Measuring and testing – Speed – velocity – or acceleration – Angular rate using gyroscopic or coriolis effect
Patent
1985-12-04
1987-09-01
Chapman, John
Measuring and testing
Speed, velocity, or acceleration
Angular rate using gyroscopic or coriolis effect
73517R, 73DIG4, 310329, 310332, 310333, 310800, G01P 904, H01L 4108
Patent
active
046899928
DESCRIPTION:
BRIEF SUMMARY
DESCRIPTION
This invention relates to a device for sensing acceleration, particularly rate of rotation, and to apparatus incorporating such devices.
It is of course well known to sense rotational acceleration by means of a gyroscope, and to provide inertial platforms and the like by a plurality of gyroscopes rotating about different axes. Such apparatus is extremely accurate but is also expensive.
An object of the present invention is to provide a simple and inexpensive rate sensor which has sufficient accuracy for certain applications.
The invention accordingly provides a device for measuring rotation, comprising a laminar assembly and means mounting said assembly so as to lie, in a rest condition, in a reference plane containing a central longitudinal axis; said assembly comprising a first piezoelectric member connected to an oscillator to produce oscillation of said assembly transverse to said reference plane, and a second piezoelectric member arranged to generate an electrical output when stressed in a direction oblique to said oscillation, said second piezoelectric member comprising two polarized polymeric piezoelectric films arranged in a common plane along said axis each with its main uniaxial mode transverse to said axis, and connected together in series; whereby said electrical output is a function of twisting of said assembly about said axis.
In a preferred form, said first piezoelectric member comprises two sheets of polarized polymeric piezoelectric material secured to and insulated from each other and having their main uniaxial mode aligned with said longitudinal axis, said two sheets being oppositely connected to said oscillator. The second piezoelectric member suitably comprises a further sheet of like material having its main uniaxial mode transverse to said longitudinal axis. The material may suitably by polyvinylidene fluoride (PVDF). A suitable form of this material is sold as KYNAR (Trade Mark) film by Pennwalt Corporation, King of Prussia, Pa. 19406, USA.
From another aspect, the invention provides apparatus including a plurality of devices as defined above arranged with their said longitudinal axes mutually perpendicular, whereby movement of the apparatus in a two-dimensional plane or in three-dimensional space may be measured.
An embodiment of the invention will now be described, by way of example, with reference to the accompanying drawings, in which:
FIG. 1 is a schematic perspective view of a device embodying the invention,
FIG. 2 is an exploded schematic view of part of the device of FIG. 1, and
FIG. 3 illustrates a modification.
The device comprises a sheet laminate 10 clamped at its top and bottom edges by parts 12,14 of a rigid housing (the remainder of which is not shown) such that in its rest position the laminate 10 lies in a reference plane having a longitudinal axis designated at 16.
As shown more clearly in FIG. 2, the laminate 10 consists of three sheets 18,20,22 bonded together. Each of these sheets is of polarised PVDF film. The first and second sheets 18 and 20 have the main uniaxial mode 19 of the film aligned with the axis 16, while the third sheet 22 has its main uniaxial mode 23 at right angles to the axis 16. The three sheets 18,20,22 are bonded together by any suitable insulating adhesive.
The first and second sheets 18 and 20 are oppositely connected to an oscillator 24. The applied electric signal thus causes one sheet to lengthen while the other contracts and vice versa, and the laminate oscillates transverse to the axis 16. The oscillator 24 suitably oscillates at the resonant frequency of the mechanical system. In this mode of operation the third sheet 22 experiences stress in a direction normal to its main uniaxial mode, and the voltage induced therein is small (a few millivolts). However, if the housing is rotated about the axis 16, as indicated by arrow 26, the oscillating laminate has an inertia which tends to resist movement out of its initial position; this results in twisting of the laminate 10, the top and bottom edges moving with the housing but
REFERENCES:
patent: 3219850 (1965-11-01), Langevin
patent: 3520195 (1970-07-01), Tehon
patent: 3903733 (1975-09-01), Murayama et al.
patent: 3971250 (1976-07-01), Taylor
patent: 4489609 (1984-12-01), Burdess et al.
Chapman John
Syrinx Innovations Limited
LandOfFree
Rotation rate sensor does not yet have a rating. At this time, there are no reviews or comments for this patent.
If you have personal experience with Rotation rate sensor, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Rotation rate sensor will most certainly appreciate the feedback.
Profile ID: LFUS-PAI-O-1257184