GB2123526A - Valve member for a butterfly valve - Google Patents

Valve member for a butterfly valve Download PDF

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Publication number
GB2123526A
GB2123526A GB08309613A GB8309613A GB2123526A GB 2123526 A GB2123526 A GB 2123526A GB 08309613 A GB08309613 A GB 08309613A GB 8309613 A GB8309613 A GB 8309613A GB 2123526 A GB2123526 A GB 2123526A
Authority
GB
United Kingdom
Prior art keywords
disc
valve member
valve
load
equalising
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.)
Withdrawn
Application number
GB08309613A
Other versions
GB8309613D0 (en
Inventor
George Aubrey Felton
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.)
AMBA TOOLS Ltd
Original Assignee
AMBA TOOLS Ltd
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 AMBA TOOLS Ltd filed Critical AMBA TOOLS Ltd
Priority to GB08309613A priority Critical patent/GB2123526A/en
Publication of GB8309613D0 publication Critical patent/GB8309613D0/en
Priority to DE19833324442 priority patent/DE3324442A1/en
Publication of GB2123526A publication Critical patent/GB2123526A/en
Withdrawn legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16KVALVES; TAPS; COCKS; ACTUATING-FLOATS; DEVICES FOR VENTING OR AERATING
    • F16K1/00Lift valves or globe valves, i.e. cut-off apparatus with closure members having at least a component of their opening and closing motion perpendicular to the closing faces
    • F16K1/16Lift valves or globe valves, i.e. cut-off apparatus with closure members having at least a component of their opening and closing motion perpendicular to the closing faces with pivoted closure-members
    • F16K1/18Lift valves or globe valves, i.e. cut-off apparatus with closure members having at least a component of their opening and closing motion perpendicular to the closing faces with pivoted closure-members with pivoted discs or flaps
    • F16K1/22Lift valves or globe valves, i.e. cut-off apparatus with closure members having at least a component of their opening and closing motion perpendicular to the closing faces with pivoted closure-members with pivoted discs or flaps with axis of rotation crossing the valve member, e.g. butterfly valves

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Lift Valve (AREA)

Abstract

The valve member comprises a sealing disc (1) having opposed trunnions (2) at or adjacent one face of the disc to provide an offset axis of rotation for said disc within the valve body (5), and a load-equalising member (3) connecting the trunnions to provide, in combination with said disc, an anti-deformation arrangement which, in use, restricts flexing of said disc. Preferably the valve member is designed so that the fluid flow is towards that face of the disc opposite to said one face, in which case, said load-equalising member acts in tension. Said load-equalising member is preferably of fixed construction, e.g. a flat plate (3), and may incorporate means (7) Fig. 3, (not shown) for preloading. <IMAGE>

Description

SPECIFICATION Improved valve member for a butterfly valve In the design of valves for the control of fluids one of the most important considerations is to minimise friction losses through the valve when fully open to fluid flow. As all such losses are directly proportional to the power required to pump the fluid through the appliance it has prime economic importance.
A common type of valve used for fluid control in large pipelines is known as the butterfly type. This valve consists essentially of a pivoted disc rotatable by a shaft which obdurates a circular hole formed by a ring casing of diameter approximately equal to that of the pipeline into which the assembly is fitted. It will be apparent that when the pivoted disc member is fully open, i.e. lying along the horizontal axis of the pipeline, it's frictional resistance will be a function of the frontal area presented by the disc in this position.
It is likewise evident that the smaller the area or blockage presented, the lower will be the friction losses and it is the aim in the design of such valves to achieve a minimum blockage. However, the attainment of this desirable feature is generally inconsistent with the structural forms necessary to provide a closure member when the disc is In the closed position at 900 to the open position. At this position the disc is required to seal against pipeline pressure and to sustain the dynamic forces involved in rotating the disc.
These particular requirements are inimical to the need for a slim form of structure and call for a compromise design where the primary emphasis is structural.
An object of the invention is to provide a butterfly valve offering very low frontal area when open and adequate structural strength in the closing mode, and a minimum deflection of the sealing disc.
According to this invention, there is provided a valve member for a butterfly valve which is in the form of a sealing disc having opposed trunnions at or adjacent one face of the disc to provide an offset axis of rotation for said disc within the valve body, and a load-equalising member connecting the trunnions to provide, in combination with said disc, an anti-deformation arrangement which, in use, restricts flexing of said disc.
Preferably, the flow of fluid is towards that face of the disc opposite to said one face, in which case, said load-equalising member acts in tension.
Said load-equalising member is preferably of fixed construction, e.g. a flat plate, and may incorporate means for preloading.
It will be appreciated that the invention includes a butterfly valve fitted with such a valve member.
In order that the invention may be readily understood and further features made apparent, a butterfly valve construction in accordance therewith will now be described with reference to the accompanying drawings, in which: Figure 1 is a front elevation, with the valve member open, Figure 2 is a view similar to Figure 1 with the valve member closed, Figure 3 is a fragmentary view of a modification, and Figure 4 is a section on-the line IV--IV through the valve and blade.
Referring to the drawings, the valve member is in the form of a relatively thin flat sealing disc 1 to the rear face of which two diametrically opposed trunnions 2 are attached to provide an axis for rotation of the sealing disc 1, perpendicular to the axis X-X, as shown in Figure 1. The trunnions are in the form of a pair of spaced walls extending parallel to the direction of fluid flow, which are fixed to said rear face of the disc 1. The walls are profiled in cross-section to present a minimum resistance to flow when in the position shown in Figure 1, and preferably are shaped along their length to provide a convergingidiverging passage 8 therebetween, as shown in Figure 2, to reduce the effect of pressure losses in fluid flowing through said passage.The sealing disc 1 is rotatably mounted via shafts 4 in the valve body 5 at a position offset from an annular sealing face 6 around the periphery of the disc 1, which face is provided by a shaped annular ring of metal or plastics material e.g. such as P.T.F.E. Parallel to the disc 1 and bridging the tops of the trunnions 2 so as to be offset on the other side of the axis of rotation relative of the disc, so as to oppose the latter, is provided a load-equalising member 3 (in this case a tensioning member) comprising a thin flat plate which may, if required, be pre-tensioned e.g. using turn-buckles 7 as shown in Figure 1.
When this valve member is in the open position within a pipeline it will present a substantially thin-walled, open box-like structure to the fluid flow and hence provide minimal blockage. On the other hand, with the valve member closed, the disc 1, trunnions 2 and tensioning member 3 will act in unison to resist flexing of the disc 1 due to fluid pressure in the following manner: Uniform hydraulic pressure on the flat plate disc member will tend to induce bowing about axis X-X and corresponding deflection of the attached trunnions 2.The provision of the loadequalising member 3 by restraining deflection of the trunnions 2, provides a fixed end condition for the plate disc 1, thereby permitting the use of a much thinner plate member than is possible with the current state of the art, which is restricted to two solutions to the problem as follows:- (a) a solid lenticular blade, and (b) an eccentrically mounted thick plate.
The summated thickness of the disc 1 and loadequalising member 3 present a frontal area when open substantially less than that obtained in the present state of the art for equal loading.
In the foregoing description of the embodiment, it is assumed that the flow of fluid is towards the front, flat face of the disc. However, the arrangement as described is bi-directional, so that fluid flow could equally well be towards the rear face of the disc 1 on which the trunnions 2 are mounted. In this case it will be appreciated that the load-equalising member would act in compression (instead of tension as described above) to resist flexing of the disc 1.
The arrangement described above may be used over a large range of sizes for the valve member: however, to reduce any tendency for the loadequalising member 3 to flutter in larger applications, e.g. for valve members of 2' 0" upwards, preferably one, or more, stiffening member 9, which may be contoured to reduce pressure losses, is connected between the rear face of the disc 1 and the load-equalising member 3, as shown dotted in the Figures.

Claims (9)

1. A valve member for a butterfly valve in the form of a sealing disc having opposed trunnions at or adjacent one face of the disc to provide an offset axis of rotation for said disc within the valve body, and a load-equalising tensioning member connecting the trunnions to provide, in combination with said disc, an anti-deformation arrangement which, in use, restricts flexing of said disc.
2. A valve member according to claim 1, designed for fluid flow which is towards that face of the disc opposite to said one face, wherein said load-equalising member is adapted to act in tension,
3. A valve member according to claim 1, or 2, wherein said load-equalising member is of fixed construction and in the form of a flat plate.
4. A valve member according to any one of claims 1 to 3, wherein the load-equalising member incorporates means for pre-loading.
5. A valve member according to any preceding claim, wherein said trunnions are in the form of a pair of spaced walls extending in the fluid flow direction which are profiled in cross-section to present minimum resistance to fluid flow with the valve member open.
6. A valve member according to claim 5, wherein the walls are shaped along their length to provide a converging/diverging passage therebetween to reduce the effect of pressure losses in fluid flowing therethrough.
7. A valve member according to any preceding claim, wherein at least one stiffening member is provided to connect said one face to an intermediate part of the load-equalising member.
8. A valve member constructed, arranged and adapted for use substantially as hereinbefore described with reference to, and as shown in, the accompanying drawing.
9. A butterfly valve incorporating a valve member according to any one of the preceding claims.
GB08309613A 1982-07-13 1983-04-08 Valve member for a butterfly valve Withdrawn GB2123526A (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
GB08309613A GB2123526A (en) 1982-07-13 1983-04-08 Valve member for a butterfly valve
DE19833324442 DE3324442A1 (en) 1982-07-13 1983-07-07 VALVE FOR A THROTTLE VALVE

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB8220254 1982-07-13
GB08309613A GB2123526A (en) 1982-07-13 1983-04-08 Valve member for a butterfly valve

Publications (2)

Publication Number Publication Date
GB8309613D0 GB8309613D0 (en) 1983-05-11
GB2123526A true GB2123526A (en) 1984-02-01

Family

ID=26283325

Family Applications (1)

Application Number Title Priority Date Filing Date
GB08309613A Withdrawn GB2123526A (en) 1982-07-13 1983-04-08 Valve member for a butterfly valve

Country Status (2)

Country Link
DE (1) DE3324442A1 (en)
GB (1) GB2123526A (en)

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB679038A (en) *
GB697113A (en) * 1950-02-17 1953-09-16 Culaud Andre Improvements in or relating to butterfly valves
GB733931A (en) * 1952-10-21 1955-07-20 Power Jets Res & Dev Ltd Jet deflectors for aircraft
GB983191A (en) * 1960-05-13 1965-02-10 Bristol Siddeley Engines Ltd Improvements in fluid flow control valves
GB1104759A (en) * 1964-07-06 1968-02-28 English Electric Co Ltd Improvements in or relating to butterfly valves
GB1135811A (en) * 1966-01-01 1968-12-04 David F Wiseman & Sons Ltd Improvements in butterfly valves
GB1259273A (en) * 1967-12-07 1972-01-05

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB679038A (en) *
GB697113A (en) * 1950-02-17 1953-09-16 Culaud Andre Improvements in or relating to butterfly valves
GB733931A (en) * 1952-10-21 1955-07-20 Power Jets Res & Dev Ltd Jet deflectors for aircraft
GB983191A (en) * 1960-05-13 1965-02-10 Bristol Siddeley Engines Ltd Improvements in fluid flow control valves
GB1104759A (en) * 1964-07-06 1968-02-28 English Electric Co Ltd Improvements in or relating to butterfly valves
GB1135811A (en) * 1966-01-01 1968-12-04 David F Wiseman & Sons Ltd Improvements in butterfly valves
GB1259273A (en) * 1967-12-07 1972-01-05

Also Published As

Publication number Publication date
GB8309613D0 (en) 1983-05-11
DE3324442A1 (en) 1984-03-22

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Legal Events

Date Code Title Description
WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)