Kuznetsov NK-93
http://dbpedia.org/resource/Kuznetsov_NK-93
Das Kusnezow NK-93 ist ein Turbofan-Triebwerk der russischen Firma Kusnezow. Der Erstflug fand am 18. Mai 2008 mit einer Il-76LL statt.
rdf:langString
The Kuznetsov NK-93 was a civilian aircraft engine, a hybrid between a turbofan and a turboprop known as a propfan. The engine was also unique in having a separate duct around the contra-rotating propellers, as most other propfans are unducted. Once described in a respected aviation encyclopedia as "potentially the most fuel-efficient aircraft jet engine ever to be tested", the NK-93 was targeted for derivatives of Soviet/Russian airliners such as the Ilyushin Il-96, Tupolev Tu-204, and Tupolev Tu-330. Five in-flight engine tests were conducted on the NK-93 from December 2006 to December 2008.
rdf:langString
NK-93（ロシア語: НК-93）は、ロシア連邦のN・D・クズネツォフ記念サマーラ科学技術複合が開発していたプロップファンエンジンである。プロップファンであるが、周りにダクトがある点が特徴である。
rdf:langString
Il Kuznetsov NK-93 è un motore aeronautico turboventola ad elevato rapporto di diluizione in fase di sviluppo sin dalla fine degli anni ottanta in Unione Sovietica (ed oggi in Russia), per equipaggiare una classe di aerei da trasporto civili e militari a medio raggio.
rdf:langString
rdf:langString
Kusnezow NK-93
rdf:langString
Kouznetsov NK-93
rdf:langString
Kuznetsov NK-93
rdf:langString
Kuznetsov NK-93
rdf:langString
クズネツォフ NK-93
xsd:integer
61358226
xsd:integer
1094597055
rdf:langString
* Europrop TP400
* General Electric GE36
* IAE SuperFan
* Pratt & Whitney/Allison 578-DX
* Progress D-27 / Progress D-627
* Progress D-236
* Rolls-Royce RB3011
rdf:langString
Takeoff: ; Cruise: at Mach 0.75, at Mach 0.8
xsd:integer
1
rdf:langString
*Width:
*Height:
*Propeller diameter:
rdf:langString
planetary gearbox providing 87% of the power
rdf:langString
* Kuznetsov NK-12
* Kuznetsov NK-92
xsd:integer
3
rdf:langString
*Propeller weight:
rdf:langString
Das Kusnezow NK-93 ist ein Turbofan-Triebwerk der russischen Firma Kusnezow. Der Erstflug fand am 18. Mai 2008 mit einer Il-76LL statt.
rdf:langString
The Kuznetsov NK-93 was a civilian aircraft engine, a hybrid between a turbofan and a turboprop known as a propfan. The engine was also unique in having a separate duct around the contra-rotating propellers, as most other propfans are unducted. Once described in a respected aviation encyclopedia as "potentially the most fuel-efficient aircraft jet engine ever to be tested", the NK-93 was targeted for derivatives of Soviet/Russian airliners such as the Ilyushin Il-96, Tupolev Tu-204, and Tupolev Tu-330. Five in-flight engine tests were conducted on the NK-93 from December 2006 to December 2008.
rdf:langString
Il Kuznetsov NK-93 è un motore aeronautico turboventola ad elevato rapporto di diluizione in fase di sviluppo sin dalla fine degli anni ottanta in Unione Sovietica (ed oggi in Russia), per equipaggiare una classe di aerei da trasporto civili e militari a medio raggio. L'inedita configurazione lo rende per certi aspetti affine ad un motore propfan col quale condivide il notevole rapporto di bypass e le pale di grande diametro a geometria variabile, ma se ne discosta per la presenza del condotto che racchiude le ventole. Fu sviluppata anche una versione in grado di usare indifferentemente come combustibile GPL o cherosene, cui venne assegnata la sigla NK-94.
rdf:langString
NK-93（ロシア語: НК-93）は、ロシア連邦のN・D・クズネツォフ記念サマーラ科学技術複合が開発していたプロップファンエンジンである。プロップファンであるが、周りにダクトがある点が特徴である。
xsd:double
16.6
rdf:langString
annular
xsd:integer
37
xsd:integer
7
xsd:integer
1989
rdf:langString
* List of aircraft engines
xsd:integer
11
rdf:langString
US$900 million as of 2001
rdf:langString
* Geared turbofan
* Propfan
xsd:nonNegativeInteger
28332
