Performance requirements and simulation of rotor operation for high-mountain rescue helicopter

• Autorzy: Stanisławski J.

Identyfikatory

DOI

10.5604/01.3001.0012.2853

• Języki publikacji: EN

Abstrakty

EN

Simulation results concerning performance of helicopter suitable for high-mountain rescue operations are presented. Including operations in regions of the highest Himalaya Mountains, the possibility of hover ceiling out of ground effect (OGE) at 10,000 m above sea level is assumed. Demand of high ratio of developed lift to power required for hover leads to choice the coaxial rotor configuration as the best for rescue helicopter, which can operate in extremely high mountain environment, and gives good stability features in wind gust conditions in comparison with single main rotor helicopter. For performance calculations the simple model of helicopter is applied, which consists of fuselage point mass and rotor disk. The cases of partial and total power loss are considered to define range of H-V zones and possibilities of flight continuation due to height of landing surface over level of sea. The rotor blades and rotor loads are calculated applying detail model of elastic blade, which includes effects of its deflections due to out-of-plane bending, in plane bending, and torsion. The Runge-Kutta method is applied to solve equations of motion of rotor blades with taken into account effects of blade pitch control and variable deflections of blades. According to Galerkin method, the blade parameters of motion are treated as a combination of torsion and bending eigen modes of the rotor blades. Elastic blade model allows defining behaviour rotor blades in selected states of flight: hover, level flight, wind gust conditions, and pull-up manoeuvre. The results of simulation for upper and lower rotor for blade deflections and loads are shown in form of time-run plots and rotor disk distributions. The simulation investigation may be applied to define features of helicopter configuration suitable for operation in extremely high mountain conditions..

Słowa kluczowe

EN

rescue helicopter; high-mountain operations; rotor blade deformation

• Wydawca: Łukasiewicz Research Network - Institute of Aviation ; European Science Society of Powertrain and Transport KONES Poland ; Wydawnictwo Instytutu Technicznego Wojsk Lotniczych
• Czasopismo: Journal of KONES
• Rocznik: 2018
• Tom: Vol. 25, No. 2
• Strony: 341--348
• Opis fizyczny: Bibliogr. 12 poz., rys.

Twórcy

autor

Stanisławski J.

• Institute of Aviation Krakowska Av. 110/114, 02-256 Warszawa, Poland tel.: [phone] ext. 362, fax: [phone]

Bibliografia

• [1] Head, E., Flight at the Extreme, Vertical, pp. 86-107, 2018.
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• [9] Stalewski, W., Aerodynamic Design and Optimisation of Rotorcraft, Wydawnictwa Naukowe Instytutu Lotnictwa, 2017.
• [10] Stanisławski, J., A comparison of helicopter main rotor features due to stiffness of rotor blade-hub connection, Transactions of the Institute of Aviation, No. 1, 250, Warszawa 2018.
• [11] Stanisławski, J., Prediction of helicopter H-V zone and cueing the emergency manoeuvre after power loss, The Archive of Mechanical Engineering, Vol. LVII, No. 1, Warszawa 2010.
• [12] Witkowski, R., Pierwsze śmigłowcowe akcje ratownicze, Prace Instytutu Lotnictwa, Nr 231, pp. 3-10, Warszawa 2013.

Uwagi

Opracowanie rekordu w ramach umowy 509/P-DUN/2018 ze środków MNiSW przeznaczonych na działalność upowszechniającą naukę (2018).