About: Critical engine     Goto   Sponge   NotDistinct   Permalink

An Entity of Type : yago:WikicatAircraftEngines, within Data Space : dbpedia.demo.openlinksw.com associated with source document(s)
QRcode icon
http://dbpedia.demo.openlinksw.com/describe/?url=http%3A%2F%2Fdbpedia.org%2Fresource%2FCritical_engine&invfp=IFP_OFF&sas=SAME_AS_OFF

The critical engine of a multi-engine fixed-wing aircraft is the engine that, in the event of failure, would most adversely affect the performance or handling abilities of an aircraft. On propeller aircraft, there is a difference in the remaining yawing moments after failure of the left or the right (outboard) engine when all propellers rotate in the same direction due to the P-factor. On turbojet and turbofan twin-engine aircraft, there usually is no difference between the yawing moments after failure of a left or right engine in no-wind condition.

AttributesValues
rdf:type
rdfs:label
  • Kritisches Triebwerk (de)
  • Critical engine (en)
  • Moteur critique (fr)
  • Motor crítico (pt)
rdfs:comment
  • Bei mehrmotorigen Flugzeugen ist das kritische Triebwerk (critical engine) jenes, „dessen Ausfall den nachteiligsten Einfluß auf die Flugeigenschaften im jeweils untersuchten Flugzustand hat“. (de)
  • The critical engine of a multi-engine fixed-wing aircraft is the engine that, in the event of failure, would most adversely affect the performance or handling abilities of an aircraft. On propeller aircraft, there is a difference in the remaining yawing moments after failure of the left or the right (outboard) engine when all propellers rotate in the same direction due to the P-factor. On turbojet and turbofan twin-engine aircraft, there usually is no difference between the yawing moments after failure of a left or right engine in no-wind condition. (en)
  • Le moteur critique d'un avion multimoteur, est celui dont la panne provoquerait les effets les plus pénalisants pour le pilotage de l'avion et ses performances. (fr)
  • O motor crítico de uma aeronave multimotora de asa fixa, é o motor cuja falha resulta nos efeitos mais adversos na manobrabilidade e performance da aeronave.(§1.1). Em aeronaves a hélice, existe uma diferença no momento em relação ao eixo longitudinal após uma falha do motor esquerdo ou direito (o que gira para fora da aeronave) quando as hélices giram na mesma direção devido ao P-factor. Em aeronaves turbojato ou turbofan, geralmente não existe nenhuma diferença entre o momento de guinada após a falha de um motor esquerdo ou direito. (pt)
foaf:depiction
  • http://commons.wikimedia.org/wiki/Special:FilePath/A400M_-_yawing_moments_after_engine_failure.png
  • http://commons.wikimedia.org/wiki/Special:FilePath/Criticalengine1.jpg
dcterms:subject
Wikipage page ID
Wikipage revision ID
Link from a Wikipage to another Wikipage
Link from a Wikipage to an external page
sameAs
dbp:wikiPageUsesTemplate
thumbnail
has abstract
  • Bei mehrmotorigen Flugzeugen ist das kritische Triebwerk (critical engine) jenes, „dessen Ausfall den nachteiligsten Einfluß auf die Flugeigenschaften im jeweils untersuchten Flugzustand hat“. (de)
  • The critical engine of a multi-engine fixed-wing aircraft is the engine that, in the event of failure, would most adversely affect the performance or handling abilities of an aircraft. On propeller aircraft, there is a difference in the remaining yawing moments after failure of the left or the right (outboard) engine when all propellers rotate in the same direction due to the P-factor. On turbojet and turbofan twin-engine aircraft, there usually is no difference between the yawing moments after failure of a left or right engine in no-wind condition. (en)
  • Le moteur critique d'un avion multimoteur, est celui dont la panne provoquerait les effets les plus pénalisants pour le pilotage de l'avion et ses performances. (fr)
  • O motor crítico de uma aeronave multimotora de asa fixa, é o motor cuja falha resulta nos efeitos mais adversos na manobrabilidade e performance da aeronave.(§1.1). Em aeronaves a hélice, existe uma diferença no momento em relação ao eixo longitudinal após uma falha do motor esquerdo ou direito (o que gira para fora da aeronave) quando as hélices giram na mesma direção devido ao P-factor. Em aeronaves turbojato ou turbofan, geralmente não existe nenhuma diferença entre o momento de guinada após a falha de um motor esquerdo ou direito. (pt)
gold:hypernym
prov:wasDerivedFrom
page length (characters) of wiki page
foaf:isPrimaryTopicOf
is Link from a Wikipage to another Wikipage of
Faceted Search & Find service v1.17_git139 as of Feb 29 2024


Alternative Linked Data Documents: ODE     Content Formats:   [cxml] [csv]     RDF   [text] [turtle] [ld+json] [rdf+json] [rdf+xml]     ODATA   [atom+xml] [odata+json]     Microdata   [microdata+json] [html]    About   
This material is Open Knowledge   W3C Semantic Web Technology [RDF Data] Valid XHTML + RDFa
OpenLink Virtuoso version 08.03.3330 as of Mar 19 2024, on Linux (x86_64-generic-linux-glibc212), Single-Server Edition (378 GB total memory, 62 GB memory in use)
Data on this page belongs to its respective rights holders.
Virtuoso Faceted Browser Copyright © 2009-2024 OpenLink Software