FLOW GUIDE FOR A TURBINE WHEEL GAS METER

Abstract: Flow guide for eliminating eddies from a gas flow in a pipe at a distance upstream of a turbine wheel gas meter which at the side facing the flow guide is provided with a blunt, rounded nose part. The flow guide comprises at least one dividing wall which is concentric with the inside wall of the pipe, a number of uniformly distributed radial dividing walls being provided on both sides of the concentric dividing wall. Device for measuring the flow rate of a gas flow in a pipe, consisting of a turbine wheel gas meter and a flow guide which is placed upstream relative to the turbine wheel gas meter, at the side facing the flow guide, the turbine wheel gas meter being provided with a blunt, rounded nose part. The flow guide consists of a number of uniformly distributed concentric and radial dividing walls.

Description: Flow guide for a turbine wheel gas meter The invention relates to a flow guide for eliminating eddies from a gas flow in a pipe at a distance upstream of a turbine wheel gas meter which at the side facing or to face the flow guide is provided with a blunt, rounded nose part. The invention also relates to a device for measuring the flow rate of a gas flow in a pipe, consisting of a turbine wheel gas meter to be placed in the pipe and a flow guide which is or should be placed upstream relative to the turbine wheel gas meter, at a distance from the turbine wheel gas meter, at the side facing the flow guide the turbine wheel gas meter being provided with a blunt, rounded nose part. Such a flow guide and such a device are known from Dutch Patent Application N -A-9400445. The turbine wheel gas meter of this known device consists of a circular symmetrical element which is mounted in the pipe by means of spo- kes. The gas flow is guided along the upstream blunt, rounded nose part of the turbine wheel gas meter to the annular gap between the central element and the inside wall of the flow pipe. A blade wheel is mounted in the turbine wheel gas meter in such a way that the blades are situated in the annular gap. The blade wheel is driven by the gas flowing through the annular gap. The flow guide is placed at a distance upstream of the nose part, which flow guide in the case of this known device consists of a plate in which a circular symmetrical holes pattern has been made. The flow guide eliminates the eddies in the gas flow. These eddies occur when there are obstacles in the gas pipe, for example at bends, transitions to other pipe diameters or at fittings. After passing through the flow guide, the gas flow is homogenized by radial impulse exchange in the space between the flow guide and the nose part, so that a homogenous or uniform flow profile is produced in the annular gap between the pipe wall and the turbine wheel gas meter. This homogenous flow profile is necessary to permit accurate measurements to be carried out by means of the turbine wheel gas meter. For that purpose, the nose part must be a rounded, slightly blunt shape which is not streamlined, so that sufficient impulse exchange with the gas flow occurs. However, the pressure loss in the case of this known device is relatively great. This is a disadvantage in particular in circumstances in which not much pressure is available, as in the case of low-pressure systems. This pressure loss is also a disadvantage if the gas is being compressed again after it passes through the turbine wheel gas meter. The compression costs are higher because of the pressure loss which has occurred. Other known flow guides were designed in the first instance for use in the case of orifice meters instead of in turbine wheel gas meters. For this, the flow guide not only has to eliminate eddies, but also to give a flow profile which within certain margins of error corresponds to a fully developed flow profile such as that which would occur at the end of a very long pipeline. The flow profile needed for an orifice meter there has to be a very specific shape. The flow guides needed for this of necessity produce a relatively high pressure loss. The object of the invention is a flow guide for a turbine wheel gas meter, which flow guide can eliminate eddies in a gas flow with the least possible pressure loss, the flow being directed in such a way that the flow has a substanti- ally circular symmetrical profile. This object of the invention is achieved by the fact that the flow guide comprises at least one dividing wall which is substantially concentric with the inside wall of the pipe, a number of uniformly distributed radial dividing walls being provided on both sides of the concentric dividing wall. This means that the open surface through which the gas can flow is at a maximum, so that the pressure loss is minimal. While in the known flow guides, consisting of a plate with circular holes, the total throughflow aperture is approximately 50 to 60% of the surface area of the cross-section of the pipe, the net throughflow aperture in the case of a flow guide according to the invention is 80 to 90% of the cross-section surface area of the pipe, or even more. It has been found that at low pressures the eddies m a gas flow are eliminated satisfactorily. US Patent US-A-4, 308, 755 discloses a flow guide which is placed upstream of a turbine wheel gas meter and consists of a number of radial dividing walls which converge in the centre. Said flow guide is intended for directing a liquid flow and is not suitable for eliminating eddies from a gas flow. The turbine wheel gas meter is placed at a short distance behind this known flow guide, and it is not provided with a blunt nose part. Owing to the absence of the nose part and the short distance between the flow guide and the turbine wheel gas meter, no radial impulse exchange, which also makes the flow homogeneous, occurs. This known flow guide is also not provided with a concentric dividing wall. The throughflow aperture is consequently divided into cake-wedge-shaped apertures. Said apertures cannot eliminate the eddies in a gas flow sufficiently, and besides they cause additional eddies. If this known flow guide were used for the elimination of eddies from a gas flow, the flow guide would have to be made very long, which would result in an impracticable length and great pressure loss. In a preferred embodiment the flow guide comprises an outermost concentric wall with substantially the same periphery as the inside wall of the pipe. This means that the flow guide connects well to the inside wall of the pipe and can be fixed easily in the pipe. The flow guide must be placed in a well-fitting manner in the pipe, so that no appreciable flow which bypasses the flow guide may occur. In order to make positioning and fixing of the flow guide in the pipe even easier, the outermost concentric wall is preferably longer in the axial direction than the dividing walls of the flow guide. The flow guide preferably comprises a substantially circular central part, the diameter of which is approximately one quarter of the periphery of the flow guide, the flow guide comprising two concentric dividing walls, and the distance between the concentric dividing walls being approximately equal to the distance between the innermost concentric wall and the central part, and also being approximately equal to the distance between the outermost concentric dividing wall and the outer periphery of the flow guide. This produces a uniform distribution of the radial and concentric dividing walls, with the result that the eddies are already efficiently eliminated by the radial dividing walls when the flow guide is of relatively short length in the axial direction. The pressure loss remains very limited by the small number of walls and the large net throughflow aperture. The number of radial dividing walls between the central part and the innermost concentric wall is preferably half the number of radial dividing walls between the two concentric dividing walls, the number of radial dividing walls between the outermost concentric dividing wall and the outer periphery of the flow guide being equal to the number of radial dividing walls between the two concentric divi- ding walls. This produces a distribution of throughflow apertures in which the size of the throughflow apertures is always approximately the same, so that as a result the eddies in the gas flow are eliminated already over a short length in the axial direction. The central part can compri- se a throughflow aperture, but can also be closed and, for example, serve as an attachment point for fixing means. The radial dividing walls between the two concentric dividing walls preferably always lie in line with the radial dividing walls between the outermost concentric dividing wall and the outer periphery of the flow guide, while the radial dividing walls between the central part and the innermost concentric dividing wall always lie in line with a pair of radial dividing walls between the innermost concentric dividing wall and the outer periphery of the flow guide. This makes the flow guide easy to manufacture by means of, for example, injection moulding. A mould can be manufactured relatively cheaply for the purpose. In another preferred embodiment, which is suitable in particular for use in pipes with larger internal diameters, the flow guide comprises a substantially circular central part with a diameter which is approximately one fifth of the diameter of the outer periphery of the flow guide, the flow guide further comprising three concentric dividing walls, the number of radial dividing walls between the outer periphery of the flow guide and the outermost concentric dividing wall being three times the number of radial dividing walls between the central part and the innermost concentric dividing wall, and the number of radial dividing walls between two adjacent concentric dividing walls being twice the number of radial dividing walls between the central part and the innermost concentric dividing wall. The object of the invention is also achieved with a device for measuring the flow rate of a gas flow in a pipe, consisting of a turbine wheel gas meter to be placed in the pipe and a flow guide which is or should be placed upstream relative to the turbine wheel gas meter, at a distance from the turbine wheel gas meter, at the side facing the flow guide the turbine wheel gas meter being provided with a blunt, rounded nose part, and the flow guide consisting of a number of uniformly distributed concentric dividing walls and a number of uniformly distributed radial dividing walls. Eddies in the gas flow are eliminated by the flow guide at low pressures. After passing through the flow guide, the gas flow is directed by radial impulse exchange in the space between the nose part and the flow guide in such a way that the flow profile is homogeneous in the annular gap between the turbine wheel gas meter and the inside wall of the pipe. The invention will be explained in greater detail with reference to the drawing, in which: Fig. 1 shows in cross-section the device according to the invention ; Fig. 2 shows in front view the flow guide according to the invention; Fig. 3 shows in rear view the flow guide according to Figure 2; Fig. 4 shows in front view another possible flow guide according to the invention. Figure 1 shows in cross-section a pipe 1 with a bend 2. A gas flows through the pipe. If the gas is flowing through a very long pipe with continuous diameter, a flow profile 3, in which the gas flows faster in the centre than near the wall 4 of the pipe 1, is obtained. Said flow profile is disturbed by obstacles in the gas pipe, for example bends, narrowings or fittings, in which case eddies are caused in the gas flow. After passing through the bend 2, the gas flow has a flow profile 5. A turbine wheel gas meter 6 is placed in the pipe 1, in order to measure the flow rate of the gas flow. The turbine wheel gas meter 6 consists of a substantially cylindrical element 7, which is suspended in the pipe 1 concentrically by means of radial spokes 8, between the inside wall of the pipe 1 and the cylindrical element of the turbine wheel gas meter 6 an annular gap 9 remaining open, through which gap the gas flows. A rotata- ble blade wheel 10 is accommodated in the turbine wheel gas meter 6, the blades 11 of which blade wheel are placed in the annular gap 9. The blade wheel 10 is set in motion by the gas flowing through the annular gap 9. The flow rate of the gas flow through the annular gap 9 can be calculated by measuring the speed of rotation of the blade wheel 10. For this purpose, the flow in the annular gap 9 must be uniform, and the gas flow must not have any eddies. If the gas flowed with a non-uniform flow profile through the annular gap 9, in which case, for example, more gas would flow at one side than at the other side of the blade wheel 10, this would lead to measuring errors. In order to ensure that the gas flow flows with a uniform flow profile through the annular gap, the turbine wheel gas meter 6 at the upstream end is provided with a blunt, rounded nose part 12, a flow guide 13 being placed at a distance upstream of the nose part 12. The flow guide 13 eliminates eddies in the gas flow. After the gas flow has passed through the flow guide 13, the flow profile thereof is free from eddies, but still not uniform. In the space 14 between the flow guide 13 and the nose part 12 the gas flow is further homogenized by radial impulse exchange. To this end, the shape of the nose part 12 is blunt in shape and is not streamlined. The flow guide 13 comprises a closed circular central part 15 and a cylindrical outside wall 16 which is placed in a well-fitting manner in the pipe 1. The space between the central part 15 and the outside wall 16 is divided up by radial dividing walls 17 and concentric dividing walls 18. The outermost wall 16 runs on in the axial direction over a certain length into an extension 19. This cylindrical extension 19 serves for fixing the flow guide 13 to the inside wall of the pipe 1. Figures 2 and 3 show in succession the flow guide 13 in front and rear view respectively. The flow guide 13 comprises a closed central part 15, two concentric dividing walls 18 and a cylindrical outside wall 16. The central part 15 is substantially circular. The diameter of the central part 15 is approximately one quarter of the periphery of the flow guide 13. The distance between the concentric dividing walls 18 is equal to the distance between the innermost concentric wall and the central part 15 and is also equal to the distance between the outermost concentric dividing wall 18 and the outside wall 16. Ten uniformly distributed radial dividing walls 17 are situated between the central part 15 and the innermost concentric dividing wall 18. Between the concentric dividing walls 18 there are twenty uniformly distributed radial dividing walls 17, and also between the outermost concentric dividing wall and the outside wall 16. The radial dividing walls 17 between the two concentric dividing walls 18 always lie in line with the radial dividing walls 17 between the outermost concentric dividing wall 18 and the outside wall 16, while the radial dividing walls 17 between the central part 15 and the innermost concentric dividing wall 18 always lie in line with a pair of radial dividing walls 17 between the innermost concentric dividing wall 18 and the outside wall 16. The radial and concentric dividing walls 17, 18 thus bound more or less equal sizes of throughflow apertures 20. At the front side of the closed central part 15 the dividing walls 17 run on slightly into radial extensions 21, tapering towards the centre of the central part 15. This means that an advantageous mould construction can be obtained. Figure 4 shows a flow guide 22 for larger pipe diameters. This flow guide 22 is designed with a substantially circular central part 15 with a diameter which is approximately one fifth of the diameter of the outside wall 16. The flow guide 22 further comprises three concentric dividing walls 18, the number of radial dividing walls 17 between the outside wall 16 and the outermost concentric dividing wall 18 being three times the number of radial dividing walls 17 between the central part 15 and the innermost concentric dividing wall 18. The number of radial dividing walls 17 between two adjacent concentric dividing walls 18 is twice the number of the radial dividing walls 17 between the central part 15 and the innermost concentric dividing wall 18, so that a relatively fine-mesh network of more or less equal and uniformly distributed throughflow apertures is obtained.

Claims: CLAIMS 1. Flow guide for eliminating eddies from a gas flow in a pipe at a distance upstream of a turbine wheel gas meter which at the side facing or to face the flow guide is provided with a blunt, rounded nose part, characterized in that the flow guide comprises at least one dividing wall which is substantially concentric with the inside wall of the pipe, a number of uniformly distributed radial dividing walls being provided on both sides of the concentric dividing wall. 2. Flow guide according to Claim 1, characterized in that the flow guide comprises an outermost concentric wall with substantially the same periphery as the inside wall of the pipe. 3. Flow guide according to Claim 2, characterized in that the outermost concentric wall is longer in the axial direction than the dividing walls of the flow guide. 4. Flow guide according to Claim 1, 2 or 3 , characterized in that the flow guide comprises a substantially circular central part, the diameter of which is approximately one quarter of the periphery of the flow guide, and in that the flow guide comprises two concentric dividing walls, the distance between the concentric dividing walls being approximately equal to the distance between the innermost concentric wall and the central part and also being approximately equal to the distance between the outermost concentric dividing wall and the outer periphery of the flow guide. 5. Flow guide according to Claim 4, characterized in that the number of radial dividing walls between the central part and the innermost concentric wall is half the number of radial dividing walls between the two concentric dividing walls and the number of radial dividing walls between the outermost concentric dividing wall and the outer periphery of the flow guide. 6. Flow guide according to Claim 4 or 5 , characterized in that the radial dividing walls between the two concentric dividing walls always lie in line with the radial dividing walls between the outermost concentric dividing wall and the outer periphery of the flow guide, while the radial dividing walls between the central part and the innermost concentric dividing wall always lie in line with a pair of radial dividing walls between the innermost concentric dividing wall and the outer periphery of the flow guide. 7. Flow guide according to Claim 1, 2 or 3 , characterized in that the flow guide comprises a substantially circular central part with a diameter which is approximately one fifth of the diameter of the outer periphery of the flow guide, and in that the flow guide further comprises three concentric dividing walls, the number of radial dividing walls between the outer periphery of the flow guide and the outermost concentric dividing wall being three times the number of radial dividing walls between the central part and the innermost concentric dividing wall, and the number of radial dividing walls between two adjacent concentric dividing walls being twice the number of radial dividing walls between the central part and the innermost concentric dividing wall. 8. Device for measuring the flow rate of a gas flow in a pipe, consisting of a turbine wheel gas meter to be placed in the pipe and a flow guide which is or should be placed upstream relative to the turbine wheel gas meter, at a distance from the turbine wheel gas meter, at the side facing the flow guide the turbine wheel gas meter being provided with a blunt, rounded nose part, characterized in that the flow guide consists of a number of uniformly distributed concentric dividing walls and a number of equally distributed radial dividing walls.

Inventors: BERGERVOET JOSEPHUS THEODORUS, OOSTENDORP FRANCISCUS JOHANNES, BERGERVOET, JOSEPHUS, THEODORUS, MARIA, OOSTENDORP, FRANCISCUS, JOHANNES, GERARDUS, MARIA
Applicants: BERGERVOET JOSEPHUS THEODORUS, INSTROMET BV, OOSTENDORP FRANCISCUS JOHANNES, BERGERVOET, JOSEPHUS, THEODORUS, MARIA, INSTROMET B.V., OOSTENDORP, FRANCISCUS, JOHANNES, GERARDUS, MARIA
Application year: 1997
Main classification: G01F1
IPC codes: G01F1