Vehicle instrument panel air bag door assembly

Abstract

An air bag deployment door mechanism for the instrument panel of an automotive vehicle. A deployment door is molded integral with the instrument panel retainer and defined by a plurality of closely spaced holes about its perimeter. The spacing between the holes define the physical connection between the deployment door and the instrument panel retainer. A tear initiator is molded into the deployment door which is activated by the inflating air bag. The tear initiator pierces the foam and decorative layers prior the severing of the physical connection between the deployment door and the instrument panel retainer.

1 . An instrument panel air bag deployment door mechanism for a vehicle comprising: 
 a molded plastic instrument panel retainer having an internal surface adjacent to which an air bag is stored prior to deployment and an outer surface that faces the passenger compartment of the vehicle;    a foam layer disposed on the outer surface of the instrument panel retainer;    a pliant external layer overlaying the foam layer;    a deployment door molded integral with the instrument panel retainer, the deployment door having a physical attachment of a selected strength to the remainder of the instrument panel retainer so that the physical connection between the deployment door and the instrument panel retainer is severed upon the application of sufficient force from an inflating air bag; and    a tear initiator molded integral with the molding of the deployment door, the tear initiator having a base flexibly attached to the deployment door and a free end adjacent to one edge of the deployment door, the free end having a pointed piercing portion that extends normally towards the external layer, the tear initiator further having an actuator portion that protrudes towards a stored air bag such that an inflating air bag contacts the actuator portion and pivots the tear initiator relative to the door causing the pointed piercing portion to pierce through the foam layer and the external layer prior to severing the physical connection between the deployment door and the instrument panel retainer.    
     
     
         2 . The deployment door mechanism of  claim 1  wherein the perimeter of the deployment door is defined by a series of holes through the instrument panel retainer, the spacing of the holes controlling the force required to sever the deployment door from the instrument panel retainer.  
     
     
         3 . The deployment door mechanism of  claim 2  wherein the holes through the instrument panel retainer are laser-scored holes.  
     
     
         4 . The deployment door mechanism of  claim 3  wherein the laser-scored holes further extend part way through the foam layer.  
     
     
         5 . The deployment door mechanism of  claim 4  wherein the depth of the laser-scored holes through the foam layer extends to within 0.2 to 0.4 millimeters of the external layer.  
     
     
         6 . The deployment door of  claim 1  wherein the pointed piercing portion of the tear initiator lies below the outer surface of the instrument panel retainer.  
     
     
         7 . The deployment door mechanism of  claim 6  wherein the pointed piercing portion is 2.0 to 5.0 millimeters wide.  
     
     
         8 . The deployment door mechanism of  claim 6  wherein the actuator portion is a portion of the tear initiator intermediate the base and the free end that is bowed away from the foam layer and the external layer.  
     
     
         9 . The deployment door mechanism of  claim 1  wherein the external layer is a decorative layer.  
     
     
         10 . The deployment door mechanism of  claim 1  wherein the foam layer is from 4 to 6 millimeters thick.