Low Leakage Turbine Shaft Seals for Advanced Combined Cycle Systems.

Abstract

Advanced combined-cycle (COGAS) steam turbine overall system complexity and reliability can profit dramatically from low-leakage seals. The most critical seal locations are the high speed mainshaft seals at the bearings. The optimum seal system was selected as utilizing the feedwater as a buffer fluid. It was further shown advantageous from at least seal performance, life and reliability standpoints to vent the turbine high pressure end also to condenser vacuum. Three candidate late state-of-the-art low/zero leakage face seal assemblies were selected for manufacture and experimental test in a specially-modified test rig. Testing demonstrated that leakage rates from zero to 11 liters/day (3 gal/day) at speeds up to 92 m/sec (310 ft/sec) could be achieved at practical values of buffer pressure. These rates therefore met both the program objective of less than 11 liters/day (3 gal/day). Higher than anticipated parasitic drag was measured. A seal design which overcomes this drag was proposed. Limited cyclic endurance testing was carried out. (Author)

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Nov 01, 1984
Accession Number
ADA149372

Entities

People

  • G. W. Hosang

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies
  • Engineered Resilient Systems

DTIC Thesaurus Topics

  • Air Force
  • Boundary Layer
  • Chemical Synthesis
  • Chemistry
  • Feed Water
  • Fluid Dynamics
  • Fluid Flow
  • Friction
  • Gas Bearings
  • Gases
  • Hydrodynamics
  • Measurement
  • Performance Tests
  • Propulsion Systems
  • Test And Evaluation
  • Turbines
  • Turbulent Flow

Fields of Study

  • Engineering

Readers

  • Internal Combustion Engine (ICE) Technology.
  • Systems Analysis and Design
  • Tribology (the study of the boundary interaction between sliding surfaces, lubrication, wear and friction).