanges 2 is isosceles trapezoid; When the edge 2-4 thickness of two flanges 2 is equal to zero, the cross section of two flanges 2 is right-angled triangle, and the transverse cross-sectional combinations of two flanges 2 is isosceles triangle; Accordingly, the degree of depth of draw-in groove 3-1 is more than or equal to the width of flange 2, the width of draw-in groove mouth 3-1-1 is less than the total thickness of two flange 2 root 2-3, the width of draw-in groove 3-1 by 3-1-2 bottom draw-in groove mouth 3-1-1 to draw-in groove gradually little (as in Fig. 6 a), or the width of draw-in groove 3-1 by the width of 3-1-2 bottom draw-in groove mouth 3-1-1 to draw-in groove equal (as in Fig. 6 b).
Embodiment two, there are special circumstances, the apparent surface 2-2 of described two flanges 2 all with the axes normal of two flanges 2, described two flanges 2 are gradually thin to edge 2-4 by root 2-3, the edge 2-4 thickness of two flanges 2 is equal to zero, namely the cross section of two flanges 2 is right-angled triangle, the transverse cross-sectional combinations of two flanges 2 is isosceles triangle, the width of draw-in groove 3-1 is gradually little by 3-1-2 bottom draw-in groove mouth 3-1-1 to draw-in groove, the bottom width of draw-in groove 3-1 is zero, namely the bottom of draw-in groove 3-1 is wedge angle, the width of draw-in groove mouth 3-1-1 is less than the total thickness of two flange 2 root 2-3, namely the cross section of draw-in groove 3-1 is isosceles triangle, and the waist of the isosceles triangle of the transverse cross-sectional combinations of two flanges 2 is identical with the waist angle of inclination of the cross section of draw-in groove 3-1, the degree of depth of this situation draw-in groove 3-1 must be less than the width of flange 2, and bottom draw-in groove 3-1-2 and two flange 2 combine after wedge angle coincide, so 3-1-2 setting deep trouth 3-1-3 will be added bottom draw-in groove, to ensure that two flanges 2 can be subject to larger opposing compression power.
Embodiment three, the apparent surface 2-2 of described two flanges 2 all with the axes normal of two flanges 2, described two flanges 2 are equal to the thickness of edge 2-4 by root 2-3, and namely the cross section of two flanges 2 is square, and the combination of the cross section of two flanges 2 is also square; Accordingly, the width of draw-in groove 3-1 is gradually little by 3-1-2 bottom draw-in groove mouth 3-1-1 to draw-in groove, namely the cross section of draw-in groove 3-1 is isosceles trapezoid or isosceles triangle, the width of draw-in groove mouth 3-1-1 is greater than the total thickness of two flange 2 edge 2-4, and bottom draw-in groove, the width of 3-1-2 is less than the total thickness of two flange 2 edge 2-4.
Optimal way one, the apparent surface 2-2 of described two flanges 2 all with the axes normal of two flanges 2, described two flanges 2 are gradually thin to edge 2-4 by root 2-3, the edge 2-4 thickness of two flanges 2 is all greater than zero, namely the cross section of two flanges 2 is right-angled trapezium, the transverse cross-sectional combinations of two flanges 2 is isosceles trapezoid, the width of draw-in groove mouth 3-1-1 is less than the total thickness of two flange 2 root 2-3, the degree of depth of draw-in groove 3-1 is more than or equal to the width of flange 2, the width of draw-in groove 3-1 is gradually little by 3-1-2 bottom draw-in groove mouth 3-1-1 to draw-in groove, the bottom width of draw-in groove 3-1 is greater than zero, namely the cross section of draw-in groove 3-1 is isosceles trapezoid, and the waist of the isosceles trapezoid of the transverse cross-sectional combinations of two flanges 2 is identical with the waist angle of inclination of the cross section of draw-in groove 3-1, contact with face between clip 3 with flange 2 when this is arranged, linkage structure is the most stable.
Optimal way two, the waist of described whole isosceles trapezoid and isosceles triangle is 5 degree of-30 degree relative to the angle that the apparent surface 2-2 of two flanges 2 tilts.
Claims (3)
1. the clamp band type linkage structure for composite material thin wall pipe, it comprises two and waits to take over (1), it is characterized in that waiting that the craft port place taking over (1) is respectively arranged with flange (2) at two, two flange (2) docking, around two flanges (2), two relative clips (3) are set, two clips (3) are connected by two or more bolt (4), be provided with and two the friction tight draw-in groove of flanges (2) (3-1) two clip (3) inner sides, a plane be parallel to each other (2-1) is set respectively in the relative both sides of each flange (2), the shape at each draw-in groove (3-1) two ends matches with described plane (2-1).
2. a kind of clamp band type linkage structure for composite material thin wall pipe as claimed in claim 1, the apparent surface (2-2) that it is characterized in that described two flanges (2) all with the axes normal of two flanges (2), described two flanges (2) are gradually thin to edge (2-4) by root (2-3), the degree of depth of draw-in groove (3-1) is more than or equal to the width of flange (2), the width of draw-in groove mouth (3-1-1) is less than the total thickness of two flanges (2) root (2-3), the width of draw-in groove (3-1) is gradually little by (3-1-2) bottom draw-in groove mouth (3-1-1) to draw-in groove, or the width of draw-in groove (3-1) is equal by the width of (3-1-2) bottom draw-in groove mouth (3-1-1) to draw-in groove.
3. a kind of clamp band type linkage structure for composite material thin wall pipe as claimed in claim 1, the apparent surface (2-2) that it is characterized in that described two flanges (2) all with the axes normal of two flanges (2), described two flanges (2) are gradually thin to edge (2-4) by root (2-3), edge (2-4) thickness of two flanges (2) is all greater than zero, the width of draw-in groove mouth (3-1-1) is less than the total thickness of two flanges (2) root (2-3), the degree of depth of draw-in groove (3-1) is more than or equal to the width of flange (2), the width of draw-in groove (3-1) is gradually little by (3-1-2) bottom draw-in groove mouth (3-1-1) to draw-in groove, the bottom width of draw-in groove (3-1) is greater than zero, and the waist of the isosceles trapezoid of the transverse cross-sectional combinations of two flanges (2) is identical with the waist angle of inclination of the cross section of draw-in groove (3-1).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN201510699420.8A CN105276310A (en) | 2015-10-26 | 2015-10-26 | Hoop type connecting structure for composite thin-walled circular pipes |
Applications Claiming Priority (1)
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CN201510699420.8A CN105276310A (en) | 2015-10-26 | 2015-10-26 | Hoop type connecting structure for composite thin-walled circular pipes |
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CN105276310A true CN105276310A (en) | 2016-01-27 |
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CN201510699420.8A Pending CN105276310A (en) | 2015-10-26 | 2015-10-26 | Hoop type connecting structure for composite thin-walled circular pipes |
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Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109185578A (en) * | 2018-09-25 | 2019-01-11 | 大连翼方科技有限公司 | A kind of hospital sewage high-efficient treatment device and method |
CN109322734A (en) * | 2018-11-02 | 2019-02-12 | 中国航空工业集团公司西安飞机设计研究所 | A kind of aircrafts exhaust pipe structure and reinforce clip |
CN112705565A (en) * | 2020-12-08 | 2021-04-27 | 江苏维诗环境科技有限公司 | Soil remediation system based on gas thermal desorption coupling bioremediation |
CN113007598A (en) * | 2021-02-20 | 2021-06-22 | 南华大学 | High-pressure gas preparation device |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
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CN2224322Y (en) * | 1995-07-07 | 1996-04-10 | 中国核动力研究设计院第二研究所 | Fastening-hoop type seal coupling mechanism for high-temp. high-pressure pipeline |
CA2707844A1 (en) * | 2007-12-05 | 2009-06-04 | Paul Brian Fahie | Lock for cam-and-groove coupler |
DE202009018707U1 (en) * | 2009-05-12 | 2012-11-26 | Hnp Mikrosysteme Gmbh | Pipe connection system |
CN103822034A (en) * | 2014-02-27 | 2014-05-28 | 苏氏工业科学技术(北京)有限公司 | Sealing hoop and connecting structure that sealing hoop connects flange plate |
-
2015
- 2015-10-26 CN CN201510699420.8A patent/CN105276310A/en active Pending
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN2224322Y (en) * | 1995-07-07 | 1996-04-10 | 中国核动力研究设计院第二研究所 | Fastening-hoop type seal coupling mechanism for high-temp. high-pressure pipeline |
CA2707844A1 (en) * | 2007-12-05 | 2009-06-04 | Paul Brian Fahie | Lock for cam-and-groove coupler |
DE202009018707U1 (en) * | 2009-05-12 | 2012-11-26 | Hnp Mikrosysteme Gmbh | Pipe connection system |
CN103822034A (en) * | 2014-02-27 | 2014-05-28 | 苏氏工业科学技术(北京)有限公司 | Sealing hoop and connecting structure that sealing hoop connects flange plate |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109185578A (en) * | 2018-09-25 | 2019-01-11 | 大连翼方科技有限公司 | A kind of hospital sewage high-efficient treatment device and method |
CN109322734A (en) * | 2018-11-02 | 2019-02-12 | 中国航空工业集团公司西安飞机设计研究所 | A kind of aircrafts exhaust pipe structure and reinforce clip |
CN112705565A (en) * | 2020-12-08 | 2021-04-27 | 江苏维诗环境科技有限公司 | Soil remediation system based on gas thermal desorption coupling bioremediation |
CN113007598A (en) * | 2021-02-20 | 2021-06-22 | 南华大学 | High-pressure gas preparation device |
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