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NASA NTRS ยท 19810007957

Self-acting geometry for noncontact seals

Abstract

Performance ot two self acting seal designs for a liquid oxygen (LOX) turbopump was predicted over ranges of pressure differential and speed. Predictions were compared with test results. Performance of a radial face seal for LOX was predicted up to 448 N/cu cm and 147 m/sec. Performance of a segmented circumferential seal for helium was predicted up to 69 N/cu cm and 189 m/sec. Results confirmed predictions of noncontact operation. Qualitative agreement between test and analysis was found. The LOX face seal evidently operated with mostly liquid in the self acting geometry and mostly gas across the dam.

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BibTeXRIS

Allen, G. P.. 1981-01-01. Self-acting geometry for noncontact seals. https://ntrs.nasa.gov/citations/19810007957

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