GB2225433A - Capacitive-effect acceleration transducer - Google Patents

Capacitive-effect acceleration transducer Download PDF

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Publication number
GB2225433A
GB2225433A GB8926379A GB8926379A GB2225433A GB 2225433 A GB2225433 A GB 2225433A GB 8926379 A GB8926379 A GB 8926379A GB 8926379 A GB8926379 A GB 8926379A GB 2225433 A GB2225433 A GB 2225433A
Authority
GB
United Kingdom
Prior art keywords
blade
capacitor
acceleration
fixed
transducer according
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
GB8926379A
Other versions
GB2225433B (en
GB8926379D0 (en
Inventor
Orto Giuseppe Dell
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.)
Marelli Europe SpA
Original Assignee
Marelli Autronica SpA
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 Marelli Autronica SpA filed Critical Marelli Autronica SpA
Publication of GB8926379D0 publication Critical patent/GB8926379D0/en
Publication of GB2225433A publication Critical patent/GB2225433A/en
Application granted granted Critical
Publication of GB2225433B publication Critical patent/GB2225433B/en
Anticipated expiration legal-status Critical
Expired - Fee Related 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
    • G01P15/125Measuring 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 by capacitive pick-up
    • 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
    • G01P2015/0805Measuring 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 being provided with a particular type of spring-mass-system for defining the displacement of a seismic mass due to an external acceleration
    • G01P2015/0822Measuring 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 being provided with a particular type of spring-mass-system for defining the displacement of a seismic mass due to an external acceleration for defining out-of-plane movement of the mass
    • G01P2015/0825Measuring 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 being provided with a particular type of spring-mass-system for defining the displacement of a seismic mass due to an external acceleration for defining out-of-plane movement of the mass for one single degree of freedom of movement of the mass
    • G01P2015/0828Measuring 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 being provided with a particular type of spring-mass-system for defining the displacement of a seismic mass due to an external acceleration for defining out-of-plane movement of the mass for one single degree of freedom of movement of the mass the mass being of the paddle type being suspended at one of its longitudinal ends

Landscapes

  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Pressure Sensors (AREA)

Abstract

The transducer includes a support plate 2 and a support 4 to which is cantilevered a flexible metal blade 6 which faces and is spaced from a fixed metal plate member 3 so as to constitute a capacitor whose capacitance is variable in dependence on the acceleration to which it is subjected. The support plate 2 is of insulating material and plate 3 may be a deposited thin metal layer, or may comprise a second metal blade also cantilevered from support 4. Detector means are provided for producing an electrical signal indicative of the capacitance of the capacitor and hence of the acceleration. The capacitor may either affect the frequency of an oscillator with subsequent voltage to frequency conversion or a fixed oscillator may be connected to a monostable with pulse duration controlled by the capacitor. <IMAGE>

Description

DESCRIPTION '1A capacitive-effect acceleration transducer" The present invention relates to a capacitive-effect acceleration transducer, characterised in that it includes in combination: - a support structure which is intended to be fixed to the body whose acceleration is to be detected7 - a metal plate member carried by the support, - a flexible metal blade having a first end by which it is cantilevered from the support structure and a second end facing and spaced from the plate member in the direction in which the acceleration is to be detected, so as to constitute therewith a capacitor whose capacitance has a predetermined value at rest and is variable in dependence on the acceleration of the body in the said direction, and - detector means for providing an electrical signal indicative of the capacitance of the capacitor.
By virtue of these characteristics, the transducer is simple, precise and reliable.
The invention will now be described in detail with reference to the appended drawings, provided purely by way of non-limiting example, in which: Figure 1 is a perspective view of an acceleration transducer according to the present invention, Figure 2 is a view taken on the arrow II of Figure 1, Figures 3, 4 and 5 are perspective views showing three alternative embodiments of the transducer according to the invention, Figure 6 is a view taken on the arrow VI of Figure 4, Figure 7 is a section taken on the line Vil-Vil of Figure 5, and Figure 8 is a block diagram showing the operation of an electronic circuit associated with the transducer according to the invention.
In the drawings, a capacitive-effect acceleration transducer is indicated 1. With reference to Figures 1 and 2, the transducer includes a support plate 2 of electrically insulating material which is intended to be fixed to the surface of the body (not shown) whose acceleration is to be detected. A plate member 3 constituted by a metal block and a support 4 whose thickness is slightly greater than that of the block 3 are fixed to the plate 2. The transducer 1 also includes a flexible metal blade 5, for example of string steel, having a first end 6 by which it is cantilevered from the support 4 and a second end 7 facing and spaced from the upper surface of the block 3. The end 7 of the blade 5 and the plate member 3 thus define a capacitor which has a predetermined value at rest.A mass 8 is provided at the end 7 of the blade 5 and is fixed to the opposite surface of the blade from the plate member 3.
When the transducer 1 is subjected to an acceleration in a direction perpendicular to the plate member 3 and the blade 5, that is, parallel with the line shown by the double arrow A in the drawings, the mass 8 is subjected to a force which causes the free end 7 of the blade to oscillate. This oscillation causes a variation in the capacitance of the capacitor defined by the plate member 3 and the blade 5. This variation in capacitance is detected by an electronic circuit, which will be described further below, to which the plate member 3 and the blade 5 are connected by means of two electrical conductors 9.
In the variant illustrated in Figure 3, the fixed plate member 3 is replaced by a second flexible blade 10 cantilevered from the support 4 to which the first blade 5 is fixed. The two blades 5 and 10 are kept apart by a layer 11 of electrically-insulating material. A mass 12 which, like the mass 8 fixed to the first blade 5, is sensitive to acceleration in the direction indicated by the double arrow A, is also fixed to the free end of the second blade 10.
In the embodiment shown in Figures 4 and 6, the support plate 2 is made of ceramics. The fixed plate member 3 is constituted by a thin metal layer deposited on the surface of the ceramic plate 2 by silk-screen printing, drying and baking. The material constituting the metal deposits is, for example, platinum-gold or palladium-silver. The flexible blade 5 may be of brass, in which case it can be soldered with tin to a metal layer 15 deposited on the ceramic plate 2. In this case, the thickness of the material added by the soldering also serves to keep the plate member 3 and the flexible blade 5 apart. Alternatively, the blade 5 can be glued to the support plate 2 and in this case it is necessary to establish an electrical connection between the blade 5 and the metal layer 15, as indicated by broken lines 16 in Figures 4 to 6.
According to a further variant shown in Figures 5 to 7, a printed circuit 18 can be used as the support plate and, in this case, the fixed , plate member is constituted by a metal layer 19 of the circuit. The flexible blade 5 is fixed to the printed circuit 18 by means of screws 20, with the interposition of a metal spacer 21. The spacer 21 connects the blade 5 electrically to a metal layer 22 of the printed circuit. The layers 18 and 22 are connected electrically to the components of an electronic circuit provided on the printed circuit 18.
Figure 8 shows a block diagram of an electronic detection circuit associated with the transducer 1.
According to a first embodiment, the capacitor constituted by the transducer 1 is connected to an oscillator 25 whose frequency depends on the capacitance of the capacitor. The signal output by the oscillator 25 is sent to a monostable circuit 26 and then te a low-pass filter 27. A frequency-voltage conversion is thus achieved. The voltage signal V output by the filter 27 is thus indicative of the value of the capacitance of the transducer 1 and hence of the acceleration to which the latter is subjected.
Alternatively, the oscillator 25 may work at a fixed frequency, whilst the transducer 1 is connected to the monostable circuit 26, as shown by the broken lines in Figure 8. The duration of the signal of the monostable circuit 26 is thus modulated and, as in the previous case, the output signal V obtained is proportional to the value of the acceleration to which the transducer 1 is subjected.

Claims (10)

1. A capacitive-effect acceleration transducer, characterised in that it includes in combination: - a support structure which is intended to be fixed to the body whose acceleration is to be detected, - a metal plate member carried by the support, - a flexible metal blade having a first end by which it is cantilevered from the support structure and a second end facing and spaced from the plate member so as to constitute therewith a capacitor whose capacitance has a predetermined value at rest and is variable in dependence on the acceleration of the body in the direction , and - detector means for providing an electrical signal indicative of the capacitance of the capacitor.
2. A transducer according to Claim 1, characterised in that the plate member is fixed and is carried by the support structure.
3. A transducer according to Claim 1, characterised in that the plate member is constituted by a second flexible metal blade also having a first end by which it is cantilevered from the support structure and its other end facing and spaced from the first blade.
4. A transducer according to any one of the preceding claims, characterised in that a mass is fixed to the first blade and is subject to the action of the acceleration to be detected in use.
5. A transducer according to Claims 3 and 4, characterised in that a mass is also fixed to the second blade and is subject to the action of the acceleration to be detected in use.
6. A transducer according to Claim 5, characterised in that the masses associated with the first blade and and with the second blade are fixed to those surfaces of the blades which do not face each other.
7. A transducer according to Claim 2, characterised in that the plate member is constituted by a layer of conductive material deposited on a support base of electrically-insulating material.
8. A transducer according to any one of the preceding claims, characterised in that the detector means comprise an electronic circuit including an oscillator whose frequency depends on the capacitance of the capacitor) and a frequency-voltage converter connected to the output of the oscillator,
9. A transducer according to any one of Claims 1 to 7, characterised in that an electronic circuit is associated with the capacitor and includes a fixed-frequency oscillator and a monostable circuit whose input is connected to the output of the oscillator the monostable circuit being adapted to output a pulse whose duration depends on the capacitance of the capacitor
10. A capacitative-effect acceleration transducer substantially as hereinbefore described with reference to Figures 1 and 2, or Figure 3, or Figures 4 and 6 or Figures 5 and 7, together with Figure 8 of the accompanying drawings.
GB8926379A 1988-11-23 1989-11-22 A capacitive-effect acceleration transducer Expired - Fee Related GB2225433B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
IT68046/88A IT1223933B (en) 1988-11-23 1988-11-23 CAPACITIVE ACCELERATION TRANSDUCER

Publications (3)

Publication Number Publication Date
GB8926379D0 GB8926379D0 (en) 1990-01-10
GB2225433A true GB2225433A (en) 1990-05-30
GB2225433B GB2225433B (en) 1993-01-27

Family

ID=11307438

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8926379A Expired - Fee Related GB2225433B (en) 1988-11-23 1989-11-22 A capacitive-effect acceleration transducer

Country Status (5)

Country Link
DE (1) DE8913756U1 (en)
ES (1) ES1012120Y (en)
FR (1) FR2639435B3 (en)
GB (1) GB2225433B (en)
IT (1) IT1223933B (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5128581A (en) * 1989-05-02 1992-07-07 Fujikura Ltd. Piezoelectric acceleration sensor and piezoelectric acceleration sensor device
US5438859A (en) * 1991-09-24 1995-08-08 Murata Manufacturing Co. Ltd. Acceleration sensor having fault diagnosing device

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5239871A (en) * 1990-12-17 1993-08-31 Texas Instruments Incorporated Capacitive accelerometer
DE4244560A1 (en) * 1992-12-30 1994-07-07 Akebono Brake Ind Acceleration detection method providing 2-dimensional acceleration measurements
US5555766A (en) * 1993-11-04 1996-09-17 Texas Instruments Incorporated Acceleration sensor apparatus and method for making same
DE10053309B4 (en) * 2000-10-27 2005-02-24 Eads Deutschland Gmbh Micromechanical acceleration sensor

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1303025A (en) * 1970-11-12 1973-01-17
WO1987007729A1 (en) * 1986-06-10 1987-12-17 Metravib R.D.S. Silicon-integrated pick-up for measuring mechanical magnitudes, and method of fabrication
US4736629A (en) * 1985-12-20 1988-04-12 Silicon Designs, Inc. Micro-miniature accelerometer

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4951510A (en) * 1988-07-14 1990-08-28 University Of Hawaii Multidimensional force sensor

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1303025A (en) * 1970-11-12 1973-01-17
US4736629A (en) * 1985-12-20 1988-04-12 Silicon Designs, Inc. Micro-miniature accelerometer
WO1987007729A1 (en) * 1986-06-10 1987-12-17 Metravib R.D.S. Silicon-integrated pick-up for measuring mechanical magnitudes, and method of fabrication

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5128581A (en) * 1989-05-02 1992-07-07 Fujikura Ltd. Piezoelectric acceleration sensor and piezoelectric acceleration sensor device
US5438859A (en) * 1991-09-24 1995-08-08 Murata Manufacturing Co. Ltd. Acceleration sensor having fault diagnosing device
US5517845A (en) * 1991-09-24 1996-05-21 Murata Manufacturing Co., Ltd. Acceleration sensor having fault diagnosing device

Also Published As

Publication number Publication date
ES1012120Y (en) 1991-01-01
ES1012120U (en) 1990-07-01
FR2639435B3 (en) 1990-10-12
GB2225433B (en) 1993-01-27
DE8913756U1 (en) 1990-01-11
GB8926379D0 (en) 1990-01-10
FR2639435A3 (en) 1990-05-25
IT1223933B (en) 1990-09-29
IT8868046A0 (en) 1988-11-23

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PCNP Patent ceased through non-payment of renewal fee

Effective date: 19991122