GB1282579A - Angular velocity sensors - Google Patents

Angular velocity sensors

Info

Publication number
GB1282579A
GB1282579A GB60711/69A GB6071169A GB1282579A GB 1282579 A GB1282579 A GB 1282579A GB 60711/69 A GB60711/69 A GB 60711/69A GB 6071169 A GB6071169 A GB 6071169A GB 1282579 A GB1282579 A GB 1282579A
Authority
GB
United Kingdom
Prior art keywords
axis
angular velocity
output
accelerometer
disc
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.)
Expired
Application number
GB60711/69A
Inventor
Vernon H Aske
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.)
Honeywell Inc
Original Assignee
Honeywell Inc
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 Honeywell Inc filed Critical Honeywell Inc
Publication of GB1282579A publication Critical patent/GB1282579A/en
Expired legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01PMEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
    • G01P15/00Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration
    • G01P15/02Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses
    • G01P15/08Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses with conversion into electric or magnetic values
    • G01P15/0888Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses with conversion into electric or magnetic values for indicating angular acceleration
    • 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
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01PMEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
    • G01P15/00Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration
    • G01P15/02Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses
    • G01P15/08Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses with conversion into electric or magnetic values
    • 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
    • G01P3/42Devices characterised by the use of electric or magnetic means
    • G01P3/44Devices characterised by the use of electric or magnetic means for measuring angular speed
    • G01P3/46Devices characterised by the use of electric or magnetic means for measuring angular speed by measuring amplitude of generated current or voltage

Abstract

1282579 Measuring angular velocity electrically HONEYWELL Inc 12 Dec 1969 [19 Dec 1968] 60711/69 Heading G1N An arrangement for measuring angular velocity about an axis (axis 1) comprises an accelerometer sensitive to angular acceleration about an axis (axis 11) and means for moving, e.g. oscillating or rotating, the accelerometer so that the angle between the two axes varies whereby the accelerometer gives an output dependent on the angular velocity about axis 1. Consider an accelerometer, shown as a disc 7, sensitive to acceleration about an axis 11 perpendicular to the disc. Now consider rotation about an axis in space 1 at a constant angular velocity w m , which it is desired to measure. In the position shown in Fig. 1A the accelerometer would give no output since w m is constant. Now consider rotation of the disc about an axis 10 at some angular velocity w, say 8000r.p.m. The disc rotates through the positions shown in Fig. 1B, 1C, 1D. In Fig.1C the "heads" side of the disc is now lowermost instead of uppermost as in 1A. The rotation w m is now anti-clockwise with respect to this "heads" side i. e. to the sensitive axis 11, instead of clockwise in Fig. 1A. The change in rotation indicates that the accelerometer has been subject to acceleration about the axis 11, and it will therefore yield an output as the disc rotates. 'This output therefore has a sinusoidal form, Fig. 1E, whose frequency depends on the rotational velocity and whose maximum amplitude depends on the rotational velocity w m . It will be clear that the axis M about which angular velocity is to be measured could lie along the direction 2 instead of the direction 1, or indeed in any direction in the plane of 1 and 2 since these are all scanned by the axis 11 during rotation about 10. Similarly since any other direction can be resolved into one input in this plane and one component in the direction 10, it is possible to obtain a measure of angular velocity about any axis except direction 10. The accelerometer which is shown in Fig.2 functions on the principle of an MHD generator. A radially magnetized annular magnet 22 produces flux which passes radially through an annulus of mercury 25 in a casing, and returns through ferromagnetic slugs 22. Movement of the mercury develops an emf resulting in a current which links a toroidal pick-up coil 19 in which the associated output current is developed. The casing has a projection 31 on which is mounted the rotor 30 of an induction motor which rotates the casing about the axis 10. In operation acceleration about the axis 11 will cause the magnet to rotate while under idealized conditions (such as arise when the rotational speed w r is above 1000r.p.m.) the mercury remains stationary in its plane. An output of sinusoidal form is thereby obtained whose maximum amplitude is a measure of the angular velocity about an axis within the plane of 1 and 2. A demodulating arrangement is provided to extract from this output signal components representative of the components of this velocity about the axes 1 and 2. As shown a pair of coils 33 aligned parallel with the axis 1 and a second pair (not shown) as right angles thereto are influenced by a permanent magnet on the projection 31. The output signals are fed, together with the output from coil 20 to demodulators 41, 42, to provide outputs indicative of the two components on calibrated meters 3, 4. If the mercury cannot be considered as stationary i.e. if the rotational speed w, is less than say 1000 r. p. m. the output voltage is not directly proportional to the angular velocity being measured and correction must be made for the rotational speed w,. A further form of accelerometer is disclosed, Figs. 4 and 5 (not shown) in which an annulus of mercury is again provided but the arrangement of magnets and pick-up coils is different.
GB60711/69A 1968-12-19 1969-12-12 Angular velocity sensors Expired GB1282579A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US78525268A 1968-12-19 1968-12-19

Publications (1)

Publication Number Publication Date
GB1282579A true GB1282579A (en) 1972-07-19

Family

ID=25134895

Family Applications (1)

Application Number Title Priority Date Filing Date
GB60711/69A Expired GB1282579A (en) 1968-12-19 1969-12-12 Angular velocity sensors

Country Status (12)

Country Link
JP (1) JPS4938462B1 (en)
AT (1) AT293069B (en)
BE (1) BE743266A (en)
CA (1) CA941635A (en)
CH (1) CH503997A (en)
DE (1) DE1962136C3 (en)
DK (1) DK143046C (en)
FR (1) FR2026574A1 (en)
GB (1) GB1282579A (en)
NL (1) NL6918942A (en)
SE (1) SE351296B (en)
YU (1) YU33637B (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1987002140A1 (en) * 1982-11-20 1987-04-09 Mueller Paul Process for determining speed of rotation
DE3921560A1 (en) * 1989-06-30 1991-01-10 Deutsche Forsch Luft Raumfahrt METHOD AND DEVICE FOR DETERMINING ACCELERATIONS WITH HIGH PRECISION
CN110793517B (en) * 2019-10-23 2024-04-02 天津大学 Broadband micro angular velocity measurement method based on multi-rate fusion technology
CN112379118B (en) * 2020-11-16 2021-12-07 北京理工大学 Rotational angular velocity and rotational angular acceleration integrated measuring device

Also Published As

Publication number Publication date
DE1962136A1 (en) 1970-07-02
DK143046C (en) 1981-10-12
CH503997A (en) 1971-02-28
YU33637B (en) 1977-10-31
AT293069B (en) 1971-09-27
BE743266A (en) 1970-05-28
NL6918942A (en) 1970-06-23
FR2026574A1 (en) 1970-09-18
DK143046B (en) 1981-03-16
SE351296B (en) 1972-11-20
DE1962136B2 (en) 1978-04-13
JPS4938462B1 (en) 1974-10-17
YU317369A (en) 1977-04-30
CA941635A (en) 1974-02-12
DE1962136C3 (en) 1979-01-04

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Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
PCNP Patent ceased through non-payment of renewal fee