GB2237638A - A fluid rate sensor - Google Patents

A fluid rate sensor Download PDF

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Publication number
GB2237638A
GB2237638A GB8915673A GB8915673A GB2237638A GB 2237638 A GB2237638 A GB 2237638A GB 8915673 A GB8915673 A GB 8915673A GB 8915673 A GB8915673 A GB 8915673A GB 2237638 A GB2237638 A GB 2237638A
Authority
GB
United Kingdom
Prior art keywords
fluid
rotation
cavity
rotation sensor
conducting
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.)
Granted
Application number
GB8915673A
Other versions
GB2237638B (en
GB8915673D0 (en
Inventor
Douglas Frank George Dwyer
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to GB8915673A priority Critical patent/GB2237638B/en
Publication of GB8915673D0 publication Critical patent/GB8915673D0/en
Priority to PCT/GB1990/001035 priority patent/WO1991001008A1/en
Priority to EP90909764A priority patent/EP0486503A1/en
Priority to JP2509761A priority patent/JPH04506571A/en
Publication of GB2237638A publication Critical patent/GB2237638A/en
Application granted granted Critical
Publication of GB2237638B publication Critical patent/GB2237638B/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C19/00Gyroscopes; Turn-sensitive devices using vibrating masses; Turn-sensitive devices without moving masses; Measuring angular rate using gyroscopic effects
    • G01C19/58Turn-sensitive devices without moving masses
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01PMEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
    • G01P3/00Measuring linear or angular speed; Measuring differences of linear or angular speeds
    • G01P3/26Devices characterised by the use of fluids

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  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Measuring Volume Flow (AREA)
  • Indicating Or Recording The Presence, Absence, Or Direction Of Movement (AREA)

Abstract

An angular rate sensor for measuring angular velocity about a cavity sensitive axis which includes a fluid filled cavity, means to cause rotation of the fluid in the cavity about an axis perpendicular to said sensitive axis, the fluid having parallel to said rotation axis a flow rate gradient, and means to sense a change in the flow rate grandient with rotation of the cavity about said sensitive axis. The means can be electrical, as by measuring the change in electrical potential or electrical resistance or electrical current across the flow path, or optical by measuring the change in distribution of a neutrally buoyant material in an optically transparent fluid.

Description

AN IMPROVED FLUID RATE SENSOR Inertial sensors are devices that measure and provide information on the forces acting due to movement. The information is generally used for navigational purposes where it is employed to calculate position without the use of an external reference.
One family of inertial sensors measures rotation and for this purpose a gyro is most commonly used.
A major factor limiting the wider use of inertial sensors is the cost resulting from their complexity and the precision necessary in their manufacture.
According to the present invention a cavity is filled with a fluid capable of substantially free or unimpeded movement. Some or all of the fluid is arranged to be in motion such that it follows a path around the cavity and as a consequence has angular momentum. Rotation of the cavity perpendicular to the effective axis of spin or rotation of the fluid will give rise to a force acting on the moving fluid.
The force acting on the moving fluid will give rise to a force in opposition to or at 90 degrees to the force acting which will be transferred to the cavity and may be detected directly. alternatively the force acting on the moving fluid may be detected by arranging for a gradient in fluid velocity to exist through one axis of the cavity and to establish suitable means to detect the change in the profile of the velocity gradient resulting from the force arising due to rotation of the cavity perpendicular to the effective axis of fluid spin or rotation.
Rotation of the cavity perpendicular to to the effective axis of spin will give rise to forces acting on each element of the moving fluid in proportion to the angular momentum of that element and rate of cavity rotation and therefore alter a gradient of velocity or velocity profile within the fluid.
Rotation of the cavity and the consequent change in the velocity profile may be sensed by making measurements at various points of an optical or electrical parameter or characteristic resulting from the velocity or movement of the rotating fluid with respect to the cavity.
The electrical characteristic used to provide information on the velocity of the fluid may be varying resistivity or the generation of an alternating or direct electrical potential resulting from the movement of a conducting fluid through a magnetic field developed by a permanent magnet or a solenoid energised with a direct or an alternating current and fixed to the cavity.
The optical characteristics may be varying transmission or reflection due to inhomogenities deliberately introduced into a transparent rotating fluid.
A specific embodyment of the invention will now be described by way of a non-limitative sxample with reference to the accompanying drawingsin which: Fig 1 Shows a container with an annular cavity filled with mercury and shaped to provide appropriate flow characteristics. The mercury is caused to flow round the cavity as a result of the field established by the permanent magnets and the current that passes through the mercury via electrodes. A second set of magnets and electrodes are used for the measurement of the potentials generated as a result of the flow of the conductive fluid.
Fig 2 shows the above cavity in section to show the rotating fluid and electrodes.
Fig 3 shows schematically typical electrical connections and an amplifier to increase the output from the sensor.
Referring to the drawings the rotation sensor comprises a container 10 that will be generally but not necessarily electrically insulating. Fixed to the container will be permanent magnets 11 and 12 with North and South poles as shown.
Within the cavity formed by the container a conductive fluid 13 rotates as a consequence of the electrical current passing through the fluid originating from electrodes 14 and within the field from magnets 11.
Inset graph 18 shows the symmetrical distribution, with no cavity rotation, of the fluid velocity around the centre line and along the axis of rotation of the fluid (continuous line) and the asymmetric distribution of velocity (dotted line) due to rotation of the cavity perpendicular to the axis of rotation of the fluid. The electrical potentials resulting from the movement of the conducting fluid through the field established by magnets 12 is conducted out of the cavity by means of electrodes 15 and 16.
The electrical connections in Fig 3. show the sensor arranged to provide a balanced output from electrodes 15 centre tapped to ground electrode 16. When the cavity is at rest the velocity gradient will be symmetrically disposed about the ground electrode 16 and the voltages appearing at electrodes 15 will be equal and opposite and therefore cancel, with the cavity rotating in the apropriate sensitive axis a torque will be applied to the rotating fluid which will be displaced in proportion to its velocity and will therefore unbalance the the output from electrodes 15 and provide an output in proportion to the rate of rotation of the cavity in the sensitive axis, amplifier 17 will raise the output to a useful level.

Claims (4)

1 A rotation sensor with an electrical output resulting from a gyroscopic torque in opposition to or at 90 degrees to an applied rotation and comprising a cavity filled with a conductive fluid and equipped with electrically conductive probes immersed in the conductive fluid and magnets fixed to the cavity such that the conductive fluid may be caused to rotate following a closed path around the cavity.
2 A rotation sensor as claimed in Claim 1 with alternating current exitation and alternating magnetic field to cause rotation of the conductive fluid following a closed path around the cavity.
3 A rotation sensor as claimed in claim 2 where rotation of the conductive fluid is by means of alternating electromagnetic fields with a controlled phase relationship such as to generate eddy currents in the conductive fluid to cause rotation.
4. A rotation sensor as in claims 1 to 3 where a second set of permanent magnets and electrodes is employed to develop electrical potentials in proportion to the distribution of velocity of flow of conductive fluid through a magnetic field and equipped with external electrical circuitry to develop an electrical output in proportion to the changing velocity distribution through the fluid brought about by rotation of the container.
5 A rotation sensor as in Claims 1 to 4 where the cavity is cylindrical.
6 A rotation sensor as in Claims 1 to 4 where the cavity is an annulus.
7 A rotation sensor as in Claims 1 to 4 where the cavity shape is torroidal.
8 A rotation sensor as in Claims 1 to 4 where the cavity is spherical or is the space between an inner sphere and an outer sphere and may provide outputs for rotation in two axes.
9 A rotation sensor as in Claims 1 to 8 where the cavity shape is designed to provide a radius of flow for the rotating fluid which varies along the axis and or circumference of fluid rotation to optimise flow profile for a particular application.
10 A rotation sensor as in claims 1 to 9 where the permanent magnets used for gradient sensing are replaced by solenoids energised by an alternating current and the electrodes immersed in the conducting fluid replaced by coils arranged to sense the field generated by currents induced in the conducting fluid by the previously mentioned solenoids energised by an alternating current. The relative amplitude and phase of the currents in the sense coils providing information on relative fow velocity in the conducting fluid.
11 A rotation sensor as in claims 1 to 10 where the cavity is electrically conducting and potentials resulting from a rotating conducting fluid are measured on the surface of the conducting container.
12 A rotation sensor as in claims 1 to 9 where the rotating fluid is optically transparent and rotation is sensed by variation in optical reflection or transmission due to the presence of a neutrally buoyant opaque or reflecting material capable of rotation with and within the rotating fluid.
13 A rotation sensor as in claims 1 to 9 where the rotating fluid is electrically conducting and rotation is sensed by variation of electrical resistivity due to the presence of neutrally buoyant material of differing electrical resistivity capable of rotation with and wihin the rotating fluid.
GB8915673A 1989-07-07 1989-07-07 An improved fluid rate sensor Expired - Fee Related GB2237638B (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
GB8915673A GB2237638B (en) 1989-07-07 1989-07-07 An improved fluid rate sensor
PCT/GB1990/001035 WO1991001008A1 (en) 1989-07-07 1990-07-05 Angular rate sentor
EP90909764A EP0486503A1 (en) 1989-07-07 1990-07-05 Angular rate sentor
JP2509761A JPH04506571A (en) 1989-07-07 1990-07-05 angular velocity sensor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB8915673A GB2237638B (en) 1989-07-07 1989-07-07 An improved fluid rate sensor

Publications (3)

Publication Number Publication Date
GB8915673D0 GB8915673D0 (en) 1989-08-23
GB2237638A true GB2237638A (en) 1991-05-08
GB2237638B GB2237638B (en) 1994-02-16

Family

ID=10659734

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8915673A Expired - Fee Related GB2237638B (en) 1989-07-07 1989-07-07 An improved fluid rate sensor

Country Status (4)

Country Link
EP (1) EP0486503A1 (en)
JP (1) JPH04506571A (en)
GB (1) GB2237638B (en)
WO (1) WO1991001008A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19633269A1 (en) * 1996-08-19 1998-02-26 Teves Gmbh Alfred Sensor for measuring yaw, pitch and / or roll movements

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110967001B (en) 2019-12-17 2023-09-26 重庆邮电大学 Cavity light mechanical vibration gyro

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB876433A (en) * 1959-09-30 1961-08-30 Vyzk A Zkusebni Letecky Ustav A gyroscopic rotor assembly
GB911355A (en) * 1960-08-30 1962-11-28 Speidel Corp Magnetohydrodynamic gyroscope
GB945800A (en) * 1959-05-26 1964-01-08 Speidel Ind Division Inc Gyroscope device
GB1125932A (en) * 1962-01-12 1968-09-05 Romald Edward Bowles Fluid vortex amplifier device exhibiting gyroscopic properties
GB1219890A (en) * 1968-01-08 1971-01-20 Harry Hirsch Herman Jr Improvements in or relating to gyroscopic devices

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4188576A (en) * 1978-09-11 1980-02-12 The United States Of America As Represented By The Secretary Of The Army Angular rate sensor
US4718276A (en) * 1986-04-10 1988-01-12 Applied Technology Associates, Inc. Angular motion sensor

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB945800A (en) * 1959-05-26 1964-01-08 Speidel Ind Division Inc Gyroscope device
GB876433A (en) * 1959-09-30 1961-08-30 Vyzk A Zkusebni Letecky Ustav A gyroscopic rotor assembly
GB911355A (en) * 1960-08-30 1962-11-28 Speidel Corp Magnetohydrodynamic gyroscope
GB1125932A (en) * 1962-01-12 1968-09-05 Romald Edward Bowles Fluid vortex amplifier device exhibiting gyroscopic properties
GB1219890A (en) * 1968-01-08 1971-01-20 Harry Hirsch Herman Jr Improvements in or relating to gyroscopic devices

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19633269A1 (en) * 1996-08-19 1998-02-26 Teves Gmbh Alfred Sensor for measuring yaw, pitch and / or roll movements
US6220095B1 (en) 1996-08-19 2001-04-24 Continental Teves Ag & Co., Ohg Sensor for measuring yaw, pitch or roll movements

Also Published As

Publication number Publication date
WO1991001008A1 (en) 1991-01-24
JPH04506571A (en) 1992-11-12
GB2237638B (en) 1994-02-16
EP0486503A4 (en) 1992-03-30
EP0486503A1 (en) 1992-05-27
GB8915673D0 (en) 1989-08-23

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Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee

Effective date: 19940516