Certain features of GTE combustion chamber open-type nozzles |
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Authors: | S V Kotsyubinskii Yu A Ravikovich |
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Institution: | 1. OAO Klimov, ul. Kantemirovskaya 11, Saint Petersburg, 194100, Russia 2. Moscow Aviation Institute (National Research University), Volokolamskoe shosse 4, Moscow, 125993, Russia
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Abstract: | In this paper, we consider the capability of GTE centrifugal open-type nozzles to recover combustion in the main combustion chamber at short-term fuel cutoffs into the fuel manifolds, when the anti-surge system operates, as well at actuation of “emergency brake” or the “dipping and shutdown valve”. We describe some features of the centrifugal open-type nozzles that make it possible to ensure the stable operation of the combustion chamber even at the “lean” blow-off boundary at α CC max ≤ 65. The possibility of combustion recovery without using the spark plugs after the anti-surge system actuation has been experimentally confirmed. |
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