. . "A folding wing is a wing configuration design feature of aircraft to save space and is typical of carrier-based aircraft that operate from the limited deck space of aircraft carriers. The folding allows the aircraft to occupy less space in a confined hangar because the folded wing normally rises over the fuselage decreasing the floor area of the aircraft. Vertical clearance is also limited in aircraft carrier hangar decks. In order to accommodate for this, some aircraft such as the Supermarine Seafire and Fairey Gannet have additional hinges to fold the wingtips downward, while others such as the S-3 Viking have folding tails. The F-14 Tomcat's variable-sweep wings could be \"overswept\" to occupy less space."@en . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . "Sklopn\u00E9 k\u0159\u00EDdlo, \u010Di skl\u00E1dac\u00ED k\u0159\u00EDdlo je ozna\u010Den\u00ED technick\u00E9ho \u0159e\u0161en\u00ED, kter\u00E9 umo\u017E\u0148uje letounu sklopit k\u0159\u00EDdla, \u010Di p\u0159\u00EDpadn\u011B jin\u00E9 konstruk\u010Dn\u00ED \u010D\u00E1sti, jako nap\u0159\u00EDklad v\u00FD\u0161kovku a \u0161et\u0159it t\u00EDm prostor na letadlov\u00FDch lod\u00EDch. V\u00FDhodou skl\u00E1dac\u00EDch k\u0159\u00EDdel je \u00FAspora zabran\u00E9ho m\u00EDsta na palub\u011B. D\u00EDky tomu je mo\u017En\u00E9 dodr\u017Eet ur\u010Dit\u00E9 standardizovan\u00E9 rozm\u011Bry pro ka\u017Ed\u00FD stroj, z hlediska v\u00FD\u0161ky, \u0161\u00ED\u0159ky a d\u00E9lky, aby se ve\u0161el na palubn\u00ED v\u00FDtah a podpalubn\u00EDho hang\u00E1ru."@cs . . . . . . . . . . . . . . . . . . . . . . . "L'aile repliable est un type d'aile utilis\u00E9 essentiellement sur les avions op\u00E9rant \u00E0 partir des porte-avions. Le gain de place permet d'une part d'en garer un plus grand nombre sur le pont et, d'autre part, facilite ou m\u00EAme seulement permet l'acc\u00E8s aux ascenseurs et aux hangars de dimensions r\u00E9duites. Les ailes repliables ont l'inconv\u00E9nient d'\u00EAtre plus lourdes que des ailes fixes et de rendre n\u00E9cessaires des structures complexes pour les connexions \u00E9lectriques, l'alimentation en carburant et les commandes a\u00E9rodynamiques."@fr . "Un'ala pieghevole \u00E8 una caratteristica di progettazione della configurazione delle ali degli aeromobili per risparmiare spazio ed \u00E8 tipica degli aeromobili basati su portaerei che operano dallo spazio di coperta limitato delle portaerei. La piegatura consente all'aeromobile di occupare meno spazio in un hangar confinato perch\u00E9 l'ala piegata normalmente sale sopra la fusoliera diminuendo l'area del pavimento dell'aeromobile. Lo spazio verticale \u00E8 inoltre limitato nei ponti dell'hangar della portaerei. Per far fronte a questo, alcuni velivoli come Supermarine Seafire e Fairey Gannet hanno cerniere aggiuntive per piegare le punte delle ali verso il basso, mentre altri come l'S-3 Viking hanno code pieghevoli. Le ali a chiusura variabile dell'F-14 Tomcat potrebbero essere \"chiuse\" per limitare "@it . . "\u6298\u308A\u7573\u307F\u7FFC"@ja . . . "Un'ala pieghevole \u00E8 una caratteristica di progettazione della configurazione delle ali degli aeromobili per risparmiare spazio ed \u00E8 tipica degli aeromobili basati su portaerei che operano dallo spazio di coperta limitato delle portaerei. La piegatura consente all'aeromobile di occupare meno spazio in un hangar confinato perch\u00E9 l'ala piegata normalmente sale sopra la fusoliera diminuendo l'area del pavimento dell'aeromobile. Lo spazio verticale \u00E8 inoltre limitato nei ponti dell'hangar della portaerei. Per far fronte a questo, alcuni velivoli come Supermarine Seafire e Fairey Gannet hanno cerniere aggiuntive per piegare le punte delle ali verso il basso, mentre altri come l'S-3 Viking hanno code pieghevoli. Le ali a chiusura variabile dell'F-14 Tomcat potrebbero essere \"chiuse\" per limitare lo spazio del ponte."@it . "Asas dobr\u00E1veis - s\u00E3o um recurso dispon\u00EDvel em avi\u00F5es, geralmente nos de m\u00E9dio porte (avi\u00F5es pequenos nem sempre tem asas extensas o suficiente para necessitarem deste recurso, enquanto que os grandes possuem asas demasiado s\u00F3lidas e espessas para terem-nas dobradas), para que seja facilitada a angaragem de avi\u00F5es, al\u00E9m tamb\u00E9m de reduzir o espa\u00E7o ocupado no interior de porta-avi\u00F5es. No caso de ca\u00E7as, que possuem suas asas em V, reduz-se seu \u00E2ngulo de abertura em rela\u00E7\u00E3o \u00E0 fuselagem."@pt . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . "Asas dobr\u00E1veis"@pt . . . "Folding wing"@en . . . . . . . "\u6298\u308A\u7573\u307F\u7FFC\uFF08\u304A\u308A\u305F\u305F\u307F\u3088\u304F\u3001folding wing\uFF09\u306F\u3001\u822A\u7A7A\u6A5F\u306E\u3001\u99D0\u6A5F\u6642\u306B\u6298\u308A\u7573\u3081\u308B\u7FFC\u3002 \u99D0\u6A5F\u6642\u306E\u5360\u6709\u7A7A\u9593\u3092\u6E1B\u3089\u3059\u3053\u3068\u304C\u3067\u304D\u3001\u7279\u306B\u98DB\u884C\u7532\u677F\u306E\u9762\u7A4D\u304C\u9650\u3089\u308C\u3066\u3044\u308B\u822A\u7A7A\u6BCD\u8266\u3067\u904B\u7528\u3055\u308C\u308B\u6D77\u8ECD\u306E\u8266\u8F09\u6A5F\u3067\u5E83\u304F\u63A1\u7528\u3055\u308C\u3066\u3044\u308B\u3002"@ja . . . . . . . . . . . . . . . . . . . . . . . . . . . . . "Aile repliable"@fr . . . . . . . . . . . . . . . . . . . . . . . . . "A folding wing is a wing configuration design feature of aircraft to save space and is typical of carrier-based aircraft that operate from the limited deck space of aircraft carriers. The folding allows the aircraft to occupy less space in a confined hangar because the folded wing normally rises over the fuselage decreasing the floor area of the aircraft. Vertical clearance is also limited in aircraft carrier hangar decks. In order to accommodate for this, some aircraft such as the Supermarine Seafire and Fairey Gannet have additional hinges to fold the wingtips downward, while others such as the S-3 Viking have folding tails. The F-14 Tomcat's variable-sweep wings could be \"overswept\" to occupy less space."@en . . . . . . . . . . . "L'aile repliable est un type d'aile utilis\u00E9 essentiellement sur les avions op\u00E9rant \u00E0 partir des porte-avions. Le gain de place permet d'une part d'en garer un plus grand nombre sur le pont et, d'autre part, facilite ou m\u00EAme seulement permet l'acc\u00E8s aux ascenseurs et aux hangars de dimensions r\u00E9duites. L'aile est repli\u00E9e vers l'arri\u00E8re, le long du fuselage gr\u00E2ce \u00E0 une double articulation ou, plus souvent, en partie repli\u00E9e vers le haut gr\u00E2ce \u00E0 une simple articulation. Afin de limiter la hauteur il est alors parfois n\u00E9cessaire de r\u00E9aliser une double pliure et/ou de replier une partie de la d\u00E9rive. (Voir photos ci-dessous). Les ailes repliables ont l'inconv\u00E9nient d'\u00EAtre plus lourdes que des ailes fixes et de rendre n\u00E9cessaires des structures complexes pour les connexions \u00E9lectriques, l'alimentation en carburant et les commandes a\u00E9rodynamiques. Le principe s'applique aussi, pour les m\u00EAmes raisons, aux pales du ou des rotors de sustentation des h\u00E9licopt\u00E8res embarqu\u00E9s. Quelques avions bas\u00E9s au sol adoptent le principe pour \u00E9viter d'utiliser des hangars de grande dimensions. C'est le cas des Sukhoi Su-47 (ailes repliables), Saab 37 Viggen et Boeing 377 Stratocruiser (d\u00E9rive repliable). Sur le Boeing B-50 Superfortress d\u00E9j\u00E0, il avait \u00E9t\u00E9 envisag\u00E9 de rendre la d\u00E9rive repliable. Short Brothers est le premier constructeur \u00E0 d\u00E9velopper et breveter d\u00E8s 1913 des ailes repliables pour des avions de l'a\u00E9ronavale. Les ailes se repliaient le long du fuselage gr\u00E2ce \u00E0 une articulation complexe \u00E0 deux axes de rotation."@fr . . . . . . . . . . . . . . . . . . . . . . . "10588"^^ . . . . . . . . "Asas dobr\u00E1veis - s\u00E3o um recurso dispon\u00EDvel em avi\u00F5es, geralmente nos de m\u00E9dio porte (avi\u00F5es pequenos nem sempre tem asas extensas o suficiente para necessitarem deste recurso, enquanto que os grandes possuem asas demasiado s\u00F3lidas e espessas para terem-nas dobradas), para que seja facilitada a angaragem de avi\u00F5es, al\u00E9m tamb\u00E9m de reduzir o espa\u00E7o ocupado no interior de porta-avi\u00F5es. No caso de ca\u00E7as, que possuem suas asas em V, reduz-se seu \u00E2ngulo de abertura em rela\u00E7\u00E3o \u00E0 fuselagem."@pt . . . . . . . . . . . . . . . . . . . . . "\u6298\u308A\u7573\u307F\u7FFC\uFF08\u304A\u308A\u305F\u305F\u307F\u3088\u304F\u3001folding wing\uFF09\u306F\u3001\u822A\u7A7A\u6A5F\u306E\u3001\u99D0\u6A5F\u6642\u306B\u6298\u308A\u7573\u3081\u308B\u7FFC\u3002 \u99D0\u6A5F\u6642\u306E\u5360\u6709\u7A7A\u9593\u3092\u6E1B\u3089\u3059\u3053\u3068\u304C\u3067\u304D\u3001\u7279\u306B\u98DB\u884C\u7532\u677F\u306E\u9762\u7A4D\u304C\u9650\u3089\u308C\u3066\u3044\u308B\u822A\u7A7A\u6BCD\u8266\u3067\u904B\u7528\u3055\u308C\u308B\u6D77\u8ECD\u306E\u8266\u8F09\u6A5F\u3067\u5E83\u304F\u63A1\u7528\u3055\u308C\u3066\u3044\u308B\u3002"@ja . . "Ala pieghevole"@it . . . . "Sklopn\u00E9 k\u0159\u00EDdlo"@cs . . . . "Sklopn\u00E9 k\u0159\u00EDdlo, \u010Di skl\u00E1dac\u00ED k\u0159\u00EDdlo je ozna\u010Den\u00ED technick\u00E9ho \u0159e\u0161en\u00ED, kter\u00E9 umo\u017E\u0148uje letounu sklopit k\u0159\u00EDdla, \u010Di p\u0159\u00EDpadn\u011B jin\u00E9 konstruk\u010Dn\u00ED \u010D\u00E1sti, jako nap\u0159\u00EDklad v\u00FD\u0161kovku a \u0161et\u0159it t\u00EDm prostor na letadlov\u00FDch lod\u00EDch. V\u00FDhodou skl\u00E1dac\u00EDch k\u0159\u00EDdel je \u00FAspora zabran\u00E9ho m\u00EDsta na palub\u011B. D\u00EDky tomu je mo\u017En\u00E9 dodr\u017Eet ur\u010Dit\u00E9 standardizovan\u00E9 rozm\u011Bry pro ka\u017Ed\u00FD stroj, z hlediska v\u00FD\u0161ky, \u0161\u00ED\u0159ky a d\u00E9lky, aby se ve\u0161el na palubn\u00ED v\u00FDtah a podpalubn\u00EDho hang\u00E1ru. Nev\u00FDhodou skl\u00E1dac\u00EDch k\u0159\u00EDdel je slo\u017Eit\u00E1 konstrukce, zvy\u0161uj\u00EDc\u00ED v\u00E1hu a zvy\u0161uj\u00EDc\u00ED n\u00E1roky na spolehlivost mechanizmu z hlediska mechaniky k\u0159\u00EDdla. Skl\u00E1dac\u00ED \u010D\u00E1st k\u0159\u00EDdla st\u00E1le vy\u017Eaduje zaji\u0161t\u011Bn\u00ED funk\u010Dnosti hydrauliky a elektrifikace."@cs . . . . . "1117634836"^^ . . . . . . . . . . . . . . . "2399832"^^ . . . . . . . . .