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Research and Development of the Joint Seals for Gas Turbine Engine High-Temperature Turbine Stator Units

  • Aircraft and Rocket Engine Design and Development
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Abstract

The porous elastic dam** metal mesh material (metal fiber) is considered as a joint seal. The features of this type of turbine seals and requirements to their application are presented. Data of the experimental studies and already created seal designs are given.

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Correspondence to A. I. Belousov.

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Russian Text © The Author(s), 2019, published in Izvestiya Vysshikh Uchebnykh Zavedenii, Aviatsionnaya Tekhnika, 2019, No. 2, pp. 89–94.

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Belousov, A.I., Borisov, V.A. & Parovai, F.V. Research and Development of the Joint Seals for Gas Turbine Engine High-Temperature Turbine Stator Units. Russ. Aeronaut. 62, 267–273 (2019). https://doi.org/10.3103/S1068799819020132

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  • DOI: https://doi.org/10.3103/S1068799819020132

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