Heavy helicopter for arctic transport system

DOI: 10.34759/vst-2021-2-52-68

Аuthors

Artamonov B. L.^1*, Zagranichnov A. S.^2**, Lisovinov A. V.^3***

1. Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia
2. ,
3. National Helicopter Center Mil & Kamov, 26/1, Garshina str., Tomilino, Moscow region, 140070, Russia

*e-mail: k102@mai.ru; abl-6124554@yandex.ru
**e-mail: senya.zagr@mail.ru
***e-mail: lisowinov.alexandr@yandex.ru

Abstract

The article deals with the project of a heavy helicopter, being one of the transport system elements of the Arctic zone of the Russian Federation. The helicopter is being created based on the PD-12V prospective domestic gas turbine engine.

The software for helicopter appearance forming, which represents a set of jointly operating modules of weight and aerodynamic calculation, was employed for the carrier system parameters selection.

The dependences of rafts, emergency water touchdown, and thermal and sound insulation weight on the helicopter weight were obtained in this work. Various combinations of the main rotor diameter values and blade aspect ratio for the selected transport operations were analyzed. Optimal values of the helicopter main rotor parameters have been selected using the reduced criterion of the helicopter efficiency.

The project helicopter outdoes the Mi-8AMTSh-VA Arctic helicopter and Mi-26 helicopter by its performance characteristics by either loading capacity and flight range, or flight hour cost. The proposed methods for the helicopter, performing the specified set of transport operations, appearance forming can be employed hereafter while other prospective rotary-winged aircraft of vertical takeoff and landing design.

Keywords:

single-rotor helicopter, appearance formation, two-stage transport operation, mathematical model of weight and aerodynamic computation, helicopter layout, composition, design features

References

1. Negenblya I.E. Nad bezgranichnoi Arktikoi (Over the Boundless Arctic), Yakutsk, Yakutskii krai, 1997, 312 p.

2. Nemudryi K.V. Trudy MAI, 2012, no. 57. URL: http://trudymai.ru/eng/published.php?ID=30712

3. Starodubtsev V. Kommersant. Review «Arkticheskii forum». Prilozhenie № 53, 29.03.2017, p. 14. URL: https://im.kommersant.ru/issues.pdf/tema/2017/05312903/kom_053_002.pdf

4. Armeiskii snegokhod AS-1. URL: http://zonwar.ru/news3/news_458_snegohod_A-1.html

5. Ryabov K. Dvukhzvennyi snegobolotokhod GAZ-3344, 19.11.2014. URL: https://topwar.ru/62827-dvuhzvennyy-snegobolotohod-gaz-3344.html

6. Rossiiskii BTR-82A: istoriya sozdaniya, opisanie i tekhnicheskie kharakteri-stiki, 2019. URL: https://militaryarms.ru/voennaya-texnika/boevye-mashiny/btr-82a/

7. SAU 2S1 Gvozdika 122-mm Dal’nost’ strel’by. Razmery. Ustroistvo. Ves. URL: http://oruzhie.info/artilleriya/132-2s1-gvozdika

8. Snegobolotokhod «TREKOL 39294». URL: https://www.trecol.ru/catalog/cars/trekol-39294.html

9. Arkticheskii transportno-shturmovoi vertolet Mi-8AMTSh-VA, 2016. URL: https://topwar.ru/105882-snegohod-s-zakrytoy-kabinoy-ttm-1901-berkut-2.html

10. Zakiev R. Pervyi «arkticheskii» vertolet peredan Minoborony RF, 2015. URL: https://rg.ru/2015/11/25/vertolet-site.html

11. Arkticheskii transportno-shturmovoi vertolet Mi-8AMTSh-VA, 2017. URL: http://bastion-karpenko.ru/mi-8amtsh-va

12. Razrabotka novogo dvigatelya PD-12V dlya vertoleta Mi-26 (Development of a new PD-12 engine for the Mi-26 helicopter), 2018. URL: https://bmpd.livejournal. com/3248518.html

13. Artamonov B.L., Zhuravlev V.N., Shaidakov V.I. Polet. Obshcherossiiskii nauchno-tekhnicheskii zhurnal, 2018, no. 1, pp. 29-43.

14. Tischehko M.N., Artamonov B.L., Zavalov O.A., Mojzyh E.I., Maslov A.D. Development of application methodology for computer-aided techniques to design rotary wing aircraft and their systems. Aerospace MAI Journal, 2005, vol. 12, no. 2, pp. 49-61.

15. Tishchenko M.N. Vybor parametrov vertoleta na nachal’noi stadii proektirovaniya (Choice of helicopter parameters at the initial stage of design), Moscow, MAI-Print, 2011, 121 p.

16. Tishchenko M.N., Nekrasov A.V., Radin A.S. Vertolety. Vybor parametrov pri proektirovanii (Helicopters. Parameters selection at design), Moscow, Mashinostroenie, 1976, 366 p.

17. Bogdanov Yu.S., Zhuravlev V.N. Materialy II nauchnykh chtenii, posvyashchennykh pamyati akademika B.N. Yur’eva «Proektirovanie i konstruktsiya vertoletov» (23-24 March 1987; Moskva), Moscow, IIET, 1988, 138 p.

18. Morskoi spasatel’nyi komplekt MSK-5. URL: https://dynaforce.ru/proizvodstvo-ru/catalog-tovarov/zashchitnoe-snaryazhenie-dlya-letnogo-sostava/m...

19. Gidrotermokostyum spasatel’nyi model’ GTKS 2004. URL: http://npfszma.ru/gtks-2004.html

20. Certification Specifications and Acceptable Means of Compliance for Large Rotorcraft CS-29. Amendment 7, 2019