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Tuesday, November 17, 2020 | History

2 edition of Seal technology in gas turbine engines found in the catalog.

Seal technology in gas turbine engines

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Propulsion and Energetics Panel.

Seal technology in gas turbine engines

papers presented at the Propulsion and Energetics Panel"s 51st (B) Specialists" Meeting in London, United Kingdom 6-7 April 1978.

by North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Propulsion and Energetics Panel.

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  • 37 Currently reading

Published by AGARD in Neuilly sur Seine, France .
Written in English

    Subjects:
  • Gas-turbines -- Congresses.

  • Edition Notes

    Includes bibliographical references.

    GenreCongresses.
    SeriesAGARD conference proceedings -- no. 237
    The Physical Object
    Pagination267 p. in various pagings :
    Number of Pages267
    ID Numbers
    Open LibraryOL19562510M
    ISBN 109283502183
    ISBN 109789283502180

      This book is intended to provide valuable information for the analysis and design of various gas turbine engines for different applications. The target audience for this book is design, maintenance, materials, aerospace and mechanical engineers. The design and maintenance engineers in the gas turbine and aircraft industry will benefit immensely from the integration and system .


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Seal technology in gas turbine engines by North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Propulsion and Energetics Panel. Download PDF EPUB FB2

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Both gas and oil seals were covered. Supplemental Notes: Papers presented at the Propulsion and Energy Panel, (B) Special Meeting, 51st, London, AprilAlso available from NTIS.

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FUNDAMENTALS OF GAS TURBINE ENGINES INTRODUCTION The gas turbine is an internal combustion engine that uses air as the working fluid. The engine extracts chemical energy from fuel and converts it to mechanical energy using the gaseous energy of the working fluid (air) to drive the engine and propeller, which, in turn, propel the airplane.

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13, No. 16 Influence of slashface leakage coupled with quasi-labyrinth seal technique on gas turbine endwall aerothermal performance and blade suction side surface phantom. Gas-turbine engine, any internal-combustion engine employing a gas as the working fluid used to turn a turbine.

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London, April has been cited by the following article. The concept of thermally sprayed abradable sealing technology has successfully been used in aero engines and industrial gas turbines for several decades now. More recently efforts were undertaken to implement the concept of seal coatings in steam turbine designs.

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Journal of Engineering for Gas Turbines and Power Vol. ; Iss. 9 A Probabilistic Secondary Flow System Design Process for Gas Turbine Engines Ramerth, Douglas L., MirzaMoghadam, Alexander V., Kiratsingh, Ashish, Banda, Gaurav. Aircraft Engines and Gas Turbines is widely used as a text in the United States and abroad, and has also become a standard reference for professionals in the aircraft engine in treating the engine as a complete system at increasing levels of sophistication, it covers all types of modern aircraft engines, including turbojets, turbofans, and turboprops, and also discusses Reviews: 5.

A method of seal leakage calculation was developed. It connects engine thermogasdynamics calculation, airflow hydraulics calculation and structural analysis of deformed parts. The main sources of heat transferred to the supporting element were determined; their numerical values and percentages for the compressor and turbine were also determined.

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Unique in treating the engine as a complete system at increasing levels of sophistication, it covers all types of modern aircraft engines, including turbojets, turbofans, and turboprops, and also discusses.