WO1991003739A1 - Flow speed meter for channels or road tunnels - Google Patents

Flow speed meter for channels or road tunnels Download PDF

Info

Publication number
WO1991003739A1
WO1991003739A1 PCT/NO1990/000130 NO9000130W WO9103739A1 WO 1991003739 A1 WO1991003739 A1 WO 1991003739A1 NO 9000130 W NO9000130 W NO 9000130W WO 9103739 A1 WO9103739 A1 WO 9103739A1
Authority
WO
WIPO (PCT)
Prior art keywords
channels
differential pressure
flow
measurement
air inlets
Prior art date
Application number
PCT/NO1990/000130
Other languages
French (fr)
Inventor
Helge NÖRSTRUD
Original Assignee
Institutt For Hydro- Og Gassdynamikk, Nth
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 Institutt For Hydro- Og Gassdynamikk, Nth filed Critical Institutt For Hydro- Og Gassdynamikk, Nth
Publication of WO1991003739A1 publication Critical patent/WO1991003739A1/en

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01PMEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
    • G01P5/00Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft
    • G01P5/14Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft by measuring differences of pressure in the fluid

Definitions

  • the invention comprises a device of the type indicated in the introduction to Claim 1 for the measurement of air velocity and flow direction in channels or road tunnels where there is air flowing through and transient flow disturbances.
  • Fan-driven air velocity meters are known for flow measurement applications in channels or road tunnels. These are exposed to mechanical wear. They are furthermore influenced by external disturbances such as transient air surges in a ventilation duct, that can be caused by doors being opened or closed. In. road tunnels, known velocity meters are influenced by passing vehicles that produce transient flow disturbances around the measurement device. Known measurement equipment therefore cannot function as satisfactory signal transmitters to control the fans and dampers that regulate the airstream in such channels etc.
  • the main objective of the invention is to create a means of measuring air flow that is less exposed to wear than known turbine meters.
  • a second objective is to create a flow meter that cannot be influenced inadvertently by transient flow disturbances in the channel where the device is located.
  • a further objective is to create a flow meter that is constructed of simple, robust components.
  • Fig. 1 shows a schematic lateral perspective of a straightforward design with an electronic delay element
  • Fig. 2 shows a perspective sketch of a sensor element in ⁇ accordance with a further means of designing the invention
  • Fig. 3 shows a schematic representation of velocity diagram for the sensor in Fig. 2.
  • Fig. 1 shows a measurement sensor 11 with a basic design that is known in principle. This consists of a circular disc 12 that is located laterally to the direction of flow. This has a central sensor inlet 13 on each side with a pipe that is connected to a pressure transducer 14 for measuring the differential pressure. The output from the transducer 14 is connected to an electronic delay circuit 15 that transmits pressure signals that have been held constant for a certain period, this may be 5-20 seconds, for example. Because of the pressure difference between the two plate sides, the size of the plates and the channel cross section, certain relationships make it possible to take a measurement of the flow velocity. The delay circuit 15 prevents transient flow disturbances influencing the measurement results.
  • a flow measurement meter is shown in Fig. 2 in a simplified design.
  • Each plate has an external pressure inlet 19 located centrally that communicates by means of an axial connecting pipe 20 with a dual channel in a support pipe 21 running down from a pressure transducer 22.
  • the space between the two pressure plates 17 and 18 i ⁇ indicated by reference number 23.
  • P'ig. 3 illustrates a flow diagram for half of the flow measurement sensor depicted in Fig. 2.
  • An eddy 24 is formed in the space between the two plates 17 and 18, which is uninfluenced by transient flow disturbances. Thus the pressure conditions are left largely unchanged, this enable the pressure measurement to be held constant during a brief period of disturbance. If there is a lasting change in direction, the eddy will be influenced which will affect th differential pressure between the two pressure plates.

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Measuring Volume Flow (AREA)
  • Measuring Fluid Pressure (AREA)
  • Excavating Of Shafts Or Tunnels (AREA)
  • Road Signs Or Road Markings (AREA)

Abstract

Device for the measurement of flow velocity in channels or road tunnels, where a sensor (11) is used to register the differential pressure. This comprises a plate-shaped organ (12) that is located at a right angle to the flow direction in the channel with air inlets (13) for the differential pressure measurements on opposite sides. An electronic delay circuit (15) enables short-term changes in the measurement results to be suppressed so that transient changes in the direction of flow do not alter the measurement results.

Description

Flow speed meter for channels or road tunnels
The invention comprises a device of the type indicated in the introduction to Claim 1 for the measurement of air velocity and flow direction in channels or road tunnels where there is air flowing through and transient flow disturbances.
Background
Fan-driven air velocity meters are known for flow measurement applications in channels or road tunnels. These are exposed to mechanical wear. They are furthermore influenced by external disturbances such as transient air surges in a ventilation duct, that can be caused by doors being opened or closed. In. road tunnels, known velocity meters are influenced by passing vehicles that produce transient flow disturbances around the measurement device. Known measurement equipment therefore cannot function as satisfactory signal transmitters to control the fans and dampers that regulate the airstream in such channels etc.
Objectives.
The main objective of the invention is to create a means of measuring air flow that is less exposed to wear than known turbine meters. A second objective is to create a flow meter that cannot be influenced inadvertently by transient flow disturbances in the channel where the device is located. A further objective is to create a flow meter that is constructed of simple, robust components.
Principles of the invention The main objective of the invention can be achieved by designing a device in accordance with the description given in the characterizing part of Claim 1.
Other advantageous aspects of the invention are indicated in the subsidiary claims. A particularly advantageous feature is the design stated in Claim 3 which reduces the number of components. Example
The drawings illustrate two means of designing the invention, where
Fig. 1 shows a schematic lateral perspective of a straightforward design with an electronic delay element,
Fig. 2 shows a perspective sketch of a sensor element in ~ accordance with a further means of designing the invention, while
Fig. 3 shows a schematic representation of velocity diagram for the sensor in Fig. 2.
Fig. 1 shows a measurement sensor 11 with a basic design that is known in principle. This consists of a circular disc 12 that is located laterally to the direction of flow. This has a central sensor inlet 13 on each side with a pipe that is connected to a pressure transducer 14 for measuring the differential pressure. The output from the transducer 14 is connected to an electronic delay circuit 15 that transmits pressure signals that have been held constant for a certain period, this may be 5-20 seconds, for example. Because of the pressure difference between the two plate sides, the size of the plates and the channel cross section, certain relationships make it possible to take a measurement of the flow velocity. The delay circuit 15 prevents transient flow disturbances influencing the measurement results. If, on the other hand, there are lasting disturbances in the air flow in a road tunnel caused by piston traffic for instance, registrations of changes in the flow direction will be made that may activate fans or dampers. This could be desirable for numerous reasons such as the removal of exhaust fumes.
A flow measurement meter is shown in Fig. 2 in a simplified design. Here, there are two pressure plates 17 and 18 that are located parallel to each other at a distance of approximately 1.5 times the diameter of the plates. Each plate has an external pressure inlet 19 located centrally that communicates by means of an axial connecting pipe 20 with a dual channel in a support pipe 21 running down from a pressure transducer 22. The space between the two pressure plates 17 and 18 iε indicated by reference number 23.
P'ig. 3 illustrates a flow diagram for half of the flow measurement sensor depicted in Fig. 2. An eddy 24 is formed in the space between the two plates 17 and 18, which is uninfluenced by transient flow disturbances. Thus the pressure conditions are left largely unchanged, this enable the pressure measurement to be held constant during a brief period of disturbance. If there is a lasting change in direction, the eddy will be influenced which will affect th differential pressure between the two pressure plates.

Claims

Cla ims :
1. Device for the measurement of flow velocity in channels or road tunnels, where a sensor (11) is used to register the differential pressure which enables the velocity to be determined, characterized by the device comprising a plate-shaped organ (12) that is located at a right angle to the direction of the channel with air inlets (13) for the differential pressure measurements on opposite sides, and further comprising a means (15) of suppressing impulses on the sensor that have a duration of less than 5-20 seconds.
2. Device as claimed in Claim 1, characterized by this comprising an electronic delay circuit (15) that suppresses short-term changes in the measurement results.
3. Device as claimed in Claim 1, characterized by this comprising two mutually parallel circular pressure plates (17,18) with external air inlets and a cylindrical space (23) between them.
4. Device as claimed in Claim 3, characterized by the distance between the pressure plates being approximately 1.5 times the diameter of the plates.
5. Device as claimed in Claims 3 or 4, characterized by the two pressure plates (17, 18) being linked to a central supporting pipe (20) the ends of which form the air inlets for the differential pressure measurements.
PCT/NO1990/000130 1989-08-29 1990-08-17 Flow speed meter for channels or road tunnels WO1991003739A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
NO893448 1989-08-29
NO893448A NO168328C (en) 1989-08-29 1989-08-29 SPEED METER WITH DIRECTION INDICATOR FOR ROAD Tunnels

Publications (1)

Publication Number Publication Date
WO1991003739A1 true WO1991003739A1 (en) 1991-03-21

Family

ID=19892352

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/NO1990/000130 WO1991003739A1 (en) 1989-08-29 1990-08-17 Flow speed meter for channels or road tunnels

Country Status (2)

Country Link
NO (1) NO168328C (en)
WO (1) WO1991003739A1 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2000075674A1 (en) * 1999-06-02 2000-12-14 The University Of British Columbia Differential pressure velocimeter with probe body having disk shape
DE10359540A1 (en) * 2003-12-17 2005-07-14 Tlt-Turbo Gmbh Device and method for determining the flow velocity

Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1056513A (en) * 1910-02-12 1913-03-18 Gen Electric Meter for measuring elastic fluids.
US2687645A (en) * 1950-03-02 1954-08-31 Askania Regulator Co Differential pressure flow rate measurement device
US4008611A (en) * 1975-07-01 1977-02-22 S. P. Kinney Engineers, Inc. Fluid flow measuring apparatus
GB1574702A (en) * 1977-01-10 1980-09-10 Tekflo Ltd Fluid flow measuring assembly
US4290315A (en) * 1979-01-25 1981-09-22 Fincoil-Teollisuus Oy Apparatus for determining the differential pressure and the volumetric fluid flow in a conduit
US4290314A (en) * 1979-04-09 1981-09-22 Rosemount Inc. Target flowmeter
WO1983003896A1 (en) * 1982-04-23 1983-11-10 Stifab Ab Measurement unit for determining gas flow through a conduit and measuring means designed to be included in such a measuring unit
SE434435B (en) * 1979-11-07 1984-07-23 Stifab Ab Measuring device for determining gas flow through ducts and pipes and use of such measuring device as a measurement indicator for air flow regulation
EP0255056A2 (en) * 1986-07-28 1988-02-03 Yamatake-Honeywell Co. Ltd. Method for measuring the speed of a gas flow

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1056513A (en) * 1910-02-12 1913-03-18 Gen Electric Meter for measuring elastic fluids.
US2687645A (en) * 1950-03-02 1954-08-31 Askania Regulator Co Differential pressure flow rate measurement device
US4008611A (en) * 1975-07-01 1977-02-22 S. P. Kinney Engineers, Inc. Fluid flow measuring apparatus
GB1574702A (en) * 1977-01-10 1980-09-10 Tekflo Ltd Fluid flow measuring assembly
US4290315A (en) * 1979-01-25 1981-09-22 Fincoil-Teollisuus Oy Apparatus for determining the differential pressure and the volumetric fluid flow in a conduit
US4290314A (en) * 1979-04-09 1981-09-22 Rosemount Inc. Target flowmeter
SE434435B (en) * 1979-11-07 1984-07-23 Stifab Ab Measuring device for determining gas flow through ducts and pipes and use of such measuring device as a measurement indicator for air flow regulation
WO1983003896A1 (en) * 1982-04-23 1983-11-10 Stifab Ab Measurement unit for determining gas flow through a conduit and measuring means designed to be included in such a measuring unit
EP0255056A2 (en) * 1986-07-28 1988-02-03 Yamatake-Honeywell Co. Ltd. Method for measuring the speed of a gas flow

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2000075674A1 (en) * 1999-06-02 2000-12-14 The University Of British Columbia Differential pressure velocimeter with probe body having disk shape
US6571645B1 (en) 1999-06-02 2003-06-03 Sheldon I. Green Differential pressure velocimeter with probe body having disk shape
DE10359540A1 (en) * 2003-12-17 2005-07-14 Tlt-Turbo Gmbh Device and method for determining the flow velocity

Also Published As

Publication number Publication date
NO168328C (en) 1992-02-05
NO893448D0 (en) 1989-08-29
NO168328B (en) 1991-10-28
NO893448L (en) 1991-03-01

Similar Documents

Publication Publication Date Title
US3564915A (en) Current meter or flow meter
AU609861B2 (en) Fluid metering system
GEP20001926B (en) Method and Device for Measuring of Fluid Flow
ES2186702T3 (en) MEASUREMENT SYSTEM.
US5095760A (en) Vortex flowmeter with dual sensors
US3705534A (en) Fluidic flow sensing method and apparatus
EP0171937B1 (en) Flow meter
US5945608A (en) Hall effect fluid flow switch and flow meter
US6435036B1 (en) Vortex flow meter
US3443432A (en) Flowmeter
WO1991003739A1 (en) Flow speed meter for channels or road tunnels
SE441704B (en) DEVICE FOR DETERMINING THE PRESSURE DIFFERENCE AND VOLYMETRIC FLUID FLOW IN A PIPE
US5767419A (en) Hall effect fluid flow switch and flow meter
US4346605A (en) Magnetic flowmeter for electrically conductive liquid
US2575492A (en) Flow-measuring apparatus
AU5200399A (en) Device for measuring the volume flow of a fluid in a pipe
KR910012666A (en) Devices for measuring displacement of inductive transducers and movable members
JPS60502228A (en) Device for measuring the liquid part of a two-phase flow of gas and liquid
JPS5829853B2 (en) Mass flow measuring device
JP3144986B2 (en) Flowmeter
GB1583490A (en) Apparatus for measuring the flow rate of a medium
US3455161A (en) Meter for measuring unsteady fluid flow
US3365955A (en) Fluid angular rate sensor
WO1995005581A1 (en) Closely coupled, dual turbine volumetric flow meter
US4756196A (en) Flow measuring apparatus

Legal Events

Date Code Title Description
AK Designated states

Kind code of ref document: A1

Designated state(s): CA JP SU US

AL Designated countries for regional patents

Kind code of ref document: A1

Designated state(s): AT BE CH DE DK ES FR GB IT LU NL SE

NENP Non-entry into the national phase

Ref country code: CA