Experimental Analysis of the Leakage Characteristics of Three Types of Annular Segmented Seals

Author:

Fourt Erwan1,Arghir Mihai2,Jolly Pascal2,Andasmas Mohamed3

Affiliation:

1. Centre Technique des Industries Mécaniques, CETIM , Nantes 44308, France

2. Institut PPRIME, UPR CNRS 3346, Université de Poitiers, ISAE ENSMA , Poitiers 86000, France

3. Safran Aicraft Engines , Moissy Cramayel 77550, France

Abstract

Abstract The present paper presents an experimental analysis of the leakage characteristics of three kinds of segmented seals. The segments of the first seal have smooth pads while the second seal has pads with pockets. The pads of the third seal are smooth but the rotor is textured with inclined grooves. The pockets or the textures lift the segments from the rotor and create a radial clearance. This is reflected by the leakage flow rate, the friction torque, and the seal's temperature. These characteristics are hereby measured on a dedicated test rig. The presented results are dimensionless, the measured values for the three types of seal types being divided by the same maximum value. This makes it possible to compare the performance of different segmented seal technologies and to evaluate the compromise between low leakage and enhanced lifespan. The assumptions made on the opening of the segmented seal with pockets during the tests are finally verified with a simple analytical model.

Publisher

ASME International

Subject

Mechanical Engineering,Energy Engineering and Power Technology,Aerospace Engineering,Fuel Technology,Nuclear Energy and Engineering

Reference18 articles.

1. New Circumferential Seal Design Concept Using Self-Acting Lift Geometries,1972

2. Mainshaft Seals for Small Gas Turbine Engines,1974

3. Liquid Rocket Engine Turbopump Rotating-Shaft Seal,1978

4. High-Speed Cryogenic Self-Acting Shaft Seals for Liquid Rocket Turbopumps,1983

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