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Regional Passenger Aircraft Type of An-158 with a Hybrid Propulsion Parametric Concept

Vasyl Loginov

Vasyl Loginov

Department of Programs and Projects FED JSCKharkiv, Ukraine
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Loginov, Vasyl
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Yevgen Ukrainets

Yevgen Ukrainets

Department of the Design and Strength of Aircraft and Engines, Kharkov National Air Force University named after Ivan KozhedubKharkiv, Ukraine
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Ukrainets, Yevgen
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Igor Kravchenko

Igor Kravchenko

SE “Ivchenko-Progress”Zaporozhye, Ukraine
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Kravchenko, Igor
, 
Olexandr Yelans’ky

Olexandr Yelans’ky

SE “Ivchenko-Progress”Zaporozhye, Ukraine
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Yelans’ky, Olexandr
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Serhii Fil

Serhii Fil

SE “Antonov”Kyiv, Ukraine
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Fil, Serhii
 und 
Oleksii Pushylin

Oleksii Pushylin

SE “Ivchenko-Progress”Zaporozhye, Ukraine
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Pushylin, Oleksii
  
30. Dez. 2024
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Artikel-Kategorie: Research Article
Online veröffentlicht: 30. Dez. 2024
Seitenbereich: 14 - 26
Eingereicht: 22. Dez. 2021
Akzeptiert: 26. Juni 2024
DOI: https://doi.org/10.2478/tar-2024-0020
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© 2024 Vasyl Loginov et al., published by Sciendo
This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International License.

Fig. 1.

The base An-158 aircraft.
The base An-158 aircraft.

Fig. 2.

The An-158-TPE modification of the An-158 type aircraft with turboprop engines.
The An-158-TPE modification of the An-158 type aircraft with turboprop engines.

Fig. 3.

The An-158-HP modification of the An-158 type aircraft with hybrid propulsion.
The An-158-HP modification of the An-158 type aircraft with hybrid propulsion.

Fig. 4.

Modification of the An-158 type aircraft.
Modification of the An-158 type aircraft.

Fig. 5.

Modifications of the An-158 type aircraft: (a) with turboprop engine, (b) with hybrid propulsion.
Modifications of the An-158 type aircraft: (a) with turboprop engine, (b) with hybrid propulsion.

Results of coercive force measurements_

Operational empty weight, kg Gross weight, kg Aircraft name Payload weight, kg Aircraft flight propulsion weight, kg
10000 5476 24583 43733 An-158-TPE
10000 9645 29169 48319 An-158-HP

Main characteristics of aircraft modifications_

Parameter Aircraft modification
An-158 An-158-TPE An-158-HP
q, kg/km (specific fuel consumption per km) 2.394 2.406 2.552
Q, gram/pass (fuel consumption per passenger) 26.6 24.058 25.53
K× M (efficiency coefficient) 8.66 8.965 9.221
Peng1, hp (average power of one engine required for level flight) - 4057 4306
Tprop1, kg (average thrust of one propeller required for level flight) - 1575 1671
Wfuel, kg (total fuel consumption for the entire flight) 7100 7618 7532
Wfuel, kg (total fuel consumption for level flight) 4811 4797 5017
LTO, m (takeoff distance) 1410 1372 1535
Sprache:
Englisch
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Technik, Einführungen und Gesamtdarstellungen, Technik, andere, Geowissenschaften, Geowissenschaften, andere, Materialwissenschaft, Materialwissenschaft, andere, Physik, Physik, andere
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