Aircraft grounding receptacle

Claim 2

An aircraft grounding receptacle comprising: a unitary body of electrically conductive material; said body of electrically conductive material having a first end comprising a connector portion; said body of electrically conductive material having a second end comprising a tubular portion; said tubular portion comprising a relatively small diameter portion extending from the connector portion and a relatively large diameter flange situated at said end of the body said flange extending perpendicularly to the tubular portion and comprising a substantial mass relative thereto; said flange and said tubular portion being separated into segments by a plurality of slots extending into the body from said second end thereof toward the connector portion; said body of electrically conductive material having a bore therethrough dimensioned to receive an aircraft grounding plug and including a reduced diameter portion situated adjacent said second end of the body which is adapted for mating engagement with the terminal groove of the aircraft grounding plug.

Claim 3

The aircraft grounding receptacle according to claim 1 wherein the connector portion of the body of electrically conductive material comprises an external thread situated at said one end of the body and a hexagonal portion situated adjacent the thread.

Claim 4

The aircraft grounding receptacle according to claim 1 wherein the tubular portion of the body of electrically conductive material is characterized by a total of four slots extending into the body from said second end thereof.

Claim 5

An aircraft grounding receptacle comprising: a unitary body of electrically conductive material; said body of electrically conductive material having a first end comprising a connector portion; said body of electrically conductive material having a second end comprising a tubular portion; said tubular portion comprising a relative small diameter portion extending from the connector portion and a relatively large diameter flange situated at said second end of the body; said tubular portion being separated into segments by a total of four slots extending into the body from said second end thereof toward the connector portion; said body of electrically conductive material having a bore therethrough dimensioned to receive an aircraft grounding plug and including a reduced diameter portion situated adjacent said second end of the body which is adapted for mating engagement with the terminal groove of the aircraft grounding plug; said flange of the tubular portion of the body of conductive material being hexagonal in shape and wherein the four slots intersect the flange adjacent to but spaced apart from four of the six points comprising the hexagonal shape of the flange.

Claim 6

An aircraft grounding receptacle comprising: a unitary body of electrically conductive material; said body of electrically conductive material having a first end comprising a connector portion; said body of electrically conductive material having a second end comprising a tubular portion; said tubular portion comprising a relative small diameter portion extending from the connector portion and a relatively large diameter flange situated at said second end of the body; said tubular portion being separated into segments by a total of four slots extending into the body from said second end thereof toward the connector portion; said body of electrically conductive material having a bore therethrough dimensioned to receive an aircraft grounding plug and including a reduced diameter portion situated adjacent said second end of the body which is adapted for mating engagement with the terminal groove of the aircraft grounding plug; said flange of the tubular portion of the body of conductive material being hexagonal in shape and wherein the four slots intersect the flange adjacent to but spaced apart from four of the six points comprising the hexagonal shape of the flange.

Claim 7

The aircraft grounding receptacle according to claim 4 further including a hole formed through the hexagonal flange for receiving a grounding lead.

Claim 8

An aircraft grounding receptacle comprising: a unitary body of electrically conductive material, having first and second ends; a connector portion including an external thread formed adjacent said first end of the body of electrically conductive material and a hexagonal portion situated at the end of the external thread remote from said first end of the body; a tubular portion extending from the hexagonal portion of the connector portion to the second end of the body of electrically conductive material and including a relatively small diameter portion extending from the hexagonal portion toward the second end of the body and a hexagonal flange located at the second end of the body of electrically conductive material; said tubular portion including four slots extending into the body from the second end thereof and separating the tubular portion of the body into four segments, said slots intersecting the hexagonal flange at locations adjacent to but spaced apart from four of the six points comprising the hexagonal shape of the flange; a bore extending through the body of electrically conductive material and dimensioned to receive an aircraft grounding plug therein; and said bore including reduced diameter portions located adjacent the second end of the body adapted for mating engagement with the terminal groove of the aircraft grounding plug.

Claim 9

An aircraft grounding receptacle comprising: a unitary body of electrically conductive material, having first and second ends; a connector portion including an external thread formed adjacent said first end of the body of electrically conductive material and a hexagonal portion situated at the end of the external thread remote from said first end of the body; a tubular portion extending from the hexagonal portion of the connector portion to the second end of the body of electrically conductive material and including a relatively small diameter portion extending from the hexagonal portion toward the second end of the body and a hexagonal flange located at the second end of the body of electrically conductive material; said tubular portion including four slots extending into the body from the second end thereof and separating the tubular portion of the body into four segments, said slots intersecting the hexagonal flange at locations adjacent to but spaced apart from four of the six points comprising the hexagonal shape of the flange; a bore extending through the body of electrically conductive material and dimensioned to receive an aircraft grounding plug therein; and said bore including reduced diameter portions located adjacent the second end of the body adapted for mating engagement with the terminal groove of the aircraft grounding plug.