Background of the Invention
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This invention relates to a switch for sensing
acceleration and, more particularly, to a switch that is
actuated by a predetermined acceleration level, where the
predetermined level may be electrically adjusted.
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Automotive occupant restraint systems have, in prior
times, used a distributed array of inertia-operated
mechanical switches to sense the onset of a collision and
trigger the actuation of the restraint system (e.g., a seat
belt retractor or an air bag). More recently, the
distributed arrays of mechanical switches have been
replaced by one or more electronic acceleration sensors
working in cooperation with a microprocessor and
sophisticated software. The sensors provide electronic
signals proportional to vehicle acceleration. The
microprocessor assesses the frequent and rapid changes in
the vehicle's acceleration and determines from this whether
a crash event is in progress that requires the actuation of
the occupant restraint systems.
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Systems using acceleration sensors typically still
include one inertia-operated mechanical switch, usually
referred to as a "safing switch", for providing a redundant
level of detection of the crash event. The safing switch
is designed and calibrated to close at a relatively early
stage in a crash event. Closure of the safing switch is a
necessary condition but not the sole determinant in
controlling actuation of the occupant restraint, however.
The occupant restraint is only actuated when the
microprocessor determines that the severity of the crash is
sufficient to warrant such actuation.
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Safing switches presently in use employ an inertial
mass which moves, upon vehicle deceleration, against the
resilience of a spring. Electrical contacts associated
with the switch are coupled to the mass in such a way that
the contacts close when the mass moves a certain distance
from its initial, or rest, position. Since the
deceleration impulse representative of a significant crash
varies from one vehicle type to another, the switch design
often must be modified to some extent from one vehicle type
to another such that the switch will, in each case, close
at the appropriate time for that particular vehicle type.
Normal manufacturing tolerances, however, still cause the
switch actuation point to vary from switch to switch.
Thus, each individual safing switch is calibrated during
manufacture to "fine tuned" the switch closure to the proper
deceleration impulse point selected for that vehicle type.
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Safing switches now in use are manufactured by
processes generally similar to those used to assemble other
small mechanical devices. Efforts have been made, however,
to develop smaller switches which could be manufactured
using techniques like those used to manufacture
semiconductor components and/or micromachined silicon
elements. Patents describing such micromachined switch
devices include U.S. Patent Nos. 5,177,331, 4,855,544,
and 4,543,457.
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U.S. Patent No. 5,177,331 discloses an "impact sensor"
formed of micromachined silicon. The "impact sensor"
includes contacts that close when the sensor is subjected
to an impact. The sensor further includes electrodes
between which an electrostatic field appears, creating a
force tending to urge the contacts to close. When the
contacts are in their unactuated position, the force is too
small to perturb the contacts into the closed position.
When the contacts close due to an impact, however, the
nearness of the electrodes substantially increases the
magnitude of the electrostatic field and the resulting
force. The increased electrostatic force latches the
contacts in the closed position until the field is
released.
Summary of the Invention
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It is a primary object of the present invention to
provide an acceleration switch that will be actuated when
subjected to a force greater than a predetermined
magnitude, where the magnitude of the force required to
actuate the switch can be electrically adjusted.
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In accordance with the present invention, a switch is
provided that is responsive to a predetermined acceleration
force. The switch includes an inertial mass member ("IMM")
movable from a hold condition to an operative condition,
wherein the member is capable of being deflected out of its
hold condition in response to a predetermined acceleration
force. The switch also includes electrical contacts
associated with the IMM for changing between "closed" and
"open" states when said IMM moves from a hold condition to
an operative condition. A hold electrode generates an
electrostatic field urging the IMM into its hold position,
and the magnitude of the field can be adjusted by adjusting
the voltage applied to the hold electrode. The IMM remains
in said hold condition when subjected to accelerating
forces that are less than the predetermined acceleration
force established by said electrostatic field and deflects
to its operating condition in response to said
predetermined acceleration force greater than said
predetermined acceleration force.
Brief Description of the Drawings
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The foregoing and other objects and advantages of the
present invention will be better understood from the
following description, appended claims, and accompanying
drawings wherein:
- Figure 1 is an exploded perspective view of one
embodiment of a safing switch incorporating the teachings
of the present invention;
- Figure 1A is a side elevation sectional view of the
embodiment of Figure 1 taken along lines 1A-1A;
- Figure 2 is a simplified top view of another form of
IMM useful in the device of Figure 1;
- Figure 3 is a simplified side view of a safing switch,
showing an alternative arrangement wherein the electrical
contacts are below the IMM;
- Figure 4 is a simplified side view of a safing switch,
showing another embodiment in which dual pairs of aligned
contacts are employed;
- Figure 5 is a simplified side view of another safing
switch, showing the use of a stop that limit movement
between the IMM and the hold plate;
- Figure 6 is a simplified side view of a yet another
safing switch, showing the interchangeability of the hold
plate and the self-test plate;
- Figure 7 is a simplified side view of a another safing
switch, showing the use of a torsion bar and the formation
of multiple lever arms on the same safing switch;
- Figure 8 is a simplified side view of a still another
safing switch, showing another multiple arms arrangement;
- Figure 9 is a simplified side view of a further safing
switch, showing the hold plate and the IMM fabricated using
doped polysilicon as the conductor for the hold plate and
for the IMM;
- Figure 10 is a simplified side view of a safing
switch, showing a hold plate formed by diffusing into the
substrate having an n+ or p+ diffusion;
- Figure 11 is a simplified sketch showing a planarized
IMM and the safing switch with a p+ silicon IMM and hold
plate formed by a p+ diffusion into the substrate;
- Figure 12 is an illustrative sketch showing a
planarized contour of the IMM formed of doped polysilicon
and a hold plate beneath the IMM in a well formed of
polysilicon as the conductor and silicon nitride as the
insulator;
- Figure 13 is a simplified end view of a safing switch
with an alternative switch contact layout;
- Figures 14A and 14B are simplified top and partial
perspective view, respectively, of a still another safing
switch, showing a "hinged" arrangement of the IMM; and
- Figure 15 is a block diagram of a control system for a
vehicle occupant restraint system wherein the system uses a
safing switch constructed in accordance with the present
invention.
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Description of Preferred Embodiments
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Figure 1 is an exploded perspective sketch of a
preferred embodiment of the safing switch 10 made in
accordance with the present invention, implemented in a
fabricated microchip. The safing switch 10 includes a
cantilever mounted inertial mass member (IMM) 12 which is
formed of plated metal, such as nickel, fabricated on a
substrate 14. The substrate 14 may be formed of a
semiconductor material, such as oxidized silicon or gallium
arsenide, or an insulator material such as glass or
alumina.
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The IMM 12 includes a platform 16 that is attached to
a base support 18 by a pair of cantilever arms 20. The
base support 18 and the arms 20 as well as the platform 16
are made of electrically conductive metal. The base
support 18 is affixed to the substrate 14 and has
sufficient height so that the IMM is supported above the
substrate 14 in a cantilever manner by the arms 20. The
cantilever arms 20 impart spring-like properties to the
IMM 12 so that it possesses a natural frequency of
vibration. The cantilever arms 20 have a sufficient degree
of stiffness, however, to support the platform in a
suspended position above the substrate 14 in the absence of
a force having a component acting in a direction normal to
the substrate. An air space 22, best seen in Figure 1A,
therefore exists between the platform 16 of the IMM and the
substrate 14.
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The natural frequency of vibration of the IMM is
related to the spring constant and length of the cantilever
arms, and the mass of the IMM. The frequency can be
conveniently adjusted in several ways, e.g. by adjusting
the mass of the IMM through the addition to the platform of
a mass 36 of suitable size, to move the natural frequency
above or below the frequency range that might be
encountered by the device in its system use. Once the
device has been fabricated, however, the natural frequency
of vibration of the cantilevered IMM is fixed.
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The cantilever mounting of the IMM permits it to
respond to the application of a force normal to the
substrate by swinging up or down relative to the
substrate 14. More specifically, when the substrate is
accelerated in a direction normal to the substrate and
downward (as viewed in Figure 1) the arms 20 flex
increasing the space between the platform 16 and the
substrate 14 as the platform tries to stay at rest. The
safing switch is equipped with a pair of electrical
contacts that close when a certain amount of deflection of
the platform 16 has occurred relative to the substrate.
Within certain limits, the deflection of the IMM is related
to the acceleration imparted to the substrate. Thus, the
contacts close when the switch has been exposed to
acceleration of more than a certain amount.
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The contacts include upper and lower electrical
contacts 30 and 32. The contacts will preferably comprise
gold contact pads. The lower contact 32 is affixed to the
top of the IMM 12 at the distal end of the platform 16.
The upper contact 30 is affixed to the underside of a
contact support structure 34. The contact support
structure 34 is rigidly mounted on the substrate 14. The
upper contact is aligned above the lower contact such that
the two contacts meet upon sufficient upward deflection of
the IMM 12. The lower contact 32 is electrically connected
to the base support 18 through the platform 16 and arms 20
(it will be recalled that both platform 16 and arms 20 are
formed of electrically conductive material).
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The upper contact 30 and the base support 18 are
electrically connected to respective contact pads 30'
and 32' secured to the substrate 14. The electrical
resistance between the two pads is normally very high
(effectively infinite). When the device is accelerated
downward (as viewed in Figure 1) by more than a certain
amount, however, flexing of the cantilever arms 20 causes
the contacts 30 and 32 to meet, thereby creating a short
circuit between pads 30' and 32'. Thus, in accordance with
one embodiment of the present invention, the safing switch
is normally "open", but "closes" when subjected to
acceleration above a certain threshold.
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The safing switch further includes a hold plate 24 for
calibrating the acceleration level necessary to force the
contacts 30 and 32 into physical and electrical contact.
The hold plate comprises a conductor plate 28 secured to
the substrate 14 and covered with an insulating
material 26. The insulating material may, for example, be
silicon dioxide, silicon nitride, aluminum oxide, or other
insulator or combination of insulators. The conductive
plate 28 is disposed beneath platform 16 and is spaced from
the platform by a small air gap.
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The conductive plate 28 is electrically connected to a
contact pad 24'. Since the entire platform 16 is formed of
a conductive metal and is connected to the contact pad 32',
the application of a voltage across contact pads 24'
and 32' will cause an electrostatic field to be established
between platform 16 and hold plate 24. The electrostatic
field will create an attractive force between the platform
and the hold plate. The applied voltage is great enough
that the resultant attractive force will draw the platform
and hold plate together against the resilience of the
cantilever arms 20. As the platform and plate approach one
another, the separation between the two will diminish,
resulting in an increase in the electrostatic field and a
corresponding increase in the electrostatic force.
Assuming a voltage of sufficient magnitude is applied
across the pads, the platform will continue to move
downward toward the hold plate until feet 44A and 44B on
the underside of the platform 16 come into contact with the
insulating layer 26. (The purpose of feet 44A and 44B will
be described hereafter with reference to Figure 5.) The
platform will remain in this hold position abutting
insulating layer 26 until either the electrostatic field is
released, or the platform is forced away from the hold
plate by a force of sufficient magnitude and duration to
overcome the electrostatic attraction. Such a force may
arise from acceleration caused, e.g., by an acceleration of
the device in a downward direction as viewed in Figure 1.
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The acceleration necessary to trigger the safing
switch can be adjusted by adjusting the voltage applied
between pads 24' and 32' (the "holding voltage"). If the
holding voltage is increased, then greater acceleration
will be required to overcome the electrostatic attraction
and more of an acceleration will be required to trigger the
switch. If the holding voltage is reduced, then less
acceleration will required to overcome the electrostatic
attraction and correspondingly less acceleration will be
required to trigger the switch. Thus, the trigger point of
the switch can be electrically adjusted following
manufacture of the switch.
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Another method of adjusting the sensitivity of the
switch relates to the size of the hold plates. The
electrostatic force restraining the switch against
actuation will vary directly as a function of the surface
area of the hold plates to which the holding voltage is
applied. Thus, the sensitivity of the switch may be
adjusted by adjusting the surface area of the hold plate.
One method of doing this is to modify the Figure 1 design
to include multiple hold plates, each electrically isolated
from the others. The sensitivity of the safing switch may
then be adjusted by selecting a particular plate or group
of plates to which the holding voltage is to be applied.
This may be done at the time of manufacture by wire bonding
a selected one of, or a selected group of, the hold plates
to the pad 24'. Alternatively, each hold plate may be
electrically connected to a separate pad, with external
circuitry applying a holding voltage only to selected ones
of the pads.
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The trigger point of the switch will also depend upon
the spacing between the electrical contacts 30 and 32. The
further the initial spacing, the greater the acceleration
needed to overcome the resilience of the arms 20.
Therefore, the threshold can be adjusted by adjusting the
contact spacing. Switch closure will only occur when the
acceleration to which the switch is subjected exceeds a
threshold for a period of time adequate for the contact 32
to move across the gap and touch contact 30. Increasing
the distance will also increase the time needed to move
across the gap and, thereby, adjust the timing point at
which switch closure occurs. In most applications,
including most automotive crash sensing applications, the
spacing of the IMM from the hold plate will be small so
that needed flexure of the IMM is minimized.
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Alternatively, the hold plate may be spaced from the
IMM by a sufficient distance that the IMM flexes a
substantial amount in being pulled back to its hold
position. A significant spring force will then exist,
tending to pull the IMM away from the hold position and
toward the contact closed position. Thus, the switch will
snap from an "off" position (platform resting against
insulating layer 26) to an "on" position ( contacts 30
and 32 in electrical and physical contact) rather abruptly
when the acceleration to which the switch is subjected
exceeds a certain threshold. The snap action will be
enhanced because the electrostatic restraining force
between the platform and hold plate will rapidly diminish
as the IMM pulls away from the hold plate upon being
dislodged by an acceleration. The reduction in
electrostatic restraining force acts as positive feedback,
tending to cooperate with the IMM spring force in urging
the contacts toward closure. As stated above, this mode of
operation will not be preferred for most applications.
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In the safing switch device illustrated in Figure 1,
an additional self-test plate is provided for self-test
purposes. The self-test plate will be formed of a
conductive material, such as nickel. The self-test
plate 38 is supported on a pair of supports 40 running
longitudinally on either side of, and spaced transversely
from, the IMM. The supports have sufficient height that
self-test plate 38 extends above the platform 16 and is
spaced from the platform by an air space 42, best seen in
Figure 1A. Self-test plate 38 is connected to a contact
pad 38', whereby an electrostatic field may be established
across the gap between the self-test plate 38 and the
platform 16 by applying a voltage across contact pads 32'
and 38'. Any such electrostatic field will create a
corresponding electrostatic force that will tend to pull
the platform 16 towards the self-test plate 38, effectively
simulating a force caused by a downward acceleration of the
switch. The application of a voltage of sufficient
magnitude (a "test signal") will cause the platform 16 to
be pulled away from the hold plate and the switch to close.
Thus, proper functioning of the switch can be verified
through application of a test signal across pads 32'
and 38'.
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The self-test plate 38 may also be used to latch
closed the contacts 30 and 32. To accomplish this, an
external latch control circuit (not shown in Figure 1) will
monitor the contacts 30 and 32. When the contacts close,
the circuit will immediately apply a test signal to the
plate 38. The resulting electrostatic force will pull the
IMM upward, thereby preventing the contacts from breaking.
The contacts will remain closed until the test signal is
removed. With such an arrangement, the contacts will
initially close in response to acceleration above a
threshold, but will latch in the closed position and remain
closed until released by the external latch control
circuit. Such an arrangement may be useful in certain
vehicle occupant restraint systems, where it is desirable
to extend the period of time that the safing switch
contacts are closed to prevent the current arcing that
might arise if the contacts were opened too early and
insure that current flow continues long enough to ignite a
squib.
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A series of holes 46 and 48 are formed in the
self-test plate 38 and the platform 16, respectively. The
holes 46 and 48 are in alignment and permit the movement of
air through the holes. The holes serve to control damping
and the time response of the IMM 12 as it moves between the
air spaces 22 and 42 in response to an acceleration of
switch 10.
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The entire device 10 will be mounted inside a housing
(not shown). The housing will preferably be filled with an
inert gas such as nitrogen. The contact pads 24', 30',
32', and 38' will be connected to exterior electrical pins
or contacts of the device, and thus will be accessible to
connection with other electrical devices.
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The structure can easily accommodate multiple pole
switch arrangements. For example, a second or third set of
electrical contacts may be affixed to second or third
electrically isolated supports and connected to additional
pads on the substrate. Such multi-poled switches can be
employed to operate other independent circuits or devices
in response to acceleration forces.
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Figure 2 is a simplified plan view of an IMM of
somewhat different design, wherein the IMM is resiliently
supported by torsion bars 66 rather than the cantilever
arms 20 shown in Figure 1. The IMM 60 of Figure 2 is
generally similar in construction to the IMM 12 of
Figure 1, and includes a platform 61 carrying through-holes
65. Suitable contacts and additional masses, neither of
which are shown in Figure 2, are also provided on the
platform 61 as necessary. The platform is integral with a
generally rectangular frame 62 having a generally
rectangular central opening. A base 64 is centrally
disposed within the rectangular opening of the frame 62.
The base 64 is connected to the inner perimeter of the
frame by two torsion bars 66 projecting transversely from
either side of the base 64. The base is joined to the
substrate to thereby mount the IMM in the correct alignment
relative to the other components of the switch. The other
components may be as shown in Figure 1. The torsion
mounting arrangement of Figure 2 permits the IMM 60 to
swing towards or away from the substrate, in a direction
substantially normal to the plane of the IMM.
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The IMM may also be supported by other means that can
be fabricated using micro machining techniques. The IMM
may be supported by any type of micromachined hinge,
provided that the hold voltage creates an electrostatic
force sufficiently large to pull the IMM into the hold
position from its initial, rest position. A micromachined
hinge type support would have an advantage of not having a
natural frequency of vibration. Such a hinge arrangement
is described below with regard to Figures 14A and 14B.
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Figures 3 and 4 show contact arrangements and hold
plate locations that are alternatives to those associated
with the preferred structure of Figure 1. In Figure 3, a
pair of aligned upper and lower contacts 68 and 70 are
disposed on the underside of the IMM 72 and on the top of
the substrate 73, respectively. The hold plate 78 is
suspended above the IMM by a support (not shown) similar to
supports 40 of Figure 1. The insulating layer 76 is
deposited on the upper surface of the IMM rather than on
the hold plate. The hold plate is spaced from the IMM and
its associated insulating layer by an air space 80. The
direction of the acceleration to be sensed is indicated by
the arrow 82. Acceleration of the substrate in the
direction indicated by arrow 82 will force the IMM downward
(as viewed in Figure 3), thus tending to bring the
contacts 68 and 70 to closure. From a functional
standpoint, the sensing devices of Figures 1 and 3 are
similar.
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Figure 4 shows a safing switch similar to that of
Figure 3, with the exception that two pairs of aligned
electrical contacts are provided, one pair above and one
pair below the IMM. The lower contacts are included to
permit verification that the IMM is in the correct holding
position under the influence of the holding plate.
Contacts 98 and 100 provide the desired verification by
closing when the IMM is in the correct holding position.
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A first pair of normally open electrical contacts 84
and 86 is positioned on top of the IMM 88. The direction
of the acceleration tending to cause the deflection of the
IMM 88 from the holding position is indicated by the
arrow 90. The electrostatic force opposing the
acceleration 90 is generated by a hold plate 92 made up of
a metal plate 96 on which an insulator layer 94 has been
deposited. Absent the predetermined acceleration 90, the
hold plate normally pulls the IMM down, closing the
contacts 98 and 100 and thereby confirming that the hold
plate 92 is functioning and is retaining the IMM in the
correct holding position. Of course, the safing switch in
Figure 4 may also be produced without contacts 84 and 86
and the associated contact support if it is desired to
produce a simple "normally closed" switch.
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The safing switch 101 of Figure 5 has much the same
construction as the switch 10 in Figure 1. An IMM 102 is
mounted on the substrate 104 along with a hold plate 103.
The hold plate 103 comprises a metal plate 105 upon which
has been deposited an insulation layer 106. As in the
Figure 1 embodiment, the IMM 102 is formed with integral
depending feet 107 which cause most of the IMM 102 (i.e.,
all of the IMM except the feet) to stand off from the hold
plate 103 when the IMM 102 is being held in the hold
position by the hold plate 103. The stand off distance is
equal to the height of the feet. This stand off distance
is useful in reducing the strength of the electrostatic
force holding the IMM 102 to the hold plate 103, in
reducing the amount by which the IMM must flex to reach the
hold position, and in providing open space across most of
the IMM between the hold plate and the IMM. The open space
is beneficial during the manufacture of the switch.
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If the feet 107 were not included, (and assuming that
a hold voltage of adequate magnitude to pull the IMM
against the insulating layer 106 were applied to the hold
plate 103) the entire IMM 102 would be held against the
hold plate, spaced from the hold plate by only the
thickness of the insulating layer. Because of the
relatively large surface area of the IMM 102, the
electrostatic force holding the IMM 102 to the hold
plate 103 at this close spacing would be too large. The
force or attraction could be reduced by reducing the
voltage applied to the hold plate or by reducing the
surface area of the hold plate. However, the voltage
applied to the hold plate 103 cannot be made too small (nor
can the hold plate be made too small) or the hold plate
will be unable to "pull-in" the IMM from the larger spacing
that exists when the IMM is in its undeflected position.
By including feet 107, a hold voltage of suitably great
magnitude may be employed without producing too great a
holding force. The holding force will then primarily
appear between the feet 107 and the hold plate 103, since
the feet are then much closer to the hold plate than the
remainder of the IMM, and will be adequate to pull the IMM
from its undeflected rest position into the holding
position.
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In addition to the feet 107, the substrate is equipped
with stops 108A and 108B that are electrically isolated
from the IMM and the contacts and plates. One of the
stops 108A is formed on the substrate under the IMM, while
the other stop 108B is formed (at the same time that
feet 107 are formed) on the underside of the IMM in a
position aligned above the stop 108A. The heights of the
stops 108A and 108B are selected such that, as the IMM 102
is drawn toward the substrate, the opposing faces of the
stops meet before the feet 107 come into contact with the
hold plate 103. Thus, the stops prevent the IMM 102 from
making contact with the insulating layer of the hold
plate 106. Since the stops prevent contact between the
feet and the hold plate, the insulating layer 106 is
redundant and may in some applications be omitted. In
those applications in which the insulating layer is
retained, however, the stops will advantageously eliminate
the wear that might otherwise be caused by repeated contact
between the feet and the insulating layer.
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The embodiment of Figure 6 is designed so that it may
be connected to sense accelerations directed either upwards
(arrow 124A), or downwards (arrow 124B), as viewed in the
Figure. This flexibility in the choice of the sense
direction is provided by including functionally equivalent
plates 112 and 115 above and below the IMM, respectively.
Either of the two plates may be used as the hold plate,
with the remaining plate then being used as a self-test
plate. For example, if the switch is to be used to detect
accelerations directed downwardly (in the direction
indicated by arrow 124B in Figure 6), then plate 115 may be
used as the hold plate, with plate 112 being used as a
self-test plate. As in prior embodiments, the lower
plate 115 includes a planar metal plate 118 covered by an
insulating layer 116. Also, as in prior embodiments, the
upper plate 112 is formed of a planar metal plate 114 and
is protected by an insulating layer 113 applied to the top
of the IMM 110.
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Two pairs of aligned upper and lower electrical
contacts are provided to detect deflection of the
cantilevered IMM. Contacts 119 and 120 are disposed above
the IMM, and close when the IMM flexes upward by more than
a preselected amount. More specifically, contact 119 is
attached to a downward-facing surface of a support 123 and
contact 120 is attached to the upper surface of the
IMM 110, in aligned relationship below the upper
contact 119. The closure of contacts 119 and 120 will then
indicate that acceleration in the downward direction
(indicated by arrow 124B) has exceeded the acceleration
level for which the switch has been calibrated.
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Contacts 121 and 122 are disposed below the IMM 110,
and close when the IMM flexes downward by more than a
preselected amount. More specifically, contact 121 is
attached to underside of the IMM 110 and contact 122 is
affixed to the substrate 111, in aligned relationship below
contact 121. The closure of contacts 121 and 122 will then
indicate that acceleration in the upward direction
(indicated by arrow 124A) has exceeded the acceleration
level for which the switch has been calibrated.
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As with other embodiments, the spacing between the
pairs of contacts is important in most applications since
the acceleration required to trigger the switch (i.e., to
close the contacts) is functionally related to the
distance. More accurately, the acceleration required to
dislodge the IMM from its holding position is generally
dependent upon the voltage applied across the hold plate
and IMM. The switch will only trigger (i.e., change
switching states) if the acceleration is maintained for a
certain (albeit rather brief) period of time related to the
separation of the contacts. Thus, if the switch is to have
equal sensitivity whether connected to sense upwardly or
downwardly directed accelerations, the spacing between the
pairs of contacts should be the same.
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Similarly, it is desirable that the IMM, when in its
undeflected location, be spaced by the same amount from
plate 112 as from plate 115. When the plate/IMM spacings
are equalized, the application of a given hold voltage to
either plate will result in the establishment of an
equivalent electrostatic holding force between that plate
and the IMM. Thus, a similar or identical voltage source
can be used to provide the holding voltage, regardless of
the direction of sensitivity selected for the switch.
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In the Figure 6 embodiment, the contact pairs are
mounted and spaced such that the contacts meet one another
before the IMM makes contact with the associated plate.
Thus, for example, the contacts 119 and 120 will close
before insulating layer 113 on the IMM 110 comes into
contact with the plate 114. The contact pairs thus act as
stops and prevent actual physical contact between the IMM
and either plate. For this reason, the insulating
layers 113 and 116 are largely unnecessary and may, in some
applications, be eliminated.
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As with the other devices described herein, the
switch 109 will be mounted on and housed in a suitable
hollow carrier of the type used, for example, with
integrated circuits. The carrier will in turn be mounted
on a printed circuit board carrying other electronic
components, and the printed circuit board will be mounted
in an enclosure. The enclosure will be rigidly affixed to
the body whose acceleration is to be sensed. The body may
be the frame of a car or other vehicle, for example. If
the circuit must be sensitive to acceleration in two
opposing directions, then two of the switches 109 may be
conveniently attached to same face of the printed circuit
board, with one switch configured to detect acceleration in
one direction and the second configured to detect
acceleration in the opposite direction. Alternatively,
only one of the switches 109 may be attached to the printed
circuit board, but with additional circuitry provided on
the circuit board to permit the direction of sensitivity to
be switched from one direction to the opposite. As stated
previously, this may be accomplished by selective
application of a hold voltage to one of the plates 112
and 115 and monitoring of the appropriate one (diagonally
opposite, as viewed in the figure) of the pairs of
contacts.
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In the embodiment shown in Figure 7 the safing
switch 125 is equipped with an IMM 126 that is a variant of
the IMM 60 shown in Figure 2. The IMM includes a
cantilevered arm 126A supported from a base 127 by a frame
and torsion bar arrangement. The frame and the torsion
bars, which are not readily visible in the Figure 7 view,
are similar to the frame and torsion bars shown in
Figure 2. In Figure 7, however, the IMM includes a
continuation arm 126B supported on the same frame, but from
a point on the perimeter of the frame that is opposite from
the point of attachment of the cantilevered arm 126A. The
continuation arm is coplanar and collinear with
cantilevered arm 126A. Moreover, the frame is relatively
rigid and provides a relatively rigid attachment to each
arm. Because of this, arms 126A and 126B may be considered
to be two parts of a single relatively rigid arm supported
near its midpoint by torsion bars extending transversely
from the base 127. If either arm is forced to pivot in
given direction about the torsion bars, the frame will
transmit the motion to the other arm and will therefore
produce a corresponding pivoting of the other arm.
-
Arm 126B counterbalances arm 126A, thus reducing the
tendency of the arm 126A to pivot upon the application of
an acceleration to the substrate. Indeed, if the moment of
inertia of the two arms were identical, the IMM would be
completely balanced and would have no tendency to pivot in
response to applied acceleration. Since the pivoting
response to acceleration is essential to the operation of
the switch, the switch arms 126A and 126B must be
unbalanced enough that the net action of any acceleration
is to pivot the arms about the base. To unbalance the
arms, one arm must have a greater moment of inertia than
the other arm. In the embodiment illustrated in Figure 7,
this is accomplished by adding to the arm 126B an
additional mass 134. With this additional mass, the moment
of inertia of arm 126B will exceed that of arm 126A, hence
the IMM will respond to a downward acceleration of the
substrate (as viewed in Figure 7) by pivoting in a
counterclockwise direction about the torsion bars
connecting the IMM to the base. Other methods of
unbalancing the structure could be used. For example, one
of the arms could be made longer than the other to give it
a different effective moment arm length, or could be made
wider than the other to increase its mass.
-
The embodiment of Figure 7 includes self test and hold
plates similar in purpose and function to the self test and
hold plates described with respect to previous described
embodiments. The self-test plate 130 is positioned below
the arm 126A. The hold plate 131 is located beneath the
arm 126B. A pair of aligned upper and lower normally open
contacts 132 and 133, respectively, are affixed to the IMM
arm 126A and the substrate 129, respectively. It may be
desirable to equip this embodiment with suitable stops
(indicated in a schematic sense at 136) to limit movement
of the IMM 126.
-
Figure 8 shows another embodiment 138 of a safing
switch with an extended, centrally mounted IMM. The
Figure 8 embodiment is generally similar to Figure 7
embodiment, except that the contacts are mounted above the
IMM and the positions of the hold plate and self-test plate
are reversed. The safing switch 138 has an IMM 140 mounted
on a base 141 by torsion bars (not visible in Figure 8) so
that it can rock in both clockwise and counterclockwise
directions. A pair of upper and lower electrical
contacts 146 and 148, respectively, are mounted on top of
the IMM 140. The lower contact is disposed on the upper
surface of IMM 140, and the upper contact 146 is affixed to
a support 147 which is, in turn, mounted on the substrate.
The IMM 140 includes two arms 140A and 140B. Atop the
arm 140B at the extreme right side of the arm (as viewed in
Figure 8), there is an additional mass 142. The safing
switch 138 has a hold plate 137 located beneath the
arm 140A and a self-test plate 139 located beneath the
arm 140B. When the hold plate 137 is energized, the
arm 140A is pulled back against the plate and thus the
electrical contacts 146 and 148 are held open. The hold
force will be overcome, and the contacts will close, when
an acceleration of sufficient magnitude and duration is
applied to the substrate in the direction indicated by the
arrow 144. The acceleration level necessary to close the
contacts 146 and 148 can be varied by increasing or
decreasing the voltage applied to the hold plate 137.
-
The safing switches described herein may be fabricated
using several rather different fabrication technologies.
Conventional micro-machining processes can be used to
construct switches as shown, for example. These processes
involve the successive plating of metal and depositing of
insulating layers on a substrate, with plated or deposited
copper layers being used to fill those areas where voids
will exist in the finished device. Features of the design
that will ultimately be suspended above the voids are
formed on top of the copper. At a later stage in the
processing, the copper is etched away, leaving voids in the
spaces previously occupied by the copper. Because other
features of the design are formed of materials (e.g.,
nickel) that are not affected by the etching agents, those
features remain following the etching operation. Thus,
features previously formed on top of the copper (e.g.,
parts of the IMM) remain following the etching and find
themselves suspended over the void. These techniques are
well known and will not be described in detail herein.
-
Alternatively, the voltage controlled safing switch of
this invention may be fabricated using other
microelectronic processing techniques. The safing switch
may be formed on a silicon substrate with conventional
conductive, semi-conductive and insulator materials rather
than the plated metals described above in connection with
the micro machining fabrication techniques. The
alternative embodiments of Figures 9-12 illustrate devices
based on silicon technology and constructed using standard
microelectronic photolithographic techniques. The switch
is built up in layers, using standard photolithographic
processes which are old and well known, per se. The
direction of the acceleration force which is to be sensed
by the devices shown in Figures 9-12 is identified by the
arrow 149.
-
In Figure 9, the safing switch 150 is formed on a
silicon substrate 152. An insulator layer 154, comprised
of silicon nitride, covers the surface of the substrate.
The switch is formed through a series of masked deposition
and etching steps. In the resulting switch, the hold
plate 156 and the IMM 159 are each formed of doped
polysilicon and are electrically conductive. Insulator 157
is formed of silicon nitride.
-
A silicon dioxide layer is deposited on the surface of
the substrate to provide a support layer upon which can be
directly deposited the doped polysilicon for the IMM
cantilevered arm. After the IMM is formed on the silicon
dioxide layer, the silicon dioxide is etched away with
buffered HF acid to form the void under the IMM. The self
test plate 164, its supports (not shown) and contact
support 162 are formed with plated nickel or other metal
similar to the devices in Figures 1-8.
-
Figure 10 illustrates a safing switch 167 that is very
similar to the device in Figure 9. In Figure 10, however,
the hold plate is formed as part of the substrate by an n+
or p+ diffusion process. The substrate 168 is a doped
p-type silicon, and the hold plate 169 is formed by masked
diffusion into the substrate of an n+ dopant. If an n-type
silicon substrate is used, then a p+ diffusion is required.
The n+ or p+ diffusion region (as the case may be) serves
as the hold plate 169. In this case, the silicon nitride
layer 170 covering the substrate functions as the
protective cover for the hold plate. An electrical contact
(not shown) would be made to diffusion 169 to apply the
hold voltage.
-
In free-standing structures, including those pictured
in Figures 8 and 9, material stress tends to build up at
bends and turns in the structure. Such structures are
therefore somewhat more fragile and subject to fracture at
those locations. To reduce the buildup of stress in the
safing switches of the present invention, it is generally
desirable to eliminate bends or turns in various parts of
the switch. It therefore becomes desirable to produce a
safing switch in which the IMM has no bends or steps. Such
an embodiment of the invention is shown in Figure 11.
-
The embodiment of Figure 11 includes a planarized or
flat IMM 182. The IMM 182 in this embodiment is formed of
p+ doped silicon. The hold plate 186 is formed by masked
diffusion of a p+ dopant into the n- substrate 184. A n-type
silicon layer 188 is then epitaxially grown over the
substrate, and the p+ silicon IMM 182 is diffused into the
epitaxial layer 188. The silicon layer 188 is then
selectively etched away to form a cavity under the IMM 182
and thereby expose the hold plate 186. A planarized
IMM 182, lacking any bends or turns is thus left
cantilevered over the cavity and the hold plate. A
self-test plate, additional mass, a pair of aligned
electrical contacts, and contact to IMM 182 and
diffusion 186 will also be provided to the Figure 11
device. These elements have been omitted from Figure 11
for simplicity of description. Their locations may be the
same as those in Figures 9 and 10.
-
Figure 12 shows another embodiment in which a
planarized or flat IMM is formed of doped polysilicon. It
is similar in construction to the safing switch of
Figures 9 and 10, except that the IMM 198 is a flat, planar
structure. The hold plate 205 is also made of polysilicon.
The safing switch 190 is formed on a silicon substrate 192.
A well or cavity 194 is formed to an appropriate depth
within the substrate. An insulator layer 196 of silicon
nitride is applied over the inside of the cavity 194.
Another layer of doped polysilicon is deposited in the
cavity on top of the silicon nitride layer to form the hold
plate, and then a second layer 204 of silicon nitride is
deposited over the polysilicon.
-
The IMM 198 is fabricated using a planarizing
technique. Silicon dioxide is deposited into the cavity
and then planarized by one of many possible techniques
known to those skilled in the art of silicon processing.
Doped polysilicon is deposited on top of the planarized
silicon dioxide and then is patterned to form the IMM 198.
The silicon dioxide layer is then selectively etched away.
Through this process the doped polysilicon IMM 198 is left
hanging over the cavity 194, which has been uncovered
through the etching action. The hold plate 200 remains,
having been protected against the etching agent by the
layer of silicon nitride 204. As with Figure 11, certain
elements of the Figure 12 device have been omitted from the
drawing for convenience of description. The omitted
elements include the self-test plate, the additional mass,
the electrical contacts and the contacts support. The
nature, location and orientation of these elements may be
as described in the foregoing embodiments.
-
Figure 13 shows an end view of a portion of a safing
switch with an alternative contact layout. This contact
layout, which may be applied to any of the safing switch
embodiments in Figures 1 through 12, consists of a long
contact 210 above IMM 209. Contacts 208A and 208B are
supported on the substrate 206, above contact 210, by their
respective supports 207A and 207B. When the acceleration
forces overcome the holding force on the IMM, contact 210
moves toward and touches contacts 208A and 208B. This
contact configuration would be beneficial in safing
switches requiring a lower contact resistance, or in safing
switches using a material for the IMM that had a high
resistivity.
-
The contact layout of Figure 13 may readily be adapted
to the embodiments shown in Figures 4, 6, and 7 by adding a
contact similar to contact 210 on the underside of the IMM
and adding contacts similar to contacts 208A and 208B
directly on substrate 206.
-
Figures 14A and 14B show another safing switch
embodiment made in accordance with the present invention.
An electrical pad 250 is mounted to the substrate 252.
Switch 254 includes a pivot arm 256 secured to an IMM 258.
The pivot arm 256 is pivotally held against the electrical
pad 250 by upper support yokes 260, 262. The yokes 260,
262 and pivot arm 256 provide a hinge function for the
IMM 258. Preferably, the IMM 258, pivot arm 256, and
yokes, 260, 262 are also manufactured using a micro machine
process or microelectronic processing technique.
-
Electrical contact with the IMM 258 is made through
the electrical pad 250. Preferably, the electrical pad 250
is made from gold. Near one end 270 of the IMM 258, one
electrical contact 272 of a contact pair is mounted to the
substrate side of the IMM. The other electrical contact
(not shown) of the contact pair is mounted to the
substrate 252 in a manner similar to that described above.
The other end 274 of the IMM 258 has a stop member 276
mounted to the substrate side of the IMM. A mass
element 280 is secured to the top side of the IMM 258 to
add an off-balance moment of inertia to the IMM as
described above.
-
A hold plate 284 is secured to the substrate 252 and
is positioned on the side of the IMM opposite the
electrical contact 272. When a voltage is applied across
the hold plate 284 and the IMM 258, the end 274 of the IMM
is pulled downward toward the substrate 252 thereby opening
the electrical contact pair at the other end 270. This
arrangement biases the switch 254 to a normally open switch
condition. When the switch 254 is subjected to an
acceleration in the direction of the arrow 294 shown in
Figure 14B greater than a predetermined amount, the IMM
will pivot about its hinge mount axis causing the contact
pair to close. The amount of the acceleration necessary
for switch closure is, again, controlled by the voltage
level across the IMM 258 and the holding plate 284.
-
The switch 254 further includes a self-test plate 290
secured to the substrate 252 and position of the side of
the IMM having the electrical contact 272. When it is
desired to test the switch 254, a voltage is applied across
the IMM 258 and the plate 290 so as to pull the end 270
downward relative to the substrate 252 and close the switch
contact pair.
-
The switches of the present invention may be used in a
variety of different systems in cooperation with a variety
of different elements. As explained earlier herein, the
switch will have particular utility when used as part of a
system for controlling occupant restraint devices (e.g.,
air bags or seat belt retractors) in an automobile or other
vehicle. In such a system, the switches of the present
invention may be advantageously used as safing sensors.
Safing sensors typically provide a redundant level of crash
detection to assure that the occupant restraint device is
deployed under predetermined circumstances and at a
predetermined time.
-
Figure 15 is a block diagram of a controller 211 that
uses a safing switch formed in accordance with the present
invention. The Figure 15 controller controls the supply of
electrical current to a squib 212. The squib is
mechanically and functionally associated with an occupant
restraint device such as an air bag 213 or seat belt
retractor (not shown). The squib includes a material that
will ignite when current of a certain magnitude and
duration is channeled through the squib. Ignition of the
squib will cause deployment of the air bag, actuation of
the seat belt retractor, or actuation of another actuatable
restraining device.
-
The squib 212 is connected in series with two
electronic switches 214 and 216 across a power source V+
(not shown, per se). As illustrated, the high side
switch 214 is a field effect transistor ("FET") and the low
side switch 216 is an "npn" bipolar junction transistor
("BJT"). When either of the two transistors is in its
"off" or high impedance state, no current will pass through
the squib 212. Thus, the squib 212 will only receive
enough current to ignite if both transistor 214 and
transistor 216 are in their "on" or low impedance states.
-
The transistor 214 is controlled by a
microcomputer 220. An accelerometer 222 senses vehicle
acceleration and provides to the microcomputer 220 an
analog or digital signal having a value proportional to the
magnitude of acceleration experienced from moment to moment
by the vehicle on which the system is mounted. The
microcomputer analyzes the acceleration using sophisticated
software algorithms to determine whether the vehicle is
experiencing a deployment crash condition. Such algorithms
are known in the art and form no part of the present
invention. When the microcomputer determines that the
vehicle is experiencing deceleration of a size and
character sufficient to warrant the deployment of the
occupant restraint device, the microcomputer will provide a
signal on output line 224 to switch transistor 214 from its
"off" state to its "on" state.
-
The low side transistor 216 is controlled by a safing
switch 230 constructed in accordance with the present
invention. The safing switch provides an open or closed
current path between a power line 232 and an output
line 234 via two contacts represented in Figure 15 as a
single-pole single-throw switch 236. The output line 234
is connected to the base of transistor 216 through a
current limiting resistor 238. The base of transistor 216
is also connected to ground through a pull-down
resistor 240. When the switch 230 is open, the base of
transistor 216 will be pulled to a ground voltage level by
the pull-down resistor 240 and the transistor will thus be
"off." When the switch 230 is closed, however, current
will be supplied to the base of the transistor 216 from
power line 232 via switch contacts 236 and current limiting
resistor 238. Thus, when contacts 236 are closed, base
current is supplied to transistor 216 and transistor 216
will turn "on". The contacts 236 will close when the
switch 230 is exposed to acceleration along its direction
of sensitivity which is greater than the threshold
established by the voltage applied to the hold plate of the
switch.
-
The hold plate of the switch 230 is connected to a
calibration line 242. A calibration voltage source 244
supplies a predetermined calibration voltage on the
calibration line 242. The calibration voltage sets the
trigger threshold of the switch 230. The calibration
voltage will be selected during a calibration step
performed as part of the manufacturing process. During
calibration, the calibration voltage is initially set to a
high level. The switch 230 is then subjected (by means of
a centrifuge or a "thumper", for example) to the
acceleration to which the switch is to be calibrated. The
calibration voltage is then lowered until the switch
triggers. The calibration voltage at the triggering point
is then the selected voltage. It is this voltage that is
supplied to line 242 by the calibration voltage source 244.
-
It may in some cases be desirable to design voltage
source 244 so that it provides a higher voltage at its
output for a very brief time upon system power up, and then
drops down to the selected calibration voltage once the
switch has had sufficient time for its IMM to be drawn down
to the hold plate.
-
Generally, the accelerometer 222 and the safing
switch 230 will be oriented relative to the vehicle so that
their sensitive axes are parallel to one another and are
oriented in the direction in which acceleration is to be
sensed. For example, if the system is to sense frontal
collisions of a vehicle, the accelerometer 222 and
switch 230 may conveniently be disposed so that the
sensitive axis of each points toward the rear of the
vehicle. The accelerometer and switch will have their
associated axis of sensitivity oriented toward the rear of
the vehicle because vehicle deceleration, is being sensed.
This is referred to in the art as crash acceleration.
Since the accelerometer and safing switch are aligned, they
will be subjected to the same crash acceleration. When the
crash acceleration rises above the threshold to which
switch 230 has been calibrated- the contacts 236 will close
and transistor 216 will turn "on". If the crash
acceleration also manifests the characteristics to which
the microcomputer 220 has been programmed to be sensitive,
then the microcomputer 220 will cause the transistor 214 to
also turn "on." With both transistors "on", current will
flow through the squib 212, the squib will fire, and the
associated occupant restraint systems will be actuated.
-
Each time power is applied to the control system 210,
the microcomputer 220 will test the operation of the safing
sensor 230. To perform the test, the microcomputer will
supply a test voltage on an output line 250. The output
line 250 is coupled to the self-test input of the
switch 230, and is thus applied to the self-test plate of
the safing switch. When the test voltage appears at the
self-test input, the IMM of the safing switch will be
forced to move and the switch contacts to close. The
microcomputer will sense closure of the contacts, and thus
proper operation of the switch, by monitoring the voltage
on a line 252. Line 252 is connected to the output of the
safing switch. Of course, before performing the test on
the safing sensor, the microcomputer will effectively
disable the transistor 214.
-
An acceleration sensitive switch has thus been
described which can be fabricated using micro machining and
semiconductor photolithographic techniques. The switch
will be small and inexpensive. The switch will close if
subject to acceleration over a threshold, but will
otherwise remain open. The acceleration threshold of the
switch may be easily and conveniently adjusted by adjusting
a "hold" voltage applied to one terminal of the switch.
Proper operation of the switch can be verified easily by
applying a test signal to a test terminal of the switch.
Many different embodiments of the switch have been
described. The switch will have particular utility when
used as a safing switch in a control system for a vehicle
occupant restraint device.
-
Although the present invention has been described in
considerable detail with reference to certain preferred
versions thereof, it will be appreciated by those skilled
in the art that various rearrangements or alterations of
parts may be made without departing from the spirit and
scope of the present invention, as defined in the appended
claims.
-
According to its broadest aspect the invention
relates to a switch adjustably responsive to an
acceleration force, said switch comprising: an inertial
mass member ("IMM") relatively movable from a hold
position to an actuated position, said member relatively
moving when said switch is accelerated and being
deflectable out of its hold position in response to said
switch acceleration of sufficient magnitude, and hold
means.
-
It should be noted that the objects and advantages
of the invention may be attained by means of any
compatible combination(s) particularly pointed out in the
items of the following summary of the invention and the
appended claims.
SUMMARY OF THE INVENTION
-
- 1. A switch adjustably responsive to an acceleration
force, said switch comprising:
- an inertial mass member ("IMM") relatively
movable from a hold position to an actuated position, said
member relatively moving when said switch is accelerated
and being deflectable out of its hold position in response
to said switch acceleration of sufficient magnitude,
- electrical contacts, at least one of which is
coupled to said IMM, for moving between closed and open
positions when said IMM moves between said hold position
and said actuated position,
- hold means comprising at least one hold electrode
to which a hold voltage may be applied for adjustably
establishing an electrostatic field creating a restraining
force urging the IMM into its hold position, said field and
said restraining force having a magnitude functionally
related to said hold voltage, and
- means for applying a hold voltage to said hold
electrode, and
wherein said IMM remains in said hold position
when said switch is subjected to acceleration forces that
are insufficient to overcome forces tending to restrain
said IMM to said hold position, including the restraining
force established by said electrostatic field, and deflects
to said actuated position when said switch is subjected to
acceleration forces that are sufficient to overcome said
forces tending to restrain said IMM,
whereby the acceleration required to move
relatively said IMM from said hold position to said
actuated position may be adjusted by selecting the hold
voltage applied to said hold means.
- 2. A switch further
comprising means for adjusting said restraining force of
said hold means by varying said hold voltage.
- 3. A switch further
comprising a substrate adapted to be mounted on a member
whose acceleration is to be sensed, wherein said IMM
comprises a deflectable spring-like arm having a
predetermined mass, and means for suspending said arm in
cantilevered fashion above said substrate such that said
arm extends generally parallel to said substrate.
- 4. A switch wherein said
means for suspending comprises a base mounted on said
substrate, said deflectable arm being rigidly joined to
said base at the proximal end of said arm such that
deflection of said IMM results in bending of said arm.
- 5. A switch wherein said
means for suspending comprises a base mounted on said
substrate, and means for flexibly joining said deflectable
arm to said base at the proximal end of said arm such that
deflection of said IMM results in flexing of said flexible
joining means.
- 6. A switch wherein said
flexible joining means comprises first and second torsion
bars extending from said base at opposite sides thereof and
in directions generally transverse to said deflectable arm,
and means for joining said deflectable arm to the ends of
said torsion bars, whereby deflection of said IMM results
in torsional flexing of said torsion bars.
- 7. A switch , said IMM
further comprising an elongated continuation arm and means
for joining said continuation arm to said deflectable arm
and to said ends of said torsion bars such that said
continuation arm extends from said base on the opposite
side from said deflectable arm and deflects in unison with
said deflectable arms.
- 8. A switch wherein said one
of said electrical contacts is fixed to said continuation
arm.
- 9. A switch wherein said
hold electrode is disposed on said substrate, and is below
said arm.
- 10. A switch wherein said arm
has disposed thereon a second electrode generally in
registration above said hold electrode, whereby said arm
electrode and said hold electrode are generally parallel to
one another and are closely spaced from one another.
- 11. A switch wherein said
arm is formed of an electrically conductive material and
said arm electrode is an integral part thereof.
- 12. A switch wherein said
hold electrode is supported by said substrate and is
disposed above said IMM.
- 13. A switch wherein said
electrical contacts are positioned above said IMM relative
to said substrate and are adapted to be normally open and
to close when said IMM is deflected away from said
substrate.
- 14. A switch wherein the
electrical contacts are positioned below the IMM relative
to the substrate and are adapted to be normally open and to
close when said IMM is deflected toward said substrate.
- 15. A switch wherein said
electrical contacts comprise first and second pairs of
electrical contacts, with one contact of each said pair
being coupled to said IMM for movement therewith and the
other contact of said pair being coupled to said substrate.
- 16. A switch wherein one of
said pairs of electrical contacts is positioned above said
IMM relative to said substrate and is adapted to close when
said IMM moves away from said substrate, and the other of
said pairs of electrical contacts is positioned below said
IMM relative to said substrate and is adapted to close when
said IMM is moved toward said substrate.
- 17. A switch further
comprising means for damping relative movement of said IMM.
- 18. A switch wherein said IMM
moves through a fluid and has openings formed therein for
controlling the flow of the fluid past said IMM as said IMM
relatively moves in said fluid, whereby said openings
control damping of relative movement of said IMM.
- 19. A switch wherein said IMM
is electrically conductive and has at least one portion
depending toward said hold electrode, whereby said
electrostatic field interacts with said at least one
depending portion of said IMM.
- 20. A switch wherein each of
said at least one depending portions includes a generally
planar surface that is closely adjacent to, and generally
parallel to, said hold electrode.
- 21. A switch further
comprising a substrate adapted to be mounted on a member
whose acceleration is to be sensed, and hinge means for
pivotally mounting said IMM to said substrate.
- 22. A switch wherein said
hold electrode and said electrical contacts are disposed on
opposite sides of said IMM.
- 23. A switch wherein said
hold electrode and said the electrical contacts are
disposed on the same side of said IMM.
- 24. A switch further
including self test means for testing the operational
integrity of said electrical contacts.
- 25. A switch wherein said
self test means comprises a test electrode to which a
voltage may be applied for urging said IMM towards its
actuated position.
- 26. A switch wherein said
test electrode and said hold electrode are disposed on
opposite sides of said IMM.
- 27. A switch wherein said
hold electrode comprises a generally planar, electrically
conductive sheet covered with an electrically insulating
layer.
- 28. A switch wherein said
insulating layer is formed of silicon nitride.
- 29. A switch wherein said IMM
comprises plated metal.
- 30. A switch wherein said
plated metal is plated nickel.
- 31. A switch wherein said IMM
is mounted on a substrate formed of glass or alumina.
- 32. A switch wherein said IMM
is mounted on a substrate comprised of a semiconductor
material.
- 33. A switch wherein said
semiconductor is silicon or gallium arsenide.
- 34. A switch wherein said
hold electrode is formed of doped polysilicon.
- 35. A switch wherein said
hold electrode is formed by p+ diffusion into an n- silicon
layer.
- 36. A switch wherein said
hold electrode is formed by n+ diffusion into a p- silicon
layer.
- 37. A switch wherein said
hold means is disposed closely adjacent said IMM and
wherein said switch further includes stop means for
limiting the relative movement of said IMM into said hold
position so as to thereby prevent said IMM from contacting
said hold means.
- 38. A switch wherein said at
least one hold electrode comprises at least two hold
electrodes.
- 39. A switch further
comprising means for adjusting said restraining force by
controlling the application of said hold voltage to
selected ones of said at least two hold electrodes.
- 40. A system for recognizing the onset of a crash of
a vehicle and providing a control signal indicative
thereof, comprising:
- an accelerometer responsive to crash acceleration
of said vehicle for providing a crash acceleration signal
which varies as a continuous function of said crash
acceleration;
- microprocessor means responsive to the crash
acceleration signal for determining from said signal
whether said vehicle is experiencing a crash condition;
- a safing switch responsive to crash acceleration
of said vehicle, said safing switch comprising
- an inertial mass member ("IMM") supported by
a tensile force and relatively movable from a
hold position to an actuated position in response
to acceleration of said vehicle,
- electrical contact means associated with
said IMM for generating an electrical signal when
said IMM is in its actuated position,
- hold means responsive to a voltage for
applying an electrostatic force to said IMM to
bias said IMM into said hold position, and
- means for applying a voltage to said hold
means to thereby establish the magnitude of the
bias on said IMM and thus the predetermined
vehicle crash acceleration necessary to force
said IMM from its hold position to its actuated
position; and
- means responsive to said microprocessor means and
to said electrical signal provided by said electrical
contact means for providing said control signal in
accordance therewith.
- 41. The system further
comprising an occupant restraint device for restraining the
movement of a vehicle occupant upon a crash of said
vehicle, said occupant restraint device being responsive to
said control signal for controlling the operation of said
device.
- 42. The system wherein
occupant restraint device is an air bag.
- 43. The system wherein said
voltage is selected such that said IMM moves to said
actuated position upon said safing switch experiencing
acceleration of a magnitude indicating that said vehicle is
experiencing a crash.
- 44. The system wherein said
force applied by said hold means is an electrostatic
attractive force having a magnitude functionally related to
said applied voltage.
- 45. The System wherein said
safing switch further comprises self test means for
determining the operational integrity of said electrical
contacts.
- 46. The system wherein hold
means comprises a conductive substrate capable of
generating an electrostatic attractive force, and an
insulating layer covering and protecting said conductive
substrate, said conductive substrate being positioned
closely adjacent said IMM such that said electrostatic
attractive force affects said IMM.
- 47. The system wherein said
electrical contact means comprises a pair of electrical
contacts, said contacts being "closed" when said IMM is in
one of said hold and actuated positions, and "open" when
said IMM is in the other of said hold and actuated
positions.
- 48. The system wherein said
IMM is plated metal.
- 49. The system wherein said
IMM is mounted on a substrate comprised of a semiconductor
material.
- 50. The system wherein said
semiconductor is silicon or gallium arsenide.
- 51. A method of deploying occupant crash restraint
apparatus in a vehicle as a function of the crash
acceleration experienced by said vehicle comprising the
steps of:
- providing a control circuit for assessing changes
in the acceleration experienced by said vehicle, said
control circuit including a safing switch having an
inertial mass member ("IMM") that relatively moves in
response to a predetermined crash acceleration level to
generate an electrical signal indicating a crash event;
- applying an electrostatic force to said IMM to
urge said IMM in the direction opposite the direction of
acceleration movement of said safing switch, said applied
electrostatic force being selected according to the
predetermined level of acceleration to which said switch is
to be responsive;
- generating an electrical signal when said IMM
moves in response to acceleration of said switch greater
than said predetermined crash acceleration level; and
- actuating said occupant crash restraint apparatus
when said electrical signal is being generated by said IMM.
- 52. In a crash detection apparatus capable of
deploying an occupant air bag restraint, a safing switch
responsive to a predetermined acceleration force and
generating an electrical signal when said safing switch is
actuated, said safing switch comprising:
- an inertial mass member ("IMM") relatively
movable from a hold position to an actuated position in
response to each acceleration of said switch;
- electrical contact means associated with the
inertial mass member for generating an electrical signal
when said IMM is in its actuated position; and
- hold means for generating an electrostatic
attractive force urging the IMM into its hold position and
restraining the IMM from relatively moving in response to a
crash acceleration less than a predetermined crash
acceleration value;
whereby said IMM is relatively moved to its
actuated position in response to a crash acceleration which
overcomes the restraining action of the electrostatic
force, and, when said IMM is in its actuated position, the
electrical contacts means generates the electrical signal
so as to enable the deployment of said air bag.
- 53. The apparatus further
including self test means for testing the electrical
continuity of the safing switch.
- 54. The apparatus wherein
said self-test means and said hold means are
interchangeable.
- 55. The apparatus wherein
each of said self-test means and said hold means is an
electrically conductive plate, and wherein said self-test
plate and hold plate are disposed on opposite sides of said
IMM but are generally equidistant from said IMM.
- 56. The apparatus wherein
said self-test plate is adapted to latch said electrical
contact means once said predetermined acceleration force is
sensed thereby preventing interruption of the deployment of
said air bag.
- 57. The apparatus wherein
said hold force applied by said hold means is adjusted by
said applied voltage.
- 58. The apparatus wherein
said electrical contacts comprise dual pairs of aligned
electrical contacts, and wherein one pair is disposed on
one side of said IMM and the second pair is disposed on the
opposite side of said IMM.
- 59. The apparatus wherein
one of said pairs of electrical contacts confirms that said
IMM is in its hold position and the other pair generates
said electrical signal when said safing switch senses a
predetermined acceleration force.
- 60. The apparatus wherein
one of the pairs of electrical contacts is normally open.
- 61. The apparatus wherein
one of the pairs of electrical contacts is normally closed.
- 62. An acceleration responsive switch comprising:
- a base member;
- a switch arm;
- mounting means for mounting said switch arm to
said base member so that acceleration of said base member
results in relative movement between said switch arm and
said base member;
- a pair of electrical contacts, one of said
electrical contacts mounted to said switch arm and a second
of said electrical contacts mounted to said base member so
that said acceleration of said base member changes the
switching state of said pair of electrical contacts; and
- electrostatic bias means operatively coupled to
between said base member and said switch arm for providing
a bias force to resists relative movement between said
switch arm and said base member.
- 63. The apparatus wherein said
electrostatic bias means prevents said pair of electrical
contacts from changing switching state until said base
member is subjected to an acceleration greater than a
predetermined amount.
- 64. The apparatus wherein said base
member, said switch arm, said mounting means, and said
electrostatic bias means are arranged so that said
electrical contacts are normally open and said electrical
contacts close when said base member is subjected to an
acceleration greater than said predetermined amount.
- 65. A system for recognizing the onset of a crash of
a vehicle and providing a control signal indicative
thereof, comprising:
- an accelerometer responsive to crash acceleration
of said vehicle for providing a crash acceleration signal
which varies as a continuous function of said crash
acceleration;
- microprocessor means responsive to the crash
acceleration signal for determining from said signal
whether said vehicle is experiencing a crash condition;
- a safing switch responsive to crash acceleration
of said vehicle, said safing switch comprising
- a base member;
- a switch arm;
- mounting means for mounting said switch arm
to said base member so that acceleration of said
base member results in relative movement between
said switch arm and said base member;
- a pair of electrical contacts, one of said
electrical contacts mounted to said switch arm
and a second of said electrical contacts mounted
to said base member so that said acceleration of
said base member changes the switching state of
said pair of electrical contacts; and
- electrostatic bias means operatively coupled
to between said based member and said switch arm
for providing a bias force to resists relative
movement between said switch arm and said base
member; and
- means responsive to said microprocessor means and
to said change of the switching state of said pair of
electrical contacts for providing said control signal in
response thereto.
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