GAS TURBINE ENGINE LOW PRESSURE COMPRESSOR ROTOR IMPELLER (VERSIONS)

FIELD: engines and pumps.SUBSTANCE: invention relates to engine building. Gas turbine engine low-pressure compressor (GTE LPC) rotor shaft fourth stage impeller includes disc, including hub with central hole, web and rim, as well as blades each having tail and wing with profile formed by concave pre...

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Hauptverfasser: Erichev Dmitrij JUrevich, Marchukov Evgenij JUvenalevich, Skarjakina Regina JUrevna, Poljakov Konstantin Sergeevich, Kondrashov Igor Aleksandrovich, Kuznetsov Igor Sergeevich, Simonov Sergej Anatolevich
Format: Patent
Sprache:eng ; rus
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