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Record W4389540739 · doi:10.17118/11143/21179

Overview of the challenges of alternative propulsion systems applied tobusiness aircraft

2023· article· en· W4389540739 on OpenAlexaff
Nathan Louvel, Mathieu Bouchard, David Rancourt

Bibliographic record

Venuenot available
Typearticle
Languageen
FieldEngineering
TopicRocket and propulsion systems research
Canadian institutionsUniversité de Sherbrooke
Fundersnot available
KeywordsPropulsionAeronauticsAerospace engineeringComputer scienceEngineeringSystems engineering

Abstract

fetched live from OpenAlex

In order to reduce greenhouse gas emissions and reach the 2050 net-zero emissions target, the aviation sector is looking towards new propulsion architectures, such as electric, hybrid-electric, and hydrogen powertrains. The integration of these kinds of new powertrain technologies has a significant impact on aircraft performance. The loss of performance typically consists of a range reduction, a reduced payload capacity, a lower cruise speed than the baseline aircraft, etc. Cost in capabilities does not have the same impact depending on business or commercial aviation, as these are two radically different markets. The travel routes for a given airline are constant and well-known, and a loss of aircraft performance capability may therefore be acceptable; this is not the case for business aviation due to hard operational constraints. The operational constraints of business aircraft are reflected in a higher cruise speed than commercial aviation, a flight altitude above commercial traffic, a long-range capability, high volume and comfort of the cabin, the capability to takeoff and land at small regional airports, and so on. Since the operational flexibility of the aircraft is at the heart of the business aviation market and dependent on these performance indicators, these requirements are necessary to maintain the high level of competitiveness of the aircraft. The literature mainly focuses on the greenhouse gas emissions reduction of retrofitted aircraft without considerations for keeping the same level of performance as the baseline aircraft. As business aviation is expected to experience growth in deliveries over the next few years, the assessment of the impact of alternative propulsion systems on the performance of aircraft is crucial. Since all new propulsion technologies for the mitigation of aviation carbon footprint have drawbacks, the integration of these systems should result in an acceptable trade-off between the operational capabilities of the aircraft and CO2 emissions reduction. This paper presents the cost in performance and the key challenges of alternative propulsion system integration of business aircraft. The analysis focuses on three main architectures, the all-electric powertrain, hydrogen-powered aircraft, and parallel hybrid powertrain. The objective is to provide an overview of business aircraft requirements, the impact of alternative propulsion systems on such aircraft, and the key challenges to meet the operational constraints of the business aviation market.

Fetched live from OpenAlex and de-inverted. Abstracts are not stored in this database: the inverted indexes are 8.6 GB of the frame’s 9.3 GB of text, and the host has 13 GB free.

How this classification was reachedexpand

Full frame machine prediction

Teacher imitation

Not calibrated prevalence, not ground truth. Human validation pending. The Gemma side is a direct model label for every work in the frame, read from the title-only record. The Codex side is a classifier learned from the 10,348 direct Codex labels and calibrated to design-weighted sample rates; fields without enough sample support carry no Codex call. Candidate is the union of the two sides; consensus is their intersection. These outputs are machine_predicted_unvalidated and are not human labels.

metaresearch head score (Codex)0.001
metaresearch head score (Gemma)0.001
Version: metacan-v3-hybrid-931329e0061cValidation status: machine_predicted_unvalidated
Candidate categoriesnone
Consensus categoriesnone
DomainCandidate signal: none · Consensus signal: none
Study designCandidate signal: Not applicable · Consensus signal: none
GenreCandidate signal: Review · Consensus signal: Review
Teacher disagreement score0.013
Threshold uncertainty score0.042

Distilled classifier scores by category (both heads)

CategoryCodexGemma
Metaresearch0.0010.001
Meta-epidemiology (narrow)0.0010.000
Meta-epidemiology (broad)0.0000.001
Bibliometrics0.0020.002
Science and technology studies0.0010.001
Scholarly communication0.0040.004
Open science0.0010.001
Research integrity0.0020.002
Insufficient payload (model declined to judge)0.0130.004

Machine scores (provisional)

The two teacher heads of the student model, read on this work. A score orders the frame for review; it never asserts a category, and the validation status ships verbatim with every row.

Baseline scores from an immature model (maturity gate not passed, 7 training rounds). Scores rank; they never assert a category.

Opus teacher head0.093
GPT teacher head0.303
Teacher spread0.210 · how far apart the two teachers sit on this one work
Validation statusscore_only:v0-immature-baseline · verbatim from the scoring run: score_only means the number may rank works, and no category label ships from it

Classification

machine, unvalidated

Machine predicted; a candidate call from one source (direct Gemma or distilled Codex), not a consensus.

The models applied no category: nothing in the taxonomy fit this work.
Study designNot applicable
Domainnot available
GenreReview

How this classification was reached, model by model and score by score, is at the end of the page under "How this classification was reached".

Quick stats

Citations0
Published2023
Admission routes1
Has abstractyes

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