EXHAUST SYSTEM COMPONENT
An internal combustion engine exhaust system component includes an exhaust gas conduit having a metal shell. A boss is crimped to the metal shell. The boss is to threadingly mount an electrical sensor to measure an exhaust gas property. The boss includes a self-attaching nut.
1 . An exhaust system component for an internal combustion engine, the exhaust system component comprising:
an exhaust gas conduit having a metal shell; and
a boss, crimped to the metal shell;
wherein:
the boss is to threadingly mount an electrical sensor to measure an exhaust gas property; and
the boss includes a self-attaching nut.
2 . The component as defined in claim 1 wherein the electrical sensor is a Heated Exhaust Gas Oxygen (HEGO) sensor.
3 . The component as defined in claim 1 wherein the exhaust gas conduit is a catalytic converter.
4 . The component as defined in claim 1 wherein the exhaust gas conduit is a tubular member.
5 . The component as defined in claim 4 wherein the tubular member is connected to a catalytic converter to convey an exhaust gas produced by the internal combustion engine to the catalytic converter or to convey the exhaust gas from the catalytic converter.
6 . The component as defined in claim 1 wherein the metal shell defines an aperture having a central pilot portion of the self-attaching nut disposed therein.
7 . The component as defined in claim 6 wherein the aperture is defined in a flat land defined on a surface of the metal shell.
8 . The component as defined in claim 1 wherein the metal shell defines an aperture having been formed by shearing action of a central pilot portion of the self-attaching nut and a die button positioned against opposed surfaces of the metal shell, the self-attaching nut having been pressed toward the die button with a force to shear and separate a slug from the metal shell.
9 . The component as defined in claim 1 wherein the self-attaching nut comprises:
a central pilot portion having an outer side wall being annular;
an annular flange surrounding the central pilot portion, the annular flange having a planar end face defining a peripheral edge with an edge diameter greater than a wall diameter of the outer side wall of the central pilot portion;
the planar end face including a plurality of circumferentially spaced first anti-rotation elements, each of the first anti-rotation elements having a planar first top face spaced above the planar end face of the annular flange, the planar end face further including a plurality of circumferentially spaced second anti-rotation elements, each of the second anti-rotation elements having a planar second top face spaced below the planar end face of the annular flange, one of the plurality of first anti-rotation elements and the plurality of second anti-rotation elements radially extending from the peripheral edge of the annular flange to a location spaced from the outer side wall of the central pilot portion, the other of the plurality of first anti-rotation elements and the plurality of second anti-rotation elements radially extending from the outer side wall of the central pilot portion to a location spaced from the peripheral edge of the annular flange; and
the first anti-rotation elements circumferentially alternating with the second anti-rotation elements.
10 . The component as defined in claim 9 wherein the first anti-rotation elements extend radially inwardly toward the central pilot portion from the peripheral edge of the planar end face.
11 . The component as defined in claim 9 wherein each of the first top faces of the first anti-rotation elements and the second top faces of the second anti-rotation elements is inclined relative to the planar end face of the annular flange.
12 . The component as defined in claim 9 wherein the first anti-rotation elements define a trapezoidal cross-section.
13 . The component as defined in claim 9 wherein the annular flange defines an outer radial flange wall, and the first anti-rotation elements each define a distal wall aligned with the outer radial flange wall.
14 . The component as defined in claim 13 wherein the outer radial flange wall defines a polygonal shape comprising a plurality of abutting planar surfaces.
15 . The component as defined in claim 14 wherein each of the first anti-rotation elements is aligned generally centrally with one of the abutting planar surfaces.
16 . The component as defined in claim 9 wherein the second anti-rotation elements extend radially outwardly from a base of the central pilot portion.
17 . The component as defined in claim 9 wherein the central pilot portion defines an undercut, and the second anti-rotation elements extend radially outwardly from beneath the undercut upwardly to a location spaced from the edge of the annular flange.
18 . The component as defined in claim 9 wherein the central pilot portion defines a pilot end and an inclined surface, the inclined surface being spaced from the pilot end.
19 . The component as defined in claim 9 wherein the central pilot portion defines a pilot end and an inclined surface spaced from the pilot end by a cylindrical surface.
20 . The component as defined in claim 9 wherein a ratio between an angle defined between the first top face and the planar end face to an angle defined between the second top face and the planar end face is between about 1.7 and 1.1.
21 . The component as defined in claim 20 wherein the ratio is about 1.3.