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Uncooled choked-flow turbine for limited-power turbine engines

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Abstract

The gas dynamics of a choked-flow turbine is considered. An uncooled choked-flow turbine may be used in a limited-power gas-turbine engine without marked impairment of its mass and size and with considerable decrease in cost.

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References

  1. Rechkoblit, A.Ya., Development and research of choked-flow single-stage turbines, in Nauchnyi vklad v sozdanie aviatsionnykh dvigatelei (Scientific Input in to Creation of Aviation Engines), Skibin, V.A., Solonin, V.I., et al., Moscow: Tsentr. Inst. Aviats. Motorostr., 2000, pp. 228–231.

    Google Scholar 

  2. Bogdanov, V.I., Venediktov, V.D., and Yakubovskii, K.Ya., Implementation of uncooled choked-flow turbine in small gas turbine engines, II Mezhdunarodnoi tekh. konf. molodykh uchenykh i spetsialistov, Tezisy dokladov (II Int. Tech. Conf. of Young Scientists and Professionals, Abstracts of Papers), Zhukovskii: Tsentr. Aerogidrodin. Inst., 2002, pp. 40–41.

    Google Scholar 

  3. Argova, G.N., Bogdanov, V.I., and Fadin, A.A., Effective use of uncooled choked-flow turbine in small gas turbine engines, Vestn. Rybinsk. Gos. Aviats. Tekh. Univ. im P.A. Solov’eva, 2010, no. 3 (18), pp. 86–89.

    Google Scholar 

  4. Bogdanov, V.I., Yakubovskii, K.Ya., and Osipov, I.V., Unified gas generator for gas turbine engine with the capacity of 800 … 1300 horsepower, Vestn. Rybinsk. Gos. Aviats. Tekh. Univ. im P.A. Solov’eva, 2011, no. 2, pp. 85–87.

    Google Scholar 

  5. Inostrannye aviatsionnye dvigateli i gazoturbinnye ustanovki: spavochnik (Foreign Aircraft Engines and Gas Turbine Devices: Handbook), Moscow: Tsentr. Inst. Aviats. Motorostr., 2010, no.15.

  6. Bogdanov, V.I. and Fadin, A.A., The concept of singleshaft turbojet engine with an uncooled choked-flow turbine for an unmanned aircraft, Konvers. Mashinostr., 2008, no. 2, pp. 16–18.

    Google Scholar 

  7. Bogdanov, V.I. and Yakubovskii, K.Ya., The concept of a single-engine turbojet engine based on the gas generator of RD-33 engine, Aviats. Prom-st, 2013, no. 1, pp. 20–23.

    Google Scholar 

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Authors and Affiliations

  1. PAO NPO Saturn, Rybinsk, 152912, Russia

    V. I. Bogdanov

Authors
  1. V. I. Bogdanov
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Correspondence to V. I. Bogdanov.

Additional information

Original Russian Text © V.I. Bogdanov, 2017, published in Vestnik Mashinostroeniya, 2017, No. 2, pp. 40–41.

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Bogdanov, V.I. Uncooled choked-flow turbine for limited-power turbine engines. Russ. Engin. Res. 37, 386–387 (2017). https://doi.org/10.3103/S1068798X17050070

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  • DOI: https://doi.org/10.3103/S1068798X17050070

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