GB2192718A - Accelerometer or seismometer - Google Patents
Accelerometer or seismometer Download PDFInfo
- Publication number
- GB2192718A GB2192718A GB8617159A GB8617159A GB2192718A GB 2192718 A GB2192718 A GB 2192718A GB 8617159 A GB8617159 A GB 8617159A GB 8617159 A GB8617159 A GB 8617159A GB 2192718 A GB2192718 A GB 2192718A
- Authority
- GB
- United Kingdom
- Prior art keywords
- movable body
- strain gauges
- beams
- accelerometer
- seismometer
- 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
Links
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
- G01P15/00—Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration
- G01P15/02—Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses
- G01P15/08—Measuring 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
- G01P15/12—Measuring 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 alteration of electrical resistance
- G01P15/123—Measuring 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 alteration of electrical resistance by piezo-resistive elements, e.g. semiconductor strain gauges
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
- G01P15/00—Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration
- G01P15/02—Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses
- G01P15/08—Measuring 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
- G01P15/0802—Details
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
- G01P15/00—Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration
- G01P15/02—Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses
- G01P15/08—Measuring 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
- G01P2015/0805—Measuring 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
- G01P2015/0808—Measuring 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 in-plane movement of the mass, i.e. movement of the mass in the plane of the substrate
- G01P2015/0811—Measuring 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 in-plane movement of the mass, i.e. movement of the mass in the plane of the substrate for one single degree of freedom of movement of the mass
- G01P2015/0814—Measuring 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 in-plane movement of the mass, i.e. movement of the mass in the plane of the substrate for one single degree of freedom of movement of the mass for translational movement of the mass, e.g. shuttle type
Abstract
An accelerometer or seismometer element consists of a rectangular movable body (1) of silicon mounted in a gap in a frame (2) also of silicon by U-shaped beams (3), also of silicon. The frame, beams and movable body are integral. Strain gauges are diffused into the beams at the ends of their legs. Overload movement is accommodated by buckling of the U-shaped beams, which move transverse to the direction of acceleration, this movement being facilitated by a bend or buckle in the beams. <IMAGE>
Description
SPECIFICATION
Accelerometer or seismometer
This invention relates to accelerometer or seismometer elements, and to the manufacture thereof.
Such an element has to have a high degree of sensitivity, and a substantially linear response to an applied force. Further it should not be subject to damage due to overloads.
An object of the invention is to provide an accelerometer or seismometer element which is more successful in meeting the above criteria than are many known devices.
According to one aspect of the invention there is provided an accelerometer or seismometer element, which includes a movable body supported by at least one elastic beam such that movement of the body in response to acceleration provides an output signal representative thereof, wherein said beam is of generally laminar form and has a bend lying in the plane of the beam such that the beam can buckle elastically in response to displacement of the body in a direction transverse to the direction of movement caused by the acceleration.
According to another aspect of the invention there is provided an accelerometer or seismometer element, which includes a movable body supported in an opening in a rigid laminar body by elastic beams, wherein each said beam is generally U-shaped with the end of one leg of its U integral with a portion of the movable body and the end of the other leg of that U integral with a portion of the laminar body adjacent to said portion of the movable body. The preferred material for making the accelerometer or seismometer element is silicon.Hence the invention further provides an accelerometer or seismometer element, which includes a rectangular movable body of silicon supported in a rectangular opening in a rigid laminar body af silicon by elastic beams of silicon, the movable body, the beams and the laminar body all being integral, wherein the beams are rendered elastic by being considerably thinner than the movable body and the laminar body, and wherein each said beam is generally U-shaped with the end of one leg integral with a portion of the movable body and the end of the -other leg of the U integral with a portion of the laminar body adjacent to said portion of the movable body.
An embodiment of the invention will now be described with reference to the accompanying drawings, in which Fig. 1 is a plan view of an accelerometer or seismometer element embodying the invention, Fig. 2 is a partial view of an element such as that of Fig.1 installed on a support member, and Fig. 3 is an enlarged view of the arrangement of strain gauges used in a device such as that shown in Fig. 1.
The element shown in plan in Fig. 1 is an accelerometer made from silicon. It includes a movable body 1 which is integral with, and connected to an outer laminar frame body 2 by elastic beams formed by thin U-shaped flexible regions 3. The U-shaped regions carry strain gauges such as 4 diffused into the flexible region 3. Thus the motion of-the element 1 relative to the frame 2 is sensed by these strain gauges.
The thin flexible regions are produced by selective etching. Thus when using a p-type wafer of silicon as the starting point, the area which, in the final product, will be thin is diffused with an n-type dopant such es phosphorous. Separate electrical contacts are made to the p and n doped areas which are held at different potentials during the doping. Thus it is possible to cause the n-type materialto etch normally, but for the p-type material not to be etched at all.
Fig. 2 shows, partly in perspective and partly in section an element such as that of
Fig. 1 mounted to a support member 5, which could also be of silicon. It will be- seen that the edges of the movable body 1 are bevelled and that that body 1 fits into a recess 6 in the support member 5. This recess is bevelled in a similar way to the body 1, so that it restrains it from excessive movement.
Fig. 2 also shows how relative movement of the body 1 and the frame body 2 occur, with the U-shaped regions such as 3 buckling or bending to accommodate the movement. It will be noted that "end-wise" movement of the body 1 is accommodated by such buckling, and that here the sides of the recess 6 act to limit the "end-wise" movement of the body 1.
Fig. 3 shows on an enlarged scale the ar- rangements of the strain gauges on one of the
U-shaped portions, the others being similar.
We see two strain gauges 10 and 11-, one on each leg of the U, with the strain gauges set at 90 to each other. These gauges are coupled in series by conductive tracks 12 and 13, which, like the strain gauges, are diffused into the silicon of the legs of the U. Finally there are contact pads 14 and 15, connected to the strain gauge 10 and the track 73 respectively.
Setting the strain gauges at 90" is convenient for the arrangement of the pads and the tracks, and has also been found to give good results electrically.
The manner of mounting of the movable body 1 and the relative dimensions of the various parts of the element are such that the rigidity of the body 1 in the plane relative to its rigidity in the movement duration is of the order of 100:1 where the accelerations to be measured are of the order of 30 to 50G.
Thus the element can tolerate transverse accelerations of the order of 3000 to 10000G.
Devices such as described above can be used as the sensing means in accelerometers
and seismometers. Accelerometers of this sort
can be used in.-inertiel guidance systems, e.g.
in missiles or in aircraft navigation equipment.
The type of accelerometer or seismometer
element described herein has a number of ad
vantages:
(a) Because it is symmetrical, unwanted in
puts tend to cancel out.
(b) The design is compact because the U
shaped cantilevers are folded.
(c) There is no stress stiffening with larger
deflections to make the output non-linear.
(d) The arrangement of two strain gauges on each cantilever makes the design insensi
tive to curvature of the beams caused by ox
ide layers on the top surface. Such layers are
essential to passivate the strain gauges, but
tend 'to make the cantilever bend as a result
of differential thermal expansion.
(e) Oyerloads in the. direction in the plane of
the cantilevers, i.e. "send-wise deflections",
cause a harmless buckling, which allows the
seismic mass to move an appreciable distance
so that overload stops can be provided with a
reasonable clearance.
In one example of element embodying the
invention, the movable body is 6mm long and
4mm wide, and is about 2mm thick. The
body in this case is made up of a central portion:0.5mm thick, flanked in-sandwich
manner to give the overall thickness of 2mm.
The U-shaped beams then have thicknesses in
the range of 5 to 8 microns.
Claims (7)
1-. An accelerometer or seismometer ele
ment, which includes a movable body sup -ported by at least one elastic beam such that
movement of the body in response to acceleraction provides. an output signal representative
thereof, wherein said beam is of generally laminar form and has a bend lying in the plane
of the beam such that the beam can buckle
elastically in response to displacement of the
body in a direction transverse to the direction .of movement caused by the acceleration.
2. An accelerometer or seismometer ele
ment, which includes a movable body sup
ported in an opening in a rigid laminar body
by elastic beams, wherein each said beam is
generally U-shaped with the end of one leg of
its U integral with a portion of-the movable -body and the. end of the other leg of that U
integral with a portion of the laminar body
adjacent to said portion of the movable body.
3. An. accelerometer or seismometer ele ment,-which includes a rectangular movable body of silicon supported in a rectangular
opening in a rigid laminar body of silicon by
elastic beams of silicon, the movable body,
the beams and the laminar body all beinginte- gral, wherein the beams are rendered elastic by being considerably thinner than the mov
able body and the laminar body, and wherein -each said beam is generally U-shaped with the end of one leg integral with a portion of the movable body and the end of the other leg of the U integral with a portion of the laminar body adjacent to said portion of the movable body.
4. An element as claimed in claim 2 or 3, wherein the U-shaped beams carry strain gauges, with each said beam carrying two strain gauges, one near the end of each leg of the U.
5. An element as claimed in claim 4, wherein the strain gauges are each of zig-zag shape with the two strain gauges of a said U set at right angles to each other, and wherein the strain gauges of the same U are connected in series by conductive tracks on the
U.
6. An element as claimed in claim 5, wherein the strain gauges and the associated tracks are produced by diffusion.
7. An accelerometer or seismometer element, substantially as described with reference to the accompanying drawings.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB8617159A GB2192718B (en) | 1986-07-15 | 1986-07-15 | Accelerometer or seismometer |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB8617159A GB2192718B (en) | 1986-07-15 | 1986-07-15 | Accelerometer or seismometer |
Publications (3)
Publication Number | Publication Date |
---|---|
GB8617159D0 GB8617159D0 (en) | 1986-11-26 |
GB2192718A true GB2192718A (en) | 1988-01-20 |
GB2192718B GB2192718B (en) | 1990-06-13 |
Family
ID=10601052
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB8617159A Expired - Fee Related GB2192718B (en) | 1986-07-15 | 1986-07-15 | Accelerometer or seismometer |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB2192718B (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1031837A1 (en) * | 1999-02-23 | 2000-08-30 | First Inertia Switch Limited | Acceleration sensitive devices |
EP1096260A1 (en) * | 1999-10-29 | 2001-05-02 | SensoNor asa | Micromechanical device |
WO2001044823A1 (en) * | 1999-12-16 | 2001-06-21 | Robert Bosch Gmbh | Micromechanical spring structure, especially for a rotational speed sensor |
WO2003016919A1 (en) * | 2001-08-20 | 2003-02-27 | Honeywell International Inc. | Micro-machined electromechanical system (mems) accelerometer device having arcuately shaped flexures |
US7140250B2 (en) | 2005-02-18 | 2006-11-28 | Honeywell International Inc. | MEMS teeter-totter accelerometer having reduced non-linearty |
-
1986
- 1986-07-15 GB GB8617159A patent/GB2192718B/en not_active Expired - Fee Related
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1031837A1 (en) * | 1999-02-23 | 2000-08-30 | First Inertia Switch Limited | Acceleration sensitive devices |
EP1096260A1 (en) * | 1999-10-29 | 2001-05-02 | SensoNor asa | Micromechanical device |
WO2001044823A1 (en) * | 1999-12-16 | 2001-06-21 | Robert Bosch Gmbh | Micromechanical spring structure, especially for a rotational speed sensor |
JP2003517612A (en) * | 1999-12-16 | 2003-05-27 | ローベルト ボツシユ ゲゼルシヤフト ミツト ベシユレンクテル ハフツング | Micromechanical spring structure, especially for yaw rate sensors |
US6571629B1 (en) | 1999-12-16 | 2003-06-03 | Robert Bosch Gmbh | Micromechanical spring structure, in particular, for a rotation rate sensor |
WO2003016919A1 (en) * | 2001-08-20 | 2003-02-27 | Honeywell International Inc. | Micro-machined electromechanical system (mems) accelerometer device having arcuately shaped flexures |
US6897538B2 (en) | 2001-08-20 | 2005-05-24 | Honeywell International, Inc. | Micro-machined electromechanical system (MEMS) accelerometer device having arcuately shaped flexures |
US6991957B2 (en) | 2001-08-20 | 2006-01-31 | Honeywell International, Inc. | Micro-machined electromechanical system (MEMS) accelerometer device having arcuately shaped flexures |
US7140250B2 (en) | 2005-02-18 | 2006-11-28 | Honeywell International Inc. | MEMS teeter-totter accelerometer having reduced non-linearty |
Also Published As
Publication number | Publication date |
---|---|
GB2192718B (en) | 1990-06-13 |
GB8617159D0 (en) | 1986-11-26 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
732E | Amendments to the register in respect of changes of name or changes affecting rights (sect. 32/1977) | ||
732E | Amendments to the register in respect of changes of name or changes affecting rights (sect. 32/1977) | ||
PCNP | Patent ceased through non-payment of renewal fee |
Effective date: 20040715 |