Motion Instruments Inc.

Illinois Tool Works Inc.

Randy Fette

Robert James Przykucki, Jr

David Wayne Leadingham

Michael Chartier

Drew Robert Johnson

Ralph Emerson Welch

A sensor assembly includes a shank shaped for mating with a socket in a head of a bolt about which a portion of a rear suspension of a bicycle pivots. A magnetometer (or a permanent magnet) is coupled to the shank. A permanent magnet with a north pole and a south pole (or a magnetometer) is positioned adjacent to the magnetometer (or permanent magnet) and pivotable relative thereto. A linkage couples the permanent magnet (or magnetometer) to the portion of the rear suspension that pivots about the bolt. The magnetometer senses changes in the magnetic field as the suspension pivots.

Sensor assembly for pivoting suspension of bicycle

An elongated pressure sensitive potentiometer is disposed alongside and generally parallel to a reciprocating suspension component, such as a shock absorber, and between a steel track and a rolling or static magnet. The track and contained potentiometer extend from a mount at or near the top of a cylinder of the shock absorber to a point beyond the magnet when the shock absorber is in an uncompressed state. The mount couples the track to the shaft, parallel to and spaced apart from the shaft. Magnet attraction of the track compresses the potentiometer between the track and magnet.

Magnetically actuated pressure sensitive suspension position sensor

An aircraft ground power connector for use in an aircraft ground power support system providing electrical power from a ground power unit through a ground power cable to the ground power receptacle of a parked aircraft. The axis of the portion of the connector housing which engages the aircraft ground power receptacle is angled relative to the axis of the portion of the housing which receives the ground power cable to minimize mechanical stress on the aircraft ground power receptacle when the connector is installed therein and to render the connector easier to insert and remove from the aircraft receptacle. Additionally, the ground power connector includes a capacitor connected to an electrical circuit within the connector supplying do voltage to the aircraft ground power receptacle to mitigate momentary voltage drops at the receptacle resulting from momentary surges in current demand by the aircraft.

Growing community of inventors

Santa Rosa, CA, United States of America

Randy Fette