CA2077719A1 - Safing velocity change sensor - Google Patents

Safing velocity change sensor

Info

Publication number
CA2077719A1
CA2077719A1 CA002077719A CA2077719A CA2077719A1 CA 2077719 A1 CA2077719 A1 CA 2077719A1 CA 002077719 A CA002077719 A CA 002077719A CA 2077719 A CA2077719 A CA 2077719A CA 2077719 A1 CA2077719 A1 CA 2077719A1
Authority
CA
Canada
Prior art keywords
housing
blades
inertial element
sensor
motor vehicle
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.)
Abandoned
Application number
CA002077719A
Other languages
French (fr)
Inventor
Allen K. Breed
Ted Thuen
Carl T. Grossi
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Breed Automotive Technology Inc
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Publication of CA2077719A1 publication Critical patent/CA2077719A1/en
Abandoned legal-status Critical Current

Links

Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01HELECTRIC SWITCHES; RELAYS; SELECTORS; EMERGENCY PROTECTIVE DEVICES
    • H01H35/00Switches operated by change of a physical condition
    • H01H35/14Switches operated by change of acceleration, e.g. by shock or vibration, inertia switch

Landscapes

  • Air Bags (AREA)
  • Switches Operated By Changes In Physical Conditions (AREA)

Abstract

ABSTRACT OF THE INVENTION
A safing sensor for sensing velocity changes particularly suited for passenger restraint systems in a motor vehicle for the deployment of an air bag includes a housing with contact blades and an inertial element. The movement of the inertial element is substantially undamped within the housing. Preferably, the sensor includes mounting tabs for mounting said housing on a printed circuit board.

Description

2~ 9 BACRGROlJND OF THE INVENTION

1. Field of the invention ~his invention pertains to a velocity change sensor or accelerometer used in motor vehicles for detecting sudden changes in velocity and for activating in response a passenger restraining system such as an air bag system. More particularly, this invention pertains to a safing sensor which includes an 0 element which moves to a preset position in response to a sudden deceleration to activate a pair of contact blades.

2. Backaround of the Invention Studies have been made which indicate that injuries in motor vehicle accidents, especially at high speeds, can be substantially reduced or eliminated by the use of passenger restraint systems. (The term "passenger" is used to cover the driver of a car as well.) These systems include an inflatable balloon usually termed an air bag which normally is stored away in the instrument panel or the steering wheel. When the motor I venicle is subjected to a sudden deceleration, the air bag is ll inflated and is deployed automatically in a position which ¦ cushions the passengers, restrains their movement and prevents ¦l contact between them and the automobile interior such as the ¦I windshield, the steering wheel, the instrument panel and so on.
Il Of course, a crucial element of all such systems is the velocity 1I change sensor or accelerometer which initiates the inflation and deployment of the air bags. The motion of the motor vehicle must be carefully and precisely monitored so that the air bags can be deployed very fast, before the passengers suffer any substantial I injury.
¦ I A velocity change sensor is disclosed in U.S. Patent No.
4,329,549 assigned to the same company as the present invention.
This sensor comprises a tubular housing surrounding a metallic shell, a metal ball and a magnet biasing the ball toward a first end of the shell. At the second end of the shell there is a pair I of electrical contact blades. The sensor is positioned in the motor vehicle in an orientation such that when the motor vehicle experiences a deceleration which exceeds a preset level, the ball moves from the first toward the second end, making contact with the two blades. Because the blades and the ball are made of on electrically conducting material, when the ball contacts the blades, an electrical path is established between the two blades.
This electrical path is used to initiate a signal for the deployment of the air bags.
A problem associated with the prior art concerns the safety of the system. While the deployment of an air bag during a crash is critical to insure the protection of the passenger, prevention ~1 2~ 7~ 9 ! of a false deployment is equally critical. Once an air bag is deployed,iit seriously impairs the movement of the driver.
¦ Therefore, if an air bag is falsely activated, i.e. while the I vehicle is moving and is not involved in a serious accident, ¦I rather than protecting the driver, the air bag may actually I hamper him or her from proper operation of a vehicle.
i, i i, OBJECTIVE8 AND 8~ RY OF THB INVBNTION
I! In view of the above mentioned disadvantages of the prior !l art, it is an objective of the present invention to provide a ¦j restraint system with an inexpensive safing sensor which provides ¦
~! redundancy for the operation of the restraint system.
¦~ A further objective is to provide a restraint system with a safing sensor in which an inertial moving element causes a l contact between two electrical contact blades substantially, lS ¦ simultaneously.
Other objectives and advantages of the invention shall become apparent from the following description. An accelerometer constructed in accordance with the invention includes a housing with at least one pair of contact blades; and an inertial element moving in a predetermined path in response to a change in velocity of the motor vehicle. The two contact blades are disposed in the path of the moving inertial element in such a manner that a direct electrical path is established through the contact by the element. In one embodiment, a crash is sensed when an electric contact is established through the inertial element. In another embodiment, one contact is bent under the influence of the inertial element to touch another contact.
Importantly, the movement of the inertial element is undamped to insure a quick operation for the sensor.

Il BRIEF DESCRIPTION OF THE FIGURES
Figure 1 shows a block diagram for a restraint system constructed in accordance with this invention;
¦ Figure 2 side elevational view of an accelerometer ! constructed in accordance with the invention;
Figure 3 shows the sensor of Figure 2 with its contacts closed;
on the fifth page of drawings I Figure 4*shows a top view of an alternate embodiment;
¦ Figure 5 shows a side elevational view of the embodiment of ¦ Figure 4;
I Figure 6 shows a bottom view of the embodiment of Figure 5;
Figure 7 shows a side elevational view similar to Figure 5 with inertial mass moved in response to a deceleration; and i Figure 8 shows a partial side elevational view of a diagnostic ~ sensor mounted on a printed circuit board.

DETAILED DESCRIPTION OF TRE INVENTION
To illustrate more clearly the operation of a safing sensor, reference is now made to Figure 1 wherein a block diagram of a passenger restraint system 10 is shown, said restraint system including a safing sensor 12 coupled to a primary or discriminating sensor 14. Primary sensor 14 in turn triggers an inflator device 16 for inflating an air bag 18. The primary sensor 14 may be a damped sensor constructed and arranged to discriminate between crashes, and more particularly to differentiate between low speed and high speed crashes.
Turning now to the remaining Figures, a safing sensor 12 constructed in accordance with this invention is usually mounted on the motor vehicle (not shown).
The sensor has a tubular portion 20 terminating with a flared end 22 and an open end 24 closed by a potting material.
Alternatively, the junction between plug 28 and end 24 may be ¦ sealed by other means. A plug 2~Ls'di's~ ~ d adjacent to potting 26 as shown, with a spherical depression 30. The tubular portion 20 is preferably made of a plastic material, and holds an inertial element such as a metal ball 34.
j Flared end 22 is provided with a peripheral flange 32, and is covered by an axially disposed retainer 44. Retainer 44 may be attached to portion 20 by any well known means such as with an ¦ adhesive or by crimping. Mounted on retainer 44 there are four ! blades 46, 48, 50 and 52. For the sake of convenience, blades 46 I and 48 shall be referred to as the lower blades while blades 50 and 52 shall be referred to as the upper blades. Each of these blades has a straight portion which passes through a hole 56 in ¦ retainer 44. Each blade is maintained in place by insulating ¦ bushings such as bushings 54, and is made of a relatively thin ¦ and flat conductive material such as copper. Lower blades 46 and 48 are terminated at their upper portions with respective curved sections 58 and 60 as shown in Figure 2. Upper blades 50, 52 extend further radially inward into the passageway 40 of tubular portion 20 and their tips 62, 64 are preferably coated with an insulating material, such as a plastic material. In addition, or alternatively, ball 34 may be covered by an insulating material.
Disposed within portion 20, there are shoulders 66, 68 for presetting the blades 46, 48, to the positions shown in Figure 2.
Passageway 40 is defined by a plurality of ribs such as 70 constructed and arranged to guide ball 30 therethrough without any substantial aero dynamic damping. Mounted on retainer 44, there is a stop 72 with an inner spherical surface 74 in opposed relation to surface 30. The surfaces 74 and 30 have radii of curvature equal to the radius of ball 34.
Secured to flange 32, there is an outer cap 80 which defines a chamber 82 with flange 32 and inner retainer 44. Within J77~ 9 j chamber 82, there can be a printed circuit board 84 used to mount various circuit elements such as resistors 86. Blades 46, 48, 50, 52 extend to board 84 as shown. Cap 80 has a mounting tab 88 ¦
for mounting sensor 10 on the fire wall 90 of a motor vehicle, , through insulating pad 92.
~ A plug 94 connected through cap 80 is used to couple the ¦! board 84 to sensor 12 as well as to provide power.
I The sensor 12 operates in the following manner. Safing ¦ sensor 12 can be mounted, for example, on the fire wall or passenger compartment of a vehicle while the primary sensor 14 may be mounted either in the passenger compartment or in the crush zone. Upper blades 50, 52 are arranged and constructed to bias ball 34 against wall 30 as shown in Figure 2. The sensor 12 ' is positioned in such an orientation that, if the vehicle experiences a deceleration, ball 34 is urged in the direction indicated by arrow A in Figure 2. If this deceleration is greater than a preselected threshold level (defined by the biasing force of blades 50, 52) the force of deceleration overcomes the biasing force and the ball 34 is projected in direction A along the passageway 40. Initially, the ball 34 is in contact with the tips of the upper blades 50, 52. As the ball moves in the direction A, it bends blades 50, 52 in the same direction until these blades come into contact with the curved sections 58, 60, as shown in Figure 3. An electrical path is 2S then formed between blades 48, 50 and another electrical path between blades 46 and 52. These electrical paths may be used to generate electrical signals which may be sent, for example, from the conductors of plug 94 to sensor 12 as described above.
Figures 4-8 show a different embodiment of a safing sensor which is biased magnetically rather than mechanically. More specifically, safing sensor 100 includes a housing 102 made up of , 2~ ~ ~7.~9 two portions: an elongated tubular portion 104 and a base portion 106. The base portion may be rouncled at the corners as at 108 (Fig. 4). Housing 102 is made of a plastic or non-magnetic I metallic material. Base 106 is terminated at one end by a I retainer 110 made of a material similar to housing 102.
¦l Inside, housing portion 104 is divided into two coaxially ¦! arranged chambers 112, 114 by a wall 113. Chamber 112 houses a permanent magnet 115. Chamber 114 defines a path of movement for¦
! an inertial element in the shape of a ball 116. The ball is I preferably made of a magnetizable material and its surface is ¦ electrically conductive. Chamber 114 is also provided with a plurality of longitudinal ribs 118 which define a path of movement for ball 116. The ribs are arranged to permit air flow I around the ball 116 as the ball moves through the housing to I insure that the ball movement is substantially undamped. Dis-posed around housing portion 104 there is a member 120. As shown in Figure 5 member 120 extends only part way along housing portion 104 so that it does not overlap housing portion 106.
This member 120 is made of a magnetizable material and is used to concentrate the magnetic field generated by magnet 112 to chamber 114. In this manner, the size of the magnet, and therefore the size of the sensor can be minimized. This member is described in more detail in U.S. Application S.N.418,147 filed October 6, 1989. Member 120 can be held in place on housing portion 104 by tabs 122.
Housing portion 106 defines another chamber 124. Inside this chamber 124 there are two contact blades 126, 128. Blades 126, 128 are made of flexible, electrically conductive material.
Each blade is secured to retainer 110 by straight portions 130, 132. Chamber 124 is in communication with chamber 114 as shown.
At the interface between these two chambers there is a cylindri-~11 2~t~7~ 9 ii cal shoulder 134. Blades 126, 128 are shaped so that they are j normally biased against the shoulder 134. In this manner the position of the blades is preset in a manner similar to the one ' described in U.S. application S.N. 417,914 filed October 6, 1989, 1 ,~ now Also within chamber 124, mounted on cap 110 is a stop 138 which defines the end of travel of ball 116.
As shown in more detail in Figures 5, 6 and 8, blades 126, 1', 128 extend through retainer 110 and are connected at their outer l! ends 130, 132 to wires 140, 142 disposed, for example, ' ¦~ perpendicularly to the blades. In addition, housing 102 is also provided with a mounting leg 144 extending in parallel with wires 140, 142. As shown in Figure 8, these elements are used to mount the sensor 100 on a printed circuit board 146. Preferably wires ~ 140, 142 are connected to conductors (not shown) on the board 1, 146, while leg 144 is used to support the sensor on the board 146. Board 146 holds other electronic components used for controlling the inflator device 16 and air bag 18. In addition, the primary or discriminating sensor 14 may also be mounted on I board 146.
li In operation, inertial mass or ball 116 normally is biased against wall 113 by magnet 115. When the motor vehicle is involved in a crash, ball 116 moves away from wall 113 toward stop 138. When the ball touches the tips of contact blades 130, 132 an electrical path is established from one blade through the ball to the second blade thereby indicating that a crash has occurred. This action causes a signal to be applied to the ¦discriminating sensor which determines whether the passenger ¦restraint system should be deployed.
Obviously, numerous modifications may be made to the invention without departing from its scope as defined in the appended claims.

Claims (15)

1. A accelerometer for sensing velocity changes in a motor vehicle comprising:
housing means with a housing portion with a first end and a second end opposite said first end for defining a passageway;
an inertial element disposed in said housing and dimensioned for movement in said passageway without substantial damping; and first and second contact means disposed in said housing means, said first contact means being flexible for biasing said inertial element toward said first end, said inertial element moving without substantial damping through said passageway in response to a deceleration to bend said first contact means toward said second contact means.
2. The accelerometer of claim 1 wherein said first and second contact means each includes a pair of contact blades.
3. The accelerometer of claim 1 wherein one of said inertial element and said contact means is provided with a insulating coating to prevent an electrical path through said sensing element.
4. A passenger restraint system for a motor vehicle comprising:
an air bag disposed in the motor vehicle;
a control unit for selectively deploying said air bag in said motor vehicle for protecting a passenger in a crash;
a primary sensor for sensing a velocity change of said motor vehicle coupled to said control unit; and safing sensor including:

a housing disposed in said motor vehicle and defining a passageway;
a pair of contact blades axially disposed in said housing:
an inertial element disposed in said passageway, said inertial element being dimensioned to move through said passageway without damping; and biasing means for biasing said inertial element to a preselected position.
5. The passenger restraint system of claim 4 wherein said biasing means comprises a magnetic biasing means for biasing said inertial element.
6. The passenger restraint system of claim 4 wherein said biasing means urges said contacting element toward a first position away from said contact blades.
7. The passenger restraint system of claim 4 wherein said housing is arranged in a position in which said contacting element is urged toward said contact blades when said motor vehicle is decelerated.
8. The passenger restraint system of claim 5 wherein said biasing means further comprises a conductive member disposed outside said housing for applying said magnetic force to said sensing element.
9. The passenger restraint system of claim 8 wherein said contacting element comprises a ball.
10. The passenger restraint system of claim 4 wherein said contact blades have an insulated coating for insulating said blades from said ball.
11. The passenger restraint system of claim 10 comprising a first pair of blades disposed in the path of said inertial element and a second pair of blades spaced away from said first pair of blades by said inertial element to form two electrical paths through said second pair of blades.
12. The passenger restraint system of claim 4 wherein said control unit includes a printed circuit board and said safing sensor includes mounting means for mounting said safing sensor on said printed circuit board.
13. A safing crash sensor assembly for a motor vehicle comprising:
a housing including a pair of contacts;
an inertial element disposed in said housing, said housing defining an undamped pattern of movement for said inertial element in respect to a velocity change;
biasing means disposed in said housing for biasing said inertial mass toward a first position along said path, said inertial mass moving away from said first position in response to said velocity change to establish an electrical path between said pair of contacts;

a printed circuit board; and mounting means for mounting said housing on said printed circuit board.
14. The sensor of claim 13 wherein said biasing means includes a magnet and said inertial element is made of a magnetic material.
15. The sensor of claim 14 wherein said contacts extend through said housing for mounting on said printed circuit board.
CA002077719A 1991-09-24 1992-09-08 Safing velocity change sensor Abandoned CA2077719A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US76501691A 1991-09-24 1991-09-24
US765,016 1991-09-24

Publications (1)

Publication Number Publication Date
CA2077719A1 true CA2077719A1 (en) 1993-03-25

Family

ID=25072411

Family Applications (1)

Application Number Title Priority Date Filing Date
CA002077719A Abandoned CA2077719A1 (en) 1991-09-24 1992-09-08 Safing velocity change sensor

Country Status (7)

Country Link
JP (1) JPH0795078B2 (en)
CA (1) CA2077719A1 (en)
DE (1) DE4231873A1 (en)
FR (1) FR2681695B1 (en)
GB (1) GB2260028B (en)
IT (1) IT1257091B (en)
SE (1) SE9202740L (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE4314296A1 (en) * 1993-04-30 1994-11-03 Hydac Electronic Gmbh Sensor unit with holding clip

Family Cites Families (16)

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Publication number Priority date Publication date Assignee Title
US3452175A (en) * 1967-05-29 1969-06-24 Atomic Energy Commission Roller-band devices
JPS5425294B1 (en) * 1971-03-16 1979-08-27
US3812726A (en) * 1972-09-28 1974-05-28 Technar Inc Velocity responsive apparatus
US4329549A (en) * 1980-04-29 1982-05-11 Breed Corporation Magnetically biased velocity change sensor
JPH0711537B2 (en) * 1986-02-27 1995-02-08 本田技研工業株式会社 Deceleration sensor
DE3713698C1 (en) * 1987-04-24 1988-07-14 Hopt & Schuler Ddm Acceleration switch
JPH03500348A (en) * 1988-07-14 1991-01-24 ノートン,ピーター Compact collision detection switch with air channel and diagnostic system
WO1990010302A1 (en) * 1989-02-23 1990-09-07 Automotive Technologies International, Inc. Improved automobile crash sensors for use with passive restraints
SE9001951L (en) * 1989-10-06 1991-04-07 Breed Automotive Tech SENSOR MAKES SPEED CHANGE WITH SETTING SCREW
DE4031327A1 (en) * 1989-10-06 1991-04-11 Breed Automotive Tech ACCELERATION SENSOR, IN PARTICULAR FOR Passenger Restraint Systems In A VEHICLE
US5031931A (en) * 1989-12-06 1991-07-16 Breed Automotive Corporation Velocity change sensor with spring bias
SE513091C2 (en) * 1989-10-06 2000-07-03 Breed Automotive Tech Accelerometer for detecting speed changes in a vehicle
US5011182A (en) * 1989-10-06 1991-04-30 Breed Automotive Technology, Inc. Velocity change sensor with contact retainer
US5098122A (en) * 1989-12-06 1992-03-24 Breed Automotive Velocity change sensor with improved spring bias
GB2239562A (en) * 1989-12-27 1991-07-03 Autoliv Dev Inertia switch
US5012050A (en) * 1990-02-23 1991-04-30 Siemens Automotive Limited Dual pole switch assembly for an inertia actuated switch

Also Published As

Publication number Publication date
ITTO920739A1 (en) 1994-03-04
JPH05223841A (en) 1993-09-03
ITTO920739A0 (en) 1992-09-04
GB2260028B (en) 1995-10-25
DE4231873A1 (en) 1993-03-25
IT1257091B (en) 1996-01-05
GB9220118D0 (en) 1992-11-04
GB2260028A (en) 1993-03-31
SE9202740D0 (en) 1992-09-23
JPH0795078B2 (en) 1995-10-11
SE9202740L (en) 1993-03-25
FR2681695B1 (en) 1997-01-10
FR2681695A1 (en) 1993-03-26

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Legal Events

Date Code Title Description
EEER Examination request
FZDE Discontinued