Electro-Mechanical Actuators for Safety-Critical Aerospace Applications / / edited by Gianpietro Di Rito.

Aircraft electrification is one of the most important and strategic initiatives currently supporting the innovation of the aviation industry. This manifests in the well-known more-electric aircraft concept (with the ultimate aim of achieving the all-electric long-term target), which aims to graduall...

Full description

Saved in:
Bibliographic Details
TeilnehmendeR:
Place / Publishing House:Basel, Switzerland : : MDPI - Multidisciplinary Digital Publishing Institute,, [2023]
©2023
Year of Publication:2023
Language:English
Physical Description:1 online resource (286 pages)
Tags: Add Tag
No Tags, Be the first to tag this record!
id 993610557704498
ctrlnum (CKB)5470000002907770
(NjHacI)995470000002907770
(EXLCZ)995470000002907770
collection bib_alma
record_format marc
spelling Electro-Mechanical Actuators for Safety-Critical Aerospace Applications / edited by Gianpietro Di Rito.
Basel, Switzerland : MDPI - Multidisciplinary Digital Publishing Institute, [2023]
©2023
1 online resource (286 pages)
text txt rdacontent
computer c rdamedia
online resource cr rdacarrier
Description based on publisher supplied metadata and other sources.
Aircraft electrification is one of the most important and strategic initiatives currently supporting the innovation of the aviation industry. This manifests in the well-known more-electric aircraft concept (with the ultimate aim of achieving the all-electric long-term target), which aims to gradually replace onboard systems based on mechanical, hydraulic, or pneumatic power sources with electrically powered ones to reduce the weight and costs, optimize energy, and increase the eco-compatibility and reliability of future aircrafts. A key technological enabler for pursuing these challenging objectives is electro-mechanical actuation. The applicability of electro-mechanical actuators (EMAs) in aerospace has been proved in terms of dynamic performances, but it still entails several concerns in terms of reliability/safety and operation in a harsh environment. In civil aircrafts, EMAs are often avoided for safety-critical functions (flight controls, brakes, landing gears, and nose wheel steering), essentially because the statistical database on the components' fault modes is poor. This Special Issue is thus focused on advancements and innovations in the design, modelling/simulation, architectural definition, reliability/safety analysis, control, condition-monitoring, and experimental testing of EMAs developed for safety-critical aerospace applications. The research papers included in this Special Issue will undoubtedly contribute to progress towards the objective of more electric flights.
Aerospace engineering.
Airplanes Electric equipment.
3-0365-7932-X
Di Rito, Gianpietro, editor.
language English
format eBook
author2 Di Rito, Gianpietro,
author_facet Di Rito, Gianpietro,
author2_variant r g d rg rgd
author2_role TeilnehmendeR
title Electro-Mechanical Actuators for Safety-Critical Aerospace Applications /
spellingShingle Electro-Mechanical Actuators for Safety-Critical Aerospace Applications /
title_full Electro-Mechanical Actuators for Safety-Critical Aerospace Applications / edited by Gianpietro Di Rito.
title_fullStr Electro-Mechanical Actuators for Safety-Critical Aerospace Applications / edited by Gianpietro Di Rito.
title_full_unstemmed Electro-Mechanical Actuators for Safety-Critical Aerospace Applications / edited by Gianpietro Di Rito.
title_auth Electro-Mechanical Actuators for Safety-Critical Aerospace Applications /
title_new Electro-Mechanical Actuators for Safety-Critical Aerospace Applications /
title_sort electro-mechanical actuators for safety-critical aerospace applications /
publisher MDPI - Multidisciplinary Digital Publishing Institute,
publishDate 2023
physical 1 online resource (286 pages)
isbn 3-0365-7932-X
callnumber-first T - Technology
callnumber-subject TL - Motor Vehicles and Aeronautics
callnumber-label TL545
callnumber-sort TL 3545 E443 42023
illustrated Not Illustrated
dewey-hundreds 600 - Technology
dewey-tens 620 - Engineering
dewey-ones 629 - Other branches of engineering
dewey-full 629.1
dewey-sort 3629.1
dewey-raw 629.1
dewey-search 629.1
work_keys_str_mv AT diritogianpietro electromechanicalactuatorsforsafetycriticalaerospaceapplications
status_str n
ids_txt_mv (CKB)5470000002907770
(NjHacI)995470000002907770
(EXLCZ)995470000002907770
carrierType_str_mv cr
is_hierarchy_title Electro-Mechanical Actuators for Safety-Critical Aerospace Applications /
author2_original_writing_str_mv noLinkedField
_version_ 1796653283921625091
fullrecord <?xml version="1.0" encoding="UTF-8"?><collection xmlns="http://www.loc.gov/MARC21/slim"><record><leader>02592nam a2200313 i 4500</leader><controlfield tag="001">993610557704498</controlfield><controlfield tag="005">20230816101115.0</controlfield><controlfield tag="006">m o d </controlfield><controlfield tag="007">cr |||||||||||</controlfield><controlfield tag="008">230816s2023 sz o 000 0 eng d</controlfield><datafield tag="024" ind1="7" ind2=" "><subfield code="a">10.3390/books978-3-0365-7932-0</subfield><subfield code="2">doi</subfield></datafield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(CKB)5470000002907770</subfield></datafield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(NjHacI)995470000002907770</subfield></datafield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(EXLCZ)995470000002907770</subfield></datafield><datafield tag="040" ind1=" " ind2=" "><subfield code="a">NjHacI</subfield><subfield code="b">eng</subfield><subfield code="e">rda</subfield><subfield code="c">NjHacl</subfield></datafield><datafield tag="050" ind1=" " ind2="4"><subfield code="a">TL545</subfield><subfield code="b">.E443 2023</subfield></datafield><datafield tag="082" ind1="0" ind2="4"><subfield code="a">629.1</subfield><subfield code="2">23</subfield></datafield><datafield tag="245" ind1="0" ind2="0"><subfield code="a">Electro-Mechanical Actuators for Safety-Critical Aerospace Applications /</subfield><subfield code="c">edited by Gianpietro Di Rito.</subfield></datafield><datafield tag="264" ind1=" " ind2="1"><subfield code="a">Basel, Switzerland :</subfield><subfield code="b">MDPI - Multidisciplinary Digital Publishing Institute,</subfield><subfield code="c">[2023]</subfield></datafield><datafield tag="264" ind1=" " ind2="4"><subfield code="c">©2023</subfield></datafield><datafield tag="300" ind1=" " ind2=" "><subfield code="a">1 online resource (286 pages)</subfield></datafield><datafield tag="336" ind1=" " ind2=" "><subfield code="a">text</subfield><subfield code="b">txt</subfield><subfield code="2">rdacontent</subfield></datafield><datafield tag="337" ind1=" " ind2=" "><subfield code="a">computer</subfield><subfield code="b">c</subfield><subfield code="2">rdamedia</subfield></datafield><datafield tag="338" ind1=" " ind2=" "><subfield code="a">online resource</subfield><subfield code="b">cr</subfield><subfield code="2">rdacarrier</subfield></datafield><datafield tag="588" ind1=" " ind2=" "><subfield code="a">Description based on publisher supplied metadata and other sources.</subfield></datafield><datafield tag="520" ind1=" " ind2=" "><subfield code="a">Aircraft electrification is one of the most important and strategic initiatives currently supporting the innovation of the aviation industry. This manifests in the well-known more-electric aircraft concept (with the ultimate aim of achieving the all-electric long-term target), which aims to gradually replace onboard systems based on mechanical, hydraulic, or pneumatic power sources with electrically powered ones to reduce the weight and costs, optimize energy, and increase the eco-compatibility and reliability of future aircrafts. A key technological enabler for pursuing these challenging objectives is electro-mechanical actuation. The applicability of electro-mechanical actuators (EMAs) in aerospace has been proved in terms of dynamic performances, but it still entails several concerns in terms of reliability/safety and operation in a harsh environment. In civil aircrafts, EMAs are often avoided for safety-critical functions (flight controls, brakes, landing gears, and nose wheel steering), essentially because the statistical database on the components' fault modes is poor. This Special Issue is thus focused on advancements and innovations in the design, modelling/simulation, architectural definition, reliability/safety analysis, control, condition-monitoring, and experimental testing of EMAs developed for safety-critical aerospace applications. The research papers included in this Special Issue will undoubtedly contribute to progress towards the objective of more electric flights.</subfield></datafield><datafield tag="650" ind1=" " ind2="0"><subfield code="a">Aerospace engineering.</subfield></datafield><datafield tag="650" ind1=" " ind2="0"><subfield code="a">Airplanes</subfield><subfield code="x">Electric equipment.</subfield></datafield><datafield tag="776" ind1=" " ind2=" "><subfield code="z">3-0365-7932-X</subfield></datafield><datafield tag="700" ind1="1" ind2=" "><subfield code="a">Di Rito, Gianpietro,</subfield><subfield code="e">editor.</subfield></datafield><datafield tag="906" ind1=" " ind2=" "><subfield code="a">BOOK</subfield></datafield><datafield tag="ADM" ind1=" " ind2=" "><subfield code="b">2023-08-18 03:31:59 Europe/Vienna</subfield><subfield code="f">system</subfield><subfield code="c">marc21</subfield><subfield code="a">2023-07-04 13:45:39 Europe/Vienna</subfield><subfield code="g">false</subfield></datafield><datafield tag="AVE" ind1=" " ind2=" "><subfield code="i">DOAB Directory of Open Access Books</subfield><subfield code="P">DOAB Directory of Open Access Books</subfield><subfield code="x">https://eu02.alma.exlibrisgroup.com/view/uresolver/43ACC_OEAW/openurl?u.ignore_date_coverage=true&amp;portfolio_pid=5346846280004498&amp;Force_direct=true</subfield><subfield code="Z">5346846280004498</subfield><subfield code="b">Available</subfield><subfield code="8">5346846280004498</subfield></datafield></record></collection>