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Design study of shaft face seal with self-acting lift augmentation. 4: Force balance (1972)

Ludwig, L. P. ; Zuk, J. ; Johnson, R. L.

In: CASI

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Publication Date: 2019-06-27

Description: A method for predicting the operating film thickness of self-acting seals is described. The analysis considers a 16.76-cm mean diameter seal that is typical of large gas turbines for aircraft. Four design points were selected to cover a wide range of operation for advanced engines. This operating range covered sliding speeds of 61 to 153 m/sec, sealed pressures of 45 to 217 N/sq cm abs, and gas temperatures of 311 to 977 K. The force balance analysis revealed that the seal operated without contact over the operating range with gas film thicknesses ranging between 0.00046 to 0.00119 cm, and with gas leakage rates between 0.01 to 0.39 scmm.

Keywords: MACHINE ELEMENTS AND PROCESSES

Type: NASA-TN-D-6568 , E-6458

Format: application/pdf

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