Analysis and design of hybrid electric regional turboprop aircraft

Voskuijl, Mark; Bogaert, Joris van; Rao, Arvind Gangoli

doi:10.1007/s13272-017-0272-1

Cited by 117 publications

(53 citation statements)

References 27 publications

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“…Generally, by developing the technology for electric / hybrid aircraft the design space increases dramatically [46] that requires radically new solutions like synergetic, tightly-coupled morphological and systems integration emphasizing propulsion -as exemplified by the potential afforded by distributed propulsion solutions [46 -48]. Investigation of the potential and limitations [49] introduced by electric flight concept [19,23,24,28,33,50] leads to rethinking the conventional conceptual design methodologies of aircraft. The developers may define new constraints partly subjectively.…”

Section: New Conceptual Design Methodology For Developing the Electrimentioning

confidence: 99%

Effect of Energy Balance Evaluation on Conceptual Design of Electric and Hybrid Aircraft

Rohács¹,

Rohács²

2018

Preprint

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Nowadays, all the stakeholders, policy makers, regulators, aircraft designers, producers, operators, etc.) are intensively working on development of the aircraft with full electric and hybrid propulsion systems. However, the technical, technological constrains (like limit on accumulator energy density) require introducing a new approach to conceptual design of such aircraft. The new methods is based on energy and mass balance evaluation. This paper analyses the identified constrains; integrates the energy and mass balance equations into the preliminary definition and calculations of the aircraft performance. By this way, the technological constrains might be transferred into the limitation on the aircraft energy and mass breakdown, that initiates a new approach to aircraft conceptual design uses the knowledge based multidisciplinary optimization. The paper describes the developed methodology for conceptual design of aircraft. It show results of implementing this new development philosophy to conceptual design of a four-seat small electric/hybrid aircraft and a special hybrid cargo UAV. The discussion of the results including got by using the emerging and enabling new technologies and new methods and solutions (including for example distributed propulsion system, unconventional forms, morphing, biomimics, etc.), demonstrates the possible implementation of the new development philosophy, new approach to aircraft conceptual design.

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Section: New Conceptual Design Methodology For Developing the Electrimentioning

confidence: 99%

Effect of Energy Balance Evaluation on Conceptual Design of Electric and Hybrid Aircraft

Rohács¹,

Rohács²

2018

Preprint

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“…An aircraft conceptual design by TU-Delft made for the regional segment, for 70 PAX with parallel hybrid electric configuration with a design range of 1528 km, based on Li-air batteries with a specific energy of 1000 Wh/kg, providing 34% of the shaft power throughout the mission, yields a reduction in emissions of 28% [116]. A 70-passenger aircraft design for the regional market, with a mission range of 1530 km, was assessed with different variants in propulsion system configuration: parallel, serial, and parallel/serial for the fuel/energy consumption assessment.…”

Section: System Studies Portfoliomentioning

confidence: 99%

A Review of Concepts, Benefits, and Challenges for Future Electrical Propulsion-Based Aircraft

2020

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Electrification of the propulsion system has opened the door to a new paradigm of propulsion system configurations and novel aircraft designs, which was never envisioned before. Despite lofty promises, the concept must overcome the design and sizing challenges to make it realizable. A suitable modeling framework is desired in order to explore the design space at the conceptual level. A greater investment in enabling technologies, and infrastructural developments, is expected to facilitate its successful application in the market. In this review paper, several scholarly articles were surveyed to get an insight into the current landscape of research endeavors and the formulated derivations related to electric aircraft developments. The barriers and the needed future technological development paths are discussed. The paper also includes detailed assessments of the implications and other needs pertaining to future technology, regulation, certification, and infrastructure developments, in order to make the next generation electric aircraft operation commercially worthy.

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“…Recently, Voskuijl et al in [40] analysed a parallel-hybrid configuration introducing two different approaches: constant power split ( = ) and constant operating mode of gas…”

Section: Journal Of Advanced Transportationmentioning

confidence: 99%

“…In [40], the authors stated, when using a constant power split for all the mission phases, the supplied power ratio has approximately the same value as for the power split.…”

Section: Journal Of Advanced Transportationmentioning

confidence: 99%

“…For this reason, the definitions of hybridisation parameters employed to investigate feasibility and benefit of dual-energy sources for aircraft are the ones referring to the electric and conventional installed powers reported in (7) and (8). Considering a constant power split for each mission segment, as suggested in [40], the DoH for power and for energy are linked to each other by means of the chain efficiencies so that they can be written as follows…”

Section: Journal Of Advanced Transportationmentioning

confidence: 99%

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Approach to the Weight Estimation in the Conceptual Design of Hybrid-Electric-Powered Unconventional Regional Aircraft

Centracchio

Rossetti

Iemma

2018

Journal of Advanced Transportation

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The present work deals with the development of an innovative approach to the weight estimation in the conceptual design of a Hybrid-Electric-Powered (HEP) Blended Wing Body (BWB) commercial aircraft. In the last few decades, the improvement of the environmental impact of civil aviation has been the major concern of the aeronautical engineering community, in order to guarantee the sustainable development of the system in presence of a constantly growing market demand. The sustained effort in the improvement of the overall efficiency of conventional aircraft has produced a new generation of vehicles with an extremely low level of emissions and noise, capable of covering the community requirements in the short term. Unfortunately, the remarkable improvements achieved represent the asymptotic limit reachable through the incremental enhancement of existing concepts. Any further improvement to conform to the strict future environmental target will be possible only through the introduction of breakthrough concepts. The aeronautical engineering community is thus concentrating the research on unconventional airframes, innovative low-noise technologies, and alternative propulsion systems. The BWB is one of the most promising layouts in terms of noise emissions and chemical pollution. The further reduction of fuel consumption that can be achieved with gas/electric hybridisation of the power-plant is herein addressed in the context of multidisciplinary analyses. In particular, the payload and range limits are assessed in relation to the technological development of the electric components of the propulsion system. The present work explores the potentialities of an energy-based approach for the initial sizing of a HEP unconventional aircraft in the early conceptual phase of the design. A detailed parametric analysis has been carried out to emphasise how payload, range, and degree of hybridisation are strictly connected in terms of feasible mission requirements and related to the reasonable expectations of development of electric components suitable for aeronautical applications.

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Analysis and design of hybrid electric regional turboprop aircraft

Cited by 117 publications

References 27 publications

Effect of Energy Balance Evaluation on Conceptual Design of Electric and Hybrid Aircraft

Effect of Energy Balance Evaluation on Conceptual Design of Electric and Hybrid Aircraft

A Review of Concepts, Benefits, and Challenges for Future Electrical Propulsion-Based Aircraft

Approach to the Weight Estimation in the Conceptual Design of Hybrid-Electric-Powered Unconventional Regional Aircraft

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