Regenerative braking for aircraft landing roll phase using an electric machine

Grigore-Müler, Octavian; Barbelian, Mihai

doi:10.1109/optim.2012.6231843

Cited by 12 publications

(5 citation statements)

References 13 publications

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“…The model of the electrical power generation and distribution system of the B737-300 aircraft is performed in Simulink / Matlab v.9.0. The input data, the parameters of the aircraft engine, were presented in detail in [5], where the Simulink model of the CSD was also explained.…”

Section: Simulation and Resultsmentioning

confidence: 99%

“…This paper presents for the first time in a specialized paper a simulation with the Simulink/Matlab of an aircraft EPS that uses a CSD to drive the BSG, just as it happens otherwise in reality. Using the scenario from [5], it can be seen that frequency and terminal voltages are well regulated, both to the variation of the load and the rotational speed. Some of the challenges were to tune both frequency and voltage regulators to obtain the qualitative parameters of energy as regulated by standards.…”

Section: Discussionmentioning

confidence: 99%

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Modeling and Simulation of an Aircraft Electrical Power System

GRIGORE-MULER

2023

RRST-EE

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Although recent developments in aircraft electrical technology have had a significant impact on aircraft electrical power systems (EPS), thus reminding the development and production of more electric aircraft (MEA), but also important steps in the development of all-electric aircraft (AEA), still the EPS of the latest aircraft produced by the two big players in the market, the Neo series from Airbus and the NG or Max from Boeing respectively, is completely traditional – a constant speed constant frequency (CSCF) system. Thus, for an alternating current one, it is composed of the power source – the integrated drive generator (IDG), the command and control system – the generator control unit (GCU), the transmission and distribution system, the protection system – the CBs (circuit breaker) and electrical loads. This paper presents the design and simulation of an aircraft EPS using Simulink’s Simscape package, a MATLAB program, and for the first time in the specialized literature, a model of the constant speed drive (CSD) generated with the same program is used to drive the synchronous generator (SG) in the IDG.

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Section: Simulation and Resultsmentioning

confidence: 99%

Section: Discussionmentioning

confidence: 99%

Modeling and Simulation of an Aircraft Electrical Power System

GRIGORE-MULER

2023

RRST-EE

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“…A similar concept has been adopted in electric propelled gliders [24]. Electric machines that can perform as a motor and generator can be integrated to the propellers or to be built into the hub of the main gear wheel for regenerative braking by using landing gear-based motors [25]. Permanent magnet machines and switched reluctance machines can operate as either a motor or generator.…”

Section: Energy Harvesting For Aircraft Propulsionmentioning

confidence: 99%

“…Figure 4. Structure of the piezo-windmill[25], where piezo-cantilevers are excited by the interactive repulsive force between the two magnets, which are located on the rotating part and attached to the piezoelectric device.…”

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confidence: 99%

Energy Harvesting: An Overview of Techniques for Use Within the Transport Industry

White

Zaghari

2022

IEEE Electr. Insul. Mag.

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This paper gives an overview of energy harvesting techniques for generating electrical power from ambient energy such as vibration, heat and light. Typically, the electrical power is used to energise sensing systems and their associated communication channels, which are often wireless in nature. The amount of electrical power generated is in the region of tens of micro watts to hundreds of milli watts. The use of assets in service generally results in some form of ageing as a consequence of elevated temperature, chemical degradation, absorption of energetic radiation, mechanical wear, etc. and, as a consequence, as time progresses, the probability of failure increases. In some situations, it may be acceptable on grounds of cost and consequent impact to accept periodic failure and asset replacement while, in many others, such a strategy is unacceptable such that regular maintenance, condition assessment, life prediction and pre-emptive replacement must be carried out. A clear example of this is in connection with mass transport, notably aviation, where the impact of catastrophic failure can be dire. Condition assessment may be achieved through periodic examination or by continuous monitoring but, in many circumstances, the latter approach has much to recommend it. This commonly involves the measurement of relevant parameters and the subsequent export of data for decision making. Such systems require sensors, data logging, communications hardware, etc. plus a source of energy. A broad overview of energy scavenging techniques is presented, along with an assessment of useful materials for each mode of harvesting.

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“…Multiphase machines represent a potential solution for increasing the power density, reducing torque ripple and improving the reliability [42]. The use of superconducting motors should be considered as an alternative for the ET motors because they have a relatively high torque density.…”

Section: B Recommendations For Further Researchmentioning

confidence: 99%

State of the Art of Electric Taxiing Systems

Lukic

Hebala

Giangrande

et al. 2018

2018 IEEE International Conference on Electrical Systems for Aircraft, Railway, Ship Propulsion and Road Vehicles &Amp; Interna

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The aviation industry represents an ever-expanding economy and the aircraft market forecast reveals an optimistic growth for the coming decades. New requirements and guidelines call for a more efficient, reliable, and environment friendly aircraft operations during both airborne and ground phases. Considering on-ground operations, the electric taxiing is one of the suggested solutions for reducing the emissions and the acoustic noise in the airport, and for lowering the fuel consumption and the flight costs. This paper provides an overview of the most important existing electric taxiing systems and also presents the basic concepts related to it. Finally, detailed comparison of the different systems is given with recommendations for the future research.

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Regenerative braking for aircraft landing roll phase using an electric machine

Cited by 12 publications

References 13 publications

Modeling and Simulation of an Aircraft Electrical Power System

Modeling and Simulation of an Aircraft Electrical Power System

Energy Harvesting: An Overview of Techniques for Use Within the Transport Industry

State of the Art of Electric Taxiing Systems

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