Transitional turbulator
AssigneeGM Global Technology Operations LLC
InventorsJared J. Keyes, Andrew G. Morse
Life of this patent
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Abstract
An air-to-air charge air cooler for cooling air supplied to an internal combustion engine includes a tube assembly including a plurality of tubes extending in a longitudinal direction. The plurality of tubes is arranged adjacent to one another. Each of the plurality of tubes includes an inlet to receive airflow and an outlet to output airflow. A turbulator is arranged in at least one of the plurality of tubes, the turbulator having a pitch defined in a direction transverse to airflow through the tube. The pitch varies in at least one of a longitudinal direction and a transverse direction of the tube.
Claims9
An air-to-air charge air cooler for cooling air supplied to an internal combustion engine, comprising:
- a tube assembly including a plurality of tubes extending in a longitudinal direction,
- wherein the plurality of tubes are arranged adjacent to one another, and
- wherein each of the plurality of tubes includes an inlet to receive airflow and an outlet to output the airflow;
- and
- a first turbulator and a second turbulator arranged in at least a first one of the plurality of tubes, each of the first and second turbulators having a pitch defined in a direction transverse to airflow through the first one of the plurality of tubes,
- wherein the pitch varies in at least one of the longitudinal direction and the transverse direction of the first one of the plurality of tubes,
- wherein the first turbulator has a first pitch and the second turbulator has a second pitch that is less than the first pitch,
- wherein the first turbulator is arranged adjacent to the second turbulator in the transverse direction in the first one of the plurality of tubes, and
- wherein the amount by which the second turbulator extends in the transverse direction is in a range from 25% to 75% of the width of the first one of the plurality of tubes.
Dependencies are inferred from the claim text.